HP d212 Bedienungsanleitung PDF herunterladen (Seite 77)

FMS-D212-725-1

Page 3-1

This document is private and confidential and is supplied on the express condition that it is not to be used for any

purpose or copied or communicated to any other person without written permission from Dart Aerospace Ltd.

Revision:

TC Approved Date: 08.12.17

Section 3

Emergency Procedures

Table of Contents

3.1

Introduction ...................................................................................... 3-3

3.2 Definitions ........................................................................................ 3-3

3.3 Engine .............................................................................................. 3-4

3.3.1 Engine Failure ............................................................................. 3-4

3.3.2 Engine Restart in Flight ............................................................... 3-5

3.3.3 Engine Driveshaft/Clutch Failure ................................................. 3-7

3.3.4 Engine Underspeed ..................................................................... 3-8

3.3.5 Engine Overspeed ....................................................................... 3-9

3.3.6 Engine Compressor Stall .......................................................... 3-10

3.3.7 Engine Hot Start/Shutdown ....................................................... 3-11

3.4 Fire ................................................................................................. 3-11

3.4.1 Engine Fire ................................................................................ 3-11

3.4.2 Cabin Smoke or Fumes............................................................. 3-13

3.4.3 Cargo Compartment Fire .......................................................... 3-14

3.5 Tail Rotor ....................................................................................... 3-14

3.5.1 Complete Loss of Tail Rotor Thrust .......................................... 3-14

3.5.2 Loss of Tail Rotor Components ................................................. 3-17

3.5.3 Tail Rotor Fixed Pitch Failures .................................................. 3-17

3.5.4 Fixed Pitch Failure at a Hover ................................................... 3-17

3.5.5 Fixed Pitch Failure in Flight ....................................................... 3-18

3.5.6 Loss of Pitch Change Control Linkage ...................................... 3-20

3.6 Hydraulic System ........................................................................... 3-20

3.7 Electrical System ........................................................................... 3-21

3.7.1 DC Power Failure ...................................................................... 3-21

3.8 Fuel System ................................................................................... 3-21

3.8.1 Fuel boost pump failure ............................................................. 3-21

3.8.2 Fuel Filter Partially Blocked ....................................................... 3-22

3.8.3 Fuel Quantity Indication Malfunctions ....................................... 3-22

3.9 Communications System ............................................................... 3-23

3.9.1 Intercom Failure ........................................................................ 3-23

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