TD 22 Daily questions Flashcards

1
Q

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 obstacles are cleared, adjust attitude to attain _____ KIAS and adjust collective to maintain _____ or below

A
collective
rotor limits
trim
max
30
45
2.5min OEI
12
200
cleared
65
OEI max continuous power
How well did you know this?
1
Not at all
2
3
4
5
Perfectly
2
Q
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

  1. Collective lever- _____
  2. rotor speed- _____
  3. airspeed- gain, 65 Kias- _____

After reaching safe altitude:

  1. Collective lever- _____
  2. Affected engine- _____
  3. Single engine emergency shutdown- _____
  4. Land as soon as _____
A
adjust to maintain rotor RPM
increase if possible
establish
raise as needed to stop descent and cushion landing
identify
perform
adjust to OEI Limits of below
trim to maximum
gain, 65 KIAS
reduce to OEI MCP or below
identify
perform
practicable
How well did you know this?
1
Not at all
2
3
4
5
Perfectly
3
Q
AEO hover ---> after single engine failure:
initial attitude nose down: \_\_\_\_\_
at \_\_\_\_\_ KIAS- raise nose to near level
accelerate to Vtoss: \_\_\_\_\_ KIAS
Climb with Vtoss= \_\_\_\_\_ KIAS
A

20-25 degrees
30kts
45
45

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
4
Q

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

A

a. in a range of min 101% at high air density up to max of 103.5% in low air density during hover/low airspeed 55kts
b. range of min 96% at high air density up to max of 102% in low air density during forward flight more than 55kts

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
5
Q

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

A

engine failure

torque split of more than 15%

How well did you know this?
1
Not at all
2
3
4
5
Perfectly