Annual Checkride GA8 Flashcards

1
Q

Maximum Continuous HP

A

300

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2
Q

Total Fuel Capacity

A

92.2

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3
Q

Total Usable Fuel

A

87.7

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4
Q

Total Fuel Each Tank

A

44.9

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5
Q

Total Usable Fuel Each Tank

A

43.85

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6
Q

Maximum Fuel Imbalance

A

26.4

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7
Q

Maximum fuel in sump tank

A

2.4

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8
Q

Maximum fuel pressure

A

65psi

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9
Q

Normal Fuel pressure range

A

27-65

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10
Q

Total Oil capacity with sump

A

12

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11
Q

TIT maximum Temp

A

1650

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12
Q

CHT maximum temp

A

500

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13
Q

Max speed with Auto Pilot Engaged

A

130

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14
Q

Minimum speed with Autopilot engaged

A

80

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15
Q

Max Glide, 4200 lbs

A

86

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16
Q

Max Glide, 4000 lbs

A

84

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17
Q

Engine Failure during takeoff run Bold face items

A

Throttle- Closed

Brakes- Apply

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18
Q

Engine failure immediately after takeoff

A

Airspeed 64-73

19
Q

Engine Failure during flight

A
Airspeed- 74-84
Boost Pump - on
Camera - up
Alternate air - on
Mixture - Rich
Fuel Shutoff - confirm in
20
Q

Engine Fire in flight

A
Fuel shutoff - off
Boost pump - off
Throttle - Idle
Mixture - idle cutoff
Cowl Flaps - closed
Master Switches - off
Vents - closed
Airspeed -140
Forced landing - execute
21
Q

Electrical Fire in flight

A

Master switches - off
Electrical switches - off
Extinguisher - activate

22
Q

Cabin Fire

A

Master Switches - off
Vents - closed
Fire extinguisher - activate

23
Q

Wing Length

A

40’ 8 1/2”

24
Q

Max Ramp weight

A

4200

25
Q

Max Takeoff weight

A

4200

26
Q

Max landing weight

A

4100

27
Q

Max weight in the aft bin

A

50 lbs

28
Q

Flaps Takeoff range

A

0-14

29
Q

Flaps Landing Range

A

0-38

30
Q

Vtoss

A

71

31
Q

Vne

A

190

32
Q

Vno

A

147

33
Q

Va

A

121

34
Q

Vfe

A

100

35
Q

Vy

A

80

36
Q

Vx

A

70

37
Q

Normal Climb, Flaps up

A

81

38
Q

Normal en route climb

A

81-90

39
Q

Vso

A

61

40
Q

Vs1

A

66

41
Q

Flight load Factor limits

A

Flaps up — +3.79/ -1.52

Flaps Down — +2.0/ -0

42
Q

Max glide (4200, 4000,3527,3086)

A

4200- 86
4000- 74
3600- 80
3086- 69

43
Q

Landing without engine power (speed) flaps 38*

A

75