Eurocopter BK 117 C-2 User Manual

NAVIGATION MANAGEMENT SYSTEM - CMA–9000
FLIGHT MANUAL BK 117 C-2
9.2-51 – 1
EASA APPROVED
Rev. 0
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.
System/Equipment Designation
Effectivity
NMS (CMA-9000)
Software 169-614876-022 or subsequent
All
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 Approved by EASA:
EASA approval no.: R.C.03105
date – see entry above

Eurocopter BK 117 C-2 Specifications

General

Brand	Eurocopter
Model	BK 117 C-2
Category	Toy
Language	English

Summary

GENERAL

LIMITATIONS

Specifies operational constraints and restrictions for the NMS.

EMERGENCY AND MALFUNCTION PROCEDURES

CAUTION INDICATIONS

Guides on responding to system caution alerts and warnings.

SYSTEM ALERT MESSAGES

Explains system alert messages and required pilot actions.

FAILURE OF NMS SYNCHRONIZATION

Procedures for troubleshooting NMS synchronization issues.

NORMAL PROCEDURES

PREFLIGHT CHECK

Steps for confirming NMS readiness before flight.

FUNCTIONAL TEST

Procedures for testing specific NMS functions.

PRE-TAKEOFF CHECK

Final system checks before aircraft departure.

OPERATION

Entering user waypoints and user routes

Transdown to Hover - function

SAR pattern

APPROACH PROCEDURES

Approved GPS non-precision approach

Guidance for GPS-based non-precision approaches.

ENROUTE AND TERMINAL NAVIGATION

AFCS coupling in DME / DME or VOR / DME navigation

DME / DME navigation

VOR / DME navigation

Tactical DIRECT-TO navigation (VFR only)

TRANSDOWN TO HOVER FUNCTION

VERIFICATION OF SOFTWARE VERSION AND DATABASE VALIDITY