Maneuver Standards Flashcards

1
Q

TASK 1040
Perform Visual Meteorological Conditions (VMC) Takeoff

A
  1. Maintain takeoff heading ±10 degrees below 50 feet or until clear of the obstacles, or limited power takeoff until through ETL.
  2. Maintain ground track alignment with the takeoff direction.
  3. Maintain the aircraft in trim above 50 feet AGL or as appropriate for obstacle avoidance.
  4. Accelerate to desired airspeed ±10 knots.
  5. Apply takeoff power, not to exceed maximum available for the selected takeoff, until reaching desired altitude, minimum single engine airspeed, or as conditions permit
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2
Q

TASK 1062
Perform Slope Operations

A
  1. Set the parking brake prior to landing.
  2. Maintain heading ±5 degrees.
  3. Maintain minimum drift after wheel contact with the ground.
  4. Do not exceed slope limits of the current operator’s manual.
  5. Perform a smooth, controlled descent and touchdown.
  6. Perform a smooth, controlled ascent
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3
Q

TASK 1064
Perform a Roll-On Landing

A
  1. Touchdown at or above ETL
  2. Maintain ground track alignment with the landing direction with minimum drift.
  3. Maintain a constant approach angle to the desired point of touchdown with deviations for surface conditions or obstacles in the landing area.
  4. Maintain runway or suitable landing area alignment +/-5 degree
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4
Q

TASK 1114
Perform Rolling Takeoff: Before liftoff

A

a. Position the stabilator to 0 degrees trailing edge down (TED).
b. Establish and maintain a simulated power limit of 10% below hover power ±3 % or, when IGE hover power is limited or not available, as described in the Task 1010 procedures ±3 %.
c. Coordinate accelerating the aircraft while maintaining aircraft longitudinal alignment in coincidence with the takeoff area’s heading/direction±5 degrees.
d. Do not allow the aircraft nose to drop below the fuselage level until the aircraft departs the takeoff surface

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5
Q

standards: hover heading

A

±10 degeees

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6
Q

standards: hover altitude IGE/OGe

A

3 feet
12 feet

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7
Q

standards: hover drift IGE and OGE (80 ft)

A

3 feet IGE
12 feet OGE

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8
Q

standards: hover ground track

A

3 feet

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9
Q

standards: in flight heading

A

±10 degrees

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10
Q

standards: in flight altitude

A

±100 feet

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11
Q

standards: in flight airspeed

A

± 10 knots

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12
Q

standards: in flight trim

A

± Ball

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13
Q

Minimum safe altitude

A

Above the surface or obstacles to which the aircraft can descend in a masked condition

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14
Q

Minimum maneuvering altitude

A

Altitude above the mask or barriers at which the aircraft may safely hover

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15
Q

How can you determine OGE hover capability

A

Compare hover torque OGE to Max Tq (dual engine)
Compare max GWT OGE to current GWT

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16
Q

Ground taxi TQ

A

25-30

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17
Q

Standards: ground track for ground Taxi

18
Q

Full scale deflection if velocity vector in hover mode is:

A

6 knots ground speed

19
Q

Full scale deflection if velocity vector in transition mode is:

20
Q

Standards: VMC Takeoff

A

TQ 10% above hover
Heading 10 degrees Below 50 Ft
Above 50 ft in trim
Desired airspeed ± 10 knots (50 vx)

21
Q

Bingo fuel

A

Minimum fuel necessary to fly to a refuel site

22
Q

Joker fuel

A

The fuel point where training is terminated above bingo

23
Q

Buster

A

Max continuous speed

24
Q

Liner

A

Max range fuel

25
Saunter
Best endurancr
26
Standards: Slope operations heading
± 5
27
Standards: slopes center cyclic with no less than-
25% TQ to avoid droop stop pounding
28
Roll on landing aerodynamic braking
25% SE 50% DE
29
Standards: roll on alignment
± 5 degrees
30
Standards SE landing speed
Maintain speed at or above VSSE until 30 ft to the 1st 1/3 of the usable runway
31
Standards: Autorotation call outs
Nr (rotor), speed, trim
32
Standards: Autorotation speed
No less than 70 knots prior to decel
33
Standards: Rolling takeoff
Zero stab 10% below hover ± 5 Heading Nose can’t drop below fuselage lvl
34
Continuous angle TO
Power: robust
35
Altitude over airspeed take off
Power: marginal oge
36
Airspeed over altitude takeoff
Power: OGE pwr not available
37
Low level flight
80-200ft
38
Contour
25-80ft
39
NOE
Up to 25ft
40
When to abort a slope
Upslope landing gear slides Brakes don’t hold Cyclic stop encountered Comfort margin exceeded
41
Standards: Limited power TO
Hover power available Cond not suitable for rolling TO Determine: ETL and abort point Speed: no less than VSDE ±5
42
VMC level accel
TQ 10% above hover Heading 10 degrees Below 50 Ft Above 50 ft in trim Speed min VSSE prior to climb