Maneuvers

Question 1

Rolling TO

Answer 1

1. Stabilator 0° TED + transition symbology
2. Adequate runway
3. Simulated TQ 10° +/- 3 below IGE HVR TQ
4. HDG +/- 5°
5. 90 KT attitude

Question 2

VMC takeoff

Answer 2

We have adequate power
Watch my TQ, 10% above hover power
Before takeoff
Clearance

Question 3

VMC Level acceleration takeoff

Answer 3

It is the preferred takeoff to stay out of the avoid region
Monitor TQ (10%above hover) and VSSE
Before takeoff
Clearance

Question 4

Limited power takeoff

Answer 4

We only have IGE power and our surface does not allow us to do a rolling
Monitor TQ and when through ETL
ETL point
Abort point (3 rotor discs from barrier)

Question 5

Rolling landing

Answer 5

Announce Roll On
Land at or above ETL
Method of braking (25% TQ)

Question 6

When to abort a slope

Answer 6

upslope landing gear begins to slide,
aircraft brakes do not hold,
a physical cyclic stop is encountered,
crewmember’s comfort margin is exceeded

Question 7

Aerodynamic Braking

Answer 7

DE - 25% TQ minimum
SE - 50% TQ minimum

Question 8

Rolling landing Speed DE

Answer 8

At or above ETL

Question 9

Single-Engine Landing speed

Answer 9

Above VSSE until 30 feet above TD

Question 10

Steady state autorotation Factors

Answer 10

NR
Airspeed
TQ
Trim
Position to land

Question 11

Slope

Answer 11

Before LDG Check
TW lock
Suitable landing area
Set Parking Brake prior to LDG
Do not exceed slope limits (5° asymmetrical)
20% TQ – center cyclic before further reduction Collective full down

Question 12

OGE SE Failure

Answer 12

Fly away plan
Immediate reduction in torque
10-15% nose low
POWER

Question 13

SE Landing

Answer 13

1. Maintain airspeed at or above VSSE until 30 feet above landing
2. Maintain ground track alignment with the landing direction
3. Maintain a constant approach angle to the first 1/3 of lane
4. Maintain runway alignment ±5 degrees.

Question 14

Hover Standards

Answer 14

Maintain heading ±10 degrees.
Maintain altitude ±2 feet IGE or ±10 feet OGE
Do not allow drift to exceed 3 feet IGE or 12 feet OGE
Fly away plan

Question 15

Flight Standards

Answer 15

Maintain heading ±10 degrees.
Maintain ground track alignment with minimum drift.
Maintain altitude ±100 feet.
Maintain airspeed ±10 knots.
Maintain rate of climb or descent ±200 feet per minute (FPM).
Maintain trim ±ball width.
Acknowledge the low altitude warning audio.

Question 16

Power Acronym

Answer 16

Power required - OGE, robust, marginal, none
Obstacles
Winds
Escape plan
Reaction time - full left, fwd cyclic, and collective reduce (altitude permit)

Question 17

Hover Power Check

Answer 17

• Hovering at 5’ AGL at __ TQ
• Below GO/NO GO TQ
• No maneuver restrictions
• CG and FLT CNTRLS feel normal

Question 18

3 things to terminate a maneuver

Answer 18

1. MAX R/C or desired A/S
2. Clear of obstacles
3. Positive R/C

Question 19

SE -FAIL (CONT FLIGHT POSSIBLE)

Answer 19

1. FADEC-F – RAASH – FRC Cards
2. Announce underlined step
3. Select a suitable landing area (Ex: Ech)
4. PERF PAGE - VSSE and TQ
5. Confirm BIG 3
6. Touchdown at or above ETL
7. A/S > VSSE until 30’ AGL
8. Ground track alignment with LDG dir. with minimum drift
9. Maintain constant approach angle to first 1/3
10. Maintain runway alignment +/- 5° 11. Aerodynamic braking (25% simulated/50% actual TQ & aft cyclic)

Question 20

LIMITED PWR T/O

Answer 20

1. ETL Point (ATM: 3 rotor discs away*)
2. Abort Point (Ex: End of runway/lane)
3. HVR PWR = Max Torque
4. HDG +/_ 10°
5. Accelerate through ETL
6. TRIM after ETL
7. After ETL: 5° nose low (recommended)
8. Consider MAX END prior to climb or 50 KTS

Question 21

DE fail auto

Answer 21

1. Suitable landing area
2. Enter at 90 KTS and desired altitude
3. Collective below 10%
4. Right pedal, aft cyclic
5. Call out Rotor, Airspeed, Trim
6. Steady State by 200’ AGL (RATT- P)
7. A/S > 70 KTS prior to deceleration
8. Decel. no lower than 80’ AGL (130-80’ AGL)
9. Terminate with power