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NAVIGATION MANAGEMENT SYSTEM - CMA–9000

FLIGHT MANUAL BK 117 C-2

9.2-51 – 23

EASA APPROVED
Rev. 1

PROG

REF

OFST

FAIL

SMS

MSG

POS

NPA

GSM

B C D E

K L M

P Q R S

V W X Y

CLR

INIT

ARR

DEP

RTE

LEGS

RADIO ANS

HOLD FIX

BRT

EC135_FLH_01

15_R

Annunciators

Auto-brightness

control sensor

Line–select

keys

Scratchpad

Alphanumeric

keyboard

Function

keys

Space key

Clear/Delete key

EXEC

annunciator

Screen

SQK

Caution indicators

3L
4L

5L
6L

3R
4R

5R
6R

Plus–minus key

Slash key

Decimal key

Line–select

keys

Function key

(disabled)

Alternative Key Funktions:

ANS

SQK

changes to

FUEL

MARK

Fig. 2 NMS front panel display (typical)

MANUFACTURER’S DATA

Summary of Contents for BK 117 C-2

Page 1: ...MANAGEMENT SYSTEM NMS CMA 9000 has been installed System Equipment Designation Effectivity NMS CMA 9000 Software 169 614876 022 or subsequent All NOTE Additional operating instructions and other infor...

Page 2: ...9 2 51 8 0 R 9 2 51 15 1 R 9 2 51 2 1 9 2 51 9 0 R 9 2 51 16 1 R 9 2 51 3 1 9 2 51 10 0 R 9 2 51 17 1 R 9 2 51 4 1 9 2 51 11 0 R 9 2 51 18 1 9 2 51 5 0 9 2 51 12 0 R 9 2 51 19 1 9 2 51 6 0 R 9 2 51 13...

Page 3: ...ach RAIM Receiver Autonomeous Integrity Monitoring RNP Required Navigation Performance RMS Radio Management System SSR Secondary Surveillance Radar TAD Turn Anticipation Distance TAS True Airspeed TDN...

Page 4: ...n was correctly entered The following NMS functions are limited to VFR operations only Moving Waypoint DMAP waypoint to NMS Mark on Top Transdown to Hover SAR Patterns 2 2 CONFIGURATION REQUIREMENTS F...

Page 5: ...l pb e g PROG Press to acknowledge and exit recall page MSG caution indica tion disappears 4 ON OFF sw and or circuit breaker of indi cated system Check 5 Continue flight CAUTION INDICATIONS FAIL NMS...

Page 6: ...NS FAIL and or on NMS 1 and NMS 2 on CAD NMS 1 and NMS 2 and and NMS 1 NMS 1 NMS 2 NMS 2 pushbutton amber Conditions Indications Both NMS or connected systems have failed In case of complete NMS failu...

Page 7: ...are displayed on the MSG RECALL pages A list of system failures provided on the MAINT MSG subpage of the MSG RECALL page The following table contains an extract of the alert messages that require pilo...

Page 8: ...ypoint in the flight path prior to a route discontinuity NMS steering becomes invalid Enter next waypoint or close up route disconti nuity and engage AFCS when intended COURSE CHANGE 125 AHEAD At the...

Page 9: ...he combination of TAS and com puted wind may cause the ICAO hold ing pattern protected airspace to be exceeded Reduce speed prior to reaching the holding fix MANUAL DME 1 or 2 FAILED Loss of distance...

Page 10: ...ical databases NAV database CUSTOM da tabase and USER database are used The USER database includes user waypoints user routes and map waypoints To compare user waypoint databases press on each NMS the...

Page 11: ...eception on third channel of DME No action is required Message will disappear in flight at a certain altitude D Make sure that both NMS are synchronized D Make sure that the activated flight plans in...

Page 12: ...th the name of the radio Check the radio then continue with step 3 5 LSK6R pb on both NMS Press check READY appears indicates that the radio tests are switched off NOTE D During the test the tuning of...

Page 13: ...y This massage may occur after activation of flight plan and is triggered regardless if VFR or IFR flight plan is activated For detailed information concerning the advisory messages see OPS Manual CMA...

Page 14: ...d value of 70 kts is configured which shall be re spected by the flight crew to provide proper guidance information towards the TDN way point If higher speeds are flown the turn area will be presented...

Page 15: ...overshoot of the first SAR pattern waypoints In order to correctly activate the desired SAR pattern SQUARE SECTOR or LADDER the prompted ACTIVATE must be pressed LSK6R prior to execute the flight pla...

Page 16: ...Moving waypoint Only one moving waypoint can be activated in the flight plan For detailed information refer to the OPS Manual CMA 9000 Software 169 614876 022 The moving waypoint will be automatically...

Page 17: ...once To manually activate VOR autotuning mode perform the following RADIO key as often as to access RADIO page 1 4 page Press CLR key Press LSK adjacent to NAV radio to be set into VOR autotuning mode...

Page 18: ...selects the DEP ARR INDEX page 2 DEP ARR INDEX page Select desired ARR 3 ARRIVALS PAGE Select APPROACH and TRANS 4 LEGS key Check selected approach poce dure with published procedures 5 EXEC key Press...

Page 19: ...e missed approach CAUTION WHEN PRESSING GA TO ENGAGE THE MISSED APPROACH THE AUTOPILOT NAVMODE WILL BE DISENGAGED Continue with Missed Approach procedure NOTE D To initiate a missed approach before th...

Page 20: ...ailed information refer to the OPS Manual CMA 9000 Software 169 614876 022 4 6 4 Tactical DIRECT TO navigation VFR only For detailed information refer to the OPS Manual CMA 9000 Software 169 614876 02...

Page 21: ...S Manual CMA 9000 Software 169 614876 022 4 6 7 DME HOLD RADIO page 1 4 Select RADIO DETAILS LSK 6R Press NAV 1 or NAV 2 Select DME HOLD LSK 4L or LSK 4R Press to toggle DME HOLD The held DME frequenc...

Page 22: ...igation guidance information are generated in both geograph ic and track related reference frames for display to the pilot It also provides LNAVsteering suitably formatted for use by an Automatic Flig...

Page 23: ...FIX BRT EC135_FLH_0115_R Annunciators Auto brightness control sensor Line select keys Scratchpad Alphanumeric keyboard Function keys Space key Clear Delete key EXEC annunciator Screen ID SQK Caution i...

Page 24: ...for incoming voice call on mobile phone SMS Illuminates when Short Message Service text message has been received MENU Currently not used EXEC Illuminates when the EXEC key is active Auto brightness c...

Page 25: ...active route Function keys EXEC Cause execution of modified data after verification thus com pleting data entry procedures Only active when MOD status is shown in reverse video on title line of displa...

Page 26: ...CMA 9000 9 2 51 26 EASA APPROVED Rev 1 7 1 ADDITIONAL ANNUNCIATORS AND PUSH BUTTONS optional example Instrument Panel version in combination with other optionals Fig 3 Additional annunciators and pb...

Page 27: ...shall not be exceeded by the guid ance and it is computed based on the maximum ground speed during the turn The display is re computed every 10 seconds until the helicopter reaches the arc start ing p...

Page 28: ...YSTEM CMA 9000 9 2 51 28 EASA APPROVED Rev 0 7 3 VERIFICATION OF SOFTWARE VERSION AND DATABASE VALIDITY To verify the software version installed and to check the validity of the database 1 INIT REF ke...

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