Honeywell BENDIXKing APEX EDGE Series Pilot'S Manual Download Page 37

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Honeywell Bendix/King KFD 840 Primary Flight Display

KFD 840 PG PN 7450-0840-01 Attitude Area
Rev C May 28, 2010 3-9

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

FLIGHT DIRECTOR COMMAND BARS

The flight director command bars, shown below, are displayed as a
single cue wedge

The flight director command bars are removed when the flight
director is not engaged or not installed.

Single Cue Command Bar

The single-cue command bar consists of two solid magenta wedges
that move as shown in the figures below:

Pitch up command

Pitch down command

Summary of Contents for BENDIXKing APEX EDGE Series

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Page 3: ...l Inc Do not copy without express permission of Honeywell Honeywell International Inc 23500 W 105th Street Olathe KS 66061 U S A CAGE 22373 Telephone 800 601 3099 U S A Canada Telephone 602 365 3099 International APEX EDGE SERIES KFD 840 Primary Flight Display Pilot s Guide ...

Page 4: ...e products subject to an applicable product support agreement their wholly owned subsidiaries or a formally designated third party service provider thereunder and direct recipients of 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 anot...

Page 5: ... these Materials contain information that is confidential and proprietary to Honeywell You agree to take all reasonable efforts to maintain the confidentiality of these Materials 4 Assignment And Transfer This License Agreement may be assigned to a formally designated service designee to the extent allowed under an applicable product support agreement or transferred to a subsequent owner or operat...

Page 6: ...RINGEMENT OF INTELLECTUAL PROPERTY RIGHTS OF THIRD PARTIES EVEN IF HONEYWELL HAS BEEN ADVISED OF ANY SUCH INFRINGEMENT IN NO EVENT WILL HONEYWELL BE LIABLE FOR ANY INCIDENTAL DAMAGES CONSEQUENTIAL DAMAGES 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 AN...

Page 7: ...1 Honeywell International Inc Do not copy without express permission of Honeywell Revision History and Instructions Manual KFD 840 Primary Flight Display Pilot s Guide Revision D July 12 2010 Summary Added a clarification for when the heading SYNC button is pressed when the aircraft is on a 360 degree heading See page 7 3 ...

Page 8: ...cord of Revisions KFD 840 PG PN 7450 0840 01 RR 2 Rev D July 12 2010 Honeywell International Inc Do not copy without express permission of Honeywell Record of Revisions REVISION NUMBER REVISION DATE A B Sept 13 2009 C Sept 23 2009 D May 28 2010 July 12 2010 ...

Page 9: ...y 28 2010 Introduction 1 1 May 28 2010 1 2 May 28 2010 Getting Started 2 1 May 28 2010 2 2 May 28 2010 2 3 May 28 2010 2 4 May 28 2010 2 5 May 28 2010 2 6 May 28 2010 2 7 May 28 2010 2 8 May 28 2010 2 9 May 28 2010 2 10 May 28 2010 2 11 May 28 2010 Subheading and Page Date 2 12 May 28 2010 Attitude Area 3 1 May 28 2010 3 2 May 28 2010 3 3 May 28 2010 3 4 July 12 2010 3 5 July 12 2010 3 6 May 28 20...

Page 10: ...2010 7 3 July 12 2010 7 4 May 28 2010 7 5 May 28 2010 7 6 May 28 2010 7 7 May 28 2010 7 8 May 28 2010 7 9 May 28 2010 7 10 May 28 2010 Checklist Area 8 1 May 28 2010 8 2 May 28 2010 8 3 May 28 2010 8 4 May 28 2010 8 5 May 28 2010 8 6 May 28 2010 Miscellaneous Navigation Area 9 1 May 28 2010 9 2 May 28 2010 Emergency Operations 10 1 May 28 2010 10 2 May 28 2010 10 3 May 28 2010 10 4 May 28 2010 10 ...

Page 11: ...ion Keys 2 9 Display Brightness BRT 2 10 Aircraft Configuration CONF 2 10 3 ATTITUDE AREA 3 1 ATTITUDE DIRECTOR INDICATOR ADI WINDOW 3 1 ARTIFICIAL HORIZON 3 2 AIRCRAFT REFERENCE SYMBOL 3 4 ATTITUDE PITCH TAPE 3 4 Excessive Attitude ChevronsError Bookmark not defined ATTITUDE ROLL POINTER AND SCALE 3 6 SLIP SKID STANDARD RATE TURN MARKER DISPLAY 3 8 FLIGHT DIRECTOR COMMAND BARS 3 9 Single Cue Comm...

Page 12: ...NIMUM ALTITUDE ALERT CONDITION ARMED 5 7 VERTICAL DEVIATION SCALE AND POINTER 5 8 Vertical Deviation Invalid 5 8 6 VSI AREA 6 1 VERTICAL SPEED VS DISPLAY 6 1 Vertical Speed Scale and Pointer 6 2 Vertical Speed Digital Readout 6 2 Vertical Speed Data Invalid 6 3 7 HSI AREA 7 1 HORIZONTAL SITUATION INDICATOR HSI WINDOW DISPLAYS AND ANNUNCIATORS 7 1 Full Compass 360 HSI Partial Compass ARC HSI Headin...

Page 13: ...ANEOUS DATA AREA 9 1 WIND GROUND SPEED TRUE AIRSPEED AND OUTSIDE AIR TEMPERATURE 9 1 Wind 9 1 Ground Speed 9 2 True Airspeed 9 2 Outside Air Temperature 9 2 10 EMERGENCY OPERATIONS 10 1 ADC AIR DATA COMPUTER FAILURE 10 1 ATTITUDE FAILURE AHRS FAILURE 10 2 HDG HEADING FAIL CRM FAILURE COMPASS REMOTE MAGNETOMETER 10 3 IN FLIGHT RESTART 10 4 CONFIGURATION MODULE ERRORS 10 5 MINOR FAILURE INDICATIONS ...

Page 14: ...e 3 4 Attitude Failure Indication 3 3 Figure 3 5 Attitude Roll Pointer and Scale 3 6 Figure 3 6 Attitude Sky Pointer and Scale 3 7 Figure 3 7 Slip Skip Standard Rate Turn Marker Display 3 8 Figure 4 1 Airspeed Tape 4 1 Figure 5 1 Altitude Display 5 1 Figure 6 1 VSI Display 6 1 Figure 7 1 HSI Display 7 1 Figure 7 2 Partial Compass ARC HSI 7 2 Figure 7 3 Selected Heading Readout and Bug 7 3 Figure 7...

Page 15: ... SUPPORT For more information including details regarding your warranty visit www bendixking com kfd840pcutility For technical support of this product please contact your local Bendix King Dealer To locate the Bendix King Dealer nearest you visit www bendixking com kfd840pcutility For additional support contact Honeywell Customer Product Support at US Canada 1 877 712 2386 All other countries 1 91...

Page 16: ...Publications Web site at https portal honeywell com wps portal aero to Download or see publications online Make an order for a publication Tell Honeywell of a possible data error in a publication If you do not have access to the Honeywell Online Technical Publications web site and need technical publications information Send an e mail message to the complete customer care center at cas publication...

Page 17: ...ED The KFD 840 is a primary flight display PFD that provides all necessary information to the flight crew for complete navigation throughout the flight envelope The KFD 840 displays the normal flight instruments attitude heading airspeed and altitude GENERAL INFORMATION This section provides an overview of the operating controls and displays of the KFD 840 The PFD is shown below Figure 2 1 Control...

Page 18: ...ion of Honeywell 1 Course Knob CRS 6 Symbolic Aircraft 2 Function select buttons 7 Attitude Direction Indicator ADI 3 Heading Knob HDG 8 Airspeed Tape 4 Horizontal Situation Indicator Display HSI 9 SD Card Reader 5 Altitude Tape 10 Photocell Main Display Areas The PFD display is divided into different display areas as shown on the figures below Figure 2 2 Display Main Areas Part 1 ...

Page 19: ...ithout express permission of Honeywell Figure 2 3 Display Main Areas Part 2 Each area contains the displays and functions listed below Attitude Area ADI window o Attitude o Slip skid indicator o Roll index and pointer o Flight director command bars o Rate of turn Airspeed Area o Airspeed tape rolling digits and trend vector o Selected airspeed readout and bug ...

Page 20: ...ector o Altitude rolling digits and tape o Metric altitude o Minimum altitude MIN and bug o Barometric setting o Vertical deviation scale and pointer HSI area o Primary navigation CDI source o Course select o Lateral deviation scale and pointer o Compass scale o Selected heading readout and bug o Bearing Pointers o Waypoint Information o Bearing Information Vertical Speed Area o Vertical speed rea...

Page 21: ...gation Data left and right of the HSI o Wind speed and direction cross wind and headwind o Ground speed o True Airspeed o Outside Air Temperature The following section provides a detailed explanation of the symbology and displays available on the KFD 840 In this example the CDI needle has been turned ON and Bearing sources are being displayed The CDI is shown centered in a TO condition Figure 2 4 ...

Page 22: ...Window 7 Airspeed Trend Line 8 Symbolic Aircraft 9 Bank Angle Scale 10 Flight Director 11 Vertical Guidance Window 12 Selected Altitude Bug 13 Selected Altitude Digits 14 Vertical Speed Digital Readout 15 Vertical Speed Pointer 16 Altitude Window 17 Vertical Speed Indicator VSI 18 Minimum Alert Altitude Bug MIN 19 Glide slope glide path deviation pointer 20 MIN Altitude bug value 21 Barometric set...

Page 23: ...sed to select and control additional functions These functions are selected by pressing the knob The operation of both the right and left knobs are identical Pressing the knob once and releasing it in less than 2 seconds displays the menu for the additional functions which can be controlled by that knob Pressing the knob when the menu is displayed advances the menu selection up The selection is hi...

Page 24: ... rotary knob is pressed and released within two seconds while indicating the BARO function the system will display a menu list of available controls for the knob with the next selection on the menu ALT will be boxed highlighted and the menu selection displayed above the knob will change to ALT to indicate that it is now the active selection For each subsequent press release the individual selectio...

Page 25: ... pointer O BRG Bearing 2 pointer BRG and course deviation indicator CDI Pressing any key once brings up the first menu selection for that function key The menu selection advances one selection for each press of the key Each time a menu is activated the menu display will remain active for 5 seconds Detailed operation of each selection is provided later in this manual The flowchart below provides a ...

Page 26: ... the red X is displayed Press any knob or button other than the knob or button with the red X to restore system operation If the stuck button was temporary and the red X extinguishes press any button or knob to restore system operation Display Brightness BRT Display brightness is controlled by the left knob A photocell senses ambient lighting and determines day or night mode Day mode controls dimm...

Page 27: ... express permission of Honeywell NOTE The CONF and INFO menu selections are disabled when airspeed is above 40 kts 46 mph The KFD 840 will automatically revert to PFD display above this speed To access the CONF page press the left knob until the CONF is highlighted in the menu The KFD Flight Settings page will be displayed Figure 2 8 KFD Flight Settings Page Part 1 ...

Page 28: ... 2 9 KFD Flight Settings Page Part 2 When the desired selection is highlighted turn the right knob to change the setting of the highlighted parameter To save the setting change press the SAVE function below the display The SAVE annunciation will be removed indicating the setting has been saved To exit the KFD Flight Settings page after saving the settings press the RETURN function key To exit the ...

Page 29: ...International Inc Do not copy without express permission of Honeywell 3 ATTITUDE AREA ATTITUDE DIRECTOR INDICATOR ADI WINDOW The attitude director indicator ADI centered in the top half of the PFD is shown below The descriptions of the elements of the ADI are given in the following paragraphs Figure 3 1 Attitude Director Window ...

Page 30: ...te horizon line Figure 3 2 Artificial Horizon Any attitude more than 40 o pitch up is displayed as almost all sky blue with a thin slice or eyebrow of ground retained for reference For pitch down attitudes more that 40 o the attitude display is almost all ground brown with an eyebrow of sky blue Figure 3 3 Artificial Horizon with Large Pitch Angles NOTE The 30 up and 30 down markings on the attitu...

Page 31: ...010 3 3 Honeywell International Inc Do not copy without express permission of Honeywell When attitude data is invalid the entire attitude sphere changes to black The pitch tape roll pointer and slip skid indicator are removed the ATTITUDE FAILURE annunciator is displayed Figure 3 4 Attitude Failure Indication ...

Page 32: ...ircraft pitch and roll The single cue aircraft symbol is displayed as triangular white wedges shaded gray in the lower half Peak is centered in the ADI ATTITUDE PITCH TAPE The attitude pitch tape identifies the current aircraft pitch attitude The attitude pitch tape is displayed through the center of the attitude display The attitude pitch tape is labeled with numeric values to 60 o pitch angle On...

Page 33: ... are displayed at approximately 30 45 and 60 NOTE The 30 markings and chevrons on the attitiude tape will appear when the aircraft is pitched up or down approximently 18 When aircraft pitch exceeds 30º nose up or 30º nose down or when roll is greater than 75º the PFD is decluttered by removing all but the most critical data These symbols and data are restored when the roll angle is between 63º rig...

Page 34: ...rks at 30 and 60 Inverted hollow triangles are displayed at 0 and 45 The KFD 840 has two options for the roll pointer and scale Figure 3 5 Attitude Roll Pointer and Scale The first option is a roll pointer In this option the roll arc is stationary with respect to the horizon and the pointer moves back and forth across the arc The attitude roll pointer indicates the current aircraft roll attitude T...

Page 35: ...the roll arc moves to the left and right of the roll pointer The attitude roll pointer indicates the current aircraft roll attitude The roll scale is the same as the option above The roll scale moves to the left as the roll angle increases and moves to the right as the roll angle decreases The type of pointer is set at installation to match the type of pointer on the standby attitude indicator The...

Page 36: ... to the ball in a standard turn and bank indicator The trapezoidal bottom half of the roll pointer is used as the slip skid lateral acceleration indicator When the trapezoid is displayed offset one width this is equal to one ball out The inverted V marks on either side of the center mark of the roll scale mark the bank angle that must be flown to maintain a standard rate turn The position of these...

Page 37: ...f Honeywell FLIGHT DIRECTOR COMMAND BARS The flight director command bars shown below are displayed as a single cue wedge The flight director command bars are removed when the flight director is not engaged or not installed Single Cue Command Bar The single cue command bar consists of two solid magenta wedges that move as shown in the figures below Pitch up command Pitch down command ...

Page 38: ...ight Display Attitude Area KFD 840 PG PN 7450 0840 01 3 10 Rev C May 28 2010 Honeywell International Inc Do not copy without express permission of Honeywell Roll right command Roll left command The command bar moves behind the aircraft symbol ...

Page 39: ...express permission of Honeywell 4 AIRSPEED AREA AIRSPEED DISPLAY The airspeed display shown below is in the upper left of the PFD The following items are displayed on the airspeed display 1 Airspeed tape 2 Airspeed window 3 Never Exceed Airspeed VNE 4 Selected Airspeed reference digital readout 5 Airspeed Trend Bar 6 Selected Airspeed Bug Figure 4 1 Airspeed Tape ...

Page 40: ... are selected during time of installation and are not pilot selectable When the selected airspeed exceeds the displayed range the bug parks at the top or bottom of the display with half the bug visible to indicate the direction to the selected airspeed AIRSPEED TAPE AND ROLLING DIGITS The airspeed tape is a moving scale with an airspeed reference line and airspeed marks with a range of 30 to 240 k...

Page 41: ...speed rolling digits display is removed Loss of air data will also cause the loss of TAS true airspeed standard rate of turn indicator and winds if installed AIRSPEED TREND VECTOR Airspeed trend is represented by a white vertical bar positioned along the right side of the airspeed tape depicting the airspeed in 6 seconds if the current acceleration deceleration trend continues The airspeed trend v...

Page 42: ...s permission of Honeywell AIRSPEED COLOR BANDS The airspeed tape color bands are Red Barber Pole Bar Over speed warning Red Horizontal Bar VNE Yellow Vertical Bar VNO VNE Blue Horizontal Bar VYSE Green Vertical Bar VS1 VNO Red Horizontal Bar VMCA White Vertical Bar VSO VFE Red Vertical Bar Low speed awareness bar NOTE VYSE and VMCA are only used in multi engine aircraft ...

Page 43: ...he full width of the airspeed tape at VNE Additionally a vertical red barber pole starting at VNE is displayed on the right side of the airspeed tape at and above VNE LOW SPEED AWARENESS BAR A red low speed awareness bar is always displayed along the lower right side of the airspeed tape extending up from the bottom of the tape The top of the low speed awareness thermometer bar is a representation...

Page 44: ...ix King KFD 840 Primary Flight Display Airspeed Area KFD 840 PG PN 7450 0840 01 4 6 Rev C May 28 2010 Honeywell International Inc Do not copy without express permission of Honeywell This Page Intentionally Left Blank ...

Page 45: ... express permission of Honeywell 5 ALTITUDE AREA ALTITUDE DISPLAY The altitude display shown below includes the following 1 Selected Altitude Bug 2 Altitude Trend Vector 3 Minimum Alert Altitude Bug 4 Minimum Alert Indicator MIN 5 MIN Digits 6 Baro Setting 7 Metric Altitude 8 Altitude window 9 Altitude Tape 10 Selected Altitude Digits Figure 5 1 Altitude Display ...

Page 46: ...tape are labeled in 500 foot increments A chevron is displayed at 500 foot and 1000 foot intervals to emphasize the incrementations The 1000 foot marks show double chevrons while the 500 foot marks show single chevrons ALTITUDE ROLLING DIGITS The altitude rolling digits are displayed in conjunction with the altitude tape to depict the current barometric altitude The actual altitude value is displa...

Page 47: ...he ground When metric altitude is displayed feet are still displayed on the altitude rolling digits The digits in the Metric window are displayed in white followed by a white M to indicate meters The metric altitude range is limited from 610 to 10 363 meters with a resolution of 5 meters ALTITUDE TREND VECTOR The altitude trend vector is a white bar starting at the altitude reference line on the l...

Page 48: ...r the entire altitude tape area Loss of air data will also cause the loss of TAS true airspeed standard rate of turn indicator and winds if installed ALTITUDE SELECT READOUT AND BUG Press the right knob three times to activate the Altitude bug ALT Turn the knob clockwise to increase the ALT bug setting and counterclockwise to decrease the value Pressing and holding the right knob for more than 2 s...

Page 49: ...on corresponds to the altitude select value in the readout When the selected altitude exceeds the displayed range the bug parks at the top or bottom of the display with half the bug visible to indicate the direction of the selected altitude The digital readout is displayed in either feet or metric units Metric units are displayed when metric altitude is ENABLED from the CONF page When altitude is ...

Page 50: ...to 30 98 inHg rounded to a resolution of 01 The range limit for hectopascals is 745 HPA to 1049 HPA rounded to a resolution of 1 When the BARO is highlighted pushing and holding the knob will cause the baro setting to go to the standard barometric correction STD 29 92 inHg or 1013 HPA IN or HPA is a pilot selectable on the CONF page MINIMUM ALTITUDE ALERT MIN BUG Minimum Altitude Alert MIN must be...

Page 51: ...ution of 10 feet The Minimum Alert Altitude display is removed when the value is less than 20 feet MIN is displayed on power up and returns to the value set when the unit power was removed MINIMUM ALTITUDE ALERT CONDITION ARMED When a minimum altitude is set and the barometric altitude is within 50 feet of the set minimum a yellow boxed window is displayed in the lower right corner of the ADI abov...

Page 52: ...white rectangular center point with two white hollow dots above and below and a pointer indicating current glide slope glide path deviation When vertical deviation is outside the limits of the scale the deviation pointer parks at the appropriate end of the scale with half the pointer out of view Vertical Deviation Invalid If vertical deviation data is invalid the pointer is removed and a red X is ...

Page 53: ...ional Inc Do not copy without express permission of Honeywell 6 VSI AREA VERTICAL SPEED VS DISPLAY The vertical speed display with the rate of altitude changes measured in feet per minute fpm is shown below The VS display includes the following Vertical speed scale and pointer Vertical speed digital readout Figure 6 1 VSI Display ...

Page 54: ... of 3000 fpm the pointer parks off the top or bottom of the scale Vertical Speed Digital Readout The vertical speed digital readout indicates the rate of climb or descent and is used in conjunction with the vertical speed scale and pointer The readout is displayed above the vertical speed scale when the rate of ascent is greater than or equal to 300 fpm and below the vertical speed scale when the ...

Page 55: ...0840 01 VSI Area Rev C May 28 2010 6 3 Honeywell International Inc Do not copy without express permission of Honeywell Vertical Speed Data Invalid If pressure altitude or vertical speed data is invalid the vertical speed scale markings and pointer are replaced with a red X ...

Page 56: ...ndix King KFD 840 Primary Flight Display VSI Area KFD 840 PG PN 7450 0840 01 6 4 Rev C May 28 2010 Honeywell International Inc Do not copy without express permission of Honeywell This Page Intentionally Left Blank ...

Page 57: ...CIATORS The HSI window is located in the lower portion of the PFD The following paragraphs describe the displays and annunciators located on the HSI Full Compass 360 HSI Partial Compass ARC HSI Heading Scale The full 360 HSI compass and partial arc ARC HSI compass consist of a 360 degree heading display that moves clockwise and counterclockwise for heading changes The full compass is shown below F...

Page 58: ... the aircraft symbol Aircraft heading is displayed at the white lubber line triangle at the top of the compass Cardinal headings are labeled N S E and W Intermediate headings at 30 60 120 150 210 240 300 and 330 degree increments are labeled with one or two digit degree markings for instance 060 degrees is 06 330 degrees is 33 The short scale tick markings are in 5 degree increments and the long o...

Page 59: ...ding select bug notched magenta rectangle moves around the compass when the HDG knob is rotated The selected heading readout is displayed below the selected heading annunciator in a three digit format in the upper left portion of the HSI The readout range is 001 to 360 Selecting HDG with the HDG knob will allow the selected heading to be set Pushing and holding the HDG knob will SYNC synchronize t...

Page 60: ...eading select bug goes beyond the range a magenta off scale arrow on the side of the compass arc that is nearer to the selected heading points toward the magenta bug Figure 7 4 Heading Select Bug Off Scale Heading Data Invalid If heading data is invalid cardinal and intermediate headings are removed the heading course selection distance readout and identifier are replaced with amber dashes a red H...

Page 61: ...hen a CDI source VOR or LOC is selected on the unit the course pointer is positioned by turning the CRS knob When a VOR source is received pushing and holding the left knob for more than 2 seconds SYNC button synchronizes the course pointer with the current course heading NOTE When changing course in OBS Mode or doing a Direct To in OBS mode on a KLN 900 or KLN 90 A B the course on the KFD 840 wil...

Page 62: ...t For deviation values outside the limits of the scale the deviation pointer parks at the end of the scale closer to the deviation value When lateral deviation is invalid the deviation needle is replaced with a red X Figure 7 5 Lateral Deviation Invalid Bearing Pointers Figure 7 6 Bearing Pointers Two green bearing pointers that point to the selected NAV source are displayed The source is either V...

Page 63: ...pointer source is selected with the O BRG and BRG soft keys on the unit The digital bearing to the station is displayed next to the selected source If the bearing data is invalid the readout displays amber dashes If the bearing data is invalid the bearing pointer is removed If the bearing source is GPS and magnetic variation data is invalid the bearing pointer is removed GPS Identifier and Distanc...

Page 64: ...ected using the CDI button with the following available sources on the HSI VLOC 1 VLOC 2 GPS 1 or GPS 2 The navigation source for the CDI is identified by an annunciator near the top right of the HSI above the selected course heading readout If the selected navigation source data is invalid the navigation source course information changes to amber dashes The full menu of navigation selections is d...

Page 65: ...onal Inc Do not copy without express permission of Honeywell To From Pointer The To From pointer is a colored triangle shown near the center of the full or partial arc compass The pointer indicates whether the aircraft is flying to or from the selected navigation source or GPS waypoint Figure 7 8 TO Pointer Figure 7 9 FROM Pointer ...

Page 66: ...ndix King KFD 840 Primary Flight Display HSI Area KFD 840 PG PN 7450 0840 01 7 10 Rev C May 28 2010 Honeywell International Inc Do not copy without express permission of Honeywell This Page Intentionally Left Blank ...

Page 67: ...HECKLIST AREA CHECK LIST FUNCTION The Checklist pages can be accessed using two of the function select buttons on the bottom of the unit Press the MENU function select button to display the CHK LST HSI menu Press the button again to highlight and select CHK LST The CHK LST menu of CHK ON CHK OFF will be displayed above the CHK LST button as shown in the figure below Figure 8 1 Checklist Menu CHK O...

Page 68: ...e CHK LST select button which is now labeled CHK LST to select either CHK ON CHK OFF If CHK ON is selected the Check Lists will be displayed on the upper right corner of the display to the right of the ADI as shown in the figure below Figure 8 2 Checklist Menu CHK ON Press the right knob four times until CHK LST is highlighted Turn the knob to move through the checklist pages as shown in the figur...

Page 69: ... and save them to the KFD 840 Each file contains multiple checklists as determined by the PC tool Selecting the READ button provides users with summary data including the number of checklists and a brief description of their use To read checklist files from the SD card use the following procedure NOTE The SD Card can be inserted and removed from the KFD 840 with power on or off the unit without da...

Page 70: ... bottom middle of the screen 5 Depress the left hand knob twice to get into the Checklist mode 6 Depress button 1 READ The files on the SD card will be displayed in the Checklist box Figure 8 4 Check Maintenance Mode 7 Rotate the right hand knob to SELECT the desired checklist and then press the OPEN button 8 Use the N LIST or P LIST Next or Previous button to review the pages in the file Make sur...

Page 71: ...ist Area Rev C May 28 2010 8 5 Honeywell International Inc Do not copy without express permission of Honeywell Figure 8 5 Checklist Pages on SD Card 9 If the checklist is ok depress the SAVE button This will save the selected Checklist to the KFD 840 Figure 8 6 Checklist Saved to KFD 840 ...

Page 72: ...ng website using the following URL http www bendixking com kfd840pcutility This utility allows the installer to download and enter the appropriate Checklist page for a particular aircraft onto an SD Card which can then be loaded into the KFD 840 using the instructions noted above Once the checklist pages have been loaded the installer is responsible for verifying the function of the checklist page...

Page 73: ...t must be a digital GPS If GPS1 is analog or is inoperable wind information will not be displayed Wind will not be available if the installed GPS does not provide track data Wind display will be removed if GPS TAS or OAT fails X Y Cartesian format consists of a lateral XW Crosswind digital wind speed and arrow and a longitudinal HW Headwind digital wind speed and arrow The HW head wind label does ...

Page 74: ...correct the indicated airspeed to calibrated airspeed using the aircraft AFM POH airspeed corrections if available then calculate the true airspeed Speeds between 30 and 999 kts mph are displayed in white with a trailing gray KTS or MPH label If TAS data is invalid the true airspeed digits are removed and the standard rate of turn indicator will be removed from the display Outside Air Temperature ...

Page 75: ...screen with a large red X or red failure message in the appropriate area of the screen ADC Failure Air Data Computer ATTITUDE FAILURE AHRS Failure Attitude Heading Reference System HDG FAIL CRM Failure Compass Remote Magnetometer Heading Failure Figure 10 1 Failure Modes ADC AIR DATA COMPUTER FAILURE The KFD 840 will display an ADC Air Data Computer failure by displaying red X s over the airspeed ...

Page 76: ...rt s Symptoms of a blockage of the Pitot Static system would manifest themselves in a manner similar to a traditional Pitot Static system ATTITUDE FAILURE AHRS FAILURE The ATTITUDE FAILURE message indicates that the AHRS Attitude and Heading Reference System has failed and the data can no longer be expected to be accurate The KFD 840 will display a black background with the ATTITUDE FAILURE messag...

Page 77: ...URE COMPASS REMOTE MAGNETOMETER A HDG FAIL message indicates that the CRM500 Compass Remote Magnetometer has either failed or lost communication with the KFD 840 Loss of communication or internal failure will remove all heading data from the display however it will not have any impact on the pitch or roll attitude display The pilot must fly using the standby instruments when the magnetometer has f...

Page 78: ...t and level flight until the alignment is completed or as long as possible without compromising the safety of the flight If an internal fault is detected Only on P N 8350 0840 06 or higher the unit may automatically attempt a reset The pilot must fly using the standby instruments following an in flight restart Figure 10 4 In Flight Reinitialation Once the unit has repowered in flight altitude and ...

Page 79: ... standby instruments will be required CONFIGURATION MODULE AND INTERNAL CHECKSUM FAILURE NO FLIGHT OBTAIN MAINTENANCE There is a problem in the system configuration that has been detected on power up The display will be locked and normal operation will not be possible If this message is displayed during ground operations flight is prohibited If this message is displayed in flight continued flight ...

Page 80: ...E FLIGHT OK PRESS MIDDLE BUTTON TO CONTINUE This message is to provide pilot awareness that there is a difference between the configuration module and the PFD data The display information stored in the PFD will be used Flight and continued flight is permitted It is recommended obtaining maintenance at the next available opportunity NO CONFIGURATION MODULE FLIGHT OK PRESS MIDDLE BUTTON TO CONTINUE ...

Page 81: ...re defined as follows TERMS DEFINITION ADI attitude direction indicator ADC air data computer AHRS attitude heading reference system ALT altitude BARO barometric BRG bearing CDI course deviation indicator CRM compass remote magnetometer CRS course FD flight director FPM feet per minute GP glide path GPS global positioning system GS ground speed GS glide slope HDG heading HSI horizontal situation i...

Page 82: ...l International Inc Do not copy without express permission of Honeywell TERMS DEFINITION LOC localizer m meters MIN minimum min minutes mph miles per hour NAV navigation NM nautical miles OAT outside air temperature PFD primary flight display TAS true Airspeed VOR VHF omnidirectional range VLOC VOR localizer XW crosswind ...

Page 83: ...ovided as a reference to the pilot for a record of the configuration of the KFD 840 as it is installed in the aircraft ITEM RESOL UTION INPUT VALUE RANGE UNITS CONFIGURATION Roll Adjust 0 1 0 180 0 DEG Pitch Adjust 0 1 0 90 0 DEG S R Pointer SKY ROLL VS0 1 0 0 240 276 Kts MPH VS1 1 0 0 240 276 Kts MPH VFE 1 0 0 240 276 Kts MPH VNO 1 0 0 240 276 Kts MPH VNE 1 0 0 240 276 Kts MPH VMCA 1 0 0 240 276 ...

Page 84: ... Do not copy without express permission of Honeywell ITEM RESOL UTION INPUT VALUE RANGE UNITS CONFIGURATION GPS1 Type NONE ARINC ANALOG GPS2 Type NONE ARINC ANALOG VOR1 Type NONE ARINC ANALOG SERIAL VOR2 Type NONE ARINC ANALOG SERIAL AP Type NONE ARINC ANALOG ALT BUG ON ON OFF MAX DIM BUS 0 14999 ACCEPT MIN DIM BUS ACCEPT BUS ENABLE ON OFF ...

Page 85: ...in 1 1 10 2560 FD Roll Gain 1 1 999 FD Pitch Filt 1 1 10 2560 FD Roll Filt 1 1 999 NOTE 1 Only on P N 8350 0840 06 or higher Each of the items noted above can be selected using the right control knob and adjusted to the parameters listed If the installer alters an item the category description is highlighted in yellow to indicate a change Once the appropriate settings have been entered the data ca...

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