TD 15

Question 1

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

Answer 1

constant, 50, 40, 50, 300, touchdown speed, ETL, three ft.

Question 2

Main Transmission Oil Pressure

Minimum:
Caution Range:
Continuous Operation:
Maximum:

NOTE: XMSN OIL PRESS warning illumination is ____ in the range from ____ BAR during the pressure build up phase.

Answer 2

Minimum: 1.0 BAR
Caution Range: 1.0 BAR - 1.5 BAR
Continuous Operation: 1.5 BAR - 5.0 BAR
Maximum: 5.0 BAR

acceptable, 1.0 to 1.4

Question 3

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

Answer 3

1. Power - Reduce
2. LAND AS SOON AS PRACTICABLE
   If both indications are below 1.0 BAR:
3. LAND IMMEDIATELY

Question 4

Main Transmission Oil Temperature
Continuous Operation:
Maximum:

Answer 4

Continuous Operation: -10 degrees C

Maximum: 110 degrees C

Question 5

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 limits:
      2. Power - \_\_\_\_
If oil temperature and oil pressure indication remains above:
      3. LAND AS SOON AS \_\_\_\_

Answer 5

1. XMSN oil temperature and oil pressure indication - Check indications
   If indications are within limits:
   
   2. LAND AS SOON AS PRACTICABLE
      If indications are above limits:
   3. Power - Reduce, as much as possible
      If oil temperature and oil pressure indication remains above:
   4. LAND AS SOON AS POSSIBLE

Question 6

SINGLE ENGINE FAILURE - IGE HOVER

Procedure
1. Collective Lever - \_\_\_\_
2. Landing attitude - \_\_\_\_
3. Collective lever - \_\_\_\_
After Landing:
4. Affected Engine - \_\_\_\_
5. Single engine emergency shutdown - \_\_\_\_

Answer 6

1. Collective Lever - Adjust OEI limits or below
2. Landing attitude - Establish
3. Collective lever - Raise as necessary to stop descent and cushion landing
   After Landing:
4. Affected Engine - Identify
5. Single engine emergency shutdown - Perform

Question 7

SINGLE ENGINE FAILURE -

Procedure

1. OEI flight condition -____
2. Rotor Speed - ____
3. Affected engine- ____
4. Single engine emergency shutdown - ____
5. LAND AS SOON AS ____

Answer 7

1. OEI flight condition - Establish
2. Rotor Speed - Trim to maximum
3. Affected engine -Identify
4. Single engine emergency shutdown - Perform
5. LAND AS SOON AS PRACTICABLE

Question 8

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

Answer 8

72 hours.

Question 9

After consuming alcohol, aircrew members will not fly for a period of ____ and until ____

Answer 9

12 hours, no residual effects remain