TD 15 Flashcards

1
Q

For Running Landing use a _______ approach to arrive at ___ feet AGL at ___ KIAS. Maintain the aircraft in trim above 50 feet AGL and align with the landing direction below _____ feet AGL. Do not exceed _____ FPM rate of descent at touchdown and adjust the cyclic to attain an aircraft attitude that maintains ETL to slightly above ___. For termination to a hover, terminate the maneuver to approximately a ____ hover.

A

shallow

50

40

50

300

ETL

3 ft

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2
Q

Main transmission oil pressure

Minimum: ___
Caution range: ___
Continuous operation: ___
Maximum: ___

NOTE: XMSN OIL PRESS warning light illumination is _________ in the range from ________ bar during the pressure build-up phase.

A
  1. 0 bar
  2. 0 – 1.5 bar
  3. 5 – 5.0 bar
  4. 0 bar

acceptable

1.0 – 1.4

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3
Q

WARNING LIGHT INDICATIONS, XMSN OIL PRESS

Procedure
If one XMSN oil pressure indication is below 1.0 bar:
1. Power – \_\_\_\_\_\_\_\_
2. LAND AS SOON AS \_\_\_\_\_\_\_\_
If both indications are below 1.0 bar:
3. LAND \_\_\_\_\_\_\_\_
NOTE Descend with minimum power
A

Reduce

PRACTICABLE

IMMEDIATELY

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4
Q

Main transmission oil temperature

Continuous operation: ______
Maximum: ______

A

-10° – 105° C

105° C

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5
Q

CAUTION INDICATIONS, XMSN OIL TEMP

Procedure
1. XMSN oil temperature and oil pressure indication – \_\_\_\_\_\_\_\_\_\_\_\_\_
If indications are within limits:
2. LAND AS SOON AS \_\_\_\_\_\_\_\_\_\_\_\_
If indications are above limit:
2. Power – \_\_\_\_\_\_\_\_\_\_\_\_
If oil temperature indication remains above limit:
3. LAND AS SOON AS \_\_\_\_\_\_\_\_\_\_\_\_\_
A

Check

PRACTICABLE

Reduce, as much as possible

POSSIBLE

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6
Q

Single engine failure, hover IGE

Procedure
1. Collective lever – \_\_\_\_\_\_\_\_\_\_
2. Landing attitude – \_\_\_\_\_\_\_\_\_\_
3. Collective lever – \_\_\_\_\_\_\_\_\_\_
After landing:
4. Affected engine – \_\_\_\_\_\_\_\_\_\_
5. Single engine emergency shutdown – \_\_\_\_\_\_\_\_\_\_
A

Adjust to OEI limits or below

Establish

Raise as necessary to stop descent and cushion landing

Identify

Perform

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7
Q

Single engine failure, in flight

Procedure

  1. OEI flight condition – _________
  2. Rotor speed – ________
  3. Affected engine – ________
  4. Single engine emergency shutdown – _________
  5. LAND AS SOON AS _________
A

Establish

Trim to maximum

Identify

Perform

PRACTICABLE

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8
Q

After donating blood (200 cc or more) aircrew members will be restricted from flying duties for _________.

A

72 hours

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9
Q

After consuming alcohol, aircrew members will not fly for a period of _________ and until ________________.

A

12 hours

no residual effects

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