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Flight Management System (FMS) for the Agusta AW139/AB139 Helicopter

A28--1146--181

REV 3 Mar 2009

3-21

System Components

Honeywell International Inc. Do not copy without express permission of Honeywell.

—

GPS RAIM UNAVAILABLE -- This is an alerting system message

indicating the GPS current RAIM is not available.

—

GPS X UNAVAILABLE -- This is an alerting system message

indicating a GPS has been dropped from the FMS navigation

solution and X represents the GPS number.

—

HELIPAD NOT FOUND -- This is an advisory operator message

indicating the database does not contain the entered helipad at

the designated heliport.

—

HIGH HOLDING GRD SPD -- This is an alerting system

message indicating the ground speed exceeds the limits for the

Federal Aviation Administration (FAA) allowable size of the

current holding pattern.

—

HIGH PCDR TURN GRD SPD -- This is an alerting system

message indicating the ground speed exceeds the limits for the

FAA allowable size of the current procedure turn.

—

INDEPENDENT OPERATION -- This is an alerting system

message indicating the system reverted to independent

operation due to a problem with the selected operating mode.

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INTERSECTION NOT FOUND -- This is an advisory operator

message indicating the entered place//distance does not

intersect the active flight plan.

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INVALID AIRCRAFT DB -- This is an alerting system message

indicating the aircraft database is invalid.

—

INVALID CUSTOM DB -- This is an alerting system message

indicating the custom DB has been corrupted and has been

cleared and initialized.

—

INVALID DELETE -- This is an advisory operator message

indicating the delete operation was invalid for the selected item.

—

INVALID DIRECT TO -- This is an advisory system message

indicating the direct--to operation was invalid for the selected

waypoint or altitude constraint.

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INVALID DIRECT TO ENTRY -- This is an alerting system

message indicating an invalid entry when attempting a direct--to

entry to 1L of the active flight plan pages when there is an existing

scratchpad message displayed.

—

INVALID ENTRY -- This is an advisory operator message

indicating the entry is not in the correct format and/or range.

Summary of Contents for FMZ Series

Page 1: ... of the revised pages and revision bars have been used to indicate the revised or added text Insert this highlights letter in the manual in your possession ahead of page RR 1 Record of Revisions The List of Effective Pages shows the order in which to insert the attached new pages into your guide The Record of Revisions page shows Honeywell has already put Revision No 4 dated August 2010 in the gui...

Page 2: ...thout express permission of Honeywell Page No Description of Change 7 27 Added button references PFD STBY ALTA RHT TD H MOT and WTR Deleted VNAV and FLCH buttons Changed APPR button reference to APP and LNAV button reference to NAV Abbrev 2 Abbrev 17 and Abbrev 19 Added acronyms ...

Page 3: ......

Page 4: ...ted in U S A Pub No A28 1146 181 004 August 2004 Revised August 2010 Page T 1 Honeywell International Inc Do not copy without express permission of Honeywell Honeywell International Inc 21111 N 19th Ave Phoenix Arizona 85027 2708 U S A CAGE 55939 Telephone 1 800 601 3099 U S A Canada Telephone 1 602 365 3099 International Web site http portal honeywell com wps portal aero Flight Management System ...

Page 5: ...Materials from Honeywell s Aerospace Technical Publication Distribution The terms and conditions of this License Agreement govern your use of these Materials except to the extent that any terms and conditions of another applicable agreement with Honeywell regarding the operation maintenance or repair of Honeywell aerospace products conflict with the terms and conditions of this License Agreement i...

Page 6: ...r of an aircraft containing the subject Honeywell aerospace products However the recipient of any such assignment or transfer must assume all of your obligations under this License Agreement No assignment or transfer shall relieve any party of any obligation that such party then has hereunder 5 Copies of Materials Unless you have the express written permission of Honeywell you may not make or perm...

Page 7: ...AGES SPECIAL DAMAGES INDIRECT DAMAGES LOSS OF PROFITS LOSS OF REVENUES OR LOSS OF USE EVEN IF INFORMED OF THE POSSIBILITY OF SUCH DAMAGES TO THE EXTENT PERMITTED BY APPLICABLE LAW THESE LIMITATIONS AND EXCLUSIONS WILL APPLY REGARDLESS OF WHETHER LIABILITY ARISES FROM BREACH OF CONTRACT WARRANTY TORT INCLUDING BUT NOT LIMITED TO NEGLIGENCE BY OPERATION OF LAW OR OTHERWISE 9 Controlling Law This Lic...

Page 8: ...on put the changed pages in your guide and discard the replaced pages Write the revision number and date and the date put in the guide Put your initials in the applicable columns on the Record of Revisions The initial H shows that Honeywell put the changed pages in the guide Revision Number Revision Date Insertion Date By 1 Sep 2005 Sep 2005 H 2 Jun 2007 Jun 2007 H 3 Mar 2009 Mar 2009 H 4 Aug 2010...

Page 9: ...ht Management System FMS for the Agusta AW139 AB139 Helicopter A28 1146 181 REV 3 Mar 2009 Record of Revisions RR 2 Honeywell International Inc Do not copy without express permission of Honeywell Blank Page ...

Page 10: ... 2009 TC 4 Mar 2009 TC 5 Mar 2009 TC 6 Mar 2009 TC 7 Mar 2009 TC 8 Mar 2009 TC 9 Mar 2009 TC 10 Mar 2009 TC 11 Mar 2009 TC 12 Mar 2009 TC 13 Mar 2009 TC 14 Mar 2009 TC 15 Mar 2009 TC 16 Mar 2009 Introduction 1 1 H Aug 2010 1 2 Mar 2009 1 3 Mar 2009 1 4 Mar 2009 System Description 2 1 Mar 2009 2 2 Mar 2009 2 3 Mar 2009 2 4 Mar 2009 System Components 3 1 Mar 2009 3 2 Mar 2009 3 3 Mar 2009 3 4 Mar 20...

Page 11: ...2009 4 29 Mar 2009 4 30 Mar 2009 4 31 Mar 2009 4 32 Mar 2009 4 33 Mar 2009 4 34 Mar 2009 4 35 Mar 2009 4 36 Mar 2009 4 37 Mar 2009 4 38 Mar 2009 4 39 Mar 2009 4 40 Mar 2009 4 41 Mar 2009 4 42 Mar 2009 4 43 Mar 2009 4 44 Mar 2009 4 45 Mar 2009 4 46 Mar 2009 4 47 Mar 2009 4 48 Mar 2009 4 49 Mar 2009 4 50 Mar 2009 4 51 Mar 2009 4 52 Mar 2009 Performance 5 1 Mar 2009 5 2 Mar 2009 5 3 Mar 2009 5 4 Mar ...

Page 12: ...6 27 Mar 2009 6 28 Mar 2009 6 29 Mar 2009 6 30 Mar 2009 6 31 Mar 2009 6 32 Mar 2009 6 33 Mar 2009 6 34 Mar 2009 6 35 Mar 2009 6 36 Mar 2009 6 37 Mar 2009 6 38 Mar 2009 6 39 Mar 2009 6 40 Mar 2009 6 41 Mar 2009 6 42 Mar 2009 6 43 Mar 2009 6 44 Mar 2009 6 45 Mar 2009 6 46 Mar 2009 6 47 Mar 2009 6 48 Mar 2009 6 49 Mar 2009 6 50 Mar 2009 6 51 Mar 2009 6 52 Mar 2009 6 53 Mar 2009 6 54 Mar 2009 6 55 Mar...

Page 13: ...117 Mar 2009 6 118 Mar 2009 6 119 Mar 2009 6 120 Mar 2009 6 121 Mar 2009 6 122 Mar 2009 6 123 Mar 2009 6 124 Mar 2009 6 125 Mar 2009 6 126 Mar 2009 6 127 Mar 2009 6 128 Mar 2009 6 129 Mar 2009 6 130 Mar 2009 6 131 Mar 2009 6 132 Mar 2009 6 133 Mar 2009 6 134 Mar 2009 6 135 Mar 2009 6 136 Mar 2009 6 137 Mar 2009 6 138 Mar 2009 6 139 Mar 2009 6 140 Mar 2009 6 141 Mar 2009 6 142 Mar 2009 6 143 Mar 20...

Page 14: ... 2009 6 204 Mar 2009 6 205 Mar 2009 6 206 Mar 2009 6 207 Mar 2009 6 208 Mar 2009 Flight Plan 7 1 Mar 2009 7 2 Mar 2009 7 3 Mar 2009 7 4 Mar 2009 7 5 Mar 2009 7 6 Mar 2009 7 7 Mar 2009 7 8 Mar 2009 7 9 Mar 2009 7 10 Mar 2009 7 11 Mar 2009 7 12 Mar 2009 7 13 Mar 2009 7 14 Mar 2009 7 15 Mar 2009 7 16 Mar 2009 7 17 Mar 2009 7 18 Mar 2009 7 19 Mar 2009 7 20 Mar 2009 7 21 Mar 2009 7 22 Mar 2009 7 23 Mar...

Page 15: ...9 20 Mar 2009 Multifunction Control Display Unit MCDU Entry Format 10 1 Mar 2009 10 2 Mar 2009 10 3 Mar 2009 10 4 Mar 2009 10 5 Mar 2009 10 6 Mar 2009 10 7 Mar 2009 10 8 Mar 2009 10 9 Mar 2009 10 10 Mar 2009 10 11 Mar 2009 10 12 Mar 2009 10 13 Mar 2009 10 14 Mar 2009 10 15 Mar 2009 10 16 Mar 2009 10 17 Mar 2009 10 18 Mar 2009 Messages 11 1 Mar 2009 11 2 Mar 2009 11 3 Mar 2009 11 4 Mar 2009 11 5 Ma...

Page 16: ...F A 29 A 30 Mar 2009 F A 31 A 32 Mar 2009 F A 33 A 34 Mar 2009 Acronyms and Abbreviations Abbrev 1 Mar 2009 Abbrev 2 H Aug 2010 Abbrev 3 Mar 2009 Abbrev 4 Mar 2009 Abbrev 5 Mar 2009 Abbrev 6 Mar 2009 Abbrev 7 Mar 2009 Abbrev 8 Mar 2009 Abbrev 9 Mar 2009 Abbrev 10 Mar 2009 Abbrev 11 Mar 2009 Abbrev 12 Mar 2009 Abbrev 13 Mar 2009 Abbrev 14 Mar 2009 Abbrev 15 Mar 2009 Abbrev 16 Mar 2009 Abbrev 17 H A...

Page 17: ...Management System FMS for the Agusta AW139 AB139 Helicopter A28 1146 181 REV 3 Mar 2009 List of Effective Pages LEP 8 Honeywell International Inc Do not copy without express permission of Honeywell Blank Page ...

Page 18: ...tion 2 1 Functional Description 2 3 Flight Planning 2 3 Database 2 3 Lateral Navigation LNAV 2 3 Vertical Navigation VNAV 2 4 Performance 2 4 Navigation Displays 2 4 3 SYSTEM COMPONENTS 3 1 Introduction 3 1 Multifunction Control Display Unit MCDU 3 1 MCDU Display 3 3 Alphanumeric Keys 3 4 Scratchpad 3 4 Line Select Keys LSK 3 5 Clear CLR Key 3 6 Delete DEL Key 3 6 Function Keys 3 7 Accessing Any F...

Page 19: ...e Flight Plan 4 50 Clearing of Flight Plans 4 51 5 PERFORMANCE 5 1 Introduction 5 1 Performance Index 5 2 Performance Initialization 5 3 SPD FF and Current Ground Speed FF Method 5 7 Pilot Speed Fuel Flow SPD FF Method 5 7 Performance Data 5 17 Performance Data Pages 1 and 2 Definition 5 17 Performance Data Page 3 Definition 5 20 Performance Data Page 4 Definition 5 22 Performance Plan 5 23 Wind a...

Page 20: ...ndefined Waypoints 6 33 FMS Database 6 33 Navigation Database 6 33 Custom Database 6 34 Temporary Waypoints 6 34 Departures 6 35 Arrival 6 43 Approach 6 56 Missed Approach 6 58 Position Sensors 6 61 Navigation Modes 6 61 FMS Position Update 6 63 Sensor Status Pages 6 73 Notice to Airmen 6 85 Sensors Being Used by the FMS 6 86 Position Sensor Deselection 6 87 Tuning NAV Radios 6 89 Autotune 6 93 VO...

Page 21: ...ight Plan 6 164 MOT Flight Plan 6 170 MOT Page Operation 6 172 Navigation Identification 6 175 Maintenance 6 177 Active Operating Modes 6 177 Failed Sensors 6 179 True Magnetic Selection 6 181 High Latitude Flying 6 182 Return to Service 6 183 FMS Setup Pages 6 184 Flight Configuration 6 186 Engineering Data 6 191 Position Initialization 6 193 Crossing Points 6 196 Present Position PPOS Direct 6 1...

Page 22: ...perature Compensation 7 30 VNAV Operational Scenarios 7 42 Speed Command 7 49 General Speed Command Rules 7 49 Automatic 7 50 Waypoint Speed Constraint 7 51 Manual 7 53 Speed Protection 7 54 8 PROGRESS 8 1 Introduction 8 1 Progress 1 3 Page 8 1 Progress 2 3 Page 8 2 Progress 3 3 Page 8 3 VNAV Data 8 5 Lateral Offset 8 6 Air Data 8 8 Required Navigation Performance RNP 8 9 9 DIRECT INTERCEPT 9 1 In...

Page 23: ...onyms and Abbreviations Abbrev 1 INDEX Index 1 List of Figures Figure Page 2 1 FMS System Block Diagram 2 2 3 1 MCDU Display 3 2 3 2 PERF INDEX Page 3 7 3 3 NAV INDEX Page 1 3 8 3 4 NAV INDEX Page 2 3 8 3 5 ACTIVE FLT PLAN 1 5 3 9 3 6 PROGRESS 1 3 3 10 3 7 Bright Dim Bar Level 3 28 4 1 KDAL to KHOU Flight Route 4 1 4 2 Dallas TX JPOOL9 Departure 4 2 4 3 Houston TX BLUBL Arrival 4 3 4 4 Houston TX ...

Page 24: ...CES 1 2 4 23 4 25 SIDs 1 1 4 24 4 26 DEPARTURE TRANS 1 1 4 25 4 27 PROCEDURE 1 1 4 26 4 28 ACTIVE FLT PLAN 1 5 Page 4 27 4 29 TAKEOFF 1 2 4 28 4 30 TAKEOFF 2 2 4 29 4 31 ACTIVE FLIGHT PLAN 1 5 Page 4 30 4 32 Runway Coordinates on POSITION INIT 1 1 Page 4 31 4 33 LOAD Prompt on POSITION INIT 1 1 Page 4 32 4 34 ETA on ACTIVE FLT PLAN 1 5 Page 4 33 4 35 Waypoint Sequencing on ACTIVE FLT PLAN 1 5 4 34...

Page 25: ...CE INIT 3 3 Page 5 15 5 10 PERF DATA Pages 1 4 and 2 4 5 17 5 11 PERF DATA 3 4 Page 5 20 5 12 PERF DATA 4 4 Page 5 22 5 13 PERF PLAN 1 X 5 23 5 14 WIND TEMP 2 X 5 24 5 15 WIND TEMP 5 25 5 16 TAKEOFF 1 2 Page 5 27 5 17 TAKEOFF 2 2 Page 5 31 5 18 LANDING 1 2 Page 5 32 5 19 LANDING 2 2 Page 5 35 5 20 FUEL MGT LB 1 2 5 36 5 21 FUEL MGT LB 2 2 5 38 6 1 NAV INDEX 1 2 6 1 6 2 NAV INDEX 2 2 6 3 6 3 FLIGHT...

Page 26: ...BASE WPT 1 1 NB 6 29 6 28 DATA BASE WPT 1 1 ILS 6 30 6 29 DATA BASE WPT 1 1 Intersections 6 31 6 30 WAYPOINT SELECT 1 2 6 32 6 31 Denver CO PIKES4 Departure 6 36 6 32 DEPARTURE SURFACES 2 3 6 37 6 33 SIDs 1 1 Page 6 38 6 34 DEPARTURE TRANS 1 1 Page 6 39 6 35 PROCEDURE 1 1 Page 6 40 6 36 SID REVIEW 1 2 6 41 6 37 SID REVIEW 2 2 6 42 6 38 Minneapolis MN KASPR2 Arrival 6 45 6 39 ARRIVAL 1 1 Page 6 47 ...

Page 27: ...6 70 NAV Prompt on PROGRESS 1 3 Page 6 90 6 71 Desired Station 6 90 6 72 TFD Tune 6 91 6 73 Enter DELETE Into Scratchpad 6 94 6 74 FMS Switches to Autotune 6 94 6 75 CONVERSION 1 4 6 96 6 76 CONVERSION 1 4 Page 6 97 6 77 CONVERSION 2 4 6 98 6 78 CONVERSION 3 4 6 99 6 79 CONVERSION 3 4 Page 6 100 6 80 Average Specific Weight Variation of Aviation Fuels and Lubricants 6 101 6 81 CONVERSION 4 4 6 102...

Page 28: ...Flight Plan 6 140 6 113 Suspend Waypoint on ACTIVE FLT PLAN 6 141 6 114 PATTERNS Prompt on NAV INDEX Page 6 142 6 115 PATTERNS 1 1 SEARCH Prompt 6 143 6 116 SEARCH PATTERNS Page 6 144 6 117 Expanding Square Search Definition 6 145 6 118 SQUARE SEARCH 6 146 6 119 Sector Search Definition 6 149 6 120 SECTOR SEARCH 6 150 6 121 Creeping Ladder Search Definition 6 153 6 122 LADDER SEARCH 6 154 6 123 Pa...

Page 29: ...99 6 150 CROSS LAT LON 1 1 Page 6 200 6 151 Accessing Database Crossloading 6 201 6 152 CUSTOM DB Prompt 6 202 6 153 TO FMS 2 Prompt 6 203 6 154 CONFIRM YES or NO 6 204 6 155 Progress Monitoring 6 205 6 156 FLIGHT SUMMARY 1 1 Page 6 206 7 1 ACTIVE FLT PLAN Example 7 10 7 2 Recall Flight Plan 7 11 7 3 FLIGHT PLAN LIST 1 1 Page 7 12 7 4 Required Flight Plan 7 12 7 5 Flight Plan Identifier 7 13 7 6 F...

Page 30: ...ually Entered Speed 7 53 7 32 Latched Speed Protection 7 55 8 1 Progress 1 3 Page 8 1 8 2 PROGRESS 2 3 Page 8 2 8 3 PROGRESS 3 3 Page 8 4 8 4 VNAV DATA 1 1 8 5 8 6 AIR DATA 1 1 1 Page 8 8 8 7 RNP 1 1 Page 8 9 9 1 DIRECT Prompt on ACTIVE FLT PLAN 1 4 Page 9 1 9 2 Direct To Waypoint 9 3 9 3 INTERCEPT in Scratchpad 9 5 9 4 INTERCEPT 1 1 Page 9 6 9 5 30 Degree Radial From Drake 9 7 9 6 Inbound Radial ...

Page 31: ...atterns Page Tree A 15 A 8 Pos Sensors Page Tree A 17 A 9 Maintenance Page Tree A 19 A 10 NAV Ident Position Init Page Tree A 21 A 11 Active Flight Plan Alternate Flight Plan Page Tree A 23 A 12 Performance Init Page Tree A 25 A 13 Departure Page Tree A 27 A 14 Takeoff Data Page Tree A 29 A 15 Arrival Missed Approach Page Tree A 31 A 16 Landing Page Tree A 33 List of Tables Table Page 3 1 MCDU Col...

Page 32: ...t Stations 6 89 6 14 NAV Tuning by Identifier 6 91 6 15 NAV Tuning by Frequency 6 92 6 16 NAV Tuning by Selecting Autotune 6 93 6 17 Holding Pattern Definitions and Review 6 109 6 18 Holding at Present Position 6 116 6 19 Deleting a Holding Pattern From the Active Flight Plan Pages 6 117 6 20 Deleting a Holding Pattern From the Holding Pattern Page 6 118 6 21 Flyover Pattern Definitions 6 127 6 22...

Page 33: ...NAV Offset Definition 7 20 7 2 FMS Temperature Compensation Configuration 7 30 7 3 Review and Insert Temperature Compensated Altitude Constraints Into Flight Plan 7 34 7 4 Remove Temperature Compensation 7 39 7 5 Inserting a Waypoint Speed Constraint 7 52 7 6 Removing a Waypoint Speed Constraint 7 53 8 1 Lateral Offset Entry 8 6 9 1 Vertical Direct To 9 2 9 2 Direct To Recovery 9 3 9 3 Intercept U...

Page 34: ... the FMS capabilities and components Section 4 describes a normal operational example for the FMS Sections 5 through 9 detail the features and specialized capabilities of the FMS Since many topics are covered in this guide use the index to find specific topics There are also many cross references within the guide This revision reflects inclusions to software version 7 1 This pilot guide reflects t...

Page 35: ...ough a Honeywell repair facility All articles are inspected by quality control personnel to verify proper workmanship and conformity to type design and to certify that the article meets all controlling documentation Reconditioned specification criteria are on file at Honeywell facilities and are available for review All exchange units are updated with the latest performance reliability modificatio...

Page 36: ...he Global Customer Care is available if you need to D Identify a change of address telephone number or e mail address D Register for revisions of this guide Honeywell Aerospace Technical Publications If you have access to the Internet go to the Honeywell Online Technical Publications web site at http portal honeywell com wps portal aero to D Download or see publications online D Make an order for ...

Page 37: ...Flight Management System FMS for the Agusta AW139 AB139 Helicopter A28 1146 181 REV 3 Mar 2009 Introduction 1 4 Honeywell International Inc Do not copy without express permission of Honeywell Blank Page ...

Page 38: ...sed on a blend or mix of sensor inputs Based on the position and the flight plan the FMS generates information to be displayed on the multifunction control display unit MCDU and electronic display system EDS The lateral navigation function of the FMS calculates navigation information relative to selected geographical points The pilot can define flight plan routes worldwide The system outputs advis...

Page 39: ...Agusta AW139 AB139 Helicopter A28 1146 181 REV 3 Mar 2009 System Description 2 2 Honeywell International Inc Do not copy without express permission of Honeywell The FMS has the following major functions Figure 2 1 FMS System Block Diagram ...

Page 40: ...automatically blends or selects position sensors to compute an optimum position The pilot deselects individual sensors when required Flight Planning The flight planning function computes the active flight plan with both lateral and vertical definition Flight plans are loaded from a laptop personal computer PC using the data multiplexing unit DMU interface Database The database contains worldwide c...

Page 41: ...h the lateral flight plan Performance Performance contains fuel management and time estimates for the flight Performance estimates optimum altitudes cruise modes and fuel utilization Performance has automatic speed targets for each phase of flight Navigation Displays Navigation displays are shown on the EDS Electronic maps integrate route map data with auxiliary navigation data to show the aircraf...

Page 42: ...l display unit MCDU shown in Figure 3 1 is the principal pilot interface to the system The function of the MCDU is described in this section The pilot must know the general rules and operating characteristics of the MCDU to understand the specific operations of the flight management system FMS MCDU operation is designed to be simple and to minimize crew workload in all phases of flight The MCDU se...

Page 43: ...nagement System FMS for the Agusta AW139 AB139 Helicopter A28 1146 181 REV 3 Mar 2009 System Components 3 2 Honeywell International Inc Do not copy without express permission of Honeywell Figure 3 1 MCDU Display ...

Page 44: ...possible with other displays Refer to Table 3 1 for a definition of color assignments Table 3 1 MCDU Color Coding Scheme Assigned Color Parameter Cyan Vertical Performance and Atmospheric Data Green Caution Lateral Modes Amber Warnings FROM Waypoint Flight Plan Names Magenta TO Waypoint electronic flight instrument system EFIS presents TO waypoint information in cyan unless the TO waypoint is the ...

Page 45: ...cter in the scratchpad The plus minus key is used to enter a or in the scratchpad Pushing the key initially results in a being entered A subsequent pushing changes the to a Continued pushing of key toggles the display Scratchpad The bottom line on the MCDU is the scratchpad The scratchpad is a working area where the pilot enters data and or verifies data before line selecting the data into its pro...

Page 46: ...ctions are displayed in the following priority D Bright dim control bar D Alerting messages D Advisory messages D Delete function D Entry and line selection Line Select Keys LSK There are six line select keys on each side of the MCDU display Data is selected to a line from the scratchpad or vice versa using the LSKs These keys are identified from top to bottom as 1L through 6L on the left side and...

Page 47: ...tes the message D When a scratchpad entry begins with an asterisk or pound sign pushing the CLR key removes the entire entry D When an alphanumeric entry is made in the scratchpad one character is cleared from the scratchpad from right to left eachtime the CLR key is pushed When the CLR key is held down after the first character is cleared other characters are cleared one at a time until the key i...

Page 48: ...ge selection D PERF Key The PERF INDEX page shown in Figure 3 2 is displayed by pushing PERF function key Performance pages show FMS performance computations such as wind fuel management and takeoff and landing data The pilot is able to select any of the performance index functions by pushing the respective LSK Figure 3 2 PERF INDEX Page The performance index page give the pilot access to the foll...

Page 49: ...f Honeywell D NAV Key Pushing the NAV function key shows page 1 and 2 of the navigation index shown in Figures 3 3 and 3 4 The navigation index pages give access to position sensor data stored flight plans waypoints and maintenance pages The pilot selects any of the index functions by pushing the respective LSK 00606 13 Figure 3 3 NAV INDEX Page 1 00607 09 Figure 3 4 NAV INDEX Page 2 ...

Page 50: ...age changing D FPL Key Pushing the flight plan FPL key shows the first page of the active flight plan shown in Figure 3 5 The flight plan pages provide flight plan data for each leg in the planned flight plan including course distance and speed altitude constraints When no flight plan is entered the pilot does the following Manually creates a flight plan Selects a stored flight plan Loads a flight...

Page 51: ...djacent to the respective function Figure 3 6 PROGRESS 1 3 D DIR Key Pushing the direct DIR function key shows the active flight plan page with the DIRECT PATTERN and INTERCEPT prompts When other than an active flight plan page is displayed when pushing the button the first page of the flight plan is displayed When the active flight plan is already displayed when pushing the button the display rem...

Page 52: ... PROG RADIO MENU or DIR keys 2 Select the appropriate PERF NAV FPL PROG or DIR key 3 When PERF or NAV is selected read the menu list for the required function or feature 4 Select the correct function or feature 5 The function or feature selected is displayed by the FMS 6 Continue working using the prompts at 6L and 6R when part of a sequence such as initialization is being completed Annunciators A...

Page 53: ...e approved sensors for the flight phases are listed in Table 3 2 Table 3 2 Approved Sensors for Flight Phase Approved Sensors Navigation Mode Flight Phase GPS DME DME VOR DME Departure or Terminal X X X En route X X X Oceanic X X X VOR DME or VOR Approach X X X GPS Approach X NDB Approach X X The DGR annunciator is displayed on the horizontal situation indicator HSI or primary flight display PFD p...

Page 54: ...e pilot as to system status and are divided into the following three groups 1 ADVISORY MESSAGES Advisory messages contain information helpful to the pilot Advisory messages are normally the result of a pilot action on the MCDU e g making an entry with the incorrect format Advisory messages have a low priority and are displayed after any alerting messages 2 ALERTING MESSAGES Alerting messages alert...

Page 55: ...s below the minimum gross weight in the aircraft database ACDB BRG CRS MUST BE IN TRUE This is an advisory operator message indicating the bearing entry must be followed by a T for TRUE because the referenced waypoint is outside the coverage of the magnetic variation table BUSY REENTER LAST CHG This is an advisory operator message indicating changes to the custom database was attempted when the cr...

Page 56: ...d 02 No response to STATUS command 03 Illegal database file header 04 No response to READ command 05 Error getting the first flight plan record 06 Flight plan record too long 08 Status command failed 09 CRC is illegal 0A EE size in header is bad 0B File size in header is bad 0C Database size or serial number is 0 0D Database size in header is odd 0E Serial number is locked out 0F CRC lockout 10 Ba...

Page 57: ...D File header locked out 1E Error getting identifier 1F Error getting latitude 20 Error getting longitude 21 Error getting speed constraint 22 Error getting flight level constraint 23 Error getting spot wind 24 Error getting spot temperature 25 Error getting metro flight level 26 Error getting first debug monitor record 27 Record greater than 80 characters 28 Read file not open 29 Read attempted a...

Page 58: ...dicating the planned fuel at the destination is equal to or less than zero CHECK FLIGHT ENVELOPE This is an alerting system message indicating the pressure or density altitude is greater than 14 000 ft CHECK FLIGHT ID This is an advisory system message indicating the MRC Flight ID number does not match the pilot entered FMS Flight ID number following 7 seconds after the pilot entry CHECK GPSX POSI...

Page 59: ... is less than 40 C or the OAT is greater than the value obtained from the HD Limit ISA 35 Table CHECK VOR DME X POSITION This is an alerting system message indicating the radio position is out of limits and X represents the radio number CHECK PD PLACEMENT This is an advisory operator message indicating the waypoint was inserted someplace other than the intended leg as indicated by the entry COMPAR...

Page 60: ...an advisory operator message indicating the flight plan name entered to save the active flight plan already exists in the custom database END OF FLIGHT PLAN This is an alerting system message indicating the last defined waypoint has been passed This message does not apply to the destination waypoint ENDING WPT NOT FOUND This is an advisory operator message indicating the ending waypoint of a fligh...

Page 61: ...ing a pattern in a stored flight plan FLT PLAN RECEIVED This is an alerting system message indicating a flight plan has been received through a datalink This message is displayed when datalink indicates a new flight plan has been received FMS EXITING HOLD This is an alerting system message indicating the hold termination altitude has been reached and the HOLD is automatically exiting FMS POSITIONS...

Page 62: ...ocedure turn INDEPENDENT OPERATION This is an alerting system message indicating the system reverted to independent operation due to a problem with the selected operating mode INTERSECTION NOT FOUND This is an advisory operator message indicating the entered place distance does not intersect the active flight plan INVALID AIRCRAFT DB This is an alerting system message indicating the aircraft datab...

Page 63: ...SA deviation to be exceeded at the altitude LABEL CAN NOT BE CHANGED This is an advisory message indicating the label specified in the aircraft database is a required label for the aircraft and can not be changed LAST LEG This is an alerting system message indicating the active leg is the last leg of the flight plan and the TO waypoint is not the destination LIST FULL This is an advisory operator ...

Page 64: ...ested requiring the present position In addition this message is displayed when an FMS mode key is selected and there is no present position NOT A NAVAID This is an advisory operator message displayed when an entry is required to be a navaid and something other than a navaid is entered NOT A HELIPORT This is an advisory operator message displayed when an entry is required to be a heliport and some...

Page 65: ...UESTED DATA NOT RCVD This is an advisory system message indicating the FMS has timed out while waiting for the requested data to be received from the datalink RESET ALT SEL This is an alerting system message indicating the FMS is commanding a new altitude but the altitude selector has not been reset The aircraft does not make altitude changes until the selector has been reset RUNWAY NOT FOUND This...

Page 66: ...ude constraint UNABLE OFFSET This is an advisory operator message indicating the pilot attempted to insert an offset while holding a standard terminal arrival route STAR or a standard instrument departure SID UNABLE PCDR TURN CHANGE This is an advisory operator message indicating the pilot attempted to adjust the procedure turn after sequencing on to the procedure turn UNABLE RNP This is an alerti...

Page 67: ... MAX ANG This is an advisory system message indicating a vertical direct to is greater than 6 degrees VERT DIR UNDER MIN ANG This is an advisory system message indicating a vertical direct to is less than one VGP UNAVAILABLE This is an alerting system message indicating vertical glide path VGP is not available WAYPOINT NOT FOUND This is an advisory operator message indicating the entered waypoint ...

Page 68: ...vigation database When no approach or an instrument landing system ILS localizer LOC LOC BC landing directional aid LDA simplified directional facility SDF or microwave landing system MLS approach is selected the APP annunciator does not light The aircraft position is between 2 NM outside the final approach fix FAF and the missed approach point MAP The DGR annunciator must be removed or turned off...

Page 69: ...the MCDU display brightness When manually selected a bright dim bar is displayed in the scratchpad as shown in Figure 3 7 The bright dim bar level is controlled by pushing BRT or DIM on the MCDU display Figure 3 7 Bright Dim Bar Level Following manual adjustment the photo sensors monitor the ambient light and maintain the brightness level of the MCDU display over various lighting conditions Note t...

Page 70: ...he JPOOL9 departure with the College Station CLL transition KDAL RW13L JPOOL9 CLL shown in Figure 4 2 The flight arrives to Houston with the instrument landing system ILS approach for runway 4 BLUBL1 is selected with the CLL transition BLUBL1 CLL RW4 KHOU shown in Figures 4 3 and 4 4 The standard instrument departure SID standard terminal arrival route STAR approach waypoints and airways used in t...

Page 71: ...al or East Houston terminal area airports or via J 87 to overfly TNV TORNN TRANSITION For aircraft landing at Lafayette Lake Charles or Beaumont Port Arthur airports 114 8 CEDAR CREEK D L CQY N32 11 1 W096 13 1 LOC DME 111 1 ILVF 1 At 1300 5 5 D M E IL VF or IV O W hdg 360 TSA Gliderport 156 166 176 186 37 35 35 36 ARDIA JPOOL9 ARDIA JASPA JPOOL9 JASPA D D D D JASPA ARDIA N32 17 1 W096 56 3 N32 17...

Page 72: ...t System FMS for the Agusta AW139 AB139 Helicopter A28 1146 181 REV 3 Mar 2009 4 3 Operational Example Honeywell International Inc Do not copy without express permission of Honeywell Figure 4 3 Houston TX BLUBL Arrival ...

Page 73: ...t System FMS for the Agusta AW139 AB139 Helicopter A28 1146 181 REV 3 Mar 2009 Operational Example 4 4 Honeywell International Inc Do not copy without express permission of Honeywell Figure 4 4 Houston TX ILS Approach ...

Page 74: ...s permission of Honeywell PREDEPARTURE The FMS guides the pilot through the ground initialization process using the lower right line select key 6R After completing the page or pages for each step pushing the lower right key 6R moves to the next step Figure 4 5 is a flow chart showing the preflight procedure for a normal flight Figure 4 5 FMS Preflight Procedure Flow Chart ...

Page 75: ...oftware identifier is displayed at 3L for verification The software identifier must be referenced when maintenance action is requested The maintenance prompt 6L is used to verify the FMS system operating configuration Navigation database information is displayed on the right side of the NAV IDENT page The active database dates are shown at 1R The dates for the alternate period are shown at 2R On p...

Page 76: ...e LAST POS coordinates at 1L At 2L the closest RAMPX within 3 nautical miles NM of the last position 1L is displayed When no RAMPX waypoint is available the closest airport reference point ARP or Heliport within 3 NM of the last position 1L is displayed When no ARP is available the pilot is prompted to enter a waypoint or coordinates In this example the KDAL ARP is shown At 3L the coordinates of t...

Page 77: ...position the appropriate LOAD prompt 1R 2R or 3R is pushed The selected position becomes the FMS position as shown in Figure 4 8 Selecting the LOAD prompt initializes connected sensors receiving inputs from the FMS The position loaded on one FMS is transferred to the cross side FMS so that both have the same initial position Selecting the LOAD prompt continues the preflight process Figure 4 8 POSI...

Page 78: ...abase the airport KDAL in this example is already loaded in the ORIGIN line as shown in Figure 4 9 An entry of estimated time of departure ETD as an option is entered in order to give the estimated time of arrivals ETAs prior to takeoff To enter an ETD type the estimated departure time in the scratchpad preceded by a slash for example 1435 and put the entry into 1L Entering an ETD supports predict...

Page 79: ...ll International Inc Do not copy without express permission of Honeywell The destination KHOU is entered in the scratchpad and line selected to the DEST prompt at 2R as shown in Figure 4 10 01773 03 Figure 4 10 ACTIVE FLT PLAN 1 2 The FLT PLAN LIST page is displayed when a stored flight plan has the same origin and destination ...

Page 80: ...er in the scratchpad and using the line select key adjacent to the VIA TO prompt 01774 06 Figure 4 11 ACTIVE FLT PLAN 1 2 Page The upper right corner of the ACTIVE FLT PLAN page indicates there are two pages for the active flight plan The next page of the active flight plan is displayed by pushing the NEXT function key The previousactive flight plan page is displayed by pushing the PREV function k...

Page 81: ...01774 07 Figure 4 12 ACTIVE FLT PLAN The line select key adjacent to the VIA TO prompt 3L is pushed to close the flight plan as shown in Figure 4 13 The destination must be included as the last flight plan waypoint for estimated time en route ETE to the destination on the PROGRESS page The destination is also required to calculate performance data Figure 4 13 Destination on ACTIVE FLT PLAN 1 2 Pag...

Page 82: ...thout express permission of Honeywell The alternate flight plan example is entered by selecting the ALTERNATE FPL page shown in Figure 4 14 by pushing the NEXT function key 01783 04 Figure 4 14 ALTERNATE FPL 5 5 The alternate destination is entered in 1R San Antonio KSAT is used for this example as shown in Figure 4 15 01784 05 Figure 4 15 ALTERNATE FPL 5 5 Page ...

Page 83: ...The alternate flight plan is entered the same way as for the en route flight plan The alternate flight plan is closed by moving KSAT to the VIA TO line as shown in Figure 4 16 01785 05 Figure 4 16 Alternate Flight Plan Page Moving KSAT to the VIA TO line completes the flight plan definition Pushing the lower right line select key 6R begins performance initialization PERF INIT When performance has ...

Page 84: ...m the previous flight or aircraft database ACDB Assuming the aircraft is flown the same way each flight performance initialization consists of verifying the default values making changes where required and entering items such as wind and weight Depending on the pilot selected weight configuration from the multifunction display MFD systems dropdown menu weights are displayed in either pounds or kil...

Page 85: ... Honeywell International Inc Do not copy without express permission of Honeywell D PERFORMANCE INIT 1 3 The PERFORMANCE INIT 1 3 page is displayed in Figure 4 17 The following is displayed on the PERFORMANCE INIT 1 3 page Aircraft type 1L Selected performance mode 2L Tail Number 1R Figure 4 17 PERFORMANCE INIT 1 3 Page ...

Page 86: ...ode is done by entering the calibrated airspeed CAS data directly Default values are restored by using the DELETE function on the appropriate line Figure 4 18 PERFORMANCE INIT 2 3 The descent angle entered on the PERFORMANCE INIT 2 3 page is used as the default value for each path In addition the descent angle is used for computing top of descent TOD points The FMS uses the climb cruise and descen...

Page 87: ...nal Example 4 18 Honeywell International Inc Do not copy without express permission of Honeywell D PERFORMANCE INIT 3 3 The PERFORMANCE INIT 3 3 page is displayed in Figure 4 19 Data associated with the weight of the aircraft is displayed on the PERFORMANCE INIT 3 3 page Figure 4 19 PERFORMANCE INIT 3 3 ...

Page 88: ... important performance calculations made by the FMS such as the hover ceiling velocity hover limit and velocity flyaway limit Category A ceiling altitudes best range and endurance are also displayed D PERF DATA 1 4 The PERF DATA 1 4 page shown in Figure 4 20 shows information computed by the FMS Hover ceiling velocity hover limit and velocity flyaway limit are determined by using density altitude ...

Page 89: ...ing velocity hover limit and velocity flyaway limit are displayed on the PERF DATA 2 4 page shown in Figure 4 21 Hover ceiling velocity hover limit and velocity flyaway limit are determined by using density altitude information computed by the FMS and the tables in the Agusta ECM Current range speed and distance are displayed on line 4 and current endurance speed and distance are displayed on line...

Page 90: ...Mar 2009 4 21 Operational Example Honeywell International Inc Do not copy without express permission of Honeywell D PERF DATA 3 4 Category A ceiling altitudes for various types of takeoffs and landings are displayed on the PERF DATA 3 4 page shown in Figure 4 22 Figure 4 22 PERF DATA 3 4 ...

Page 91: ...ational Example 4 22 Honeywell International Inc Do not copy without express permission of Honeywell D PERF DATA 4 4 The status of the environmental control system ECS engine air particle separator EAPS and heater are displayed on the PERF DATA 4 4 page shown in Figure 4 23 Figure 4 23 PERF DATA 4 4 ...

Page 92: ...ed using four pages D DEPARTURE SURFACES The DEPARTURE SURFACES page shown in Figure 4 24 is displayed by pushing the DEPARTURE prompt on the ACTIVE FLT PLAN page The available surfaces for the origin airport are displayed In this example surface 13L is selected with line select key 2L 02134 02 Figure 4 24 DEPARTURE SURFACES 1 2 The DEPARTURE prompt is selected after the CONFIRM INIT on PERF INIT ...

Page 93: ...not copy without express permission of Honeywell D SIDs After the runway is selected the SIDs page shown in Figure 4 25 is displayed with the possible departure procedures For this example JPOOL9 at 2R is selected When no SID is to be used the ACTIVATE prompt 6R selects the runway and the ACTIVE FLT PLAN page is displayed 00660 08 Figure 4 25 SIDs 1 1 ...

Page 94: ...Inc Do not copy without express permission of Honeywell D DEPARTURE TRANS When a SID is selected the DEPARTURE TRANS page shown in Figure 4 26 is displayed The DEPARTURE TRANS page lists the en route transitions for the selected departure For this flight the College Station CLL transition 5L is selected 00661 07 Figure 4 26 DEPARTURE TRANS 1 1 ...

Page 95: ...active flight plan The SID contains both the lateral waypoints and any vertical constraints for the procedure contained in the database 00662 07 Figure 4 27 PROCEDURE 1 1 Flight Plan Discontinuities When a discontinuity occurs in a flight plan while adding a SID or STAR the discontinuity is caused by the lack of a common point between the flight plan and the inserted SID or STAR The discontinuity ...

Page 96: ...pter A28 1146 181 REV 3 Mar 2009 4 27 Operational Example Honeywell International Inc Do not copy without express permission of Honeywell The ACTIVE FLT PLAN page shown in Figure 4 28 is displayed when activating the departure Figure 4 28 ACTIVE FLT PLAN 1 5 Page ...

Page 97: ... or helipad number and International Civil Aviation Organization ICAO identifier 1L Runway heading when a runway is selected 1L Runway length or helipad dimensions 1R Temperature 2L Surface wind 2R Pressure altitude 3L BARO barometric setting 3L Surface elevation 3R Figure 4 29 TAKEOFF 1 2 Surface information is retrieved from the database Temperature is sensed or entered Barometric setting BARO s...

Page 98: ... Honeywell D TAKEOFF 2 2 The TAKEOFF 2 2 page is displayed in Figure 4 30 The following is displayed on the TAKEOFF 2 2 page when a runway is selected as the departure surface When a helipad is selected only density altitude is displayed Surface slope 1L Surface width 1L Surface threshold 1R Surface stopway 2L Headwind tailwind and crosswind 2R Density altitude 3L Figure 4 30 TAKEOFF 2 2 ...

Page 99: ... the prompt RW POS at 6R is displayed on the ACTIVE FLT PLAN page Once the aircraft is at the surface threshold the FMS is updated to the surface threshold position NOTE This is an option as FMS position is equal to GPS position when installed Updates are made by pushing the line select key 6R adjacent to the RW POS prompt on the ACTIVE FLT PLAN page as shown in Figure 4 31 The POSITION INIT page ...

Page 100: ...le Honeywell International Inc Do not copy without express permission of Honeywell D POSITION INIT 1 1 The coordinates for the selected surface RW13L are displayed on the POSITION INIT 1 1 page shown in Figure 4 32 and makes the coordinates available for loading Figure 4 32 Runway Coordinates on POSITION INIT 1 1 Page ...

Page 101: ...xample 4 32 Honeywell International Inc Do not copy without express permission of Honeywell D Threshold Position Update Pushing the line select key 2R adjacent to the surface coordinates loads the surface threshold position into the FMS as shown in Figure 4 33 Figure 4 33 LOAD Prompt on POSITION INIT 1 1 Page ...

Page 102: ...n the ground when an ETD is entered prior to takeoff Once airborne the ETA for the FROM waypoint is replaced with the actual crossing time ETEs for any waypoint in the flight plan are available on PERF PLAN pages or PROGRESS page 1 Figure 4 34 ETA on ACTIVE FLT PLAN 1 5 Page The FMS is selected and coupled to the flight director shortly after take off Initially the FMS is armed on the flight direc...

Page 103: ...ssion of Honeywell D Waypoint Sequencing On takeoff the surface becomes the FROM waypoint and remains on the top line of the ACTIVE FLT PLAN page The TO waypoint is shown on the second line As the aircraft passes the TO waypoint all waypoints scroll up one line as shown in Figure 4 35 This process is called waypoint sequencing Figure 4 35 Waypoint Sequencing on ACTIVE FLT PLAN 1 5 ...

Page 104: ...Honeywell D PROGRESS 1 3 Information available on the PROGRESS 1 3 page shown in Figure 4 36 is displayed by pushing the PROG key The PROGRESS 1 3 page includes the navigation mode DME DME in the example shown and the required and estimated position uncertainty Figure 4 36 PROGRESS 1 3 Page ACTIVE FLT PLAN page 1 and PROGRESS page 1 are considered the primary pages of the FMS during flight ...

Page 105: ...ed The following is displayed on the PROGRESS 2 3 page Speed command 1L Altitude command 1L Distance and TOC 2L Current fuel quantity 2R Distance and TOD 3L Current gross weight 3R Figure 4 37 PROGRESS 2 3 Page The TOC and TOD points are not displayed as waypoints as part of the ACTIVE FLT PLAN However they are displayed on the map and vertical profile when available The positions of these waypoin...

Page 106: ...ll D PROGRESS 3 3 Information available on the PROGRESS 3 3 page shown in Figure 4 38 is displayed by pushing the NEXT key when the PROGRESS 2 3 page is displayed The following information is displayed on the PROGRESS 3 3 page Cross track error 1L Offset 1R Track and drift 2L Heading 2R FMS computed wind headwind and crosswind 3L FMS computed ground speed 3R 01574 02 Figure 4 38 PROGRESS 3 3 Page ...

Page 107: ... Altitude restrictions associated with a waypoint are entered on the multifunction control display unit MCDU adjacent to the appropriate waypoint The 7000 feet at constraint on ARDIA was entered at 2R as shown in Figure 4 39 Figure 4 39 Constraint Information on ACTIVE FLT PLAN 1 5 The PERF DATA prompt at 6R is displayed after takeoff until the aircraft is within 200 NM of the destination The PERF...

Page 108: ...the revision is after the TO waypoint the flight plan is modified by adding or deleting waypoints 2 When the revision effects the TO waypoint such as clearance direct from present position to another point that is done by pushing the DIR key The ACTIVE FLT PLAN page 1 is displayed by pushing the DIR function key regardless of what page is currently being displayed When the direct to waypoint is al...

Page 109: ...elevationand any entered altitude constraints Once in descent the FMS sets the target altitude to the altitude selector or the next constraint whichever is higher ARRIVAL When within 200 flight plan miles of the destination airport the ARRIVAL prompt is displayed at 6R as shown in Figure 4 41 Pushing the ARRIVAL prompt selects an arrival procedure or surface The ARRIVAL page is always accessed fro...

Page 110: ...l D ARRIVAL Page The ARRIVAL page shown in Figure 4 42 is displayed when the ARRIVAL prompt on the APPROACH page is selected The destination airport is displayed at 1R with access to selecting the surface approach and or STAR While the selection is made in any order this example selects 2L to choose an approach Selecting an approach automatically selects a surface 02131 05 Figure 4 42 ARRIVAL 1 1 ...

Page 111: ...ut express permission of Honeywell D APPROACH Page The APPROACH page shown in Figure 4 43 is displayed with the available approach procedures to permit selection of the assigned or required approach Selecting an approach also includes the missed approach procedure From the KHOU APPROACH page the ILS 04 approach 5R is selected 01867 02 Figure 4 43 KHOU APPROACH 1 2 ...

Page 112: ...n in Figure 4 44 is displayed Selection of the appropriate transition is accomplished on the APPROACH TRANS page For this example the CARCO 2L approach transition is selected The default vectors course into the final approach fix FAF is shown in 1L The default course is automatically provided using information from the navigational database NDB When no default course is available dashes are displa...

Page 113: ...without express permission of Honeywell D STAR Page After the approach is selected the STAR page is displayed with the available arrival procedures as shown in Figure 4 45 When an arrival procedure has been assigned selection from the list is accomplished on the STAR page From the STAR page the BLUBL2 arrival is selected 1L 0 1869 03 Figure 4 45 KHOU STAR 1 1 ...

Page 114: ...he assigned STAR transition is accomplished on the STAR TRANS page For the current example the CLL transition 1L is selected After the transition is selected the ARRIVAL page is displayed with a summary of the selections as shown in Figure 4 47 When no STAR and or STAR TRANS is to be used the ARRIVAL prompt 6R returns the system to the ARRIVAL summary page having the ACTIVATE prompt as shown in Fi...

Page 115: ...ress permission of Honeywell Figure 4 47 KHOU ARRIVAL 1 1 APPROACH Once the arrival selection is activated the FMS guidesthe aircraft along the STAR and approach procedure When a localizer based approach is selected as in this example final approach is flown using the flight director When a nonprecision approach is selected the FMS is used for guidance on final approach ...

Page 116: ... is displayed in Figure4 48 The following is displayed on the LANDING page Surface identifier 1L Surface heading 1L Runway length or helipad dimensions 1R Temperature 2L Surface wind 2R Pressure altitude barometric BARO setting 3L Surface elevation 3R Figure 4 48 LANDING 1 2 Surface information is retrieved from the database For landing both surface temperature and wind are required entries for la...

Page 117: ...express permission of Honeywell D LANDING 2 2 The following values are displayed on the LANDING 2 2 page shown in Figure 4 49 when a runway is selected When a runway is not selected DENSITY ALT only is displayed on the LANDING 2 2 page Surface slope 1L Surface width 1L Surface threshold 1R Headwind tailwind and crosswind 2R Density altitude 3L Figure 4 49 LANDING 2 2 ...

Page 118: ...int MAP TheMAP is also in the active flight plan When activated the missed approach is inserted into the active flight plan after the MAP Figure 4 50 MISSED APRCH 4 5 The MISSED APPR prompt is displayed at 6L on the ACTIVE FLT PLAN page when 2 NM before sequencing the final approach fix FAF or 5 NM from the surface end The missed approach is activated by selecting the MISSED APPR prompt 6L or push...

Page 119: ... an alternate has been entered the ALTERNATE prompt is displayed on the ACTIVE FLT PLAN page when the aircraft is within 25 NM of the destination When the flight plan contains an approach the ALTERNATE prompt is displayed only after the missed approach has been activated When an ALTERNATE is selected before the destination is reached the FMS guides the aircraft to the original destination and then...

Page 120: ...ight plan is inserted into the active flight plan as a string of waypoints starting at the point of insertion Flight plans are also cleared one waypoint at a time using the DEL key While on the ground entering a new origin after some or all of the flight plan has been defined is permitted When the new origin is already a waypoint in the flight plan the waypoints before the first appearance of the ...

Page 121: ...ht Management System FMS for the Agusta AW139 AB139 Helicopter A28 1146 181 REV 3 Mar 2009 Operational Example 4 52 Honeywell International Inc Do not copy without express permission of Honeywell Blank Page ...

Page 122: ...st be reviewed and the CONFIRM INIT prompt at 6R on the last page of initialization must be pushed Performance calculationscan take some time to be displayed after initializing or after the flight condition is changed NOTE Performance information in the FMS is based on data entered by the pilot and calculated by the FMS Mission planning data has not been evaluated by the Federal Aviation Administr...

Page 123: ... selectable at any time Pushing the line select key adjacent to the respective function selects the function Figure 5 1 PERF INDEX 1 1 The following figures correspond to the line select keys shown in Figure 5 1 The associated functions are described later in this section D 1L PERF INIT is shown in Figure 5 2 page 5 3 D 2L TAKEOFF is shown in Figure 5 16 page 5 27 D 3L PERF PLAN is shown in Figure...

Page 124: ...selected to complete performance initialization D Pilot Speed Fuel Flow The FMS uses pilot entered speed schedules and winds to perform time calculations The fuel calculations are based on pilot entered cruise fuel flow Adjustments are made for the higher fuel flow in climb D Current Ground Speed Fuel Flow The fuel calculations are based on the current fuel flow shown on the FUEL MGT page When a f...

Page 125: ...Flight Management System FMS for the Agusta AW139 AB139 Helicopter A28 1146 181 REV 3 Mar 2009 Performance 5 4 Honeywell International Inc Do not copy without express permission of Honeywell Blank Page ...

Page 126: ...em FMS for the Agusta AW139 AB139 Helicopter A28 1146 181 REV 3 Mar 2009 Performance 5 5 5 6 Honeywell International Inc Do not copy without express permission of Honeywell Figure 5 3 Performance Initialization Block Diagram ...

Page 127: ...ss gauge value is available D Baggage weight D Pilot and passenger weight An average cruise wind is entered when available Pilot Speed Fuel Flow SPD FF Method The PILOT SPD FF method of performance initialization has a total of three pages D PERFORMANCE INIT 1 3 The following information is displayed on the PERFORMANCE INIT 1 3 page shown in Figure 5 4 1L Aircraft type ACFT TYPE is displayed at 1L...

Page 128: ...ion is required on future flights The tail number is used for the following two purposes 1 Naming of the aircraft database file When the aircraft database file is saved to disk the database file is named using the tail number 2 Data management unit DMU The tail number is used by DMU for the loading of the navigation database The tail number is also used to upload and download the custom and aircra...

Page 129: ...w However when on the ground the FMS default ground speed is used The FMS default ground speed is displayed at 1R on the first page of anystored flight plan Once airborne the current ground speed is used The current fuel flow is displayed at 1R of the FUEL MGT 1 2 page The fuel flow value is permitted to be overridden by pilot entry and is then used 3L Selecting PILOT SPD FF bases performance calc...

Page 130: ...hase of flight Figure 5 6 PERFORMANCE INIT Page 2 3 1L The CLIMB speed schedule is displayed in calibrated airspeed CAS Changes are made by entering a CAS in the scratchpad and pushing 1L A pilot entered climb speed schedule is stored from previous operation and is displayed on initial power up Entering DELETE returns to the default climb speed schedule as defined in the ACDB Pilot entered values ...

Page 131: ...eturns to the default descent speed schedule as defined in the ACDB Pilot entered values between 60 and Vne are permitted Any value entered outside of this range and the INVALID ENTRY scratchpad message is displayed A default value of 140 knots is displayed at 3L if the ACDB is invalid or unavailable In addition to the speed entries a default descent angle is displayed at 3L When the angle is ente...

Page 132: ...fault CRUISE WINDS value is zero In addition the altitude is entered before the cruise wind is accepted Entering DELETE returns the default value of zero 5R 5R is associated with 5L and gives the pilot the ability to specify the cruise wind altitude Data entry is consistent with entry of cruise altitude on other FMS pages The default value is set to zero In addition the FMS gives the pilot the abi...

Page 133: ...efault value is the value from the aircraft database 4L This field is used to enter the final approach distance The default value is the value from the aircraft database 6L The vertical navigation VNAV DATA prompt is used to return to the VNAV DATA 1 1 page without making any selections 1R The RETURN prompt is used to return to the PERFORMANCE INIT 2 3 page without making any selections When an in...

Page 134: ...s line shows the go around speed for the clean configuration The default value is the value from the aircraft database Pilot entry is permitted Entering DELETE returns the default value 1R The RETURN prompt is used to return to the PERFORMANCE INIT 2 3 page without making any selections D PERFORMANCE INIT LB 3 3 The data associated with the weight of the aircraft is displayed on the PERFORMANCE IN...

Page 135: ...set to the previous values from the prior flight or the dashed if the ACDB is invalid or unavailable The value displayed in 1R is meters M when the selected units are KG or inches IN when the selected units are LB 2L The aircraft fuel is entered at 2L The fuel gauge value is also displayed at 2L 2R Weights carried in stretchers which comes as an option is entered at 2R The STR F A weights are defa...

Page 136: ...s the GROSS WT is calculated as the sum of the other weight fields GROSS WT is periodically re calculated every 10 seconds The following indication is provided when the GROSS WT is outside of the minimum or maximum max values D The GROSS WT value is displayed in cyan reverse video D A BELOW GROSS WT scratchpad message is displayed when the GROSS WEIGHT is below the minimum gross weight in the ACDB...

Page 137: ...ade by the FMS such as the hover ceiling velocity hover limit and velocity flyaway limit Category A ceiling altitudes and best range and endurance are also displayed The performance data pages are displayed when an active flight plan and performance initialization is completed When changes are made to the flight plan performance data computations are updated In flight factors such as unexpected wi...

Page 138: ...OPE is displayed in the scratchpad When the density altitude is greater than 20 000 ft the OAT is less than 40 C or the OAT is greater than the value obtained from the HD Limit ISA 35 Table the message CHECK FLIGHT ENVELOPE is displayed in the scratchpad D 2L The hover ceiling in ground effect HOV CEIL IGE is the maximum allowable density altitude for hovering when the helicopter is in ground effe...

Page 139: ...splayed in reverse video and no pilot entry is permitted D 4L Performance Data Page 1 The best range speed BST RANGE SPD is displayed in KIAS at 4L Best range speed is the speed at which the aircraft achieves the best range for the average gross weight pressure altitude and OAT When the hook load is greater than zero the best range speed is limited to 90 knots D 4L Performance Data Page 2 The curr...

Page 140: ...ed D 5R Performance Data Page 2 The current endurance time CUR ENDUR TIME is displayed at 5R The current endurance time is the time aloft time remaining in air when the aircraft is flown at the CUR ENDUR SPD at 5L No pilot entry is permitted D 6L The prompt CAT A is displayed at 6L and is used to access the PERF DATA page 3 D 6R Performance Data Page 1 The prompt CURRENT SPD is is displayed at 6R ...

Page 141: ...he DENS ALT 1R the CATEGORY A CEILING HELIPAD altitude is displayed in reverse video D 3R The CATEGORY A CEILING HD for takeoff to a landing SHORT FLD area with limited obstacle clearance is displayed at 3R The category A ceiling density altitude is obtained from Agusta performance tables using current OAT and gross weight When the CATEGORY A CEILING SHORT FLD altitude is less than the DENS ALT 1R...

Page 142: ...ir particle separator EAPS and heater is displayed on the PERF DATA 4 4 page shown in Figure 5 12 Figure 5 12 PERF DATA 4 4 Page The following line select keys correspond to the associated definitions on the PERFORMANCE DATA page 4 shown in Figure 5 12 D 1L The operational status of the ECS is displayed at 1L D 2L The EAPS INSTALLED is displayed at 2L D 3L The operational status of the EAPS when i...

Page 143: ... The estimated fuel remaining and estimated time en route ETE for each leg of the flight as shown in Figure 5 13 is displayed on the PERF PLAN pages No flight plan changes are made from this page The PREV and NEXT keys are used to review the entire flight plan In addition to this information this page shows a wind temperature W T prompt right line selects for each waypoint 00558 05 Figure 5 13 PER...

Page 144: ... 00564 07 Figure 5 14 WIND TEMP 2 X D 1L The waypoint is displayed No entry is permitted However the PREV and NEXT keys are used to cycle through the waypoints in the flight plan D 1R Pushing this line select key returns the display to the PERF PLAN page D 2L The predicted altitude from the performance computations is displayed here Altitude entries are permitted Altitude entries are used to assig...

Page 145: ...s displayed as shown in Figure 5 15 A valid wind temperature entry requires entry of an altitude and entry of wind and or temperature When an entry is valid the data is displayed in reverse video and the ENTER prompt is displayed 00564 05 Figure 5 15 WIND TEMP WIND AND TEMPERATURE MODEL BLENDING The FMS wind and temperature model blends wind and temperature entries with the current position sensed...

Page 146: ...e at an individual waypoint the entry erases any previous entry The entry is applied to each waypoint forward in the flight plan until a waypoint with another entry is encountered Applying the entry to forward waypoints permits long flight plans to be subdivided into segments for the purpose of making wind temperature entries After an entry has been made the 6L prompt CLEAR is displayed The CLEAR ...

Page 147: ...creased temperature also effects the fuel flow the MAX attainable altitude and so on Therefore the closer the entered winds and temperatures are to the actual encountered conditions the better the FMS performance predictions Takeoff Pages Database information about the departure surface when one has been selected is displayed on the TAKEOFF 1 2 page shown in Figure 5 16 Figure 5 16 TAKEOFF 1 2 Pag...

Page 148: ...the database is displayed in feet When no runway has been selected an entry is made at 1L or when a different length is desired The pilot enters a runway length on this line Entering DELETE returns the default length or prompts When the surface is a helipad DIMENSIONS is displayed in small white font Dimensions are displayed in length and width format or diameter as provided by the database When a...

Page 149: ...yed in inches of mercury or millibars The last entered pilot values are displayed for pilot entered values The form used on the primary flight display is displayed for the sensed values The default is set in inches of mercury The pilot enters elevation or pressure altitude and or baro set When an entry is made the value not entered is calculated from the entered value For example when the pilot en...

Page 150: ...evation or pressure altitude When an entry is made the value not entered is calculated from the entered value For example when the pilot enters an elevation the pressure altitude is calculated When the pressure altitude is entered the elevation is calculated When baro set is entered the parameter being calculated is recalculated Entry of DELETE removes any pilot entry and the highest priority valu...

Page 151: ... line is blank No entry is permitted D 1R The threshold of the takeoff runway is displayed When no surface has been selected entry prompts are displayed When the takeoff surface is a helipad this line is blank D 2L The stopway of the takeoff runway is displayed When no surface has been selected entry prompts are displayed When the takeoff surface is a helipad this line is blank D 2R Head tailwind ...

Page 152: ...ed in the flight plan or a different runway is desired entry of the runway number or runway heading is made on this line PIlot entries are displayed in magnetic heading For example an entry of 29 is displayed as 290_ No airport is displayed when a runway number is entered Entering DELETE returns the flight plan runway or prompts The runway heading is used to resolve the surface winds Entry of a ne...

Page 153: ...lue is followed by DIA and is separated by a space When the selected surface is a helipad the pilot entries are inhibited 2L The outside air temperature is displayed in this field An entry is made in degrees Celsius or degrees Fahrenheit but not both The celsius temperature is displayed in the scratchpad by pushing 2L Entering DELETE removes the temperature and displays prompts When temperature co...

Page 154: ...pilot enters a pressure altitude the elevation is calculated When the pilot enters a baro set the parameter being calculated is recalculated When the pilot enters a baro set when both sensed pressure altitude and sensed baro altitude are displayed pressure altitude is calculated based on the entered baro set and the elevation is displayed 3R The runway helipad elevation from the database is displa...

Page 155: ...P page is displayed when the TEMP COMP prompt is pushed 5R Selection of this line accesses the ARRIVAL page 6L Access to DESCENT is on this line when the performance mode is FULL PERF 6R Selection of this line gives access to the ACTIVE FLT PLAN page D The calculated data from the information on the LANDING 1 2 page is displayed on the LANDING 2 2 page shown in Figure 5 19 The LANDING 2 2 page is ...

Page 156: ...e airspeed ground specific range and air specific range are displayed on the FUEL MGT LB page shown in Figure 5 20 00600 05 Figure 5 20 FUEL MGT LB 1 2 1L The current fuel weight calculated by the FMS is displayed in large characters and is the same value as the fuel weight on the PERFORMANCE INIT 3 3 page When the performance initialization has not been completed dashes are displayed Entering a f...

Page 157: ...eight based on engine usage and leakage when a leak exists The scratchpad message COMPARE FUEL QUANTITY is displayed when the FMS fuel weight differs from the gauge value by more than 2 5 of the BOW This message is inhibited when the fuel quantity has been manually entered on the PERFORMANCE INIT 3 3 page Entering a manual fuel flow can create significant differences between the FMS fuel quantity ...

Page 158: ... on the ground The total fuel used is the same as displayed at 2L on the FLIGHT SUMMARY page Resetting fuel used on the FLIGHT SUMMARY page also resets individual engine fuel used on this page AIRCRAFT DATABASE The aircraft database includes information specific to an aircraft type The aircraft database is furnished by Honeywell The aircraft database is downloaded from the aircraft using a data lo...

Page 159: ... are seen in Figures 6 1 and 6 2 When the NAV button is pushed NAV INDEX 1 2 page shown in Figure 6 1 is displayed NAV INDEX 2 2 page shown in Figure 6 2 is displayed by using either the PREV or NEXT paging keys These pages show navigation functions that are selected at any time Selection of each function is accomplished by pushing the line select key adjacent to the respective function Page numbe...

Page 160: ... Figure 6 10 page 6 12 D 3L NAV IDENT is shown in Figure 6 129 page 6 175 D 4L POS SENSORS is shown in Figure 6 48 page 6 62 D 5L CROSS PTS is shown in Figure 6 146 page 6 196 D 6L DEPARTURE is shown in Figure 6 32 page 6 37 D 1R FPL SEL is shown in Figure 6 7 page 6 9 D 2R DATA BASE is shown in Figure 6 17 page 6 19 D 3R FLT SUM is shown in Figure 6 156 page 6 206 D 5R PATTERNS is shown in Figure...

Page 161: ...well The following figures correspond to the line select keys shown in Figure 6 2 and the associated functions are described further in this section 00607 09 Figure 6 2 NAV INDEX 2 2 D 1L POS INIT is shown in Figure 6 143 page 6 193 D 2L DATA LOAD is shown in Figure 6 151 page 6 201 D 1R CONVERSION is shown in Figure 6 75 page 6 96 D 2R MAINTENANCE is shown in Figure 6 131 page 6 177 ...

Page 162: ...Honeywell FLIGHT PLAN LIST The FLIGHT PLAN LIST page lists pilot defined flight plans stored in the flight management system FMS memory From this page the pilot defines a flight plan deletes flight plans or selects a flight plan to activate When no flight plans are stored in the FMS the flight plan list page is blank as shown in Figure 6 3 01592 01 Figure 6 3 FLIGHT PLAN LIST 1 1 ...

Page 163: ...ter A28 1146 181 REV 3 Mar 2009 6 5 Navigation Honeywell International Inc Do not copy without express permission of Honeywell When flight plans have been defined the page lists the flight plans by name as shown in Figure 6 4 01593 01 Figure 6 4 Flight Plan Defined ...

Page 164: ...between any two nontemporary waypoints navaids intersections airports etc A flight plan from Phoenix to Minneapolis is used to illustrate how to define a flight plan Refer to Procedure 6 1 Step Procedure 6 1 Stored Flight Plans 1 Selecting FPL LIST from the NAV INDEX 2 Enter the flight plan name into the scratchpad In this example KPHX KMSP is entered refer to Figure 6 5 for flight plan name forma...

Page 165: ... identifier separated by a dash the FMS automatically fills in the origin and destination A single alphanumeric character is added following the destination identifier to distinguish multiple flight plans between the same origin and destination When other formats for the flight plan name are used the pilot fills in the origin and destination 5 Enter ground speed at 1R when a speed other than the o...

Page 166: ...onfiguration is set to ON a larger selection of patterns is stored 8 Close the flight plan by entering the destination waypoint as the last waypoint in the flight plan Entering the destination waypoint as the last waypoint is done by line selecting the destination from the right side of the page and inserting the last waypoint on the left side of the page Deleting Stored Flight Plans The DEL key i...

Page 167: ...age also calculates performance data of the stored flight plan The FLT PLAN SELECT page is accessed from the FLIGHT PLAN LIST page prompt at 6L or from the NAV INDEX page 01596 02 Figure 6 7 FLT PLAN SELECT 1 1 Selecting and activating a stored flight plan is accomplished by following Procedure 6 3 Step Procedure 6 3 Select and Activate a Stored Flight Plan 1 Select FPL LIST from the NAV INDEX 2 S...

Page 168: ...lect key adjacent to the FLT PLAN prompt 1L to insert the flight plan name As an alternative the flight plan name is able to be entered directly from the key pad instead of being selected from the list When a flight plan name is entered that has not been previously defined the FMS shows pages that are used to enter an undefined flight plan 5 Select ACTIVATE by pushing 1R and INVERT ACTIVATE by pus...

Page 169: ...International Inc Do not copy without express permission of Honeywell Step Procedure 6 3 Select and Activate a Stored Flight Plan 6 An active flight plan exists when one of the activate prompts is selected The FMS requires a confirmation step as shown in Figure 6 9 01598 01 Figure 6 9 CONFIRM REPLACING ACTIVE FLIGHT PLAN ...

Page 170: ... shows a list of pilot defined waypoints stored in memory and any temporary waypoints refer to temporary waypoints 00617 04 Figure 6 10 PILOT WPT LIST 1 1 Procedure 6 4 and Procedure 6 5 describes the two different ways to store pilot defined waypoints Step Procedure 6 4 Stored Waypoints Option One 1 Select WPT LIST from the NAV INDEX 2 Enter an identifier of one to five characters and line select...

Page 171: ...int names A page similar to Figure 6 11 is displayed when an undefined waypoint is entered on any page that accepts waypoint entries except the position initialization POS INIT page For these cases the RETURN prompt is displayed at 1R The RETURN prompt is used before or after a waypoint is defined The RETURN prompt is used to return to the page where the undefined waypoint was entered When the way...

Page 172: ...e 6 4 Stored Waypoints Option One 5 The defined waypoint is displayed as shown in Figure 6 12 Figure 6 12 Defined Waypoint 6 OR Enter place bearing distance and select to 3L Use the example PXR 126 7 where PXR defines place 126 defines bearing in degrees and 7 defines distance in nautical miles NM Bearing inputs are assumed magnetic True bearings are designated by placing the letter T after the be...

Page 173: ...ne 7 The defined waypoint is displayed as shown in Figure 6 13 Figure 6 13 PILOT WAYPOINT Defined 8 OR Enter Place Bearing Place Bearing and select to 3L Use the example PXR 130 TFD 358 where PXR defines a place 130 is the radial from PXR in degrees TFD defines a second place and 358 defines the radial from TFD in degrees Bearing inputs are assumed to be magnetic True bearings are designated by pl...

Page 174: ... Honeywell International Inc Do not copy without express permission of Honeywell Step Procedure 6 4 Stored Waypoints Option One 9 The defined waypoint is displayed as shown in Figure 6 14 When a waypoint is defined by P B P B only the coordinates are stored and displayed Figure 6 14 Waypoint Defined by P B P B ...

Page 175: ...46 181 REV 3 Mar 2009 6 17 Navigation Honeywell International Inc Do not copy without express permission of Honeywell Step Procedure 6 5 Stored Waypoints Option Two 1 Enter latitude longitude and select to 1L N3320 77W11152 58 is used in Figure 6 15 Figure 6 15 Show Waypoint ...

Page 176: ...Waypoints Option Two 2 The PILOT WAYPOINT page is displayed shown in Figure 6 16 Figure 6 16 PILOT WAYPOINT Page 3 Enter an identifier of one to five characters and line select to show WAYPOINT line 1L When an identifier was previously used or matched an identifier in the navigation database NDB or custom database CDB the ALREADY EXISTS scratchpad message is displayed This prevents the duplication...

Page 177: ...d using the DATA BASE function as shown in Figure 6 17 00625 03 Figure 6 17 DATA BASE WPT 1 1 A waypoint identifier of the database is entered in the upper left line by entering the identifier into the scratchpad and pushing 1L The following items are displayed from the navigation database D Airports D Heliports D Runways D Helipads D Navaids D ILSs D Intersections The waypoint list WPT LIST 6L an...

Page 178: ... 20 Honeywell International Inc Do not copy without express permission of Honeywell Airports Heliports The following airport or heliport data is displayed in Figures 6 18 through 6 20 D DATA BASE WPT 1 3 Identifier 1L Waypoint type 1R Airport heliport name 2L Country 3L 00621 04 Figure 6 18 DATA BASE WPT 1 3 ...

Page 179: ...ter A28 1146 181 REV 3 Mar 2009 6 21 Navigation Honeywell International Inc Do not copy without express permission of Honeywell D DATA BASE WPT 2 3 Identifier 1L Coordinate position 2L Field elevation 3L Magnetic variation 3R 00622 05 Figure 6 19 DATA BASE WPT 2 3 ...

Page 180: ...181 REV 3 Mar 2009 Navigation 6 22 Honeywell International Inc Do not copy without express permission of Honeywell D DATA BASE WPT 3 3 Identifier 1L Access to airport runways 2L when available Access to heliport helipads 3L when available 01601 02 Figure 6 20 DATA BASE WPT 3 3 ...

Page 181: ...ion Honeywell International Inc Do not copy without express permission of Honeywell The associated RUNWAY or HELIPAD page is displayed when the prompt 2L or 3L on DATA BASE WPT 3 3 is pushed The RUNWAYS page shown in Figure 6 21 is displayed in this example by pushing 2L 01091 04 Figure 6 21 KPHX RUNWAYS 1 1 ...

Page 182: ...ywell International Inc Do not copy without express permission of Honeywell When one of the runways is selected the runway data is displayed as shown in Figure 6 22 The airport RUNWAYS page shown in Figure 6 21 is displayed when the RETURN prompt in 6R is selected 00623 04 Figure 6 22 DATA BASE WPT 1 3 Return Prompt ...

Page 183: ...without express permission of Honeywell Surfaces Helipads The following information for runways is displayed in Figures 6 23 through 6 25 Similar information is obtained for helipads D DATA BASE WPT 1 3 Runway or helipad identifier 1L Waypoint type 1R Airport or heliport name 2L and country 3L 01603 02 Figure 6 23 DATA BASE WPT 1 3 for Runway Helipad ...

Page 184: ...py without express permission of Honeywell D DATA BASE WPT 2 3 Identifier 1L Runway heading and front or back course when the runway has an associated instrument landing system ILS 1R Heliport dimensions when a heliport is selected 1R Coordinate position 2L Elevation 3L Magnetic variation 3R 01604 02 Figure 6 24 DATA BASE WPT 2 3 for Runway Helipad ...

Page 185: ...well D DATA BASE WPT 3 3 This page is only available when a runway is selected Helipad information is contained on DATA BASE WPT pages one and two Identifier 1L Stopway 1R Width 2L This field is blank when runway width is not available in the navigation database Length 2R ILS glideslope when applicable 3L Displaced threshold 3R 01605 03 Figure 6 25 DATA BASE WPT 3 3 for Runway Helipad ...

Page 186: ...hown in Figure 6 26 shows the following information about navaids D Waypoint identifier 1L D Country 1L D Frequency 1R D Type 2L DME distance measuring equipment N DME noncolocated TACAN N TACAN noncolocated VORTAC VORDME VOR N VOR noncolocated D Class 2R HA high altitude LA low altitude T terminal UR unrestricted D Coordinate position 2L D Elevation 3L D Magnetic declination 3R 00626 03 Figure 6 ...

Page 187: ...the difference between the zero degree radial of the station and true north For many navaids this is not equal to the local magnetic variation due to the constantly changing earth magnetic field When magnetic declination is not available magnetic variation is displayed Figure 6 27 shows the DATA BASE WPT page for a nondirectional beacon The letters NB are entered after the identifier 01607 02 Figu...

Page 188: ...t Landing Systems The following data for instrument landing systems is displayed on the DATA BASE WPT 1 1 page shown in Figure 6 28 D ILS identifier 1L D Country 1L D Front course 1R D Frequency 1R D Type 2L ILS LOC localizer LOCDME localizer with DME ILSDME ILS with DME MLS D Category 2R I II III D Localizer antenna coordinates 2L D Magnetic declination 3R 00627 03 Figure 6 28 DATA BASE WPT 1 1 I...

Page 189: ...national Inc Do not copy without express permission of Honeywell Intersections The following data for intersections is displayed on the DATA BASE WPT 1 1 page shown in Figure 6 29 D Intersection identifier 1L D Country 1L D Intersection coordinates 2L D Magnetic variation 3R 00628 03 Figure 6 29 DATA BASE WPT 1 1 Intersections ...

Page 190: ...us waypoint is shown at the top of the page For all other cases the location closest to the aircraft position is shown at the top of the page For example when Thermal California TRM is entered on the DATA BASE WPT page the FMS shows all the TRM waypoints found on the WAYPOINT SELECT page as shown in Figure 6 30 00629 05 Figure 6 30 WAYPOINT SELECT 1 2 Pushing the line select key adjacent to the de...

Page 191: ...n database about waypoints and procedures used in flight planning and to tune navaids for position determination The database supplied by Honeywell is updated every 28 days The navigation database is designated with a version number region name and cycle number e g Version 3 01 WORLD3 310 The FMS uses a Version 3 01 navigation database or other approved version number The region name e g WORLD 3 N...

Page 192: ...waypoints for the airway Custom Database The custom database consists of pilot defined waypoints and stored flight plans Up to 1000 pilot defined waypoints are permitted to be stored The pilot stores commonly flown routes using the pilot defined flight plan procedure The pilot activates a flight plan from the FMS custom database rather than repeat the flight plan entry procedure The FMS custom dat...

Page 193: ...o KDEN is used as the origin of the active flight plan Figure 6 31 shows the PIKES4 departure for KDEN Refer to Procedure 6 6 for departure selection The beginning of the selection process isdisplayed when at any point in the departure selection process an airport or heliport is entered in 1L Following selection of a SID the following methods must be used to modify the departure procedure in the a...

Page 194: ...ent System FMS for the Agusta AW139 AB139 Helicopter A28 1146 181 REV 3 Mar 2009 Navigation 6 36 Honeywell International Inc Do not copy without express permission of Honeywell Figure 6 31 Denver CO PIKES4 Departure ...

Page 195: ...of the origin and a DEST is entered Access to the DEPARTURE page is always available from the NAV INDEX The default airport at 1L is the origin of the active flight plan When the origin is not defined or when the origin is not an airport or heliport prompts are displayed for entry of an airport When the origin waypoint is not an airport access to SIDs is for review only When the active flight plan...

Page 196: ...6 181 REV 3 Mar 2009 Navigation 6 38 Honeywell International Inc Do not copy without express permission of Honeywell Step Procedure 6 6 Departure Selection 3 Select the SID from the SIDs page shown in Figure 6 33 PIKES4 3L is selected in this example Figure 6 33 SIDs 1 1 Page ...

Page 197: ...09 6 39 Navigation Honeywell International Inc Do not copy without express permission of Honeywell Step Procedure 6 6 Departure Selection 4 Select the departure transition from the DEPARTURE TRANS page shown in Figure 6 34 ALS 2L is selected in this example Figure 6 34 DEPARTURE TRANS 1 1 Page ...

Page 198: ...VIEW is selected in this example Figure 6 35 PROCEDURE 1 1 Page DETAILS Select REVIEW to review the selected procedure or select ACTIVATE to insert the selected procedure into the active flight plan The ACTIVATE prompt is displayed on these pages only when the airport is the origin airport of the flight plan Selecting REVIEW or ACTIVATE partway through the selection procedure ends the departure se...

Page 199: ...e 6 36 Changing to the next review page is done by pushing the NEXT key Figure 6 36 SID REVIEW 1 2 SID REVIEW 1 X Figure 6 36 shows the selected runway SID and transition as they would look when ACTIVATED into the flight plan The runway threshold elevation of 5350 feet is displayed in blue on the right side of the page The first leg after the discontinuity removable with the DELETE button is a cli...

Page 200: ...t page or review in this example Select CLEAR 6L or ACTIVATE 6R Figure 6 37 SID REVIEW 2 2 SID REVIEW 2 X Figure 6 37 consists of a heading of 195_ to waypoint TEHEV followed by a heading of 185_ to waypoint BINKE then ALS Pushing the CLEAR prompt 6L clears the selected procedure The DEPARTURES SURFACES page is displayed when pushing the CLEAR prompt 6L Selecting the ACTIVATE prompt 6R inserts the...

Page 201: ... activated selecting a surface is possible without affecting the previously selected procedure At any point in the selection process returning to the ARRIVAL page and review and or activate the selected items is possible On the ARRIVAL page when a new surface is selected not supported by a previously selected STAR or approach the previous procedures are not displayed for selection into the active ...

Page 202: ... procedure by performing a direct to a waypoint in the active flight plan or alternate flight plan D Delete the procedure by activating a flight plan from the custom database D Delete the FROM waypoint in the active flight plan D Delete the procedure turn waypoint in the active flight plan D Delete the hold attribute from the course reversal hold waypoint Figure 6 38 shows the STAR plate Refer to ...

Page 203: ...nt System FMS for the Agusta AW139 AB139 Helicopter A28 1146 181 REV 3 Mar 2009 6 45 Navigation Honeywell International Inc Do not copy without express permission of Honeywell Figure 6 38 Minneapolis MN KASPR2 Arrival ...

Page 204: ...REV 3 Mar 2009 Navigation 6 46 Honeywell International Inc Do not copy without express permission of Honeywell Step Procedure 6 7 Arrival Selection 1 Select ARRIVAL from the active flight plan or NAV INDEX 2 Select RUNWAY APPROACH or STAR from the ARRIVAL page shown in Figure 6 39 ...

Page 205: ...hen the aircraft is within 200 flight plan miles of the destination The default airport at 1R is the destination of the active flight plan When the destination is not defined or when the destination is not an airport heliport prompts are displayed to enter the airport heliport Previous selections are displayed on this page Selections are also deleted on this page The surface approach or STAR is se...

Page 206: ...copy without express permission of Honeywell Step Procedure 6 7 Arrival Selection 3 Select the desired surface from the RUNWAY page shown in Figure 6 40 In this example runway 30L 5L is selected 02135 01 Figure 6 40 KMSP SURFACE 1 1 Any previously selected surface is labeled as ACT or SEL When necessary more than one page of runways is displayed ...

Page 207: ...p Procedure 6 7 Arrival Selection 4 Select the approach from the APPROACH page When the surface is selected first the FMS shows only the approaches for the selected surface as shown in Figure 6 41 In this example ILS 30L 2L is selected 01600 02 Figure 6 41 KMSP APPROACH 1 1 When only the straight in portion of an approach is desired select the approach without selecting an approach transition ...

Page 208: ...42 The VECTORS approach into the final approach fix FAF is shown in 1L The default course into the FAF is automatically provided using information from the NDB When no default course is available dashes are displayed The course is modified by upselecting a value into 1L The VECTORS approach is automatically selected as the default and is accepted by pushing the ARRIVAL prompt on 6R Otherwise any o...

Page 209: ...1 REV 3 Mar 2009 6 51 Navigation Honeywell International Inc Do not copy without express permission of Honeywell Step Procedure 6 7 Arrival Selection 6 Select the STAR from the STAR page shown in Figure 6 43 In this example KASPR2 4L is selected 00699 05 Figure 6 43 KMSP STAR 1 1 ...

Page 210: ...r 2009 Navigation 6 52 Honeywell International Inc Do not copy without express permission of Honeywell Step Procedure 6 7 Arrival Selection 7 Select the STAR transition from the STAR TRANS page shown in Figure 6 44 In this example MCW 3L is selected 00700 05 Figure 6 44 KMSP STAR TRANS 1 1 ...

Page 211: ...on of Honeywell Step Procedure 6 7 Arrival Selection 8 Once all selections have been made the ARRIVAL page shown in Figure 6 45 is automatically displayed The choices from this page are to repeat the selection process when necessary ACTIVATE 6R inserts the selection in the flight plan or REVIEW 6L In this example REVIEW 6L is selected 02126 01 Figure 6 45 ARRIVAL 1 1 REVIEW ...

Page 212: ...ll International Inc Do not copy without express permission of Honeywell Step Procedure 6 7 Arrival Selection 9 Review to verify the selection prior to activation into the active flight plan Page 2 4 is displayed by pushing the NEXT paging keys from page 1 4 shown in Figure 6 46 00701 07 Figure 6 46 ARRIVAL REVIEW 1 4 ...

Page 213: ...tep Procedure 6 7 Arrival Selection 10 At any time in the review process the ACTIVATE prompt 6R as shown in Figure 6 47 activates the approach into the active flight plan The CLEAR prompt 6L returns to the selection process The review process is continued by using the paging keys through the end of the procedure including the missed approach procedure 00702 05 Figure 6 47 ARRIVAL REVIEW 2 4 ...

Page 214: ...pproaches since the FMS is not authorized to be coupled during localizer approaches The degraded DGRAD annunciator must be off throughout the approach When the DGRAD annunciator turns on the FMS must not be used for the remainder of the approach The flight crew can continue the approach using raw data or conduct the missed approach procedure D When FMS VNAV guidance is used on the approach verify ...

Page 215: ...differential global positioning system These approaches are flown by displaying the localizer data and by using the flight director autopilot However these procedures are selected and activated on the FMS to enhance situational awareness The FMS shows the approach on the EFIS map displays The FMS is used to fly the approach transition and the missed approach phases of precision approaches When the...

Page 216: ...ucting a direct to activating another approach or activating another flight plan and then continue to fly the procedure Changing an altitude or angle constraint associated with an approach waypoint Add holding patterns orbits or radial intercepts to approach waypoints Changing the destination and then continue to fly the approach procedure to the original destination The examples listed in Table 6...

Page 217: ...B139 Helicopter A28 1146 181 REV 3 Mar 2009 6 59 Navigation Honeywell International Inc Do not copy without express permission of Honeywell Table 6 1 Typical FMS Pattern Displays Approach Transition Chart Depiction FMS Groundtrack DME Arc Procedure Turn ...

Page 218: ...proach Transition FMS Groundtrack Chart Depiction Holding Pattern Course Reversal Teardrop See Note NOTE Following sequence of WPT the FMS turns to capture the final approach course The FMS is not flying a defined ground track during this maneuver Depending on speed and teardrop geometry the FMS can roll wings level on a 45_ intercept to the final approach course Typically the aircraft banks until...

Page 219: ... position differences from the FMS position Other sensors do not contribute to the FMS position unless GPS becomes unavailable or inaccurate When the DME DME navigation mode is used the FMS automatically tunes the scanning DMEs to give the best position from DME DME In VOR DME mode the bearing error increases with distance from the navaid thus reducing the accuracy of the VOR DME position as the a...

Page 220: ... airspace FMS position assessment is done by checking the navigation mode on PROGRESS page 1 and cross checking FMS position with raw VOR DME information The PPOS DIRECT crossing points page assists in cross checking by giving the FMS bearing and distance to the selected station and comparing that to raw VOR DME data The POS SENSORS page shown in Figure 6 48 is selected from the NAV INDEX page or ...

Page 221: ...vated the FMS position is corrected to the selected position The FMS UPDATE page shown in Figure 6 49 isdisplayed bypushing the line select key adjacent to the UPDATE prompt 1R on the POS SENSORS page shown in Figures 6 48 The FMS UPDATE page shows the current FMS POSITION 1L MANUAL prompt 2L and a SENSOR prompt 2R 00711 03 Figure 6 49 FMS UPDATE 1 1 Procedure 6 8 uses the manual position UPDATE f...

Page 222: ...Navigation 6 64 Honeywell International Inc Do not copy without express permission of Honeywell Step Procedure 6 8 FMS Manual Position Update by Flyover 1 Select POS SENSORS from the NAV INDEX 2 Before reaching ZUN select the UPDATE prompt 1R as shown in Figure 6 50 Figure 6 50 POS SENSORS UPDATE ...

Page 223: ... crosses over the navaid select the MANUAL prompt 2L as shown in Figure 6 51 00711 03 Figure 6 51 FMS UPDATE 1 1 Page DETAILS The FMS position is recorded when the MANUAL prompt is pushed as the aircraft crosses over ZUN This recorded position labeled FREEZE POSITION is displayed as shown in Figure 6 52 The FREEZE POSITION is not the current FMS position but is the FMS position when the manual pro...

Page 224: ...3 Mar 2009 Navigation 6 66 Honeywell International Inc Do not copy without express permission of Honeywell Step Procedure 6 8 FMS Manual Position Update by Flyover 4 Enter either an identifier or coordinates for the REF WPT For this example enter ZUN as the REF WPT Figure 6 52 REF WPT ...

Page 225: ...e difference between ZUN and the FREEZE POSITION FMS position when the aircraft overflew ZUN Figure 6 53 shows the FMS position was 3 0 NM 1 3 NM South and 2 7 NM West from ZUN when the aircraft flew over the navaid At this point one of two selections is made When the ENTER prompt is pushed a 3 NM correction is added to the present FMS position 1 3 NM North and 2 7 NM East This jumps the current F...

Page 226: ... Do not copy without express permission of Honeywell Step Procedure 6 8 FMS Manual Position Update by Flyover 6 For either selection the current FMS POSITION is displayed as shown in Figure 6 54 on the FMS UPDATE page 00711 03 Figure 6 54 FMS POSITION DETAILS Any position sensor set to receive an update is also updated to the new position ...

Page 227: ...f Honeywell Updating the FMS position to one of the long range sensors is possible as described in Procedure 6 9 When the FMS position is invalid Procedure 6 9 cannot be used to update the FMS position Step Procedure 6 9 FMS Position Update to Long Range Sensor 1 Select POS SENSORS from the NAV INDEX 2 Select the UPDATE prompt 1R as shown in Figure 6 55 Figure 6 55 UPDATE Prompt ...

Page 228: ...A28 1146 181 REV 3 Mar 2009 Navigation 6 70 Honeywell International Inc Do not copy without express permission of Honeywell Step Procedure 6 9 FMS Position Update to Long Range Sensor 3 Select the SENSOR prompt as shown in Figure 6 56 00711 03 Figure 6 56 SENSOR Prompt ...

Page 229: ...well International Inc Do not copy without express permission of Honeywell Step Procedure 6 9 FMS Position Update to Long Range Sensor 4 Select the UPDATE prompt right line selects as shown in Figure 6 57 for the sensor to be used for updating the FMS In this example GPS 1 2R is selected Figure 6 57 GPS UPDATE Prompt ...

Page 230: ...re 6 9 FMS Position Update to Long Range Sensor 5 Select ENTER at 6R to update the FMS position or CLEAR 6L to reset the update function as shown in Figure 6 58 Following either selection the FMS UPDATE page shown in Figure 6 54 is displayed with the current FMS position 00713 03 Figure 6 58 Reset Update Function DETAILS Any position sensors set to receive an update are also updated to the new pos...

Page 231: ...e line select key adjacent to the STATUS prompt as shown in Figure 6 59 checks the status for that sensor on the POS SENSORS page Figure 6 59 STATUS Prompt The following paragraphs describe the status pages used for each type of sensor The POS SENSORS page shown in Figure 6 59 from where the sensor status was accessed is displayed for all sensor types by selecting the POS SENSORS prompt at the bot...

Page 232: ...4 Honeywell International Inc Do not copy without express permission of Honeywell GPS STATUS The following information is displayed on the GPS X STATUS 1 2 page shown in Figure 6 60 D GPS position D Ground speed D Altitude altitude above the earth D Miles from FMS position 00718 03 Figure 6 60 GPS 1 STATUS 1 2 ...

Page 233: ...he GPS altitude is not relative to pressure altitude but is referenced to an earth centered earth fixed ECEF coordinate system Pressure altitude is not relative to the same reference frame but relative to the standard pressure or local pressure settings Therefore significant differences are possible between GPS altitude and pressure altitude This concept is displayed in Figure 6 61 GPS ALTITUDE HE...

Page 234: ...ATUS 2 2 The following information is displayed on the GPS X STATUS 2 2 page shown in Figure 6 62 D Receiver Autonomous Integrity Monitoring RAIM D Horizontal Figure of Merit HFOM D Vertical Integrity Limit VINT D Vertical Figure of Merit VFOM D Time UTC and date D Operating mode D Satellites tracked Figure 6 62 GPS 1 STATUS 2 2 RAIM and FOM indicate current uncertainty of position expressed in NM...

Page 235: ... satellites are being tracked The GPS uses altitude from the digital air data computer DADC to aid in determining position in this mode When the GPS is operated inside a hangar or other areas where signals cannot be received a failure is detected by the GPS In this case cycling the power is necessary to restart the GPS The last line of the GPS STATUS page indicates the number of satellites being t...

Page 236: ...splayed 00720 03 Figure 6 63 PREDICTIVE RAIM 1 1 The PREDICTIVE RAIM page includes the following information D Predictive RAIM source 1L D Destination RAIM selection DEST prompt 1L D Destination identifier 2L D Estimated time of arrival ETA at destination 2L D Predicted RAIM solution for destination 3L D Pilot selection PILOT SEL prompt 1R D Pilot selected identifier 2R D Pilot entered time 3R D P...

Page 237: ...sage PREDICTIVE RAIM UNAVAILABLE is displayed on the PREDICTIVE RAIM page when the GPS fails or the interface between the FMS and GPS does not work properly Predictive RAIM is calculated using GPS almanac information The almanac within the GPS is automatically updated when the GPS is on and tracking satellites The almanac within the GPS is set invalid when the almanac is older than 3 5 days When t...

Page 238: ...1L D Destination ETA from the active flight plan 1R D Destination RAIM predicted for the ETA 1R D Destination RAIM predicted for ETA 15 minutes 2L D Destination RAIM predicted for ETA 10 minutes 3L D Destination RAIM predicted for ETA 5 minutes 3L D Destination RAIM predicted for ETA 5 minutes 2R D Destination RAIM predicted for ETA 10 minutes 3R D Destination RAIM predicted for ETA 15 minutes 3R ...

Page 239: ...he DESTINATION RAIM 2 2 page the pilot selects which GPS satellites are to be excluded from the DESTINATION RAIM predictions The pilot enters the pseudo random noise PRN code for the satellite scheduled to be out of service according to published GPS NOTAMs notice to airmen 01465 01 Figure 6 65 DESTINATION RAIM 2 2 D 2L 2R 3L and 3R The satellite PRN is entered on these lines Dashes are displayed ...

Page 240: ...e PREDICTIVE RAIM page 00722 04 Figure 6 66 PILOT SELECT RAIM 1 2 PILOT SELECT RAIM 1 2 page includes the following information D Identifier 1L D Time 1R D RAIM predicted for the ETA 1R D RAIM predicted for ETA 15 minutes 2L D RAIM predicted for ETA 10 minutes 3L D RAIM predicted for ETA 5 minutes 3L D RAIM predicted for ETA 5 minutes 2R D RAIM predicted for ETA 10 minutes 3R D RAIM predicted for ...

Page 241: ... 2L 2R 3L and 3R The satellite PRN is entered on these lines Dashes are displayed when DELETE is entered All PRN numbers are cleared after the aircraft has landed While the GPS is computing the predicted RAIM at the destination or pilot selected waypoint the message COMPUTING RAIM is displayed on the DESTINATION RAIM and PILOT SELECT RAIM pages Additional Details About PRN GPS satellites are ident...

Page 242: ...tellation A GPS receiver takes the satellite signal code and correlates the satellite code to one of the known stored 32 PRN codes within the receiver By correlation with the satellite transmitted code the receiver is able to determine which satellite is being received Knowing which satellite is being received the GPS receiver is able to make pseudo range measurements in determining a given naviga...

Page 243: ...ries in the permanent column up to 3 are stored in FMS memory until removed by pilot action Procedure 6 10 explains how to enter and delete entries from the NOTAM page Step Procedure 6 10 NOTAM Entries 1 Select POS SENSORS from NAV INDEX page 1 Select VOR DME 6L and then NOTAM 6R 2 Enter the navaid identifier into the scratchpad Push a line select key under either the permanent or temporary column...

Page 244: ...MS starts using the station to compute the aircraft position The class of a navaid and the aircraft altitude determine when the FMS can tune and use a navaid for navigation The class of a navaid is determined by entering the navaid identification on the DATA BASE WPT or PILOT WAYPOINT page The class of the navaid can differ in the FMS from the published class This is because the FMS database class...

Page 245: ...selection 1 Select POS SENSORS from the NAV INDEX 2 Push the delete key DEL DELETE is displayed in the scratchpad 3 Push the left line select key on the SENSOR page next to the sensor that is no longer used DESEL is shown adjacent to the sensor identifier and the U is removed adjacent to the sensor position 4 To reselect the deleted sensor push the delete key and DELETE is displayed in the scratch...

Page 246: ...elect the desired VOR DME by using the NEXT PREV keys 4 Push the delete key DEL DELETE is displayed in the scratchpad 5 Push the left line select key next to one of the station identifiers DESEL is displayed adjacent to all the station identifiers This action blocks the selected radio VOR and DME channels from being used by the FMS 6 To reselect the deleted radio push the delete key and DELETE is ...

Page 247: ...contains the navaids of type VOR DME VORTAC noncolocated VOR DME DME or VOR closest to the aircraft and within a maximum range of 320 NM of the aircraft The term noncolocated VOR DME also includes noncolocated VORTACs In addition the term DME includes TACANs The Candidates List is sorted such that the closest navaid to the aircraft is first The FMS assists tuning by displaying the ten closest nava...

Page 248: ...ional Inc Do not copy without express permission of Honeywell Step Procedure 6 13 NAV Tuning From Ten Closest Stations 2 cont 00827 05 Figure 6 70 NAV Prompt on PROGRESS 1 3 Page 3 Select the desired station from the ten closest stations as shown in Figure 6 71 TFD is selected in this example 00730 04 Figure 6 71 Desired Station ...

Page 249: ...7 08 Figure 6 72 TFD Tune To tune the NAV radios using the station identifier follow the steps in Procedure 6 14 Step Procedure 6 14 NAV Tuning by Identifier 1 Select PROG from the MCDU panel When Page 1 is not displayed select NEXT until Page 1 is displayed 2 Enter the station identifier into the scratchpad 3 Push the line select key 5L or 5R 4 The FMS tunes the NAV radio and the identifier and f...

Page 250: ... found the FMS searches the navaids listed in the flight plan e g ILS The frequency and identifier of the first matching navaid is displayed on the PROGRESS page When no matches are identified the identifier field remains dashed The FMS does not use ILS LOC GS data for position computations When a DME is associated with an ILS the FMS can use DME in position computation The small letter in front o...

Page 251: ... LNAV mode is selected before the pilot makes any changes to the NAV frequency When the pilot changes the NAV frequency autotune is re established by following Procedure 6 16 The FMS autotunes the localizer frequency for localizer based approaches For localizer autotuning frequency confirmation from the NAV receiver is conducted but the data is not checked by the FMS The pilot must rely on the pri...

Page 252: ...ission of Honeywell Step Procedure 6 16 NAV Tuning by Selecting Autotune 4 Use the DEL key to enter DELETE into the scratchpad as shown in Figure 6 73 Figure 6 73 Enter DELETE Into Scratchpad 5 Line select to NAV 1 5L or NAV 2 5R on the PROGRESS page The FMS switches to autotuning and the letter A is displayed as shown in Figure 6 74 Figure 6 74 FMS Switches to Autotune ...

Page 253: ...s Remote tuning by the pilot is possible while V is displayed When this is done the tuning mode changes to remote R When VOR is selected with the EFIS preview display feature autotuning is disabled Remote Tuning The tuning mode is remote when the pilot tunes the NAV radios through the FMS or from the radio tune source The FMS does not adjust pilot selected frequencies Radio tune sources are on the...

Page 254: ...s The CONVERSION1 4 page shown in Figure 6 75 gives conversion between English and metric units for length weight and volume 01634 01 Figure 6 75 CONVERSION 1 4 D 1L The equivalent meters at 1R is displayed when entry of feet is made at 1L D 1R The equivalent flight level FL in feet at 1L is displayed when entry of meters is made at 1R as shown in Figure 6 76 Note that in some locations of the wor...

Page 255: ...ernational Inc Do not copy without express permission of Honeywell 01102 01 Figure 6 76 CONVERSION 1 4 Page D 2L and 2R The equivalent weight in the opposite unit is displayed when entry of pounds or kilograms is made D 3L and 3R The equivalent weight in the opposite unit is displayed when entry of gallons or liters is made ...

Page 256: ...sion between English and metric units for temperature velocity and distance 01103 01 Figure 6 77 CONVERSION 2 4 D 1L and 1R The equivalent temperature in the opposite unit is displayed when entry of temperature is made D 2L and 2R The equivalent velocity in the opposite unit is displayed when entry of knots or meters per second is made D 3L and 3R The equivalent distance in the opposite unit is di...

Page 257: ...N 3 4 page shown in Figure 6 78 gives conversion between English and metric units for weights and volumes The conversion is based on a specific weight displayed on the page The specific weight is changed by the pilot 01635 01 Figure 6 78 CONVERSION 3 4 The remaining parameters are displayed when entry of pounds kilograms gallons or liters is made Figure 6 79 is an example with an entry of 10 000 p...

Page 258: ...based on the specific weights shown at 3L and 3R D 2L The equivalent pounds 1L kilograms 1R and liters 2R is displayed when entry of gallons is made on this line The conversion is based on the specific weights shown at 3L and 3R D 2R The equivalent pounds 1L kilograms 1R and gallons 2L is displayed when entry of liters is made on this line The conversion is based on the specific weights shown at 3...

Page 259: ...he Agusta AW139 AB139 Helicopter A28 1146 181 REV 3 Mar 2009 6 101 Navigation Honeywell International Inc Do not copy without express permission of Honeywell Figure 6 80 Average Specific Weight Variation of Aviation Fuels and Lubricants ...

Page 260: ...vel based on the local station pressure When an altimeter is set to QFE the aircraft altitude above a station is displayed With the altimeter set to QFE and the aircraft on the ground zero 0 is displayed on the altimeter Inflight QFE gives height above ground level without consideration for nonstandard temperature When an elevation exists at 1R entry of a QNH or QFE in any unit results in the rema...

Page 261: ...uivalent QNH in millibars hectopascals 3R and millimeters 4R When an elevation exists at 1R the equivalent QFE in inches of mercury 2L millibars hectopascals 3L and millimeters 4L is displayed Entering DELETE returns the default of dashes D 3R Entry of QNH in millibars hectopascals on this line results in the equivalent QNH in inches of mercury 2R and millimeters 4R being displayed When an elevati...

Page 262: ...DELETE returns thedefault of dashes D 3L The equivalent QFE in inches of mercury 2L and millimeters 4L is displayed when entry of QFE in millibars hectopascals is made on this line When an elevation exists at 1R the equivalent QNH in inches of mercury 2R millibars hectopascals 3R and millimeters 4R is displayed Entering DELETE returns thedefault of dashes D 4L The equivalent QFE in inches of mercu...

Page 263: ...In addition to the pilot defined patterns some procedures such as approach procedures contain patterns These database patterns are added to the flight plan when activating the approach procedure Pattern Definition Figure 6 83 shows each pattern type except the search patterns Procedures for using each pattern type are contained in this guide The following patterns are available in the FMS D HOLD p...

Page 264: ...out express permission of Honeywell TO NEXT WAYPOINT ENTRY LEG HOLDING PATTERN ORBIT PATTERN ORBIT FIX HOLD FIX RADIAL LEG RADIAL PATTERN PROCEDURE TURN NAVIGATION FIX INBOUND FIX INBOUND FIX TO NEXT WAYPOINT FIX PROCEDURE TURN FIX TO NEXT WAYPOINT FLYOVER PATTERN PILOT ENTERED OR PROCEDURE FIX SYSTEM GENERATED FIX fms049175 01 Figure 6 83 Pattern Formats ...

Page 265: ...n of Honeywell Pattern Review Reviewing patterns activated into the flight plan is permitted at any time This is conducted by selecting the PATTERNS prompt at 5R as shown in Figure 6 83 or by selecting the DIR key and pushing 6L PATTERN and then selecting REVIEW 6L The pilot can review all patterns of all types in the applicable flight plan 01674 02 Figure 6 84 Pattern Review ...

Page 266: ...fined on the HOLDING PATTERN page A typical holding pattern is displayed in Figure 6 85 NOTE With no constraints but a hold in descent VNAV can set up a path to the predicted altitude at hold and compute VDEV INBOUND COURSE TURN 1 HOLD FIX fms049170 01 OUTBOUND LEG INBOUND LEG TURN 2 LEG LENGTH N TURN DIRECTION Figure 6 85 Typical Holding Pattern The holding pattern entry type is based on geometry...

Page 267: ...f Honeywell DEFINING A HOLDING PATTERN A holding pattern is defined and reviewed by following Procedure 6 17 Step Procedure 6 17 Holding Pattern Definitions and Review 1 Select the DIR function key 2 Select the PATTERN prompt 6L as shown in Figure 6 87 01638 02 Figure 6 87 PATTERN Prompt DETAILS As an alternative the PATTERNS prompt can also be selected from the NAV INDEX Page 1 ...

Page 268: ...REV 3 Mar 2009 Navigation 6 110 Honeywell International Inc Do not copy without express permission of Honeywell Step Procedure 6 17 Holding Pattern Definitions and Review 3 Select the HOLD prompt at 1L as shown in Figure 6 88 HOLD is placed in the scratchpad Figure 6 88 HOLD Prompt ...

Page 269: ...ion Honeywell International Inc Do not copy without express permission of Honeywell Step Procedure 6 17 Holding Pattern Definitions and Review 4 Push the select key adjacent to the desired holding fix waypoint as shown in Figure 6 89 In this example MCW 2L is selected 00738 06 Figure 6 89 Desired Holding Fix ...

Page 270: ... necessary using the required steps 00739 07 Figure 6 90 Holding Pattern Definition DETAILS The default holding is a standard holding pattern at the designated holding fix with the inbound course set to the flight plan course into the holding fix Leg times are defaulted to 1 min 6 Enter any inbound course and or turn direction and push line select 3L The entry is made by entering the course follow...

Page 271: ... nor recommended The holding quadrant based on the inbound course entered by the pilot is displayed No entries are permitted for the entry procedure DETAILS When the holding quadrant is entered by the pilot the FMS sets the inbound course to the cardinal heading associated with the entered quadrant This can overwrite any pilot entered inbound course Thus pilot entry is not recommended for holding ...

Page 272: ...ng speed from the aircraft database c Predicted speed at waypoint d 90 kts 00739 07 Figure 6 91 Holding Speed 9 When desired enter an airspeed Entering DELETE returns the default holding speed displayed when the page was accessed DETAILS The speed command is changed to the holding speed at an appropriate distance to decelerate the aircraft by the time the holding fix is reached The holding speed i...

Page 273: ...attern Definitions and Review 11 Select the ACTIVATE 6R or the CLEAR 6L prompt as shown in Figure 6 92 ACTIVATE is selected in this example 00739 07 Figure 6 92 ACTIVATE CLEAR DETAILS When ACTIVATE is selected the holding pattern is entered into the active flight plan When CLEAR is selected the FMS does not insert the holding pattern into the active flight plan The HOLDING PATTERN page shows the h...

Page 274: ...o the holding fix on the ACTIVE FLT PLAN page shown in Figure 6 93 00740 05 Figure 6 93 Placement of Holding Pattern HOLDING AT PRESENT POSITION Procedure 6 18 describes holding at present position Refer to Procedure 6 17 for basic holding pattern definition Step Procedure 6 18 Holding at Present Position 1 Push the DIR function key 2 Select the PATTERN prompt at 6L As an alternative PATTERNS is s...

Page 275: ...ined and activated deleting the holding pattern before crossing the holding fix is possible Deleting the holding pattern is done by deleting the pattern from the ACTIVE FLIGHT PLAN page or from the HOLDING PATTERN page To delete the holding pattern from the ACTIVE FLT PLAN page follow Procedure 6 19 Refer to Procedure 6 20 for deleting holding pattern from the HOLDING PATTERN page Step Procedure 6...

Page 276: ... Inc Do not copy without express permission of Honeywell Step Procedure 6 20 Deleting a Holding Pattern From the Holding Pattern Page 1 Access the HOLDING PATTERN page Refer to Procedure 6 17 2 Select the DELETE prompt at 6R as shown in Figure 6 94 01639 03 Figure 6 94 Selecting the DELETE Prompt 3 Return to the active flight plan page ...

Page 277: ...ompt as shown in Figure 6 95 When selected before the holding fix is crossed the holding pattern is deleted from the flight plan 00741 06 Figure 6 95 Exiting a Holding Pattern After crossing the holding fix when the EXIT prompt is selected the aircraft turns back to the holding fix crosses the fix and continues with the flight plan Once the FMS starts holding at the fix and the EXIT prompt has bee...

Page 278: ...n relative to the holding pattern must be monitored When the high ground speed is maintained the aircraft can overshoot the outbound leg and possibly exceed protected airspace HOLDING PATTERN COURSE REVERSALS Holding patterns that are part of the approach transition are used to reverse the aircraft course and align the aircraft near the final approach course These procedures are only available fro...

Page 279: ...m approaches in the navigation database Using this data the FMS constructs the procedure turn with an outbound leg a turn out leg an arc leg and an inbound leg as shown in Figure 6 97 Only the outbound leg and the procedure turn PT angle are adjustable Figure 6 97 Typical Procedure Turn In the example shown in Figure 6 98 the ILS Runway 5 at KHOT approach transition contains a procedure turn that ...

Page 280: ...t System FMS for the Agusta AW139 AB139 Helicopter A28 1146 181 REV 3 Mar 2009 Navigation 6 122 Honeywell International Inc Do not copy without express permission of Honeywell 2 4 2 Figure 6 98 Hot Springs AR ILS Rwy 5 ...

Page 281: ... HOSSY The FMS is designed to keep the aircraft within protected airspace during procedure turns When the aircraft approaches the procedure turn at a ground speed resulting in the aircraft exceeding protected airspace the scratchpad message HIGH PCDR TURN GRD SPD high procedure turn ground speed is displayed 1 minute before the aircraft crosses the fix When this message is displayed the ground spe...

Page 282: ...ge A TURN prompt is displayed at 6L while the aircraft is on the outbound leg as shown in Figure 6 100 The TURN prompt is selected to immediately begin the turn out 00737 04 Figure 6 100 PROCEDURE TURN Once the procedure turn has started the active waypoint is INT01 This remains the active waypoint until INT01 is overflown on the way back to the FAF In this example the INTXX waypoint XX represents...

Page 283: ...ining a Procedure Turn The default turn angle is changed from the PROCEDURE TURN page Enter an angle between 20_ and 90_ prefixed with either an L left or R right specifying the turn out direction In addition the outbound leg is permitted to be changed by either specifying the outbound time OUTBD TIME in minutes or outbound distance OUTBD DIST in NM The controlling entry is in large capital letter...

Page 284: ... either of the following two waypoints of a procedure turn An INVALID DELETE message is displayed when an attempt is made to delete these waypoints EXITING A PROCEDURE TURN The procedure turn is flown automatically by the FMS and requires no manual exit The procedure turn is manually terminated while flying the procedure turn by selecting DELETE to either the PROCEDURE TURN header at 1L or the INT...

Page 285: ...ush DIR key 2 Select PATTERN prompt at 6L As an alternative PATTERNS are selected from the NAV INDEX page 2 3 Select the FLYOVER prompt at 2L This action places FLYOVER in the scratchpad 4 Push the left line select key adjacent to the desired flyover pattern fix waypoint The flyover is displayed as a reverse video F adjacent to the course flown to the waypoint With this option the aircraft flies t...

Page 286: ...ywell Orbit Pattern An orbit pattern shown in Figure 6 102 is used to fly an orbit circle around a given waypoint at a distance from 1 NM to 99 9 NM Orbit patterns are available only when SPECIAL MISSION is selected NOTE With no constraints and when an ORBIT is in descent VNAV is able to set up a path to the predicted altitude at the ORBIT and compute VDEV Figure 6 102 Orbit Definition ...

Page 287: ...2 Orbit Pattern Definition 1 Push the DIR key 2 Select the PATTERN prompt at 6L As an alternative PATTERNS are selected from the NAV INDEX page 2 3 Select the ORBIT prompt at 2R This action places ORBIT in the scratchpad 4 Push the left line select key adjacent to the desired orbit pattern fix waypoint 5 The ORBIT page shown in Figure 6 103 is displayed 00744 03 Figure 6 103 ORBIT 1 1 6 Enter the ...

Page 288: ... at the specified radius around the waypoint A prompt on the active flight plan page is used to reverse the direction of flight once in the orbit The reversal turn is always executed to the outside of the orbit DELETING AN ORBIT PATTERN An orbit pattern is deleted from the flight plan by selecting DELETE from the scratchpad to the appropriate waypoint On the active flight plan pages DELETE cannot ...

Page 289: ... waypoint Radial patterns are only available when SPECIAL MISSION is selected Figure 6 104 Radial Definition DEFINING A RADIAL PATTERN Follow Procedure 6 23 to define a radial pattern Step Procedure 6 23 Radial Pattern Definition 1 Push the DIR key 2 Select the PATTERN prompt at 6L As an alternative PATTERNS are selected from the NAV INDEX page 2 3 Select the RADIAL prompt at 3L This action places...

Page 290: ...plan to properly fly the radials as defined The inserted waypoints are displayed in reverse video Other waypoints cannot be inserted between radial waypoints Radial patterns are stored in a stored flight plan DELETING A RADIAL PATTERN When both the inbound and outbound radials are defined two temporary waypoints are inserted into the flight plan Either waypoint is permitted to be deleted individua...

Page 291: ...ple patterns on a given waypoint are also possible Refer to Table 6 3 for the possible combinations Table 6 3 Multiple Patterns Pattern Name Additional Pattern Permitted ORBIT RADIAL HOLDING FLYOVER PROCEDURE TURN ARC TURN NONE HOLDING FLYOVER RADIAL RADIAL HOLDING FLYOVER HOLDING FLYOVER When multiple patterns exist at a waypoint the order of delete is FLYOVER HOLD RADIAL When a HOLD or ORBIT is ...

Page 292: ... inserting this waypoint in the flight director prior to the current TO waypoint Resuming the flight plan while suspended can result in a direct to leg to the SUSXX waypoint or in a resume prompt selection from the ACTIVE FLT PLAN page The flight plan is also resumed by initiation of a direct to to the pilot entered waypoint or to any waypoint on the active flight plan DEFINING WAYPOINT SUSPEND A ...

Page 293: ...igation Honeywell International Inc Do not copy without express permission of Honeywell Step Procedure 6 24 Flight Plan Suspend Definition and Review 4 Push the select key adjacent to the desired SUSPEND waypoint as shown in Figure 6 107 In this example MCW 2L is selected Figure 6 107 ACTIVE FLT PLAN 6 9 ...

Page 294: ...tter S next to the desired suspended waypoint as shown in Figure 6 108 on the ACTIVE FLT PLAN page 01851 02 Figure 6 108 Suspended Waypoint FLIGHT PLAN SUSPEND AT PRESENT POSITION Procedure 6 25 describes flight plan suspend at the present position Refer to page 6 134 for basic suspend function definition Step Procedure 6 25 Flight Plan Suspend Definition at Present Position 1 Push the DIR button ...

Page 295: ...39 Helicopter A28 1146 181 REV 3 Mar 2009 6 137 Navigation Honeywell International Inc Do not copy without express permission of Honeywell Step Procedure 6 25 Flight Plan Suspend Definition at Present Position 3 cont 01674 02 Figure 6 109 PATTERNS Prompt ...

Page 296: ...ion 6 138 Honeywell International Inc Do not copy without express permission of Honeywell Step Procedure 6 25 Flight Plan Suspend Definition at Present Position 4 Select the SUSPEND prompt 4L as shown in Figure 6 110 This action places SUSPEND into the scratchpad Figure 6 110 PATTERNS 1 1 SUSPEND Prompt ...

Page 297: ... flight plan as shown in Figure 6 111 First waypoint on the first page of the ACTIVE FLIGHT PLAN Note The FMS names the PPOS suspend waypoint as SUSXX where XX is a two digit number Figure 6 111 PPOS Suspend Waypoint RESUMING THE FLIGHT PLAN Once a PPOS suspend has been defined and entered resuming the active flight plan is possible Resuming the flight plan is conducted from the ACTIVE FLT PLAN pa...

Page 298: ...tional Inc Do not copy without express permission of Honeywell Step Procedure 6 26 Resuming the Flight Plan 1 Display the ACTIVE FLT PLAN page showing the SUSPEND at present position as shown in Figure 6 112 Figure 6 112 Resume Flight Plan 2 Select the RESUME prompt 6L Confirm the initiation of DIR TO operation to SUS01 waypoint ...

Page 299: ...ed from the ACTIVE FLT PLAN page To delete the waypoint suspend from the ACTIVE FLT PLAN page follow Procedure 6 27 Step Procedure 6 27 Deleting a Flight Plan Suspend From the Active Flight Plan Pages 1 Display the active flight plan page showing the suspend waypoint as shown in Figure 6 113 01851 02 Figure 6 113 Suspend Waypoint on ACTIVE FLT PLAN 2 Push the DEL key DELETE is displayed in the scr...

Page 300: ...ng the pilot for surveillance and communication Four types of search and rescue patterns are supported by the FMS 1 Creeping ladder 2 Parallel 3 Expanding Square 4 Sector Defining a Search Pattern The FMS PATTERNS page includes a SEARCH prompt when search patterns are enabled by APM settings A search pattern is defined and reviewed by following Procedure 6 28 Step Procedure 6 28 Search Pattern Def...

Page 301: ...3 Mar 2009 6 143 Navigation Honeywell International Inc Do not copy without express permission of Honeywell Step Procedure 6 28 Search Pattern Definition 2 Select the SEARCH prompt 3R as shown in Figure 6 115 SEARCH is placed into the scratchpad Figure 6 115 PATTERNS 1 1 SEARCH Prompt ...

Page 302: ... pattern Figure 6 116 SEARCH PATTERNS Page The following default values are used when transition to the pattern definition page in the active flight plan occurs D When SEARCH is placed on the FROM waypoint PPOS andCUR TRK are used for the default start position and initial track respectively D When SEARCH is placed on the TO or subsequent waypoint the waypoint displayed as the default start positi...

Page 303: ... to define modify activate and cancel a square search pattern Figure 6 117 Expanding Square Search Definition DEFINING A SQUARE SEARCH PATTERN The steps in Procedure 6 29 define a square search pattern Step Procedure 6 29 Square Search Pattern Definition 1 Select the PATTERNS prompt 5R from the NAV INDEX page 2 Select the SEARCH prompt 3R This action places SEARCH into the scratchpad After SEARCH ...

Page 304: ...displayed at 1L The starting point is the flight plan waypoint selected by the pilot prior to accessing the SQUARE SEARCH page Otherwise the starting point is the PPOS when SEARCH isplaced on the FROM waypoint in the active flight plan The starting position is modifiable on the SQUARE SEARCH page All valid starting point waypoints are allowed except PBPB and PD temporary waypoints An INVALID ENTRY...

Page 305: ... and transitions back to the FMS PATTERNS page The RESTART prompt is available after the search patternbecomes active in the active flight plan When returning to the SQUARE SEARCH page the RESTART prompt is displayed when a search pattern is active When RESTART is selected the search pattern is restarted with the displayed search pattern D 2R The INIT TRK initial track used in the searchpattern is...

Page 306: ...ce or initial leg length results in an INVALID ENTRY scratchpad message The pattern radius is modifiable on the SQUARE SEARCH page D 6R Deletes search patterns activates newly defined search patterns or activates changes to the selected search pattern definition parameters During the initial definition of a new search pattern 6R is blank and not operational until all aspects of the search pattern ...

Page 307: ...ilot to define modify activate and cancel a sector search pattern Figure 6 119 Sector Search Definition DEFINING A SECTOR SEARCH PATTERN The steps in Procedure 6 30 define a sector search pattern Step Procedure 6 30 Sector Search Pattern Definition 1 Select the PATTERNS prompt 5R from the NAV INDEX page 2 Select the SEARCH prompt 3R This action places SEARCH into the scratchpad After SEARCH from t...

Page 308: ...splayed at 1L The starting point is the flight plan waypoint selected by the pilot prior to accessing the SECTOR SEARCH page Otherwise the starting point is the PPOS when SEARCH is placed on the FROM waypoint in the active flight plan The starting position is modifiable on the SECTOR SEARCH page All valid starting point waypoints are allowed except PBPB and PD temporary waypoints An INVALID ENTRY ...

Page 309: ...page D 4L A default SPEED of 90 kts is displayed and the speed is modifiable on the SECTOR SEARCH page D 6L Restores the default parameters and returns to the FMS PATTERNS page or restart the search pattern at the start position specified at 1L The CLEAR prompt is available during the initial definition of the search pattern and is available when the search pattern is not yet active Selecting CLEA...

Page 310: ...aypoints A turn anticipation distance is added to the leg spacing distance so the aircraft over flies the outbound and inbound radials specified by the pilot When the radius is smaller than the radial spacing an INVALID ENTRY scratchpad message is displayed The pattern radius is modifiable on the SECTOR SEARCH page D 6R 6R is used to delete search patterns activate newly defined search patterns or...

Page 311: ...ivate and cancel a creeping ladder search pattern Figure 6 121 Creeping Ladder Search Definition DEFINING A CREEPING LADDER SEARCH PATTERN The steps in Procedure 6 31 define a creeping ladder search pattern Step Procedure 6 31 Creeping Ladder Search Pattern Definition 1 Select the PATTERNS prompt 5R from the NAV INDEX page 2 Select the SEARCH prompt 3R This action places SEARCH into the scratchpad...

Page 312: ...s displayed at 1L The starting point is the flight plan waypoint selected by the pilot prior to accessing the LADDER SEARCH page Otherwise the starting point is the PPOS when SEARCH is placed on the FROM waypoint in the active flight plan The starting position is modifiable on the LADDER SEARCH page All valid starting point waypoints are permitted except PBPB and PD temporary waypoints An INVALID ...

Page 313: ...ER SEARCH page the RESTART prompt is displayed when a search pattern is active When RESTART is selected the search pattern is restarted with the displayed search pattern D 2R The PTRN TRK initial track used in the search pattern is defined at 2R The default heading displayed is the inbound course into the search pattern starting position waypoint when SEARCH is placed on any flight plan waypoint o...

Page 314: ...letes search patterns activates newly defined search patterns or activates changes to the selected search pattern definition parameters During the initial definition of a new search pattern 6R is blank and not operational until all aspects of the search pattern is defined When all aspects of the search pattern is defined with valid values ACTIVATE is displayed and 6R becomes operational When the S...

Page 315: ... modify activate and cancel a parallel search pattern Figure 6 123 Parallel Search Definition DEFINING A PARALLEL SEARCH PATTERN The steps in Procedure 6 32 define a parallel search pattern Step Procedure 6 32 Parallel Search Pattern Definition 1 Select the PATTERNS prompt 5R from the NAV INDEX page 2 Select the SEARCH prompt 3R This action places SEARCH into the scratchpad After SEARCH from the s...

Page 316: ...displayed at 1L The starting point is the flight plan waypoint selected by the pilot prior to accessing the PARALLEL SEARCH page Otherwise the starting point is the PPOS when SEARCH is placed on the FROM waypoint in the active flight plan The starting position is modifiable on the PARALLEL SEARCH page All valid starting point waypoints are permitted except PBPB and PD temporary waypoints An INVALI...

Page 317: ...splayed when a search pattern is active When RESTART is selected the search pattern is restarted with the displayed search pattern D 2R The INIT TRK used in the search pattern is defined at 2R The default heading displayed is the inbound course into the search pattern starting position waypoint when SEARCH is placed on any flight plan waypoint other than the FROM waypoint CUR TRK is displayed when...

Page 318: ...ition parameters During the initial definition of a new search pattern 6R is blank and not operational until all aspects of the search pattern is defined When all aspects of the search pattern is defined with valid values ACTIVATE is displayed and 6R becomes operational When the SAR pattern is activated the 6R prompt changes to DELETE Selecting the DELETE prompt removes the search pattern from the...

Page 319: ...x are consecutively numbered 000 001 002 and so on and named SPxxx where xxx is the number of the search pattern waypoint after the start waypoint to the end of the search pattern D All search pattern waypoints except the search pattern entry and exit waypoints SPAPx SPSTx SPEXx are displayed on the MFD with the waypoint number only for example SP005 is displayed as 005 A discontinuity is appended...

Page 320: ...R transitions back to the appropriate pattern definition page Figure 6 125 ACTIVE FLT PLAN Page SQUARE Prompt A FMS pattern for example hold radial or orbit placement on the search pattern waypoints is not permitted However insertion and removal of flyovers on individual waypoints is permitted When a direct to any waypoint outside the search pattern is performed the active search pattern is discon...

Page 321: ...point and subsequent search waypoint MARK ON TARGET MOT The mark on target MOT function gives the pilot the ability to mark a position as the helicopter is flying over a target and return the helicopter back to that position Often the MOT mode is used when flying a search pattern When performing a search the crew notes an object target to investigate The pilot flies the helicopter over the target ...

Page 322: ...ound maneuver so the helicopter is headed into the wind at the FHAF The FHAF is located approximately 3820 ft 1000 meters or 0 63 NM downwind of the target 2 Approach to Hover During this phase the helicopter follows FMS and automatic flight control system AFCS guidance to the hover HOV waypoint The hover waypoint is located approximately 150 ft 50 meters downwind and 150 ft 50 meters to the left ...

Page 323: ... flies a radio altitude hold VRHT until intersecting the 3 degree descent path Prior to intersecting the 3 degree descent path the FMS and AFCS remain in VALT After intersecting the 3 degree descent path the FMS provides vertical guidance by way of the vertical speed VS commands When the aircraft is above the descent path and the MOT is initiated the FMS commands a direct to descent VNAV to the FH...

Page 324: ... value when the aircraft passes the HOV waypoint D Vertical The flight director gives the vertical guidance commands based on the FMS vertical deviation signal The FMS vertical deviation signal provides the vertical deviation in feet from the 3 degree descent path into the HOV waypoint As the radar altitude approaches the final radar altitude selected by the pilot from 50 to 250 ft the flight dire...

Page 325: ...onstraint values are displayed on the MCDU next to the HOV waypoint D Sequencing The HOV waypoint remains in the flight plan until the MOT is canceled FINAL TARGET APPROACH After the HOV waypoint is reached the pilot assumes manual control of the aircraft When the pilot is finished investigating the target the MOT maneuver is normally canceled with a transition up TU maneuver The transition up man...

Page 326: ...D Vertical The MOTxx waypoint is at an altitude of 50 ft AGL based on RAD ALT D MCDU Speed Altitude Display The predicted CAS speed and altitude values associated with 0 kts GS and 50 ft AGL are displayed on the MCDU next to the MOTxx waypoint DISCONTINUITY A DISCONTINUITY is inserted after the MOTxx waypoint and before the SUSxx waypoint in the active flight plan When the MOT flight plan is activ...

Page 327: ... With MOTinitiated when flying a HOLD or ORBIT the original pattern fix is retained and the pattern terminated NOTE After MOT a subsequent return to the pattern fix results in re entering the HOLD ORBIT using normal FMS entry methodology When during an active MOT flight plan the FMS receives notification of subsequent MOT button pushes the following occurs D Pushing the MOT button for the first ti...

Page 328: ...th The FMS outputs the final glidepath angle to the hover waypoint for use by the AFCS MOT Flight Plan After engaging the MOT the FMS creates and activates an active MOT flight plan A typical MOT flight plan is displayed in Figure 6 127 Figure 6 127 Typical MOT Flight Plan The FMS creates and activates a MOT flight plan when the MOT button on the guidance controller is pushed and the following pre...

Page 329: ...x and HOV waypoint Sequencing the MOTxx waypoint is inhibited until MOT CANCEL is selected The lateral deviation scaling is set to 0 1 NM when the MOT pattern is activated and transitions to the normal RNP value for the current phase of flight when MOT is canceled NOTE After passing the FHAF waypoint the lateral deviation is displayed with a scaling of a two dot deflection equal to 0 02 NM The RNP...

Page 330: ...icates the MOT flight plan is actively being flown D 2L 5L The appropriate active waypoints in the MOT flight plan are displayed at 2L through 5L A direct to to the FHAF results in an INVALID ENTRY scratchpad message A direct to any non MOT active flight plan waypoint cancels the MOT flight plan and performs a normal direct to the selected waypoint When the MOT flight plan is performed and the fli...

Page 331: ...ume the search pattern When the MOT flight plan is created during normal flight plan operations for example no PATTERN flown a direct to the previously active TO waypoint is performed When the MOT flight plan is created during a hold or orbit the hold or orbit is removed from the flight plan D 1R The FMS speed mode and the speed command value are displayed at 1R When the MOT flight plan isactive p...

Page 332: ...de constraint Baro associated with the HOV and MOTxx waypoints are displayed After reaching the FHAF only the altitude constraints associated with the HOV and MOTxx waypoints are displayed The speed constraint is not displayed and pilot entry is not permitted to modify the MOT flight plan speed and altitude constraints D 6R When within 200 flight plan miles of the destination airport the ARRIVAL p...

Page 333: ...date time software version and active navigation database cycle are displayed on the NAV IDENT page The version size and region of the navigation database are also displayed on the NAV IDENT page NOTE To ensure proper information is used for the Helicopter FMS the pilot is to validate the aircraft database before use The date and time displayed on this page is synchronized with the GPS date and ti...

Page 334: ...he FMS date corresponds to a day during one of the navigation database cycles that cycle is displayed in green The remaining cycle is displayed in amber When both cycles are displayed in amber either the date is wrong or the navigation database has expired and must be updated The database cycle is only changed while on the ground When an active flight plan exists the active flight plan is cleared ...

Page 335: ...adio tuning commands are transferred to the other FMS automatically no pilot action required 2 Independent Only off side radio tuning commands are transferred to the other FMS automatically 3 Single The FMS in the single system mode monitors the VOR DME radio inputs and computes a radio position when possible The single FMS does not tune the VOR and DMEs However the single FMS tunes all of the oth...

Page 336: ...8 Honeywell International Inc Do not copy without express permission of Honeywell The FMS operating mode is selected using the appropriate line select key as shown in Figure 6 132 After selecting an operating mode or the RETURN prompt 1R MAINTENANCE 1 3 page is displayed 00756 07 Figure 6 132 OPERATING MODE 1 1 ...

Page 337: ...ists the currently failed sensors as determined by the FMS 00759 04 Figure 6 133 FMS 1 MAINTENANCE 2 3 The SETUP prompt 6L is used to accessthe FMSSETUP page Refer to Procedure 6 33 for further details on the accessing the FMS SETUP page A list of sensors that failed sometime after takeoff during the current flight but are not failed at the present time is displayed when pushing the SENSOR HISTORY...

Page 338: ...nt System FMS for the Agusta AW139 AB139 Helicopter A28 1146 181 REV 3 Mar 2009 Navigation 6 180 Honeywell International Inc Do not copy without express permission of Honeywell 00760 05 Figure 6 134 SENSOR HISTORY 1 1 ...

Page 339: ...es and headings displayed by the FMS are followed by the letter T When MAG is the active mode all courses and headings displayed by the FMS are followed by a degree symbol _ on the FMS pages 00797 05 Figure 6 135 FMS 1 MAINTENANCE 3 3 The active mode also reflects how courses are displayed on the HSI When the FMS is selected as the navigation source for the HSI the course displayed by the FMS is r...

Page 340: ...the FMS crosses the pole The plan mode for the EFIS map display is not useful while at or near the pole The information presented is correct but the presentation is not useful because the plan mode is presented North up When at the North pole for example everything is South Therefore the plan mode must not be used during operations at or near either pole Instead use the regular map mode Correctly ...

Page 341: ...guration information is given for display only as shown in Figure 6 136 This page shows the functional software identifier FMS software version and input output processor IOP software version Aircraft configuration data is shown in hexadecimal characters The least significant configuration byte starts at the upper left line This page gives verifiable identification for an FMS being returned to air...

Page 342: ...es for configuring operational options The setup pages are accessible from MAINTENANCE page 2 using line select key 6L as described in Procedure 6 33 From this index page the various setup pages are selected Step Procedure 6 33 FMS Setup Page Access 1 Select MAINTENANCE from the NAV INDEX page 2 2 Push the NEXT key to select page 2 3 Select SETUP prompt at 6L as shown in Figure 6 137 00759 05 Figu...

Page 343: ...85 Navigation Honeywell International Inc Do not copy without express permission of Honeywell Step Procedure 6 33 FMS Setup Page Access 4 The FMS SETUP page shown in Figure 6 138 is displayed Selectable options are as follows D 1R FLIGHT CONFIG D 2R ENGR DATA 00761 08 Figure 6 138 FMS SETUP 1 1 Page ...

Page 344: ...t many operating conditions of the FMS FLIGHT CONFIG is accessed from the FMS SETUP line select key 1R For details regarding flight configuration setup refer to Procedure 6 34 Step Procedure 6 34 Flight Configuration Setup 1 Select FLIGHT CONFIG 1R from the FMS SETUP page Refer to Procedure 6 33 2 Review the current configuration as shown in Figure 6 139 Make changes as necessary using the require...

Page 345: ...MS checks each turn against the model and increases the bank angle above the entered BANK FACTOR when required The BANK FACTOR is entered at any time but only on the master MCDU when operating in synchronous mode When the FMS configuration changes from single independent or initiated transfer to synchronous mode the master bank factor overwrites the slave bank factor value 4 Set FPL AUTO PAGE to O...

Page 346: ...display on EFIS When the option is selected ON the origin and destination airports are included in the list even when not among the closest airports The origin and destination airports are also displayed as runway symbols on modified EFIS with the ORG DEST DISPLAY ON option D ORG DEST DISPLAY OFF When the selection is OFF the origin and destination airports are included only when among the closest...

Page 347: ...N KEY PAGING to ON or OFF at 2R When ON function pages are advanced by pushing the function key instead of the NEXT key DETAILS D FUNCTION KEY PAGING OFF Each push of a function key PERF NAV FPL PROG DIR results in the first page of the function being displayed This is the default configuration D FUNCTION KEY PAGING ON Each push of a function key results in the MCDU displaying the next page of the...

Page 348: ...the OR prompt at 3R Figure 6 141 FLIGHT SUMMARY OUTPUT 1 1 Page 11 DETAILS D MCDU When selected ON the FLIGHT SUMMARY page is automatically displayed 15 seconds following landing D PRINTER Option When selected ON the PRINT prompt is displayed on the FLIGHT SUMMARY page at 6L The default configuration is OFF for PRINTER and must remain OFF unless a printer is installed on the aircraft D STORAGE Whe...

Page 349: ...ussed on page 7 30 Engineering Data The ENGINEER DATA page shown in Figure 6 142 is accessed using 2R on the FMS SETUP page The ENGINEER DATA page shows the index of available options primarily used under the direction of Honeywell engineering in finding and solving problems with the FMS 00768 08 Figure 6 142 ENGINEER DATA 1 1 Page The ENGINEERING DATA 1 1 page is used in selecting various functio...

Page 350: ...ng since memory locations differ with each database update D 3L Use CLEAR CDB CUSTOM DATA BASE to clear the custom database The options are to clear pilot defined waypoints stored flight plans and NOTAMS The FMS must be operating in independent or single mode to have access to the page Clearing the custom database while operating in dual or initiated transfer is not possible D 3R The FMS internal ...

Page 351: ... 1R The last FMS position is displayed when the aircraft is on the ground When the line select key adjacent to the LOAD prompt 1R is pushed the FMS is initialized to that position After loading a position the prompt FLT PLAN is displayed at 6R for access to the flight planning function D 2L and 2R The reference waypoint REF WPT line is below the last FMS position This line is filled automatically ...

Page 352: ...same latitude longitude the FMS selects the one with highest alphanumeric priority AIRPORT REFERENCE POINT ARP When a last position is available and no RAMPX waypoints are found within 3 NM the closest ARP within 3 NM is displayed PROMPTS When none of the previously discussed waypoints are displayed prompts are displayed by the FMS as shown in Figure 6 143 D 3L and 3R The position of the highest p...

Page 353: ...l International Inc Do not copy without express permission of Honeywell 00800 03 Figure 6 144 Position Loaded When the aircraft is in flight and the FMS position is valid the POSITION INIT page shown in Figure 6 145 is displayed The update feature of the FMS is used only in flight Figure 6 145 POSITION INIT UPDATE Prompt ...

Page 354: ...he following types of crossing points D Direct to a waypoint from the current aircraft position D Point abeam a waypoint for the current flight plan D Crossing radial from a waypoint for the current flight plan D Crossing latitude longitude given latitude longitude for the current flight plan The CROSSING POINTS 1 1 page shown in Figure 6 146 is displayed after selecting the CROSS PTS prompt from ...

Page 355: ...on of the aircraft to any given waypoint For example to determine where DEN is relative to the current aircraft position enter DEN into the scratchpad and select 1L as shown in Figure 6 147 At 1R the radial and distance from DEN to the current aircraft position is displayed The course distance ETE and the remaining fuel when the aircraft was to fly direct from the current position to DEN are displ...

Page 356: ...s pushed the FMS computes the point along the flight plan where the aircraft passes abeam the entered waypoint as shown in Figure 6 148 When necessary the PT ABEAM definition at 2L DEN 132 109 in the example is selected to the scratchpad and inserted into the flight plan as a temporary waypoint 00805 03 Figure 6 148 POINT ABEAM 1 1 Page When no POINT ABEAM exists for the current flight plan the me...

Page 357: ...long the flight plan where the aircraft crosses the designated radial The waypoint is entered at 1L and the radial is entered at 1R as shown in Figure 6 149 For example entering the 180_ radial the FMS projects the aircraft can cross the 180_ radial 117 NM from DEN The crossing radial definition at 2L is inserted as a temporary waypoint 00804 03 Figure 6 149 CROSS RADIAL 1 1 Page When the entered ...

Page 358: ...rcraft crosses the 100_ West longitude line for the current flight plan enter W100 at 1R as shown in Figure 6 150 The FMS computes the latitude The course distance ETE and fuel remaining to fly directly from the current aircraft position to N33_24 9 W100_00 0 is also displayed The computed point 2L is line selected to the scratchpad and inserted in the flight plan as a temporary waypoint When requ...

Page 359: ... REV 3 Mar 2009 6 201 Navigation Honeywell International Inc Do not copy without express permission of Honeywell DATA LOAD The DATA LOAD page shown in Figure 6 151 is used to access the database crossloading function of the FMS 00810 03 Figure 6 151 Accessing Database Crossloading ...

Page 360: ...the custom and aircraft database is permitted while the aircraft is on the ground or in the air In order to transfer data the FMSs must be turned on and have compatible software versions Only one FMS is required to complete all steps Refer to Procedure 6 35 for generalized data loading procedures Step Procedure 6 35 Database Transfer Between FMS 1 Select the appropriate prompt as shown in Figure 6...

Page 361: ... International Inc Do not copy without express permission of Honeywell Step Procedure 6 35 Database Transfer Between FMS 2 Select the prompt for the source or destination of the selected data from the menu as shown in Figure 6 153 In this example the TO FMS 2 prompt at 2L is selected 02120 02 Figure 6 153 TO FMS 2 Prompt ...

Page 362: ...Mar 2009 Navigation 6 204 Honeywell International Inc Do not copy without express permission of Honeywell Step Procedure 6 35 Database Transfer Between FMS 3 Confirm selection and select YES 6R or NO 6L on the DATA LOAD page shown in Figure 6 154 0 1723 06 Figure 6 154 CONFIRM YES or NO ...

Page 363: ...oring is shown in Figure 6 155 01724 03 Figure 6 155 Progress Monitoring The FMS indicates the percentage complete When complete the message DB TRANSFER COMPLETE is displayed and the FMS generates a restart when a navigation of aircraft database has been transferred When power is interrupted ABORT is selected or other problems that stop the loading process occur the data load process must be repea...

Page 364: ...ckturn The page is then reset to reflect the new flight Figure 6 156 FLIGHT SUMMARY 1 1 Page D 1L and 1R The takeoff landing and en route time are displayed on these lines No entry is permitted D 2L The fuel used for the flight is displayed on this line Entering DELETE results in the value being set to zero FUEL USED is then increment from zero Pilot entry of FUEL USED for the flight is not permit...

Page 365: ...UMMARY OUTPUT has been configured for STORAGE see Procedure 6 34 for more information on the configuration of FLIGHT SUMMARY OUTPUT The SAVE prompt is not displayed when OFF is selected as the STORAGE output configuration The PRINT prompt is used to print the FLIGHT SUMMARY data when the FLIGHT SUMMARY OUTPUT has been configured forthe PRINTER The PRINT prompt is not displayed when OFF is selected...

Page 366: ...Flight Management System FMS for the Agusta AW139 AB139 Helicopter A28 1146 181 REV 3 Mar 2009 Navigation 6 208 Honeywell International Inc Do not copy without express permission of Honeywell Blank Page ...

Page 367: ...are used to trackstored flight plans Flight plan names are used to recall a stored flight plan into the active flight plan Flight plan names must have a minimum of six characters and a maximum of ten A convenient naming convention is to use the origin and destination The airport identifiers are separated by a dash For more than one flight plan between the same set of identifiers add a number at th...

Page 368: ...e missed approach is activated the ALTERNATE prompt is displayed A direct to an alternate flight plan is permitted at any time ALTERNATE ORIGIN The alternate flight plan origin is alsothe primary flight plan destination D Waypoint Names Waypoints exist in the navigation database as the custom database pilot defined waypoints or as temporary waypoints Waypoint names are used for convenience in keep...

Page 369: ... definition of the waypoint directly into the active flight plan Acceptable definitions are latitude longitude place bearing distance place bearing place bearing and along the flight plan as place distance When the definition is entered in the flight plan the waypoint is assigned a name describing how the waypoint was defined and a number XX Temporary waypoints entered on the left FMS are assigned...

Page 370: ...nto the active flight plan line selecting to the scratchpad is permitted When displayed in the scratchpad the runway is in the following format AIRPORT RUNWAY BEARING A distance is permitted to be inserted to complete the definition of a waypoint on the extension line of the runway Entering an altitude constraint following the distance is also permitted Insert this definition into the flight plan ...

Page 371: ...quencing During flight the active flight plan automatically sequences so the first leg of the active flight plan is the active leg referenced to the guidance parameters Normally the FMS sequences before the waypoint for an inside turn when the aircraft is on or close to on course When the aircraft is not on course the normal sequence occurs no later than a point abeam of the waypoint Some waypoint...

Page 372: ...after a discontinuity When changing discontinuities in the flight plan are kept to the minimum There are times when a discontinuity is necessary The following rules apply When adding or deleting a single waypoint no discontinuity is permitted to be inserted in the flight plan The flight plan is directly linked between the waypoints Deleting several waypoints at a time does not result in a disconti...

Page 373: ...lternate portion of the flight plan is enabled the corresponding waypoints are incorporated into the primary portion of the flight plan At that point all active flight plan rules apply D Alternate Destination The alternate destination is entered when defining a flight plan to an alternate Like the primary flight plan the alternate destination is entered as the final waypoint to close out the alter...

Page 374: ... a value other than an increment of a thousand feet the FMS rounds off the entered altitude by a thousand feet For example when the INIT CRZ ALT target is 2500 ft the aircraft levels off at 2000 ft The FMS rounds initial cruise altitude and baro altitude to the nearest thousand feet to determine flight phase D Cruise Altitude Cruise altitude is the current altitude used by the FMS to plan the crui...

Page 375: ...e AT AT or ABOVE or AT or BELOW For example entering 10000A A following the altitude indicates AT or ABOVE Entering 10000B B following the altitude indicates AT or BELOW Entering 10000 no letter indicates AT The FMS obeys descent speed constraints at and after the waypoint containing the constraint The FMS obeys angle constraints from the TOD to the waypoint containing the constraint Normally the ...

Page 376: ... CREATING CHANGING FLIGHT PLAN An example of the ACTIVE FLT PLAN page before the flight plan is shown in Figure 7 1 00817 04 Figure 7 1 ACTIVE FLT PLAN Example The following options are made to recall or create an active flight plan D Load a flight plan from a disk 2L D Recall a previously stored flight plan 3R D Create a stored flight plan 3R D Build a flight plan by entering waypoints 2R ...

Page 377: ...all of the flight plan 01676 01 Figure 7 2 Recall Flight Plan When the name of a previously stored flight plan cannot be remembered enter the origin and destination The FMS searches the stored flight plans for those plans with the same origin and destination When a stored flight plan is found the FLIGHT PLAN LIST page is displayed with the stored flight plan names marked with an asterisk as shown ...

Page 378: ...gusta AW139 AB139 Helicopter A28 1146 181 REV 3 Mar 2009 Flight Plan 7 12 Honeywell International Inc Do not copy without express permission of Honeywell 01677 01 Figure 7 3 FLIGHT PLAN LIST 1 1 Page 01678 01 Figure 7 4 Required Flight Plan ...

Page 379: ...ned in memory for future use Storing a flight plan is done by entering the flight plan identifier on the RECALL OR CREATE FPL NAMED prompt at 3R as shown in Figure 7 1 When a flight plan name is entered at 3R the FPL PLAN SELECT page shown in Figure 7 5 is displayed to define the flight plan When the flight plan becomes defined the flight plan is activated When a flight plan name entered in 3R is ...

Page 380: ...lan is displayed and the FMS is ready for waypoint input as shown in Figure 7 6 When building a flight plan waypoints are entered on the line showing the VIA TO prompt 2L through 5L The FMS accepts a variety of inputs at the VIA TO prompt as described in the following paragraphs 01107 01 Figure 7 6 FMS Ready for Waypoint Input D Waypoint Any waypoint contained in the navigation database or the cus...

Page 381: ...e airway from GUP up to and including ALS The airway is also entered as a single input by entering GUP J102 ALS into the scratchpad and selecting the appropriate line select key 01679 01 Figure 7 7 Entering GUP Into Flight Plan D Flight Plan Names Any defined flight plan name is permitted to be entered When a defined flight plan is entered flight plans are linked together When inserting a flight p...

Page 382: ...is entered the destination waypoint must be entered as the last waypoint to close the flight To accomplish this enter the destination at the VIA TO prompt An alternate flight plan is entered using the same rules as a regular flight plan D Vertical Entries Vertical definitions for waypoints are entered using the right hand line select keys 1R through 5R as shown in Figure 7 8 0 1721 02 Figure 7 8 V...

Page 383: ...in large characters CONSTRAINT TYPE Constraint type is displayed directly above altitude constraints as shown in Figure 7 8 The constraint type shows as CLB for climb constraints and DES for descent constraints The FMS automatically assigns constraints in the first half of the flight plan as CLB unless the entered constraint is below the current aircraft altitude and those in the last half as DES ...

Page 384: ... The rules that apply are described as follows Single waypoints including temporary waypoints are permitted to be added to or deleted from the flight plan To add a waypoint to the flight plan the waypoint is line selected from the scratchpad to the appropriate line The added waypoint is displayed on the line selected When adding a waypoint the flight plan is searched forward of the point of insert...

Page 385: ... point and the end point must be on the airway When inserting a stored flight plan the pilot specifies only the flight plan name to insert the complete flight plan To insert a portion of a stored flight plan the entry is made in the form of FLIGHT PLAN NAME WAYPOINT When a stored flight plan is inserted flight planning takes the active flight plan waypoint before point of insertion and searches fo...

Page 386: ...int No waypoints are deleted with the INTERCEPT function When the pilot inserts an intercept waypoint in the flight plan and changes to another page before the definition is completed the entire operation is canceled D VNAV OFFSET ATC often issues a clearance consisting of crossing a specified distance before or after a waypoint at a specific altitude The FMS is capable of creating a temporary way...

Page 387: ...ight plan 01107 01 Figure 7 11 Prompt Below Destination The saved active flight plan must follow the same rules that apply to stored flight plans These rules are as follows 1 All terminal procedures temporary waypoints heading select and intercept legs are permitted to be removed from the active flight plan prior to being stored 2 Saving the active flight plan is only conducted when the aircraft i...

Page 388: ...igin is not already a waypoint in the flight plan the whole flight plan is deleted Deleting the origin clears the entire flight plan This applies to both active and stored flight plans Changing the database cycle NAV IDENT page line select key 2R clears the active flight plan This rules out any discrepancies between flight plan information and the new database cycle The database cycle is changed o...

Page 389: ...craft Normally the HEADING lateral mode is used to control the aircraft until the FMS changes to LNAV CAPTURE D LNAV CAPTURE The FMS begins lateral steering control when the mode changes from ARM to CAPTURE The FMS uses a 3_ per second roll rate during en route operations and up to 5 5_ per second on the approach Banks are planned between 0_ and 23_ with 25_ as a maximum In holding procedure turns...

Page 390: ... the aircraft as high as possible for as long as possible D VPATH angles are from 1_ to 6_ D Path guidance is always provided during VPATH descents unless the FMS transitions to speed reversion In this condition the FMS transitions out of VPATH D Default descent angle is part of performance initialization Changing of the default angle is permitted by the crew after the angle is displayed for each ...

Page 391: ...glideslope gives a constant angle descent VNAV gives the same constant angle descent using barometric altitude to determine when the aircraft is on path The primary objective during VPATH descents is maintaining the geometric path To maintain the geometric path VNAV computes the required vertical speed to maintain the path VNAV then sends the command to the FGC The FGC adjusts the pitch of the air...

Page 392: ...AF final approach fix the aircraft must be in ALT hold at the FAF altitude D No vertical direct to the MAP has been executed Engagement of VGP Mode The VGP mode is engaged when the following rules are met D The VGP mode is armed by the selection of APP button and meeting the conditions mentioned in the previous section D LNAV is active D The aircraft when holding must be established on the inbound...

Page 393: ...d using VFLCH Intermediate level offs are entered as waypoint constraints through the MCDU or are set with the altitude preselector VNAV never flies through the altitude preselector in any VNAV mode When an intermediate level off is required due to an FMS waypoint altitude constraint VNAV provides guidance to resume the climb after passing the waypoint when the selector is set above thecurrent air...

Page 394: ...D The TOD is the location where the aircraft commences a descent The TOD is displayed on the MFD when in range but is always displayed on the PROGRESS pages Only one TOD waypoint is permitted at a time D Descent The transition to descent is automatic assuming the altitude preselector is set lower than the present altitude On reaching the TOD VNAV initiates either a VFLCH or VPATH descent Speed Des...

Page 395: ...d while in VALT the aircraft remains in VALT D VNAV VPATH and VFLCH and Stored Instrument Approaches All stored approach procedures have altitude constraints and or associated vertical path angles Changing the altitude constraint and or path descent angle once an approach procedure has been activated is permitted The crew must verify all the approach procedure altitude requirements are met Industr...

Page 396: ... for the defined approach approach transitions and missed approach segments of the flight plan to compensate for nonstandard day temperatures The flight crew configures the FMS for three states of VNAV approach temperature compensation 1 Off assumes standard day temperature 2 COLD applies temperature compensation only when approach is flown in cold conditions 0 to 50 degrees DISA 3 HOT COLD applie...

Page 397: ...39 AB139 Helicopter A28 1146 181 REV 3 Mar 2009 7 31 Flight Plan Honeywell International Inc Do not copy without express permission of Honeywell Step Procedure 7 2 FMS Temperature Compensation Configuration 5 cont Figure 7 12 FLIGHT CONFIG 2 2 Page ...

Page 398: ...layed 15 seconds following landing apm temp options temporarily enable apm temp options temporarily disable D Loader When selected ON the FLIGHT SUMMARY page data is automatically saved 15 seconds following landing The file saved to disk uses the following naming convention FS HHMM TXT Where FS Flight Summary FMS side 1 left 2 right 3 Center hh hour mm minute The FMS posts error messages when the ...

Page 399: ...ct 2L to set temperature compensation mode to COLD D Select 3L to set the temperature compensation mode to HOT COLD NOTE The VNAV approach temperature compensation functionality can as an option be enabled as COLD only or HOT COLD When enabled as COLD the previously discussed procedures remain the same with the exception that the HOT COLD prompt is not available The FMS determines the compensated ...

Page 400: ...ompensation values in the active flight plan this procedure assumes an arrival has already been strung into the active flight plan Step Procedure 7 3 Review and Insert Temperature Compensated Altitude Constraints Into Flight Plan 1 The LANDING 1 2 page shown in Figure 7 14 is displayed by pushing the LANDING prompt on the PERF INDEX page 01874 01 Figure 7 14 LANDING From the PERF INDEX Page On the...

Page 401: ...ts Into Flight Plan 2 The 22 C TEMP COMP 1 2 page shown in Figure 7 15 is displayed by pushing the TEMP COMP prompt on the LANDING page Figure 7 15 TEMP COMP 1 2 The proposed altitudes for each of the arrival flight plan constraints is displayed in reverse video on the TEMP COMP page The temperature compensation is applied only to the altitude constraints from the navigation database No changes ar...

Page 402: ...the temperature compensated values into the flight plan The temperature compensated values are displayed in reverse video as shown in Figure 7 16 Figure 7 16 Activate Changes The pilot is able to calculate a temperature compensated approach MDA on the last page in the string of the TEMP COMP pages The last page of the TEMP COMP page is accessed by pushing the NEXT function key when viewing the TEM...

Page 403: ... is blank when a published approach MDA has not been entered at 1L The published approach MDA altitude is entered in feet by the pilot at 1L When a valid entry is made at 1L a FMS computed COMP MDA is displayed in feet at 1R as shown in Figure 7 18 Invalid entries are not permitted and attempts to do so are annunciated to the pilot with an INVALID ENTRY scratchpad message A entry is consider inval...

Page 404: ...9 Flight Plan 7 38 Honeywell International Inc Do not copy without express permission of Honeywell Figure 7 18 MDA TEMP COMP Entry Procedure 7 4 is an example of the steps necessary for removing existing values of temperature compensated arrival altitude constraints from the active flight plan ...

Page 405: ...n Honeywell International Inc Do not copy without express permission of Honeywell Step Procedure 7 4 Remove Temperature Compensation 1 Select the LANDING prompt from PERF INDEX page to display the LANDING 1 2 page shown in Figure 7 19 01874 01 Figure 7 19 LANDING 1 2 Page 2 Select TEMP COMP on the LANDING page ...

Page 406: ...xpress permission of Honeywell Step Procedure 7 4 Remove Temperature Compensation 3 Select the REMOVE prompt as shown in Figure 7 20 from the TEMP COMP review page Figure 7 20 TEMP COMP A MOD flight plan is created with the database values of the arrival altitude constraints 4 Select ACTIVATE to apply the changes in the ACTIVE FLT PLAN page shown in Figure 7 21 ...

Page 407: ...pensation 4 cont Figure 7 21 Accessing TEMP COMP The TEMP COMP review page is accessed either through LANDING page or from the FLIGHT PLAN pages For the TEMP COMP access prompt to be available on the flight plan pages the following conditions must be met D The active TEMP COMP CONFIG mode is COLD or HOT COLD D The aircraft is within 30 NM of the destination D An approach has been activated D Valid...

Page 408: ...en reviewing these scenarios VNAV CLIMB VFLCH The elements of a VNAV climb profile are shown in Figure 7 22 Figure 7 22 VNAV Climb Profile A VNAV climb profile consists of the following D VNAV is flown in a VFLCH airspeed climb 1 after takeoff D The flight guidance computer changes to ASEL to capture the altitude constraint 2 D The flight guidance computer switches to ALT at the constraint altitud...

Page 409: ...itching from VFLCH to ASEL to ALT with the normal 1000 foot selector alert and the speed command changes to the cruise value VNAV FLIGHT LEVEL CHANGE DESCENT VFLCH The elements of a VNAV FLCH IAS or MACH hold descent profile are shown in Figure 7 23 Figure 7 23 VNAV Flight Level Change Descent A VFLCH descent is flown at any time by using the following D From cruise altitude 1 dial down the altitu...

Page 410: ...he following steps apply D An altitude constraint is entered at a waypoint 1 The FMS calculates an angle and TOD 2 for the path descent D At the TOD the flight guidance computer switches from VALT to VPATH and begins a descent 2 D The altitude preselector is set to the ATC cleared altitude 3 D One minute before reaching the TOD the vertical deviation scale is displayed on the EFIS When the altitud...

Page 411: ...int 1 The FMS calculates an angle and TOD 2 for the path descent D One minute before reaching the TOD the vertical deviation scale is displayed on the EFIS When the altitude preselector is not at a lower altitude the message RESET ALT SEL is displayed D When past the TOD and more than 500 ft above the path the flight guidance computer remains in VALT D The altitude preselector is set 4 to the ATC ...

Page 412: ...26 Figure 7 26 VNAV Early Descent to Capture Path The VNAV early descent scenario is typical when ATC instructs a descent before the established TOD point is reached The steps are as follows D An altitude constraint is entered at a waypoint 1 The FMS calculates an angle and TOD 2 for the path descent D The altitude preselector is set to the ATC cleared altitude 3 D The IAS button 4 is pushed to be...

Page 413: ...h descent using vertical DIRECT TO is shown in Figure 7 27 Figure 7 27 VNAV Early Path Descent Using Vertical DIRECT TO The following steps apply D An altitude constraint is entered at a waypoint 1 The FMS calculates an angle and TOD 2 for the path descent D The altitude preselector is set 3 to the ATC cleared altitude 4 D A vertical direct to is conducted 5 to the constrained waypoint 1 The FMS c...

Page 414: ...n this scenario descent clearance is not received before the TOD is reached The following applies D An altitude constraint is entered at a waypoint 1 The FMS calculates an angle and TOD 2 for the path descent D When the altitude preselector is not at a lower altitude the message RESET ALT SEL is displayed D At the TOD 2 FMS remains in CRUISE and remains level through the TOD D The altitude presele...

Page 415: ...eed manually on the guidance control panel Manual speed command mode is not available on all aircraft types The FMS gives speed protection for automatic speed command modes This speed protection is designed to prevent the aircraft from flying too slow or too fast General Speed Command Rules D The current speed command is displayed on page 1 of the ACTIVE FLT PLAN shown in Figure 7 29 D A CAS and M...

Page 416: ...speed limit of 200 KIAS knots indicated airspeed The default departure area is 4 NM from the departure airport and less than 2500 ft AGL above ground level D Once the aircraft is clear of the departure area the speed command transitions to the climb speed schedule selected during initialization The climb speed command is limited by the speed altitude limit defined during initialization Once above ...

Page 417: ...ppropriate To reinstate the approach speed target the pilot must reenter the INIT DIST on the APPROACH SPEED page D In the event the flight director transitions to go around the speed command changes to the go around speedschedule definedduring initialization For some aircraft installations a go around speed command is permitted for each flap setting When the go around speed command is active modi...

Page 418: ... legs of the flight plan past the TOC and prior to the TOD The descent phase of flight is defined as the legs of the flight plan past the TOD To insert a waypoint speed constraint follow Procedure 7 5 Step Procedure 7 5 Inserting a Waypoint Speed Constraint 1 Completely initialize the PERFORMANCE INIT pages 2 Enter the speed constraint into the scratchpad followed by a slash The entered speed is e...

Page 419: ...Speed Constraint 1 Push the DEL key 2 Push the right line select key adjacent to the lateral waypoint on the ACTIVE FLT PLAN page Manual The pilot selects manual speed control from the guidance control panel In this mode FMS uses the manually entered speed to the manually entered speed The active flight plan page shows the manually entered speed in line 1R as shown in Figure 7 31 Manual speed comm...

Page 420: ...to the speed limit altitude when the aircraft speed exceeds the speed constraint for example 250 kts at 10 000 ft by more than 5 kts Under these conditions the FMS levels the aircraft at the speed limit altitude until the aircraft speed is 2 kts greater than the speed limit The FMS then requests a VFLCH descent down to the altitude preselector When autothrottles are not engaged or the aircraft is ...

Page 421: ... than 5 kts above the current airspeed This is also true when the BOD altitude constraint is deleted 2 A latched speed occurs when the altitude preselector is dialed while in ALT to a BOD and the current target is greater than 5 kts more than the current speed 3 When VNAV has transitioned out of VPATH and the current airspeed is not within 5 kts of the speed command 4 When VNAV is in VPATH and the...

Page 422: ...Flight Management System FMS for the Agusta AW139 AB139 Helicopter A28 1146 181 REV 3 Mar 2009 Flight Plan 7 56 Honeywell International Inc Do not copy without express permission of Honeywell Blank Page ...

Page 423: ...light to the TO waypoint and the destination aswell as the current navigation status is displayed on the PROGRESS 1 3 page shown in Figure 8 1 00827 07 Figure 8 1 Progress 1 3 Page The following line select keys correspond to the associated definitions on the PROGRESS 1 3 page D 1L 2L and 3L The distance to go DTG estimated time en route ETE and estimated fuel remaining for the TO NEXT waypoint an...

Page 424: ...required navigation performance RNP value in nautical miles NM Estimated position uncertainty EPU values indicates estimated navigation accuracy of the current navigation mode When EPU becomes larger than RNP UNABLE RNP is displayed in the scratchpad In addition the navigation NAV radios are tuned to the navaid INW frequency 112 60 The A preceding the navaid identifier indicates the radio is in au...

Page 425: ...e preselector dialed to the missed approach altitude D 2L The distance and ETE to the bottom of step climb BOSC is displayed on this line when available Otherwise the distance and ETE to the top of climb TOC is displayed D 3L The distance and ETE to the top of descent TOD is displayed on this line When the aircraft is past the TOD point the prediction is replaced with the word PAST D 2R The curren...

Page 426: ...e active leg of the flight plan is displayed on this line A 0 01 NM resolution is used when the cross track error is less than 1 NM Larger cross track errors are displayed using a 0 1 NM resolution No entry is permitted D 1R This line permits pilot entry of offset Procedure 8 1 describes how to enter and remove an offset D 2L and 2R Aircraft track drift and heading is displayedon thisline D 3L and...

Page 427: ...stance and time to top of climb D 2R Shows top of climb altitude D 3L The distance and time to TOD and or bottom of descent BOD is displayed at 3L When the next descent path type is smoothing or the aircraft is past the TOD then BOD is displayed above the TOD Otherwise the TOD is displayed above the BOD When the next descent path type is smoothing then SMOOTHING is displayed in large cyan font rig...

Page 428: ...ell LATERAL OFFSET Lateral offsets are entered on the PROGRESS 3 page The entry is described in Procedure 8 1 Step Procedure 8 1 Lateral Offset Entry 1 Select PROGRESS page 3 2 Enter lateral offset into the scratchpad Enter direction L or R and distance in NM 3 Enter the offset by pushing line select 1R 4 The PROGRESS page is shown in Figure 8 5 01574 02 Figure 8 5 Progress 3 3 Page ...

Page 429: ...lowing 1 Standard instrument departure SIDs standard terminal arrival route STARs approaches a Patterns b In the terminal area 10 NM from origin 25 NM from destination c In the polar region Offsets are automatically canceled for the following 1 Course changes greater than 90_ a SIDs STARs approaches b Patterns c Intercepts An OFFSET CANCEL NEXT WPT message is displayed before offset is automatical...

Page 430: ...tional Inc Do not copy without express permission of Honeywell Air Data The AIR DATA page shown in Figure 8 6 is accessed from PROGRESS 3 3 page The air data computer ADC data source is displayed as part of the title This page shows direct and derived data from the digital air data computer DADC Figure 8 6 AIR DATA 1 1 1 Page ...

Page 431: ...ated definitions on the RNP page D 1L This line shows the manual override RNP value When one does not exist entry prompts are displayed Entry of a new RNP value is permitted When the new RNP value is greater than the required RNP for the current phase of flight the value is displayed in reverse video and is not accepted until the pilot confirms the entry Entry of DELETE clears the manual override ...

Page 432: ...he entered value as the new manual override RNP value Otherwise this line gives access to PROGRESS page 2 NOTE When a MANUAL RNP entry or an overriding RNP entry to the default phase of flight RNP is made on the non coupled side and INDEPENDENT mode is selected on the FMS the RNP does not transfer to the coupled FMS when the operator selects the mode back to DUAL Entering a MANUAL RNP or an overri...

Page 433: ...y is pushed page 1 of the active flight plan is displayed When the active flight plan is already displayed while pushing the DIR key the display remains on the current page of the active flight plan Pushing the DIR key inserts three prompts as shown in Figure 9 1 on the ACTIVE FLT PLAN pages The three prompts are as follows 1 DIRECT 1L 2 PATTERN 6L 3 INTERCEPT 6R The three prompts are used to call...

Page 434: ...light plan D Vertical Direct To A vertical direct to is operated in a similar manner as the lateral direct to A vertical direct to is executed to an altitude constraint at a waypoint in the flight plan The altitude constraint must be in the flight plan before the vertical direct to is executed Procedure 9 1 describes how to execute a verticaldirect to NOTE The aircraft does not respond to the vert...

Page 435: ...ect to was entered are permitted to be recalled This is done as described in Procedure 9 2 Step Procedure 9 2 Direct To Recovery 1 Push the DIR key 2 Use the previous PREV key to select the page or pages displaying the waypoints having been deleted or sequenced 3 Use the line select keys to select the direct to waypoint as shown in Figure 9 2 The FMS recalls the flight plan from the selected waypo...

Page 436: ...a radial or course into a second waypoint The second type of intercept consists of the pilot flying a heading either manually or by using the flight director towards the inbound radial course for the waypoint Both types of intercepts are conducted for waypoints or arcs Intercept Using Radial Course Intercepting using radial course consists of the pilot defining a radial course out of a waypoint un...

Page 437: ...sion of Honeywell Step Procedure 9 3 Intercept Using Radial Course 3 INTERCEPT is displayed in the scratchpad as shown in Figure 9 3 Figure 9 3 INTERCEPT in Scratchpad 4 For the following example the pilot wants to fly outbound from DRK on the 30_ radial until intercepting the 110_ radial inbound to PGS Insert INTERCEPT at 3L to define an intercept waypoint between DRK and PGS ...

Page 438: ...Mar 2009 Direct Intercept 9 6 Honeywell International Inc Do not copy without express permission of Honeywell Step Procedure 9 3 Intercept Using Radial Course 5 The INTERCEPT 1 1 page shown in Figure 9 4 is displayed to define the INTERCEPT waypoint 00836 03 Figure 9 4 INTERCEPT 1 1 Page ...

Page 439: ...o not copy without express permission of Honeywell Step Procedure 9 3 Intercept Using Radial Course 6 Define the radial course out of the FROM waypoint 1L For the following example the pilot wants to fly the 30_ radial out of DRK Figure 9 5 shows the INTERCEPT page following entry of the 30_ radial 01577 01 Figure 9 5 30 Degree Radial From Drake ...

Page 440: ...cedure 9 3 Intercept Using Radial Course 7 Define the radial 3L or course 3R into the waypoint For the following example the pilot wants to fly the 110_ radial inbound to PGS The number 040 is entered at 3L as shown in Figure 9 6 The course 220 is automatically displayed 00838 03 Figure 9 6 Inbound Radial to PGS 8 Select ACTIVATE 6R or CLEAR 6L ACTIVATE is displayed at 6R after the intercept is de...

Page 441: ...9 9 Direct Intercept Honeywell International Inc Do not copy without express permission of Honeywell Step Procedure 9 3 Intercept Using Radial Course 9 The defined temporary INTERCEPT waypoint now labeled RRxx is inserted into the flight plan as shown in Figure 9 7 Figure 9 7 Temporary INTERCEPT ...

Page 442: ... waypoint the FMS monitors the capture criteria for the radial or course inbound to the second waypoint When lateral navigation LNAV is armed the FMS captures the inbound course to the second waypoint when the capture criteria is satisfied Procedure 9 4 gives an example Step Procedure 9 4 Intercept Using Heading Select 1 Push the DIR key 2 Push the line select key adjacent to the INTERCEPT prompt ...

Page 443: ...ar 2009 9 11 Direct Intercept Honeywell International Inc Do not copy without express permission of Honeywell Step Procedure 9 4 Intercept Using Heading Select 5 The INTERCEPT 1 1 page shown in Figure 9 9 is displayed to define the INTERCEPT waypoint 00836 03 Figure 9 9 INTERCEPT Defined ...

Page 444: ...nc Do not copy without express permission of Honeywell Step Procedure 9 4 Intercept Using Heading Select 6 For this example heading vectors are flown until intercepting the 040_ radial inbound to PGS Select HDG SEL at 1R as shown in Figure 9 9 FLY HDG SEL is displayed at 1L as shown in Figure 9 10 01583 01 Figure 9 10 Intercept Inbound Radial ...

Page 445: ...t express permission of Honeywell Step Procedure 9 4 Intercept Using Heading Select 7 Define the radial 3L or course 3R into the TO waypoint For the following example the pilot wants to fly the 040_ radial inbound to PGS The number 040 is entered at 3L as shown in Figure 9 11 The course 220 is automatically displayed 00837 03 Figure 9 11 Fly Inbound Radial to PGS ...

Page 446: ...EPT Waypoint When an intercept using heading select is flown the FMS disengages at the beginning of the heading select leg For the example shown in Procedure 9 4 the FMS disengages when crossing DRK The aircraft heading must be adjusted to intercept the inboundcourse Adjustingthe aircraft heading is done manually or by using the flight director heading function LNAV must be armed in preparation fo...

Page 447: ...rc The FMS supports intercepting the arc using a radial course or heading select Both types of intercepts are similar to intercepting a waypoint Procedure 9 5 explains using the intercept function to fly a radial course out of a waypoint to intercept an arc Step Procedure 9 5 Intercept an Arc Using Radial Course 1 Push the DIR key 2 Push the line select key adjacent to the INTERCEPT prompt 6R 3 IN...

Page 448: ...ot wants to fly outbound from SSI on the 250_ radial until intercepting the 7 nautical mile NM DME arc for the VOR Rwy 4 approach at KSAV The arc starts at the 302_ radial and proceeds counterclockwise around the VOR until the arc terminates at the 207_ radial Line select INTERCEPT to the second waypoint having the reverse video A this signifies the end of the arc leg For this example this would b...

Page 449: ...r A28 1146 181 REV 3 Mar 2009 9 17 Direct Intercept Honeywell International Inc Do not copy without express permission of Honeywell Step Procedure 9 5 Intercept an Arc Using Radial Course 4 cont Figure 9 14 End of Arc Leg 01580 02 Figure 9 15 ACTIVE FLT PLAN 2 6 Page ...

Page 450: ...ywell International Inc Do not copy without express permission of Honeywell Step Procedure 9 5 Intercept an Arc Using Radial Course 5 The INTERCEPT page shown in Figure 9 16 is displayed The FROM waypoint at 1L SSI is the waypoint in the active flight plan preceding the arc 01584 01 Figure 9 16 Waypoint Preceding the Arc ...

Page 451: ...t is found on the arc the message NO CRS TO ARC INTERCEPT is displayed in the scratchpad 01585 01 Figure 9 17 250_ Radial Entered 7 No entry is required for the TO waypoint since the intercept is to the arc 8 Select ACTIVATE 6R or CLEAR 6L ACTIVATE is displayed after the intercept is defined 9 The defined INTERCEPT waypoint now labeled INTxx is inserted into the flight plan as shown in Figures 9 1...

Page 452: ...181 REV 3 Mar 2009 Direct Intercept 9 20 Honeywell International Inc Do not copy without express permission of Honeywell Step Procedure 9 5 Intercept an Arc Using Radial Course 9 cont Figure 9 18 Defined Intercept Waypoint 01582 02 Figure 9 19 Defined Intercept Waypoint Entered ...

Page 453: ...in feet up to 4 digits D Leading zeros not required D Range from 0 to 9999 Airport Identifiers The flight management system FMS uses four character International Civil Aviation Organization ICAO or ICAO format airport identifiers When a U S airport has a three letter identifier in the Jeppesen charts and is normally prefixed with a K in the database Alaskan and Hawaiian airports with a three lette...

Page 454: ...t plan following the waypoint D Airway is always followed by a decimal point D Entering an airway into the active flight plan when the entry and exit waypoint are adjacent waypoints in the flight plan is permitted Enter the airway into the scratchpad followed by a decimal point and place the airway after the entry waypoint in the active flight plan Alternate Destination D The name is from one to f...

Page 455: ... to 99 999 Bank Factor D Entry is whole degrees D Range from 0 to 15 Barometer BARO Set D Entry in millibars or inches of mercury decimal required D Leading zero not required D Range from 16 00 to 32 00 in Hg 542 to 1083 millibars Basic Operating Weight BOW D Entry is pounds or kilograms depending on configuration D Entry is four to six digits D Range is from 1000 to 999 999 Cargo Weight D Entry i...

Page 456: ...is two digits Destination D The name is from one to five alphanumeric characters D First character cannot be a dash Direct To Waypoint D The name is from one to five alphanumeric characters D First character cannot be a dash Elevation D Entry format is identical to the Altitude entry format defined on page 10 2 Engine Pressure Ratio EPR D Entry range is from 1 00 to 2 00 D Trailing decimal and or ...

Page 457: ...in and destination of the stored flight plan Frequency ADF D The minimum entry is three digits D A decimal is not required when tenths position is zero D Range is 100 0 to 1799 5 KHz 2179 0 to 2185 0 KHz in 0 5 increments Frequency DGPS Runway D The minimum entry is one letter airport identifier and runway number Channel D The minimum entry is one number and a letter D Numeric range is 0 through 3...

Page 458: ...ents NOTE Not all radios are capable of this range Frequency TRANSPONDER D A four digit entry is required D The range for each digit is 0 to 7 Frequency VHF COM D The minimum entry is two digits D Decimal point and or trailing zeros are not required D Leading digit 1 is not required D Range is 118 000 to 151 975 MHz in 0 005 increments Fuel Flow D Entry is pounds or kilograms depending on configur...

Page 459: ...1 increments Hold Leg Time D The minimum entry is one digit D Range is 0 5 to 3 0 minutes in 0 1 increments Instrument Landing System ILS Identifier D The minimum entry is one character D The maximum entry is four characters Intercept Radial Course D The minimum entry is one digit D Range is from 0 to 360 degrees in 1 increments International Standard Atmosphere ISA Deviation D Entry is degrees up...

Page 460: ...inutes range is from 0 0 to 59 99 in 0 01 increments D Example of entries Entry Display N0 N0000 00 N1 N0100 00 N12 N1200 00 N123 N1230 00 N1234 N1234 00 N1234 5 N1234 50 N1234 56 N1234 56 Latitude Longitude Entry of both latitude and longitude is made by combining the latitude and longitude entry with no space between Example N50W50 Latitude Longitude Altitude Constraint D Similar to Latitude Lon...

Page 461: ...W01200 00 W123 W12300 00 W1234 W12340 00 W12345 W12345 00 W12345 6 W12345 60 W12345 67 W12345 67 Meters CONVERSION page format D Entry range is from 0 to 999 999 9 M in 0 1 increments decimal required for tenths D A decimal is not required when tenths position is zero Meters Second D Entry range is from 0 to 999 9 M S in 0 1 increments decimal required for tenths D A decimal is not required when t...

Page 462: ...ifier is in the NAV database only under the waypoint name Obstacle Distance D Entry is one to six digits D Range is from 0 to 1220 Obstacle Elevation D Entry is one to five digits D Range is from 2000 to 16 500 Oceanic Waypoints D These waypoints are named according to ARINC 424 navigation database specification D Southern hemisphere uses the letters S or W D Northern hemisphere uses the letters N...

Page 463: ...20 00 5020S N 50 00 E 020 00 5020E S 52 00 W 075 00 5275W NOTE All oceanic waypoints can not be active in the navigation database Offset lateral D The minimum entry is L or R plus one digit D Range is 0 1 to 30 0 NM in 0 1 increments Orbit Radius D Entry is in tenths of NM D Range is from 1 0 to 99 9 in 0 1 increments Orbit Speed D Minimum entry for CAS is two digits D Range of CAS is from 75 to 3...

Page 464: ...nt name D Bearing entry minimum is one digit D Distance minimum entry is one digit D Bearing range is from 0 to 360 degrees in 0 1 increments decimal required for tenths D Bearing is True by placing T after the number e g PXR 090T 30 D Distance range is from 0 to 9999 9 NM in 0 1 increments decimal required for tenths Place Bearing Distance Altitude Constraint P B D ALT D Similar to P B D but with...

Page 465: ...ired for tenths Place Distance Altitude Constraint P D ALT D Similar to P D but with the addition of an altitude constraint D The altitude constraint entry format is identical to the Altitude entry format defined on page 10 2 Pounds CONVERSION page format D Entry range is from 0 to 999 999 9 LB in 0 1 increments decimal required for tenths D A decimal is not required when tenths position is zero P...

Page 466: ...inimum entry is one alpha character D Possible entries are N NE E SE S SW W NW Radial D The minimum entry is one digit D Range is from 0 0 to 360 in 0 1 increments Radial Distance D Minimum entry of one digit D Range from 1 0 to 999 9 NM in 0 1 increments Radial Inbound and Outbound Radials D Minimum entry of one digit D Range from 0 0 to 360 0 in 0 1 increments Reference Waypoint D The name is pe...

Page 467: ...unway number Runway Identifier D Entry is Airport Runway D Range for airport name is from 1 to 5 alphanumeric characters D The runway is the runway number with a suffix e g L R or C D Range for runway number is from 01 to 36 Runway Length D Entry is in feet from 2000 to 16 000 Runway Slope D Entry can have a minus sign D Range is from 2 0 to 2 0 Runway Stopway D Entry is in feet up to four digits ...

Page 468: ...round speed entry D Minimum entry is two digits D Range from 75 to 750 kts Speed Set Title D Entry is 1 to 11 characters Step Increment D Entry in feet up to five digits D Range is from 0 to 30 000 in increments of 1000 D Entries less than 1000 are interpreted as thousands Stopway D Entry is in feet up to four digits D Range is from 0 to 9999 Temperature D Entry is in degrees and negative sign whe...

Page 469: ... list of possible entries D Airway Waypoint D Flight Plan Name Waypoint D Flight Plan Name D Waypoint D Temporary Waypoint VOR Identifier D The minimum entry is one character D The maximum entry is three characters Waypoint Name D The name is permitted to be from one to five alphanumeric characters D First character cannot be a dash Weight any weight entry D Entry is pounds or kilograms depending ...

Page 470: ...tem FMS for the Agusta AW139 AB139 Helicopter A28 1146 181 REV 3 Mar 2009 Multifunction Control Display Unit MCDU Entry Format 10 18 Honeywell International Inc Do not copy without express permission of Honeywell Blank Page ...

Page 471: ...dvisory Alerting messages are more important The external annunciator located on the pilot and copilot instrument panel and the message annunciator are lit for alerting messages Advisory messages only light on the message annunciator on the MCDU MESSAGE LIST AND DEFINITIONS Table 11 1 contains an alphabetical list of all messages The list includes the type of message and a brief explanation of wha...

Page 472: ...ntified unit APPROACH CLIMB LIMITED ALERTING The message is displayed when the landing calculations are approach climb limited BACK COMPLETE ADVISORY The message indicates you have returned as far back as possible BRG CRS MUST BE IN TRUE ALERTING The bearing entry must be in true entered xxxT because the reference waypoint is outside the coverage of the magnetic variation table BUSY REENTER LAST C...

Page 473: ...ssage is shown during climbs and descents CHECK DATA LOAD xx ADVISORY The attempted data loader operation has failed The failure reason is indicated by the value xx Refer to Maintenance Section 12 for decoding xx value CHECK DEST FUEL ALERTING The destination fuel equals zero CHECK DMU ALERTING The FMS has been waiting for a flight plan from the DMU for over 60 seconds CHECK GPS CONFIG ALERTING Mo...

Page 474: ...ess than the reserve fuel required CHECK SPD ALTITUDE LIMIT ALERTING The upcoming speed and or altitude constraint must be checked and proper action taken in order to meet the constraints CHECK SPEED CONSTRAINT ALERTING In cruise or descent in vertical navigation VNAV the aircraft is approaching a waypoint that has a speed constraint when the FMS predicts based on current speed and deceleration th...

Page 475: ... on completion of NAV database loading the NAV database is not current to the date entered in the FMS DATALOADER IN USE ADVISORY Indicates the data loader is being used DATALOADER UPDATE NEEDED ADVISORY Indicates the data loader needs an update for the requested function DB TRANSFER ABORTED ADVISORY Indicates transfer of the database has been aborted DB TRANSFER COMPLETE ADVISORY Indicates transfe...

Page 476: ...South has been entered E O PERF UNAVAIL ALERTING Indicates that engine out performance is not available EXCEEDS CEILING ALTITUDE ALERTING The cruise altitude exceeds the recommended performance altitude EXCEEDS CERT CEILING ADVISORY The entered altitude is above the certified ceiling for the aircraft EXCEEDS MAX GROSS WEIGHT ADVISORY The gross weight exceeds the maximum ramp weight in the aircraft...

Page 477: ...cation where a pattern is defined is different from when the fix location was defined in the stored flight plan FLIGHT PLAN FULL ADVISORY The flight plan is full and is displayed when the pilot attempts to enter more than 100 waypoints in a flight plan FMS BATTERY MAINT REQD ALERTING The FMS battery is low and requires maintenance within three weeks FMS POSITIONS DIFFERENT ALERTING The FMS positio...

Page 478: ... receiver autonomous integrity monitoring RAIM value is above the limit for the current phase of flight GPS RAIM UNAVAILABLE ALERTING RAIM is not being generated by the GPS receiver GRAPHIC NOT AVAILABLE ADVISORY There is no graphic function input to the CD 820 or when access is externally selectable HIGH PCDR TURN GRD SPD ALERTING The ground speed exceeds the limit for the defined procedure turn ...

Page 479: ...se is invalid and is not useable Reload the database INVALID NOTAM LIST ADVISORY Indicates the notice to airmen NOTAM is invalid and has been cleared INVALID OBSTACLE ENTRY ALERTING The obstacle distance and or elevation entry makes the limits of a table used in the calculation of obstacle clearance to be exceeded ISA DEV EXCEEDED ADVISORY The entered temperature has made the International Standar...

Page 480: ...ept to the arc is found for the input definition NO CROSSING POINT FOUND ADVISORY No crossing points are found for the CROSSING POINTS page NO DISK INSTALLED ADVISORY No disk is installed in the data loader NO FLIGHT PLAN ADVISORY Origin or origin destination is entered on the FLIGHT PLAN LIST page and there is no flight plan with the same origin or origin destination NO INPUT ALLOWED ADVISORY No ...

Page 481: ...ALERTING The sensed OAT or ISA deviation exceeds the limit OBSTACLE DIST CONFLICT ALERTING An entry of an obstacle distance is less than an entry of stopway or clearway OFFSET CANCEL ALERTING The offset has been canceled OFFSET CANCEL NEXT WPT ALERTING The offset is canceled at the next waypoint in the flight plan This message is cleared by pilot action or is automatically cleared when the offset ...

Page 482: ... FMS that accepts a regional NDB only RESET ALT SEL ALERTING The FMS is commanding a change of altitude but the altitude selector has not been reset The aircraft cannot change altitude until the selector has been reset RUNWAY NOT FOUND ADVISORY The database does not contain the entered runway at the designated airport S E PERF UNAVAIL ALERTING Indicates single engine performance is not available S...

Page 483: ...akeoff and power has been advanced for takeoff TO WEIGHT LIMITED ALERTING The current gross weight is between the maximum takeoff weight and the maximum ramp weight for the aircraft and the takeoff gross weight used by the Takeoff and Landing function has been limited to the maximum takeoff weight for the aircraft UNABLE HOLD CHANGE ADVISORY The pilot attempted to change the holding pattern defini...

Page 484: ...wledge for a linked message for 5 minutes UNABLE TUNE REQUEST ADVISORY The pilot entered a frequency while the radios were in the manual mode USED BY ACTIVE FPL ADVISORY The pilot tried to delete a waypoint from storage used in the active flight plan USED BY OFFSIDE ACT FPL ADVISORY The pilot attempted to delete a waypoint from storage used in the offside active flight plan USING CURRENT GS FF ALE...

Page 485: ...externally selectable VOR 1 FAILED VOR 2 FAILED ALERTING The FMS senses the identified VOR has failed WAYPOINT NOT FOUND ADVISORY The entered waypoint cannot be found When this results when attempting to enter an airway into a flight plan the waypoint is not part of the referenced airway WEIGHT DEFAULT LB ALERTING Indicates the weight option has defaulted to pounds Normally the result of the confi...

Page 486: ...Flight Management System FMS for the Agusta AW139 AB139 Helicopter A28 1146 181 REV 3 Mar 2009 Messages 11 16 Honeywell International Inc Do not copy without express permission of Honeywell Blank Page ...

Page 487: ...ve activity light does not go on or the FMS does not hear the response from the data loader the drive light turns ON 02 STATUS CMD NO RESPONSE See 01 03 ILLEGAL DB FILE HEADER The database disk file db bn is not a legal database file 04 READ CMD NO RESPONSE The data loader was unable to open and read data on the disk 05 GET 1ST FP RECORD FAILED The data in a flight plan file sperry dat is incorrec...

Page 488: ...orrupted 10 BAD BOW VALUE The flight plan file contains an illegal basic operating weight value 11 BAD FUEL VALUE The flight plan file contains an illegal fuel value 12 BAD CARGO VALUE The flight plan file contains an illegal cargo weight value 13 BAD PASSENGERS VALUE The flight plan file contains an illegal passenger count 14 BAD INITIAL CRUISE The flight plan file contains an illegal initial cru...

Page 489: ...plan file contains an illegal waypoint latitude 20 GET LONGITUDE FAILED The flight plan file contains an illegal waypoint longitude 21 GET SPD CONSTR FAILED The flight plan file contains an illegal waypoint speed constraint 22 GET FL CONSTR FAILED The flight plan file contains an illegal waypoint flight level constraint 23 GET SPOT WIND FAILED The flight plan file contains an illegal waypoint spot...

Page 490: ...ct tab on the disk is preventing the data loader from writing to the disk 2F DISK IS FULL There is no more free space on the disk for writing data files 30 WRITE CMD NO RESPONSE The data loader is not responding to the FMS write request 31 CLOSE CMD NO RESPONSE The data loader is not responding to the FMS open file command 32 STATUS CMD ILLEGAL VALUE The data loader sent an undecodable status resp...

Page 491: ...ON ON DISK The NAV database disk is not compatible with the current FMS version or the file is corrupted 3F WRONG PERF VERSION ON DISK The stored learning curve data files are not compatible with the current FMS version 40 REGIONAL NDB ONLY The FMS is configured to only accept a regional NDB 80 ASYNC OPEN CMD NO RESPONSE Unused 81 ASYNC DL STOPPED RESPONDING In asynchronous download mode the data ...

Page 492: ...s been exceeded This is due to excessive line noise F1 FLASH SETUP ERROR The FMS flash memory devices are defective or have exceeded the rated erase write cycles F2 FLASH CHARGE ERASE ERROR The FMS flash memory devices are defective or have exceeded the rated erase write cycles F3 FLASH WRITE ERROR The FMS flash memory devices are defective or have exceeded the rated erase write cycles These codes...

Page 493: ...h that the pilot does not have a direct viewing angle to the MCDU When the pilot does not have a direct viewing angle to the MCDU the line select prompts appear out of alignment with the physical line select keys and is called parallax Pushing PARALLAX 5R on the MCDU MAINTENANCE page accesses the PARALLAX ADJUST page shown in Figure 12 1 When the navigation computer or performance computer when in...

Page 494: ...he LEFT prompt horizontally adjusts the MCDU display to the left D 2R Pushing the RIGHT prompt horizontally adjusts the MCDU display to the right D 6L Pushing the DOWN prompt vertically adjusts the MCDU display downward D 6R Pushing the RETURN prompt returns to the SYSTEM SETUP 1 1 page or to the last page being viewed when the navigation computer or performance computer when installed is operatin...

Page 495: ...ey are accessed Table A 1 MCDU Page Access Trees Page Access Tree Figure Function Keys Page Tree A 1 Perf Index Page Tree A 2 NAV Index Page 1 2 Page Tree A 3 NAV Index Page 2 2 Page Tree A 4 Progress Page Tree A 5 Direct Page Tree A 6 Patterns Page Tree A 7 Pos Sensors Page Tree A 8 Maintenance Page Tree A 9 NAV Ident Position Init Page Tree A 10 Active Flight Plan Alternate Flight Plan Page Tree...

Page 496: ...t Management System FMS for the Agusta AW139 AB139 Helicopter A28 1146 181 REV 3 Mar 2009 MCDU Page Access Trees A 2 Honeywell International Inc Do not copy without express permission of Honeywell Blank Page ...

Page 497: ...ystem FMS for the Agusta AW139 AB139 Helicopter A28 1146 181 REV 3 Mar 2009 MCDU Page Access Trees A 3 A 4 Honeywell International Inc Do not copy without express permission of Honeywell Figure A 1 Function Keys Page Tree ...

Page 498: ...System FMS for the Agusta AW139 AB139 Helicopter A28 1146 181 REV 3 Mar 2009 MCDU Page Access Trees A 5 A 6 Honeywell International Inc Do not copy without express permission of Honeywell Figure A 2 Perf Index Page Tree ...

Page 499: ...em FMS for the Agusta AW139 AB139 Helicopter A28 1146 181 REV 3 Mar 2009 MCDU Page Access Trees A 7 A 8 Honeywell International Inc Do not copy without express permission of Honeywell Figure A 3 NAV Index Page 1 2 Page Tree ...

Page 500: ...em FMS for the Agusta AW139 AB139 Helicopter A28 1146 181 REV 3 Mar 2009 MCDU Page Access Trees A 9 A 10 Honeywell International Inc Do not copy without express permission of Honeywell Figure A 4 NAV Index Page 2 2 Page Tree ...

Page 501: ...System FMS for the Agusta AW139 AB139 Helicopter A28 1146 181 REV 3 Mar 2009 MCDU Page Access Trees A 11 A 12 Honeywell International Inc Do not copy without express permission of Honeywell Figure A 5 Progress Page Tree ...

Page 502: ... System FMS for the Agusta AW139 AB139 Helicopter A28 1146 181 REV 3 Mar 2009 MCDU Page Access Trees A 13 A 14 Honeywell International Inc Do not copy without express permission of Honeywell Figure A 6 Direct Page Tree ...

Page 503: ...System FMS for the Agusta AW139 AB139 Helicopter A28 1146 181 REV 3 Mar 2009 MCDU Page Access Trees A 15 A 16 Honeywell International Inc Do not copy without express permission of Honeywell Figure A 7 Patterns Page Tree ...

Page 504: ...ystem FMS for the Agusta AW139 AB139 Helicopter A28 1146 181 REV 3 Mar 2009 MCDU Page Access Trees A 17 A 18 Honeywell International Inc Do not copy without express permission of Honeywell Figure A 8 Pos Sensors Page Tree ...

Page 505: ...ystem FMS for the Agusta AW139 AB139 Helicopter A28 1146 181 REV 3 Mar 2009 MCDU Page Access Trees A 19 A 20 Honeywell International Inc Do not copy without express permission of Honeywell Figure A 9 Maintenance Page Tree ...

Page 506: ...MS for the Agusta AW139 AB139 Helicopter A28 1146 181 REV 3 Mar 2009 MCDU Page Access Trees A 21 A 22 Honeywell International Inc Do not copy without express permission of Honeywell Figure A 10 NAV Ident Position Init Page Tree ...

Page 507: ...he Agusta AW139 AB139 Helicopter A28 1146 181 REV 3 Mar 2009 MCDU Page Access Trees A 23 A 24 Honeywell International Inc Do not copy without express permission of Honeywell Figure A 11 Active Flight Plan Alternate Flight Plan Page Tree ...

Page 508: ...em FMS for the Agusta AW139 AB139 Helicopter A28 1146 181 REV 3 Mar 2009 MCDU Page Access Trees A 25 A 26 Honeywell International Inc Do not copy without express permission of Honeywell Figure A 12 Performance Init Page Tree ...

Page 509: ...ystem FMS for the Agusta AW139 AB139 Helicopter A28 1146 181 REV 3 Mar 2009 MCDU Page Access Trees A 27 A 28 Honeywell International Inc Do not copy without express permission of Honeywell Figure A 13 Departure Page Tree ...

Page 510: ...stem FMS for the Agusta AW139 AB139 Helicopter A28 1146 181 REV 3 Mar 2009 MCDU Page Access Trees A 29 A 30 Honeywell International Inc Do not copy without express permission of Honeywell Figure A 14 Takeoff Data Page Tree ...

Page 511: ...MS for the Agusta AW139 AB139 Helicopter A28 1146 181 REV 3 Mar 2009 MCDU Page Access Trees A 31 A 32 Honeywell International Inc Do not copy without express permission of Honeywell Figure A 15 Arrival Missed Approach Page Tree ...

Page 512: ...System FMS for the Agusta AW139 AB139 Helicopter A28 1146 181 REV 3 Mar 2009 MCDU Page Access Trees A 33 A 34 Honeywell International Inc Do not copy without express permission of Honeywell Figure A 16 Landing Page Tree ...

Page 513: ...ddressing and Reporting System ACC access air conditioning controller ACCUM accumulator ACDB aircraft database ACFT aircraft ACL accel ACMF aircraft condition monitoring function ACP audio control panel ACT active actual altitude compensated tilt ACU antenna controller unit ADA air data application ADC air data computer ADF automatic direction finder ADI attitude director indicator ADJ adjustment ...

Page 514: ...lert ALT alternate altitude ALTA altitude acquire AM amplitude modulated AMI airline modifiable information amp ampere ANG angle ANT antenna AOA ACARS over AVLC CMF angle of attack AOC Aeronautical Operational Communication AOG aircraft on ground AOR E Atlantic Ocean Region East AOR W Atlantic Ocean Region West AOSS after over station sensor AP autopilot APC audio processing card APM aircraft pers...

Page 515: ...ervice ATT attitude aux auxiliary AVAIL available AVLC Aviation VHF Link Control AZ azimuth B at or below BAC back course BAG baggage BARO baro barometric BAT Bat battery BC back course BFL balanced field length BFO beat frequency oscillator BIT built in test BITE built in test equipment BKUP backup BLW below BOD bottom of descent BOSC bottom of step climb BOW basic operating weight BPCU bus power...

Page 516: ...tified CFIT controlled flight into terrain CG center of gravity CHARS characters CHG CHNG change changing CHKLST Cklst checklist CLB climb CLR clear CLX clearance CMC central maintenance computer CMD command CMF communications management function CNS communications navigation and surveillance CNST constant COM COMM communication COMP compass compensation COMPT compartment CONFIG configuration CONS...

Page 517: ...ADC digital air data computer DAU data acquisition unit DB database DC display controller DCL data control logic DDU display driver unit DEGRAD degrade DEL delete DENS density DEOS digital engine operating system DEP DEPT departure DES descent DEST destination DEV deviation DGC display guidance computer DGPS differential global positioning system DGR DGRAD degraded DH decision height DIM dimming D...

Page 518: ...xed ECM electronic counter measures ECS environmental control system ECU electronic control unit EDM emergency decent mode EDS electronic display system EFIS electronic flight instrument system EGPWC enhanced ground proximity warning computer EGPWS enhanced ground proximity warning system EGT engine gas temperature EICAS engine instruments and crew alerting system ELEV elevation EMER emergency END...

Page 519: ...authority digital engine compute FAF final approach fix FANS future air navigation system FAX facsimile FD flight director FDR flight data recorder FF fuel flow FGC flight guidance computer FGS flight guidance system FHAF final hover approach fix FL flight level FLCH flight level change FLD field FLEX flexible FLIR forward looking infrared FLT flight FLT REF flight reference FMS flight management ...

Page 520: ...arth station GGF graphic generation function GLS GNSS landing system GPS landing system GMAP ground mapping GND ground GNSS global navigation satellite system GP glidepath GPS global positioning system GPWS ground proximity warning system GRAD gradient GRD ground FMS GS glideslope ground speed FMS GSP ground service panel GSPD ground speed GUI graphical user interface H hold HA high altitude HD he...

Page 521: ... indicator HT height HUD head up display HV height velocity Hz hertz I inner I O input output IAF initial approach fix IAS indicated airspeed ICAO International Civil Aviation Organization ICS intercom system ID IDENT identification IGE in ground effect IGN ignition IGS instrument guidance system IHBT inhibited ILS instrument landing system IMC instrument meteorological conditions IN inches Info i...

Page 522: ...ons Union JAA Joint Air Worthiness Authority KCAS knots calibrated airspeed kg kilogram kHz kilohertz KM kilometers KIAS knots indicated airspeed KPH kilograms per hour kts knots L left liters LA low altitude LANDNG LDG landing LAT lat latitude LAV lavatory LB S lb s pound s LBS Lateral beam sensor LCD liquid crystal display LCV load control valve LD landing lower sideband data LDA landing directi...

Page 523: ...r sideband voice LX lightning M meters MAG mag magnetic MAGVAR magnetic variation MAINT maintenance MAN manual MAP missed approach point MAU modular avionics unit MAX maximum mB millibars MCDU multifunction control display unit multipurpose control display unit MCT maximum continuous thrust MDA minimum descent altitude MECH mechanical MED medium MET manual electric trim METERO meterological MFD mu...

Page 524: ... terrain clearance MULTI multiple mV millivolts MWF monitor warning function MXR maximum range N north N A not applicable NAV navigation NAVAID navigational aid NAVSTAR navigation system with time and ranging NB nondirectional beacon NBAA National Business Aircraft Association NBR NO NUM number NDB navigation al database nondirectional beacon FMS NDU navigation display unit NIC network interface c...

Page 525: ...requirement table OS over station OSS over station sensor OUTBD outbound OVRD override OVSPD overspeed P pressure procedure P B D place bearing distance P B P B place bearing place bearing PA passenger address PAPI precision approach path indicator PAST pilot activated self test PBX private branch exchange PC personal computer PCDR procedure PD place distance PDC programmable data capture PDL port...

Page 526: ...ROG progress PS power supply psi pound force per square inch PT point procedure turn FMS PTRN pattern PTS points PTT push to talk PTU power transfer unit PWR power PWS predictive windshear system QFE field elevation pressure height above the ground queens field elevation QNH sea level pressure QTY quantity QUAD quadrant R remote right R T radio transmitter RA radio altitude resolution advisory TCA...

Page 527: ...vigation RNP required navigation performance RO read only ROL roll RPM revolution per minute RQST request RT receiver transmitter RTA receiver transmitter antenna RTD retard RTU radio tuning unit RW RWY runway RX receiving S south suspend S E single engine SA selective availability situational awareness SAR search and rescue SAT static air temperature SATCOM Satellite Communication System satellit...

Page 528: ...rn approach SPD speed SPEX search pattern exit spares exchange SPST search pattern start SPKR speaker SQ squelch SQNO squelch noise ST sidetone stop STAB stabilization STAR standard terminal arrival route STAT status STBY standby STD standard STK MIC stuck microphone STR stretcher SUA selects special use SUM summary SVC service SVN satellite vehicle number SVO start valve open SW switch SYM SYS SY...

Page 529: ...on approach TCS touch control steering TD H transition down to hover TDOP time dilution of precision TEMP temperature TERM terminal TERR terrain TF track to a fix TGT target turbine gas temperature THRESH threshold THROT throttle TMS thrust management system TO takeoff TOC top of climb TOD top of descent TOGA takeoff go around TOLD takeoff and landing TQA throttle quadrant assembly TR thrust rever...

Page 530: ...l altitude select VNAV altitude preselect VASI visual approach slope indicator VBS vertical beam sensor VCT vector Vdc volts direct current VDEV vertical deviation VDL VHF digital link VDOP vertical dilution of precision VDR VHF data radio VERT vertical VFLCH vertical flight level change VFOM vertical figure of merit VFS final segment climb speed VGS visual guidance system VHF very high frequency ...

Page 531: ...keoff rotation speed VREF reference speed VRHT radio altitude hold VS vertical speed VSE single engine climb speed VSPD VSPEED vertical speed VTA vertical track alert W west W S windshear W T wind temperature WARN warning WAYPT WPT waypoint WGS world geodetic system WND wind WNDSHR windshear WOW weight on wheels WT weight WTR winchman trim WX weather WX T weather turbulence XFER transfer XMIT tran...

Page 532: ...agement System FMS for the Agusta AW139 AB139 Helicopter A28 1146 181 REV 3 Mar 2009 Acronyms and Abbreviations Abbrev 20 Honeywell International Inc Do not copy without express permission of Honeywell Blank Page ...

Page 533: ... 50 Autotune 6 93 B Brightness control 3 28 Build a flight plan by entering waypoints 7 14 additions deletions to the flight plan 7 18 airway 7 15 clearing of flight plans 7 22 flight plan name 7 15 storing of active flight plan 7 21 temporary waypoint 7 14 vertical entries 7 16 VNAV offset 7 20 waypoint 7 14 C Clear CLR key 3 6 Clearing of flight plans 4 52 Climb 4 39 Conversion 6 96 conversion 1...

Page 534: ... runway extension waypoints 7 4 speed limit 7 7 speed schedule 7 7 temporary waypoints 7 3 TO waypoint 7 5 top of climb 7 8 top of descent 7 8 VNAV offset waypoints 7 4 waypoint names 7 2 Delete DEL key 3 6 Deleting stored flight plans 6 8 Departure selection 4 23 departure surfaces 4 23 departure trans 4 25 procedure 4 26 SIDs 4 24 Departures 6 35 departure surfaces 1 X 6 37 Descent 4 41 Direct t...

Page 535: ... stored flight plans 6 8 Flight plan select 6 9 FLT PLAN SELECT 1 1 6 9 Flight planning 2 3 Flight summary FLIGHT SUMMARY 1 1 6 206 Flyover pattern 6 127 FMS database 6 33 custom database 6 34 navigation database 6 33 temporary waypoints 6 34 FMS position updata 6 63 FMS product support 1 2 FMS setup pages 6 184 Fuel management 5 36 FUEL MGT LB 1 2 5 36 FUEL MGT LB 2 2 5 38 Function keys 3 7 DIR k...

Page 536: ... transfer line data to line fields 3 6 transfer line data to scratchpad 3 6 List of entries and definitions 10 1 LNAV submodes 7 23 LNAV ARM 7 23 LNAV CAPTURE 7 23 M M manual 6 92 Maintenance 6 177 active operating modes 6 177 engineering data 6 191 failed sensors 6 179 flight configuration 6 186 FMS setup pages 6 184 high latitude flying 6 182 introduction 12 1 MCDU parallax adjustment 12 7 retur...

Page 537: ...sections 6 31 navaids 6 28 surfaces helipads 6 25 departures 6 35 flight plan list 6 4 defining stored flight plans 6 6 deleting stored flight plans 6 8 flight plan select 6 9 FMS database 6 33 custom database 6 34 navigation database 6 33 temporary waypoints 6 34 identification 6 175 introduction 6 1 maintenance 6 177 active operating modes 6 177 engineering data 6 191 failed sensors 6 179 flight...

Page 538: ...osition sensor deselection 6 87 sensors being used by the FMS 6 86 O Operational example active flight plan 4 9 waypoint entry 4 11 alternate flight plan 4 51 approach 4 47 arrival 4 41 clearing of flight plans 4 52 climb 4 39 departure selection 4 23 descent 4 41 en route 4 40 introduction 4 1 landing 4 48 missed approach 4 50 performance data 4 19 performance initialization 4 15 position initial...

Page 539: ...e init 2 3 4 17 performance init 3 3 4 18 pilot speed fuel flow 5 3 Performance plan 5 23 landing pages 5 32 takeoff pages 5 27 wind and temperature pages 5 24 Phases to the MOT flight plan 6 164 Pilot defined waypoints 6 32 Pilot overview customer support 1 3 global customer care GCC 1 3 Honeywell online technical publications 1 3 FMS product support 1 2 Honeywell product support 1 2 Pilot speed ...

Page 540: ...are search 6 145 parallel search pattern 6 157 search pattern construction 6 161 search pattern operation and guidance 6 161 sector search pattern 6 149 Sector search pattern 6 149 Sensor status pages 6 73 Sensors being used by the FMS 6 86 SP search pattern 6 144 SPD FF and current gound speed FF method 5 7 pilot speed fuel flow SPD FF method 5 7 Speed command 7 49 automatic 7 50 general speed co...

Page 541: ...points 6 33 V Vertical navigation 7 24 general VNAV rules 7 24 VNAV approach temperature compensation 7 30 VNAV operation in flight 7 27 VNAV operational scenarios 7 42 VNAV special operations 7 29 VNAV submodes 7 24 Vertical navigation VNAV 2 4 VNAV approach temperature compensation 7 30 VNAV data 8 5 VNAV operation in flight 7 27 climb 7 27 cruise 7 27 descent 7 28 top of descent 7 28 VNAV opera...

Page 542: ...Flight Management System FMS for the Agusta AW139 AB139 Helicopter A28 1146 181 REV 3 Mar 2009 Index Index 10 Honeywell International Inc Do not copy without express permission of Honeywell Blank Page ...

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