R-22 POH Flashcards

1
Q

Main rotor diameter

A

25’ 2”

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2
Q

main rotor chord

A

7.2” (constant)

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3
Q

Main rotor blade twist

A

-8 degrees

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4
Q

Main rotor tip speed

A

672 FPS

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5
Q

Tail rotor diameter

A

3’ 6”

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6
Q

Tail rotor blade chord

A

4” (constant)

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7
Q

Tail rotor precone angle

A

1 degree 11 minutes

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8
Q

Tail rotor tip speed

A

599 FPS

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9
Q

usable fuel capacity with bladder

A

combine 26.3
Main 16.9
Aux 9.4

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10
Q

Flight and maneuver limitations

A
Governor off prohibited except EP training or inflight malfunction
Low G pushover prohibited
Areobatics
Doors off permitted
I Flight into known icing conditions
Minimum 1 crew
Solo right seat
Max DA 14,000
A Goal
Left seat belt buckled
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11
Q

approved fuel

A

91/96 AV fuel, 100LL Av Fuel, 100/130 av Fuel

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12
Q

VFR night

A

Navigation lights
Anti-collision lights
Instrument lights
Landing lights

ground orientation by ground objects illuminated solely by lights on ground or adequate celestial illumination

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13
Q

Mandatory operating components

A

Governor
OAT gauge
Alternator
Low warning RPM system

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14
Q

Engine max speed

A

2652 RPM (104%)

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15
Q

Rotor Speed Limits

A

110% 561
104% 530
101% 515
90% 459

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16
Q

Cylinder head temp limit

A

200-500F

17
Q

Oil Pressure and temp limit

A

25, 55, 95, 115

75-245F

18
Q

loss of tail rotor thrust hover

A
  1. roll throttle off into overtravel spring and allow aircraft to settle.
  2. Raise collective just before touchdown to cushion landing
19
Q

loss of tail rotor thrust in forward flight

A
  1. immediately enter auto
  2. maintain at least 70 Kias if practical
  3. select landing site, roll throttle off into overtravel spring, and perform auto
20
Q

Electrical fire in flight

A
  1. battery and alt - off
  2. open cabin vents
  3. land immediately
  4. fuel mixture and valve- off
  5. if time permits apply rotor brake
  6. exit helicopter
21
Q

Tach failure

A

if engine or rotor tach fail then use other tach. if not sure then let governor control RPM.