TD 16

Question 1

SAS - Off Flight Caution: the 3-axis backup SAS must not be used as a ___ flight aid, except after ___ AP failure in order to ___ the flight.

Answer 1

Primary
Complete
Finish

Question 2

Constant angle or vertical takeoff can range from vertical to almost flat. It may demand that more power is available than the power required to ____. The angle is initiated from the point of hover or ground to a point in space clear of the ___. Vertical takeoffs are ____ over ____ takeoffs and will require ____ power.

Answer 2

Hover
Obstacles
Altitude
Airspeed
OGE

Question 3

Level acceleration is used when the power required to hover is the ____ power available. The first objective is to achieve ____ without allowing the aircraft to settle to the surface. As the aircraft enters ETL make a significant forward cycle input to prevent ____. Once through ETL, the aircraft will begin to climb at the ____ power setting.

Answer 3

Maximum
ETL
Blowback
Current

Question 4

State each step in the “Emergency Response Method”

Answer 4

F - Fly the aircraft
A - Alert the crew
D - Diagnose the emergency condition or system malfunction
E - Execute emergency procedure
C - Communicate
F - Fly the aircraft

Question 5

The procedure for mass moment exceedance of greater than 77% percent will cause a MM exceed caution and will remain on until ____ and the procedure is land as soon as _____.

Answer 5

Power off
Practicable

Question 6

Condition: POWER ON - POWER OFF
Min transient (max ___ S): ______ , _____
Min Cont
GM< 2000kg: ____,_____
GM>2000kg: ____,_____
Max Cont: ____,_____
Partial power(max ___ min): ____,_____
Max transient(max ___ s): ____,_____

Answer 6

20, 85%, -
96%, 80%
96%, 85%
104%, 104%
5, 106%, 106%
12, 106%, 110%

Question 7

Warning light indications - ROTOR RPM
Conditions/indications
NRO low
•NRO ___ % or less - ____
•Audio signal - ____

NRO high
•NRO ___ % or above - ____
•Audio signal at ___ % or above - ___

Procedure
NRO low/high
1. Rotor RPM indicator - Check
2. Collective lever - _____

Answer 7

NRO at 95% or less- Steady light
audio signal: Low pitch beeping tone

NRO 106% or above
Flashing light and warning gong
Audio signal at 110% or above
Flashing light and steady high-pitch tone

Procedure
Adjust as necessary to maintain NRO within normal range

Question 8

Autorotation
1. Collective lever - ___
2. Airspeed - ___
NOTE max range airspeed: ___ KIAS
min rate-of-descent airspeed: ___ KIAS
3. Double engine emergency shutdown- ____
At approximately___ FT AGL:
4. Flare attitude - Establish (approx. ___ to ___) to reduce forward airspeed and rate of descent, control NRO
At APPROXIMATELY ___ to __ FT AGL
5. Flare attitude - reduce to approx. ___
6. Heading - Maintain
7. Collective lever - ____
8. BAT MSTR sw - ___

Answer 8

Reduce to maintain Nro within limits
75 KIAS recommended
90 KIAS
60 KIAS
Perform
100 feet AGL
15° to 20°
8 to 12 feet AGL
7°
Raise to stop descent and cushion landing
OFF