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Flashcards in Chapter 9 Deck (11)
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1
Q

Establish Single Engine Airspeed

A

Cyclic - Adjust as required
Collective - adjust as required to maintain % RPM R within normal operating range
Establish Single Engine Airspeed

2
Q

EMER ENG SHUTDOWN

A

ENG POWER CONTROL lever(s) - OFF
ENG FUEL SYS selectors - OFF
FUEL BOOST PUMP CONTROL switches - OFF

3
Q

Lockout

A

ENG POWER CONT lever- Pull down and advance full forward while maintaining downward pressure, then adjust to set % RPM R as required.

4
Q

EMER APU START

A

FUEL PUMP switch - APU BOOST

APU CONTROL switch - ON

5
Q

SINGLE ENGINE FAILURE

A
  1. ESTABLISH SINGLE ENGINE AIRSPEED
  2. EXTERNAL CARGO/STORES - Jettison (if required)
    If continued flight is not possible:
  3. LAND AS SOON AS POSSIBLE
    If continued flight is possible:
  4. LAND AS SOON AS PRACTICABLE
6
Q

DUAL ENGINE FAILURE

A

AUTOROTATE

7
Q

ECU/DEC/EDECU LOW SIDE FAILURE

A
  1. ESTABLISH SINGE ENGINE AIRSPEED
    If partial powered flight cannot be maintained:
  2. ENG POWER CONT lever (low % TRQ/TGT TEMP engine) - LOCKOUT, Maintain % TRQ Apprx 10% below other engine
  3. LAND AS SOON AS PRACTICABLE
8
Q

ECU/DEC/EDECU HIGH SIDE FAILURE

A
  1. ESTABLISH SINGLE ENGINE AIRSPEED
    2 ENG POWER CONT lever (high % TRQ/TGT TEMP engine) - Retard. Maintain % TRQ apprx 10% below other engine
  2. LAND AS SOON AS PRACTICABLE

If the affected engine does not respond to engine power cont movement between fly and idle the HMU may be malfunctioning internally; should this occur:

  1. Perform EMER ENG SHUTDOWN (affected engine)
  2. Refer to single-engine failure emergency procedure
9
Q

% RPM Increasing/decreasing (Oscillation)

A
  1. ESTABLISH SINGLE ENGINE AIRSPEED
  2. Slowly restart the ENG POWER CONT lever on the suspected engine.
    If the oscillation stops and partial powered flight cannot be maintained:
  3. Place that engine in LOCKOUT and manually control the power.
  4. LAND AS SOON AS PRACTICABLE
    If the oscillation continues:
  5. Place the ENG POWER CONT lever back to fly and retard the ENG POWER CONT lever of the other engine.
    If partial power flight cannot be maitained: Place the engine in LOCKOUT, manually control the power.
  6. LAND AS SOON AS PRACTICABLE
10
Q

ENGINE COMPRESSOR STALL

A
  1. ESTABLISH SINGLE ENGINE AIRSPEED
    If condition persists:
  2. ENG POWER CONT lever (affected engine) - retard
  3. ENG POWER CONT lever (affected engine) - FLY
    If stall condition occurs:
  4. EMER ENG SHUTDOWN (affected engine)
  5. Refer to single engine failure emergency procedures
11
Q

1 OIL FLTR BYPASS OR #2 OIL FLTR BYPASS CAUTION APPEARS

A
  1. ESTABLISH SINGLE ENGINE AIRSPEED
  2. ENG POWER CONT lever - Retard ( to reduce pressure)
  3. LAND AS SOON AS PRACTICABLE