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CAE Ground School > Flash Cards > Flashcards

Flash Cards

1
Q

Min crew

A

One pilot

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2
Q

Passenger seating limitations

A

Part 91 says 15

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3
Q

Flight load factor limit with flaps up

A

3.1 positive and 1.24 negative

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4
Q

Flight load limit with flaps down

A

2 positive and 0 negative

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5
Q

Altitude limitation using aviation gasoline with standby fuel pumps operative

A

35k ft

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6
Q

Altitude limitation using aviation gasoline with either standby fuel pump inoperative

A

Flight prohibited

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7
Q

Altitude limitation using aviation gasoline without cross feed capability

A

20k ft

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8
Q

Max operating altitude normal operation

A

35k ft

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9
Q

Maximum operating altitude if yaw damper system is inoperative

A

5k ft

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10
Q

Maximum allowable takeoff weight

A

15k lbs or as limited by takeoff climb requirements or tire speed or takeoff field length

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11
Q

Maximum landing weight

A

15k lbs or as limited by max landing weight to achieve climb requirements or max landing distance with flaps down

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12
Q

Max ramp weight

A

15100 lbs

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13
Q

Max zero fuel weight

A

12500 lbs

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14
Q

Max weight in baggage compartment

A

550 lbs

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15
Q

One engine inoperative best angle of climb Vxse

A

125 kias

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16
Q

One engine inoperative best rate of climb Vyse

A

125 Kias

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17
Q

One engine inoperative enroute climb Emergency air speed

A

125 kias

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18
Q

Air minimum control speed Vmca with flaps up

A

94 kias

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19
Q

Air minimum control speed Vmca with flaps approach

A

93 kias

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20
Q

Emergency descent speed

A

184 kias

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21
Q

Maximum range glide speed

A

135 kias

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22
Q

Max demonstrated crosswind

A

20 kias

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23
Q

Max demonstrated wind components for coupled approaches with a cross wind

A

32 kias

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24
Q

Max demonstrated wind components for coupled approaches with a tailwind

A

14 kias

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25
Q

Maneuvering speed Va

A

184 kias

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26
Q

Max flap extended speed Vfe approach

A

202 kias

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27
Q

Max flap extended speed Vfe full down

A

158 kias

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28
Q

Max landing gear operating speed Vlo extension

A

184 kias

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29
Q

Max landing gear operating speed Vlo retraction

A

166 kias

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30
Q

Max landing gear extended speed Vle

A

184 kias

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31
Q

Max operating speed Vmo in knots and Mach number

A

263 kias and .58 Mach

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32
Q

Aircraft height

A

14 ft 4 in

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33
Q

Aircraft length

A

46 ft 8 in

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34
Q

Aircraft wingspan

A

57 ft 11 in

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35
Q

Aft facing seats

A

Seat back of each occupied aft facing seat must be in upright position with headrest fully extended for takeoff and landing

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36
Q

The pilot and Co pilot air data computers must be what for takeoff

A

Operative

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37
Q

The multi function display must be what prior to engine start

A

Operational

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38
Q

The pilot PFD and MFD and Co pilots PFD must be installed and operational in what mode for takeoff

A

Normal

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39
Q

AHRS 1 and 2 must be what for takeoff

A

Operative

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40
Q

Operating in the composite mode is limited to what and what conditions

A

Training and display failure

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41
Q

Auto pilot coupled intercept angle for back course

A

70 degrees

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42
Q

Autopilot max coupled intercept angle for NAV/LOC

A

Less than 90 degrees

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43
Q

During what type of operations a pilot must be seated at the controls with seat belt and shoulder harness fastened

A

Autopilot

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44
Q

When must an autopilot preflight check be conducted

A

Must be conducted and found satisfactory prior to each flight on which auto pilot is to be used

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45
Q

Min autopilot engage height after takeoff

A

400 ft

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46
Q

Min autopilot use height during cruise

A

1000 ft

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47
Q

Min autopilot use height during approach

A

79 ft AGL

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48
Q

Min autopilot use

Height during steep approach

A

160 ft AGL

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49
Q

When must the auto pilot and yaw damper not be used

A

During takeoff and landing

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50
Q

Operation of the auto pilot with a what is prohibited

A

Pitch trim malfunction

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51
Q

When Should you not manually override the autopilot

A

During normal flight

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52
Q

Below X volts, battery must be recharged or replaced with battery indicating at least 20 volts before connecting external power

A

20

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53
Q

External power amps limit momentary

A

1000 amps

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54
Q

External power amps limit continuous

A

300 amps

55
Q

External power volt range

A

28 to 28.4

56
Q

Generator load limit in flight up to 34k ft

A

100%

57
Q

Generator load limit in flight above 34k ft

A

95%

58
Q

Generator load limit on the ground with N1 from 62 to 70%

A

75%

59
Q

Generator load limit on the ground with N1 from 70 to 100%

A

100%

60
Q

Min battery volts for battery start

A

23 VDC

61
Q

Starter limits

A

30 seconds on and 5 min off
30 seconds on and 5 min off
30 seconds on and 30 min off

62
Q

Do not put any fuel in the blank tanks unless the blank tanks are full

A

Don’t put fuel in the aux tanks unless the mains are full

63
Q

For fuel system don’t takeoff if fuel quantity gauges indicate blank arc or less than blank lbs in each wing system

A

Yellow arc or less than 265 lbs in each wing

64
Q

Fuel cross feed is permitted only when blank

A

One engine is inoperative

65
Q

Max fuel imbalance

A

300 lbs

66
Q

Total useable fuel

A

3611 lbs

67
Q

Each main fuel tank quantity useable

A

1273 lbs

68
Q

Each aux fuel tank quantity useable

A

533 lbs

69
Q

Operation of either engine with its corresponding fuel pressure annunciator (L FUEL PRESS LO or R FUEL PRESS LO) illuminated is limited to blank hours before overhaul or replacement of engine driven fuel pump (windmill time doesn’t count)

A

10 hours

70
Q

Engine anti ice shall be on in ambient temperatures of blank or below when flight free of visible moisture can’t be assured

A

5 degrees Celsius

71
Q

The left and right engine anti ice shall be off for takeoff operations in ambient temperatures above blank

A

10 degrees Celsius

72
Q

Min ambient temperature for operation of de icing boots

A

-40 degrees Celsius

73
Q

Min airspeed for sustained icing flight

A

140 kias (no flaps except takeoff and landing)

74
Q

Prop de ice ammeter normal operating range

A

26 to 32 amps

75
Q

Brake de ice temp operation limit

A

Not above 15 degrees Celsius

76
Q

Landing gear cycle limits

A

1 cycle every five minutes for 6 cycles followed by 15 min cool down

77
Q

Cabin differential pressure gauge green arc

A

0 to 6.6 psi

78
Q

Cabin differential pressure gauge red arc

A

6.6 psi to end of scale

79
Q

The CABIN ALTITUDE light illuminates when

A

Cabin altitude is above 10k ft

80
Q

CABIN ALTITUDE HI lights illuminates when

A

Cabin altitude above 12000 ft

81
Q

Above what altitude do oxygen masks automatically deploy

A

12500 ft

82
Q

Pressure where CABIN DIFF HI light illuminates

A

6.9 PSID

83
Q

Outside air temperature limit up to 25k ft PA

A

ISA plus 37 degrees Celsius

84
Q

Outside air temperature limit above 25k ft PA

A

ISA plus 31 degrees Celsius

85
Q

Engine model number and type

A

PT6A-60A, turbo prop

86
Q

Propeller type

A 
Constant speed
Full feathering
Reversing
Counter weighted
Hydraulically actuated
87
Q

When must Auto feather be armed

A

Takeoff and climb and approach and landing

88
Q

Engine torque for takeoff

A

100% (102% for 7 minutes)

89
Q

Engine torque max continuous

A

100% (102% for 7 minutes)

90
Q

Engine torque transient

A

156% (limited to 20 seconds)

91
Q

Engine torque below 1000 RPM N2

A

62%

92
Q

Engine max ITT during start

A

1000 degrees Celsius for 5 seconds

93
Q

Engine max ITT at idle

A

820 degrees Celsius

94
Q

Engine max ITT max continuous

A

820 degrees Celsius

95
Q

Engine max ITT max cruise

A

820 degrees Celsius

96
Q

Engine max ITT cruise climb

A

785 degrees Celsius

97
Q

Engine max ITT max reverse

A

760 degrees Celsius

98
Q

Engine max ITT transient

A

850 degrees Celsius for 20 seconds

99
Q

Engine gas generator (%N1) at idle

A

62% min

100
Q

Engine gas generator (%N1) at takeoff

A

104%

101
Q

Engine gas generator (%N1) max continuous

A

104%

102
Q

Engine gas generator (%N1) cruise climb

A

104%

103
Q

Engine gas generator (%N1) max cruise

A

104%

104
Q

Engine gas generator (%N1) transient

A

104%

105
Q

Engine prop RPM (N2) at idle

A

1050 min

106
Q

Engine prop RPM (N2) at takeoff

A

1700 (up to 1735 for 7 minutes)

107
Q

Engine prop RPM (N2) max continuous

A

1700 (up to 1735 for 7 minutes)

108
Q

Engine prop RPM (N2) at cruise climb

A

1700 (up to 1735 for 7 minutes)

109
Q

Engine prop RPM (N2) at max cruise

A

1700 (up to 1735 for 7 minutes)

110
Q

Engine prop RPM (N2) at max reverse

A

1650

111
Q

Engine prop RPM (N2) transient

A

1870 for 20 seconds

112
Q

Engine oil pressure starting

A

0 to 200 psi

113
Q

Engine oil pressure at idle

A

60 psi min

114
Q

Engine oil pressure at takeoff

A

90 to 135 psi

115
Q

Engine oil pressure at max continuous

A

90 to 135 psi

116
Q

Engine oil pressure at cruise climb

A

90 to 135 psi

117
Q

Engine oil pressure at max cruise

A

90 to 135 psi

118
Q

Engine oil pressure at max reverse

A

90 to 135 psi

119
Q

Engine oil pressure transient

A

200 psi

120
Q

Engine oil temperature starting

A

-40 degrees Celsius minimum

121
Q

Engine oil temperature idle

A

-40 to 110 degrees Celsius

122
Q

Engine oil temperature takeoff

A

0 to 110 degrees Celsius

123
Q

Engine oil temperature max continuous

A

0 to 110 degrees Celsius

124
Q

Engine oil temperature cruise climb

A

0 to 110 degrees Celsius

125
Q

Engine oil temperature max cruise

A

0 to 110 degrees Celsius

126
Q

Engine oil temperature max reverse

A

0 to 99 degrees Celsius

127
Q

Engine oil temperature transient

A

0 to 110 degrees Celsius

128
Q

Engine oil temperature min for fuel heat at takeoff

A

55 degrees Celsius (recommended)

129
Q

Range of primary Governor

A

1450 to 1700 RPM

130
Q

Over speed Governor governs to x RPM

A

1768 RPM

131
Q

Why should power lever not be lifted in flight

A

Leads to nose down pitch and descent rate that could lead to aircraft damage or injury to personnel

132
Q

When must the rudder boost be operational

A

All phases of flight

133
Q

Max wind any direction

A

50 kts

CAE Ground School (5 decks)

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