TD 22

Question 1

Single Engine Failure - Flight

OEI Flight Condition -
Rotor Speed -
Affected Engine -
Single Engine Emerg. Shutdown -
Land as Soon As -

Answer 1

1. Establish
2. Trim to Maximum
3. Identify
4. Perform
5. Practicable

Question 2

HOGE Fly Away
Upon detection of an engine failure, the P* will adjust the ________ to maintain _____ within limits while simultaneously applying ______ cyclic and immediately ____ RPM to ____.

Answer 2

1. Collective
2. Rotor
3. Forward
4. Trim
5. Max

Question 3

HOGE Fly Away Part 2:

Reaching ____ KIAS adjust aircraft attitude to continue acceleration to ___ KIAS while maintaining ___________ power. At _____ ft AGL and clear of obstacles, adjust aircraft attitude to attain ____ KIAS and adjust collective to maintain ____ ____ ________ ____ or below.

Answer 3

1. 30
2. 45
3. Max available 2.5 min. Power
4. 200
5. 65
6. OEI Max. Continuous Power

Question 4

Single Engine Failure - Hover OGE
Procedure
1. Collective Lever -
2. Airspeed -

Forced Landing:
1. Landing Attitude -
2. Collective Lever -
- After Landing -
3. Affected Engine -
4. Single Engine Emerg. Shutdown -

Transition to OEI - Flight:
1. Collective Lever -
2. Rotor Speed -
3. Airspeed -
- After Reaching Safe Altitude -
4. Collective Lever -
5. Affected Engine -
6. Single Engine Emerg. Shutdown -
7. Land As Soon As -

Answer 4

1. Adjust to maintain RPM
2. Increase if possible

Forced Landing:
1. Establish
2. Raise as necessary to stop descent/cushion landing
- After Landing -
3. Identify
4. Perform

Transition to OEI - Flight:
1. Adjust to OEI limits or below
2. Trim to max
3. Gain to 65 knots
- After Reaching Safe Altitude -
4. Reduce to OEI MCP or below
5. Identify
6. Perform
7. Practicable

Question 5

Hover Performance/Height Loss after Engine Failure

1. Initial Attitude Nosedown:
2. At ___ KIAs Raise Nose near to level
3. Accelerate to Vtoss ___ KIAs
4. Climb to Vtoss ___ KIAs

Answer 5

1. 20°
2. 30
3. 45
4. 45

Question 6

In the NORM mode the VARTOMS will automatically control the rotor speed as follows:

Answer 6

a. Range of 101% at high air density to a max of 103.5% at low air density, during hover, and low airspeed (below 55 KIA)

b. Range of 96.5% at high air density up to a maximum of 102% at low air density during forward flight (airspeed 55 kts or higher).

Question 7

The VARTOMS will automatically switch to the MAN-mode and the VAR NR caution will come on in the event of:

Answer 7

a. Engine failure
b. Torque split of more than 15% occurs