TD 23

Question 1

Perform Manual Throttle Operation - Emergency Mode

First standard: Perform ________
Max FLI deviation is _______
WARNING: It is critical to ensure that when the number ___ throttle is placed into the emergency area, that the _______ does not fall into position ___________. After landing, the ____ will rotate the _________ (affected engine) to ______ prior to reducing the collective lever to the full down position.

Answer 1

A. Task 1070
B. +1/-2 FLI
C. 2, Limiting Stop, Inadvertently
D. P*, Twist Grip, Idle.

Question 2

Engine Overspeed - Governor Failure

1. Collective Lever -
2. VAR NR system NORM/MAN sw -
3. N2 Trim sw -
   - If step 3 is not possible:
4. Affected engine -
5. Twist grip (affected engine) -
6. Land as soon as -

Answer 2

1. Raise as necessary to maintain N2/NRO within limits.
2. Check Man
3. Try to trim Nr to 101% with matched TRQ
4. Identify
5. Rotate toward idle until N2 and Nr stabilize in normal range, FLI needles match.
6. Practicable

Question 3

Engine Underspeed - Governor Failure

1. OEI Flight Condition -
2. Bleed air consumers -
3. VAR NR system NORM/MAN pb -
4. Affected Engine -
5. N2 Trim sw -
   - If TRQ match not possible -
6. Twist grip (affected engine) -
7. Land as soon as -
   - if no residual TRQ available -
8. Single engine Emerg. Shut down -

Answer 3

1. Establish
2. Off
3. Check MAN
4. Identify
5. Compensate N2 Nro drop/try to match TRQ
6. Release stop plate, rotate towards flight until N2/Nro stabilize in normal range/FLI needles match.
7. PRACTICBLE
8. Perform

Question 4

During a fixed pedal setting approach adjust airspeed to ___ knots or above until final. Once established on final, decelerate to ___ KIAS ___/-___ while maintaining less than ____ FPM rate of descent. If the nose is _____ of ground track and _____ the approach, if the nose is ____ then _____ approach. Arrive over the ________ of the landing area approximately ____ AGL ________. If the nose is to the left maintain altitude with the collective while _________ forward speed until the aircraft is ________ with the landing area. If the nose yaws to the _______ past the centerline apply ___________. Collective application will accelerate the right yaw. When the aircraft is aligned with the intended landing direction and a _________ can be accomplished, the IP will announce the _____________.

Answer 4

1. 70
2. 40
3. 10
4. -5
5. 300
6. Right
7. Above
8. Left
9. Continue
10. First 1/3
11. 5 ft
12. At or above ETL
13. Decreasing
14. Aligned
15. Right
16. Forward cyclic
17. Successful landing
18. Maneuver is complete

Question 5

Note: __________ component is advantageous during approach and landing. P* should consider selecting an area where a shallow approach can be accomplished with a _________.

Answer 5

1. Left crosswind
2. Left crosswind.

Question 6

Tail Rotor Drive Failure/Fixed-Pitch Tail Rotor Control Failure - Forward Flight

1. Collective lever -
2. Airspeed -
3. Suitable landing area - Select
4. Shallow approach with nose left -
   - If airspeed reduced by 40 kts w/nose still pointing to left:
5. Airspeed -
6. Landing -

Answer 6

1. Reduce to obtain minimum sideslip angle
2. Maintain 70 kts
3. Select
4. Perform
5. Reduce close to ground until nose is aligned w/direction of flight
6. Perform

Question 7

If the nose direction changes from left to right at airspeeds higher than 40 kts:
1. Airspeed -
2. Approach -
3. Autorotation -
4. As it pertains to performing the above T/R Drive Failure procedure:
a. The procedure will vary depending on flight conditions, ________ and _____ of the helicopter.
b. Landing surface should be ____ (concrete, asphalt) and _____.
c. ________ crosswind is advantageous.
d. _________ is advantageous.
e. In final phase of flare the helicopter can yaw to the _____ due to friction effects.
f. Before touchdown the ground speed should be reduced to a _______.

Answer 7

1. Increase
2. Abort, climb to satisfactory height for autorotation.
3. Perform
4. a. Power setting/mass
   b. Hard and flat
   c. Left
   d. Headwind
   e. Left
   f. Minimum