Chinook CH-47/Emergency Procedures

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1 General

This section describes the most common helicopter emergencies that may be encountered in the Chinook, and the appropriate actions to address those emergencies.

2 Definitions

The following terms apply for this section:

  • The term LAND AS SOON AS POSSIBLE is defined as a landing to the nearest suitable landing surface. Survival of the occupants is considered the highst priority.
  • The term LAND AS SOON AS PRACTICABLE means land at the nearest suitable airfield or heliport.
  • The term AUTOROTATE means adjusting the controls to establish an autorotation and landing. This generally means thurst control full down, then adjust as necessary to maintain 100% rotor RPM.


3 Emergency Warning Signals

This helicopter is equipped with a troop alarm and jump light system. The following standard signals can be used to notify occupants:

  • Prepare for ditching or crash landing - 3 short rings
  • Water contact - Sustained ring

4 Emergency Checklists

4.1 Dual Engine Failure

Indications:

  • ENG 1 FAIL and ENG 2 FAIL caution lights
  • N1 and N2 underspeed
  • Engine flameout

Procedure:

  1. AUTOROTATE
  2. External cargo - Jettison

4.2 Engine Fire

4.3 Engine Chip Light(s)

4.4 Engine or Transmission Warnings

4.5 Fuel Level Warnings

4.6 FADEC Failures

4.7 Generator Failures

4.8 FC Hydraulic Failures

4.9 Utility Hydraulic Failures

4.10 Engine Restart During Flight