Contacts Flashcards

1
Q

Minimum AGL altitude: Full Stalls

A

8000

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2
Q

Minimum AGL altitude: Dynamic Engine Cut, Approach to Stalls

A

5000, (VMC to deck or 5000 feet above cloud deck)

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3
Q

Minimum AGL altitude: Ditching recovery, slow flight, actual engine shutdown/feather.

A

4000, (Weather

conditions must allow a VMC return to the nearest suitable airport prior to actual engine shutdowns.)

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4
Q

Minimum AGL altitude: Initiate recovery from emergency descent

A

2000

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5
Q

Minimum AGL altitude: Recovered from emergency descent/overwater seat changes

A

1000

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6
Q

Minimum AGL altitude: Overland seat changes

A

800

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7
Q

Minimum AGL altitude: Simulated Single-Engine (SSE) after takeoff (IP initiated)

A

300

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8
Q

Minimum AGL altitude: SSE waveoff (IP directed)

A

200

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9
Q

Minimum AGL altitude: Normal waveoff (IP directed)

A

100

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10
Q

Normal Cruise

A

150 KIAS

1900 RPM

650-700 Q

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11
Q

Fast Cruise

A

170 KIAS

1900 RPM

900-1000 Q

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12
Q

Slow Cruise

A

130 KIAS

1900 RPM

450-550 Q

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13
Q

Cruise Climb: SL - 10K

A

150 KIAS

1900 RPM

Max Allowable Q

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14
Q

Cruise Climb: 10K - 20K

A

130 KIAS

1900 RPM

Max Allowable Q

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15
Q

Cruise Climb: 20K - 25K

A

120 KIAS

1900 RPM

Max Allowable Q

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16
Q

Vx

A

102 KIAS

1900 RPM

Max Allowable Q

17
Q

Vy

A

108 KIAS

1900 RPM

Max Allowable Q

18
Q

Vxse

A

102 KIAS

1900 RPM

Max Allowable Q

19
Q

Vyse

A

110 KIAS

1900 RPM

Max Allowable Q

20
Q

Emergency Descent

A

227 KIAS

2200 RPM

Idle

21
Q

Climb from Cruise

A
  • Raise nose to climb attitude
  • Transition to appropriate climb airspeed
  • Adjust power as required
  • Adjust pitch and power as required to maintain climb airspeed
22
Q

Cruise from Climb

A
  • 50-75 feet prior to the desired altitude, smoothly decrease pitch to the cruise attitude
  • Adjust power as necessary. Max climb power may be maintained until desired cruise airspeed in attained.
23
Q

Cruise from Descent

A
  • 50-75 feet prior to the desired altitude, smoothly increase pitch to the cruise attitude
  • Simultaneously apply cruise power
24
Q

Descent from Cruise

A
  • Reduce power as required

- Reduce pitch to obtain the airspeed/rate of descent combination desired