TD 22

Question 1

Upon detection off 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

rotor within limits

trimming the rotor

MAX

30

45

MAX available 2.5 min OEI

12

200

cleared

65

OEI max continues power

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

Adjust to maintain rotor RPM

Increase if possible

Establish

Raise as necessary to stop descend and cushion landing

Identify

Perform

Adjust to OEI-limits or below

Trim to maximum

Gain 65 KIAS (Vy)

Reduce to max continuous power or below

Identify

Perform

PRACTICABLE

Question 3

Write the appropriate numbers next to A through D below:

Answer 3

A – 20°

B – 30 KIAS

C – 45 KIAS

D – 45 KIAS

Question 4

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

Answer 4

a. In a range of min 101% at high DA up to maximum of 103.5% at low air density during hover or low speed <55 KIAS.
b. In a range of min 96.5% at high DA up to 102% at low air density during forward flight (airspeed ≥55 KIAS)

Question 5

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

Answer 5

a. engine failure

b. torque split of more than 15%