TD 22

Question 1

[HOGE Fly Away] Upon detection of an engine failure while at an OGE hover, the P* will adjust the _____ to maintain ____ and immediately ____ RPM to - ____ and simultaneously apply forward cyclic to achieve ____ KIAS, then adjust aircraft attitude to continue acceleration to ____ KIAS while maintaining ____ power (___ FLI without the training collar installed). At ___ feet AGL and/or when the obstacles are ____, adjust aircraft attitude to attain ___ KIAS and adjust collective to maintain _____ or below.

Answer 1

collective as required, rotor within limits, trim the rotor, max, 30, 45, OEI 2.5 min, 12, 200, cleared, 65, OEI MCP

Question 2

Single engine failure - hover OGE
Procedure
1. Collective lever –
2. Airspeed –

FORCED LANDING

3. Landing attitude –
4. Collective lever –

After landing:

5. Affected engine –
6. Single engine emergency shutdown –

TRANSITION TO OEI - FLIGHT

3. Collective lever –
4. Rotor speed –
5. Airspeed –

After reaching safe altitude:

6. Collective lever –
7. Affected engine –
8. Single engine emergency shutdown –
9. LAND AS SOON AS

Answer 2

Single engine failure - hover OGE
Procedure
1. Collective lever – Adjust to maintain rotor RPM
2. Airspeed – Increase if possible

FORCED LANDING
3. Landing attitude – Establish
4. Collective lever – Raise as necessary to stop
descent and cushion landing
After landing:
5. Affected engine – Identify
6. Single engine emergency shutdown – Perform

TRANSITION TO OEI - FLIGHT

3. Collective lever – Adjust to OEI-limits or below
4. Rotor speed – Trim to maximum
5. Airspeed – Gain, 65 KIAS (VY)

After reaching safe altitude:

6. Collective lever – Reduce to OEI MCP or below
7. Affected engine – Identify
8. Single engine emergency shutdown – Perform
9. LAND AS SOON AS PRACTICABLE

Question 3

HOVER PERFORMANCE/HEIGHT LOSS AFTER ENGINE FAILURE

                                  2.5 MIN POWER RATING After single engine failure:

INITIAL ATTITUDE NOSE DOWN __ degrees
AT __ KIAS-RAISE NOSE NEAR TO LEVEL
ACCELERATE TO vTOSS= __ KIAS
CLIMB WITH vTOSS= __ KIAS

Answer 3

20
30
45
45

Question 4

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

Answer 4

If the VARTOMS is not operated in the MAN-mode and

a. engine failure
b. a torque split of 15%