Transition and Emergency Procedures Maneuvers

Question 1

T/F:

A dual engine forced landing is an approved emergency procedure maneuver to practice in the aircraft?

Answer 1

False

Question 2

In addition to TO 1H-1(U)N-1 restrictions, a list of prohibited emergency procedure maneuvers can be found in the __________.

Answer 2

AFMAN 11-2UH-1N Vol 3

Question 3

Normal Takeoff

1. Select a reference point to maintain a constant ground track. Use __________________.
2. Can be flown from the ground or a hover, smoothly increase power to desired setting while accelerating forward. After passing ___________, adjust the attitude to climb targeting ___________________.
3. The Pilot flying will terminate the maneuver when reaching minimum safe single engine airspeed (or _______ if safe single engine airspeed is not available or as directed by AC).

Answer 3

1. 5-foot hover power plus 10 percent
2. effective translation lift (ETL) ; 70 KIAS by 50 feet at 500 fpm.
3. 70 KIAS

Question 4

Maximum Performance Takeoff

1. Used when an obstacle restricts use of a normal takeoff; requiring a near vertical takeoff to avoid an obstacle.
2. Simulate maximum power available as ___________________, and simulate a _____________.
3. Per TO 1H-1(U)N-1, Flight Manual, this maneuver is flow from the ground.
4. When sufficient altitude to clear the simulated obstacle is reached, smoothly accelerate without descending, then adjust the power and attitude for a normal climb.
5. The pilot flying will terminate the maneuver when clear of the simulated obstacle and above the minimum safe single engine airspeed (or ________ if safe single engine airspeed is not available or as directed by the AC).
6. An abort point should be carefully considered for every max performance takeoff.

Answer 4

2. 5-foot hover power plus 10 to 15 percent ; 100-foot obstacle.
3. 70 KIAS

Question 5

Marginal Power Takeoff

1. A marginal power takeoff is used when maximum power available/power margin is limited due to environmental factors, gross weight, or other external factors.
2. Simulate maximum power available as _________________________. Consider an abort point.
3. When sufficient altitude to clear simulated obstacle is reached, smoothly accelerate without descending, then adjust the power and attitude for a normal climb.
4. The pilot flying will terminate the maneuver when clear of the simulated obstacle and above minimum safe single engine airspeed (or ______ if safe single engine airspeed is not available or as directed by the AC).

Answer 5

2. 5-foot hover power, and simulate a 50-foot obstacle

4. 70 KIAS

Question 6

Slide Takeoff

1. The pilot flying will initiate from the ground using approximate __________________________.
2. The pilot flying will terminate the maneuver when at minimum safe single engine airspeed (or _________ if safe single engine airspeed is not available).

Answer 6

1. 5-foot hover power minus 5 percent

2. 70 KIAS

Question 7

Normal Takeoff

1. While performing a training maneuver, assume 5ft hover power is 78% Q and the maximum power available is 89% Q.
2. What would be the correct torque setting?

Answer 7

88% Q

Question 8

Maximum Performance Takeoff

1. While performing a training maneuver, assume 5ft hover power is 78% Q and the maximum power available is 89% Q.
2. What would be the most correct torque setting?

Answer 8

89% Q

Question 9

Marginal Power Takeoff

1. While performing a training maneuver, assume 5ft hover power is 78% Q and the maximum power available is 89% Q.
2. What would be the correct torque setting?

Answer 9

78%

Question 10

Steep Approach

1. Flown to clear obstacles on an approach path using an apparent ________.
2. _____ maximum descent rate.
3. Entry _____ and approximate ___________ speed.
4. Normally flown to a touchdown.
5. Reducing forward airspeed to zero before reaching hover altitude may result in settling with power.

Answer 10

1. 45° angle
2. 800 FPM
3. 300 ft AGL ; 30 knots ground

Question 11

Normal approach

1. Used to bring the aircraft to a hover over the spot when obstacles do not interfere with the approach angle.
2. Entry airspeed is normally ______, with an apparent approach angle of _________.
3. The power required, aircraft attitude, and approach speed vary with different aircraft weights, density altitude, and winds.
4. Adjust the rate of closure so ETL will be maintained until the aircraft starts to enter ground effect (about _________).
5. Use caution: at _______ the tail skid and aft skids will contact the ground simultaneously.

Answer 11

2. 70 KIAS ; 30 deg
3. 50 feet
4. 8° nose up

Question 12

Shallow Approach

1. Entry ___________.
2. Apparent ______________.
3. Maintain airspeed above ETL (or minimum single engine air speed if applicable) and allow aircraft to touch down or come to a 5-ft hover.
4. Slide landings: after contact, slower lower the collective pitch to allow skid friction to slow forward ground speed.

Answer 12

1. 300 ft AGL and 70 KIAS

2. 10° approach angle

Question 13

Steep Approach

While performing a training maneuver, what are the entry parameters for the following approach?

Answer 13

300 ft AGL/30 GS/apparent 45° angle

Question 14

Normal Approach

While performing a training maneuver, what are the entry parameters for the following approach?

Answer 14

300 ft AGL/70 KIAS/apparent 30° angle

Question 15

Shallow Approach

While performing a training maneuver, what are the entry parameters for the following approach?

Answer 15

300 ft AGL/70 KIAS/apparent 10° angle

Question 16

What are the altitude and approximate airspeed entry parameters for a steep approach?

Answer 16

300 ft AGL; 30 kts groundspeed

Question 17

When performing a marginal power takeoff the Pilot will use __________ ft hover power and clear a simulated __________ ft obstacle.

Answer 17

5; 50

Question 18

Which answer is most correct for the following? Unusual attitude training and emergency procedures involving engines (to include simulated autorotations), engine fuel systems, flight controls, or hydraulic systems will be accomplished only __________.

A. with an Evaluator Pilot observing a check ride from the cabin area.

B. with inaccurate wind data.

C. with a passenger onboard.

D. during visual meteorological conditions.

Answer 18

during visual meteorological conditions.

Question 19

T/F:

Emergency procedure training requires Airport Rescue and Fire Fighting support to be readily available.

Answer 19

True

Question 20

Entry into hydraulic system failure (single failure) must be at a minimum altitude of __________ ft AGL and __________ KIAS during straight and level flight or on the ground.

Answer 20

500; 70

Question 21

If the Fuel Control Actuation Checklist is accomplished inflight, the aircraft must be at a minimum of __________ ft AGL and __________ KIAS before initiating step 1 of the checklist.

Answer 21

500; 70