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Eurocopter BK 117 C-2 Supplement Manual

Navigation management system - cma–9000
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NAVIGATION MANAGEMENT SYSTEM - CMA–9000
This supplement shall be attached to the BK117 C-2 flight manual (subsection 9.2) when the
NAVIGATION MANAGEMENT SYSTEM - NMS - (CMA-9000) has been installed.
System/Equipment Designation
NMS (CMA-9000)
Software 169-614876-022 or subsequent
NOTE
Additional operating instructions and other information can be obtained from the
CANADIAN MARCONI NMS (CMA 9000) operational manual.
NOTE
For approving authorities and respective dates of approval refer to the log of supplements.
Date: DEC 10, 2008
EASA APPROVED
date – see entry above
Rev. 0
NAVIGATION MANAGEMENT SYSTEM - CMA–9000
F M S 9.2-51
SUPPLEMENT FOR
EASA approval no.: R.C.03105
FLIGHT MANUAL BK 117 C-2
Effectivity
All
Approved by EASA:
9.2-51 – 1

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Summary of Contents for Eurocopter BK 117 C-2

  • Page 1 FLIGHT MANUAL BK 117 C-2 NAVIGATION MANAGEMENT SYSTEM - CMA–9000 F M S 9.2-51 SUPPLEMENT FOR NAVIGATION MANAGEMENT SYSTEM - CMA–9000 This supplement shall be attached to the BK117 C-2 flight manual (subsection 9.2) when the NAVIGATION MANAGEMENT SYSTEM - NMS - (CMA-9000) has been installed.

  • Page 2: List Of Effective Pages

    FLIGHT MANUAL BK 117 C-2 NAVIGATION MANAGEMENT SYSTEM - CMA–9000 LIST OF EFFECTIVE PAGES NOTE N, R, or D indicate pages which are new, revised or deleted respectively. Remove and dis- pose of superseded pages, insert the latest revision pages and complete the record of sup- plement-revisions as necessary.

  • Page 3: List Of Abbreviations

    FLIGHT MANUAL BK 117 C-2 NAVIGATION MANAGEMENT SYSTEM - CMA–9000 GENERAL The information contained herein supplements the information of the basic flight manual; for limitations, procedures, and performance data not contained in this supplement, refer to the basic flight manual.

  • Page 4: Configuration Requirements

    FLIGHT MANUAL BK 117 C-2 NAVIGATION MANAGEMENT SYSTEM - CMA–9000 LADDER– , SQUARE– and SECTOR SEARCH PATTERN are supported. For tactical approaches (non–published ones) it is the crew’s responsibility to ensure that the appropriate transition level for the tactical approach destination was correctly entered.
  • Page 5 FLIGHT MANUAL BK 117 C-2 NAVIGATION MANAGEMENT SYSTEM - CMA–9000 EMERGENCY AND MALFUNCTION PROCEDURES CAUTION INDICATIONS CAUTION INDICATIONS (on NMS and ND (only if NMS is selected NAV source)) Conditions/Indications Failure or malfunction of a connected system or caution message from NMS.
  • Page 6 FLIGHT MANUAL BK 117 C-2 NAVIGATION MANAGEMENT SYSTEM - CMA–9000 CAUTION INDICATIONS FAIL NMS 2 NMS 2 and/or NMS 2 (on NMS 2) (on CAD) (pushbutton amber) Conditions/Indications – NMS 2 has failed or is switched off In case of complete NMS 2 failure the NMS 2 shows random operation or the display and keyboard is frozen.
  • Page 7 FLIGHT MANUAL BK 117 C-2 NAVIGATION MANAGEMENT SYSTEM - CMA–9000 CAUTION INDICATIONS NMS 1 NMS 2 and/or and/or (on NMS) (on CAD) Conditions/Indications GPS integrity is invalid. GPS NAV LOST or GPS POS UNCERTAIN come on as system alert message.
  • Page 8 FLIGHT MANUAL BK 117 C-2 NAVIGATION MANAGEMENT SYSTEM - CMA–9000 A white number indication annunciates a single side failure, whereas no number NOTE indication annunciates a dual side failure. MESSAGE DESCRIPTION PILOTS ACTION / REMARKS ADC1 FAILED ADC input failure Manual sequencing of altitude terminated legs.
  • Page 9 FLIGHT MANUAL BK 117 C-2 NAVIGATION MANAGEMENT SYSTEM - CMA–9000 MESSAGE DESCRIPTION PILOTS ACTION / REMARKS FMS CLOCK Real time clock failure detected. Switch off concerned NMS. FAILED NOTE: Normal during system start. FMS NAV IN DR NMS in dead reckoning navigation Use other means of navigation.
  • Page 10 FLIGHT MANUAL BK 117 C-2 NAVIGATION MANAGEMENT SYSTEM - CMA–9000 MESSAGE DESCRIPTION PILOTS ACTION / REMARKS SCANNING Failure of DME transceiver detected. No action required. DME1 (or 2) DMD/DME nav mode no longer avail- FAILED able. TAS FAILED Loss of true airspeed input.

  • Page 11: Normal Procedures

    FLIGHT MANUAL BK 117 C-2 NAVIGATION MANAGEMENT SYSTEM - CMA–9000 NORMAL PROCEDURES NOTE For further information observe the Operator‘s Manual. PREFLIGHT CHECK (applies equally to both systems) 4.1.1 Pre–start check When power is initially applied to the NMS (AVIO MSTR switches - ON) an internal test starts: Caution indicators/annunciators –...

  • Page 12: Functional Test

    FLIGHT MANUAL BK 117 C-2 NAVIGATION MANAGEMENT SYSTEM - CMA–9000 FUNCTIONAL TEST ( RADIO SELFTEST USING “TEST ALL” FUNCTION (ONLY AVAILABLE ON GROUND)) 1. RADIO pb – Press 2. NEXT pb – Press twice, to access RADIO SELFTEST page 3/3 3.

  • Page 13: Operation

    FLIGHT MANUAL BK 117 C-2 NAVIGATION MANAGEMENT SYSTEM - CMA–9000 OPERATION 4.4.1 Entering user waypoints and user routes CAUTION THE USER ROUTES DATABASE WILL NOT AUTOMATICALLY BE UPDATED AF- TER MODIFICATION OF USER WAYPOINTS. Before activation of an approach check correct data entry including alternate route (RTE 2).
  • Page 14 FLIGHT MANUAL BK 117 C-2 NAVIGATION MANAGEMENT SYSTEM - CMA–9000 pushbutton STD on the ICP1 is linked to the CMA9000. Assure the QNH setting on pi- lot’s side and co–pilot’s side are identical. If the QNH is required from ADC1, a manual selection can be made by means of the reconfiguration unit: select ADC1.
  • Page 15 FLIGHT MANUAL BK 117 C-2 NAVIGATION MANAGEMENT SYSTEM - CMA–9000 4.4.7 SAR pattern The NMS performs all SAR patterns using fly–by waypoint sequencing. Before reaching the next SAR WPT the NMS performs turn anticipation depending on the SAR speed. In order to prevent areas missed during turn anticipation the SAR area shall be defined ac- cordingly larger.
  • Page 16 FLIGHT MANUAL BK 117 C-2 NAVIGATION MANAGEMENT SYSTEM - CMA–9000 Alignment phase Fig. 1 Example: LADDER –Search 4.4.8 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)”.
  • Page 17 FLIGHT MANUAL BK 117 C-2 NAVIGATION MANAGEMENT SYSTEM - CMA–9000 4.4.9 VOR – Autotuning After NMS start up VOR tuning starts as default in MANUAL tuning mode. VOR–autotun- ing feature must be manually activated. Assure the NMS scratchpad is empty. If not, use the CLR key as often as necessary to delete all characters in the scratchpad.

  • Page 18: Approach Procedures

    FLIGHT MANUAL BK 117 C-2 NAVIGATION MANAGEMENT SYSTEM - CMA–9000 APPROACH PROCEDURES Before activation of an approach, check correct data entry including alternate route (RTE 2). 4.5.1 Approved GPS non–precision approach CAUTION THE NMS ALSO ALLOWS NON – APPROVED GPS OVERLAY APPROACHES TO BE SELECTED.
  • Page 19 FLIGHT MANUAL BK 117 C-2 NAVIGATION MANAGEMENT SYSTEM - CMA–9000 1. RTE or LEGS page – Select MISSED APPR (LSK6R); AFCS upper modes remain en- gaged – Automatic sequencing on NMS starts for the missed approach CAUTION WHEN PRESSING GA TO ENGAGE THE MISSED APPROACH, THE AUTOPILOT NAVMODE WILL BE DISENGAGED.
  • Page 20 FLIGHT MANUAL BK 117 C-2 NAVIGATION MANAGEMENT SYSTEM - CMA–9000 ENROUTE AND TERMINAL NAVIGATION 4.6.1 AFCS coupling in DME / DME or VOR / DME navigation NOTE If active navigation sensor has lost its integrity or failed to operate (e.g. GPS) the FMS reverts to next best available sensor navigator (e.g.

  • Page 21: Performance Data

    FLIGHT MANUAL BK 117 C-2 NAVIGATION MANAGEMENT SYSTEM - CMA–9000 4.6.5 KALMAN navigation For detailed information refer to the “OPS Manual CMA-9000 (Software 169-614876-022)”. KALMAN navigation is active for maximum 2 min 50 sec before it reverts to DR naviga- tion.

  • Page 22: Mass And Balance

    FLIGHT MANUAL BK 117 C-2 NAVIGATION MANAGEMENT SYSTEM - CMA–9000 MASS AND BALANCE Refer to equipment list entries in section 6 of the basic flight manual. SYSTEM DESCRIPTION The NMS (CMA-9000) is a self contained, cockpit mounted, radio and flight management system.
  • Page 23 FLIGHT MANUAL BK 117 C-2 NAVIGATION MANAGEMENT SYSTEM - CMA–9000 Caution indicators Annunciators Screen FAIL OFST Auto-brightness control sensor Line–select Line–select keys keys Scratchpad EXEC annunciator Function key INIT LEGS PROG (disabled) Function keys RADIO ANS HOLD FIX Alphanumeric keyboard...
  • Page 24 FLIGHT MANUAL BK 117 C-2 NAVIGATION MANAGEMENT SYSTEM - CMA–9000 NMS (CMA-9000) Functional Description FAIL Illuminates when a NMS failure condition exists. Caution Illuminates when position does not meet accuracy requirement for current phase of flight. Illuminates when new caution or warning messages are availa- ble.
  • Page 25 FLIGHT MANUAL BK 117 C-2 NAVIGATION MANAGEMENT SYSTEM - CMA–9000 MENU Not operational in this configuration. PREV Proceed to previous screen page. NEXT Proceed to next screen page. Provides access to pre-flight initialization pages and various ref- erence data pages, and enables access to all FMS functions not...
  • Page 26 FLIGHT MANUAL BK 117 C-2 NAVIGATION MANAGEMENT SYSTEM - CMA–9000 ADDITIONAL ANNUNCIATORS AND PUSH-BUTTONS (optional / example) – Instrument Panel (version in combination with other optionals): Fig. 3 Additional annunciators and pb’s on I–panel (typical installation) MANUFACTURER’S DATA EASA APPROVED 9.2-51 –...
  • Page 27 FLIGHT MANUAL BK 117 C-2 NAVIGATION MANAGEMENT SYSTEM - CMA–9000 TRANSDOWN TO HOVER FUNCTION EXAMPLE The hover procedure trajectory displayed on the FCDS is the protected area envelope of the procedure, but the guidance will not follow it. The area envelope of protection shows the limit that shall not be exceeded by the guid- ance and it is computed based on the maximum ground speed during the turn.
  • Page 28 FLIGHT MANUAL BK 117 C-2 NAVIGATION MANAGEMENT SYSTEM - CMA–9000 VERIFICATION OF SOFTWARE VERSION AND DATABASE VALIDITY To verify the software version installed and to check the validity of the database: 1. INIT/REF key – Press 2. IDENT (LSK1L) – Press MANUFACTURER’S DATA...

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