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Memory Flash Cards

0
Q

Engine fire, engine failure, or inadvertent thrust reverser deployment

After V1 - Takeoff continued

A
  1. LANDING GEAR - up
  2. MAIN AIR VLVs 1&2 - close
  3. F/DK VLV close
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1
Q

Engine fire, engine failure, inadvertent thrust reverser deployment during takeoff

Below V1 - takeoff aborted

A
  1. Thrust levers - close
  2. Brakes - apply
  3. Air brakes - deploy
  4. Thrust reversers- deploy
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2
Q

Engine fire in flight

A 
1. Thrust lever (affected engine) - close
If fire persists:
2. HP COCK (affected engine) - close
3. LP COCK (affected engine) - close
4. ENG EXT (affected engine)  - shot 1
If engine shutdown occurs during initial climb out:
5. MAIN AIR VLVs 1 & 2 - close
6. F/DK VLV - close
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3
Q

Engine fire on ground

A
  1. START PWR switch (starting only) - push for abort
  2. HP COCK (affected engine) - close
  3. LP COCK (affected engine) - close
  4. ENG EXT (affected engine) - shot 1
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4
Q

Enine computer failure

A

ENG CMPTR - off

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5
Q

Oil low pressure

A
  1. OIL PRESSURE - check gauge
    If below 49 psi:
  2. HP COCK - CLOSE
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6
Q

Inadvertent thrust reverser deployment in flight

A
  1. HP COCK - close
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7
Q

Double engine failure in flight

A
  1. Thrust levers - close
  2. Crew oxygen - don masks if above 15,000 ft
  3. MIC selector - OXY MIC if above 15,000 ft
  4. Engine indications - monitor
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8
Q

Depressurization

A
  1. Crew oxygen - don masks

2. MIC selector - OXY-MIC

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9
Q

Rear equipment bay overheat

A
  1. MAIN AIR VLV 1 & 2 - close

2. F/DK VLV - open fully

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10
Q

High pressure air overheat

A
  1. MAIN AIR VLV (affected engine) - close

2. F/DK VLV - close

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11
Q

Emergency descent

A
  1. Thrust levers - close
  2. Speed - Mmo/Vmo (unless structural damage suspected)
  3. AIR BRAKE - deploy
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12
Q

Electrical fire or smoke

A
  1. Crew oxygen - don masks 100% EMERG
  2. MIC selector - OXY MIC
  3. Cabin notices - on
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13
Q

Fuselage fire or smoke

Fire or smoke from any source other than avionics/electronics

A
  1. Crew oxygen - don masks 100% EMERG
  2. MIC selector - OXY MIC
  3. Cabin notices - on
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14
Q

Smoke from air conditioning ducts

A
  1. Crew oxygen - don masks 100% EMERG
  2. MIC selector- OXY MIC
  3. Cabin notices- on
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15
Q

Brake failure

A
  1. Brake pedals - release
  2. WHEEL BRAKE lever - EMERGY
  3. Brake pedals - apply gently in one continuous application
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16
Q

EGPWS warning

A
  1. Go-around button - pushed
  2. Thrust - takeoff N1
  3. Pitch - increase and climb as required to avoid obstacle
  4. APR - OVRD
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17
Q

Windshear warning

A
  1. Go-around button - push
  2. Thrust - takeoff N1
  3. Pitch - pitch up to stick shaker
  4. APR - OVRD
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18
Q

Emergency evacuation

A
  1. Airplane - stop
  2. WHEEL BRAKE - lock
  3. HP COCKs - close
  4. LP COCKs - close
  5. EMERG LIGHTS (if required) - MAN
  6. PA - order evacuation
  7. DUMP VALVE - open
  8. BATT - off
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19
Q

Vmo, ventral fuel tanks empty, flaps 0

A

335 KIAS (sfc - 12,000ft)

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20
Q

Vmo

Ventral tanks not empty, flaps 0

A

280 KIAS

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21
Q

Mmo

A

Mach .80

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22
Q

Mmo

Mach trim system Inop and autopilot disengaged

A

Mach .73

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23
Q

Va

A

196 KIAS

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24
Q

Vfe/Vfo - flaps 15 deg.

A

220 KIAS

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25
Q

Vfe/Vfo - flaps 25 deg

A

175 KIAS

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26
Q

Vfe/Vfo - flaps 45 deg.

A

165 KIAS

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27
Q

Max operating speed for air brakes - flaps 0

A

No limit

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28
Q

Vlo/Vle

A

220 KIAS

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29
Q

Bird strike - normal conditions

A

280 KIAS to 8,000ft

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30
Q

Bird strike

Heat off <-10deg C

A

257 KIAS to 8,000ft

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31
Q

Max tailwind component for takeoff and landing

A

10 KIAS

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32
Q

Max ramp weight

A

28,120 lbs

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33
Q

Max takeoff weight

A

28,000 lbs

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34
Q

Max landing weight

A

23,350 lbs

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35
Q

Min operating weight

A

16,100 lbs

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36
Q

Max zero fuel weight

A

18,450 lbs

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37
Q

Min zero fuel weight

A

14,120 lbs

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38
Q

Max wing fuel out of balance

A

500 lbs

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39
Q

Wing fuel contents fuel ventral fuel transfer

A

3,300 lbs/side

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40
Q

Max operating altitude

A

41,000 ft

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41
Q

Max altitude flaps or gear extended

A

20,000 ft

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42
Q

Max altitude - flaps 15

Descent and holding

A

15,000 ft

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43
Q

Min field PA for takeoff or landing

A

-2,000

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44
Q

Max field PA for takeoff or landing

45
Q

Max battery amps before takeoff

B1 and B2

46
Q

Max continuous generator load

47
Q

Max transient generator load

A

400 amps for up to 2 mins

48
Q

Starter limits

A

30 secs/1 min - 30 secs/1 min - 30 secs/30 mins

49
Q

Takeoff - N1

50
Q

Takeoff - N2

51
Q

Takeoff - ITT

APR not operating

A

999 deg C

5 min

52
Q

Takeoff (APR operating) - N1

53
Q

Takeoff (APR operating) - N2

54
Q

Takeoff (APR operating) - ITT

A

1022 C

5 mins

55
Q

Max continuous N1

56
Q

Max continuous N2

57
Q

Max continuous ITT

58
Q

Max cruise ITT

A

974 C

Not a limitation, but will extend engine life

59
Q

Max overspeed N1

A

100.5% rpm

10 sec

60
Q

Max overspeed N2

A

102.5%

10 secs

61
Q

Starting ITT

Unrestricted

62
Q

Max oil temp

Surface to 30,500 ft

63
Q

Max oil temp above 30,500 ft

64
Q

Max transient oil temp

A

149C

2 mins

65
Q

Min oil temp

Starting

66
Q

Min oil temp

Takeoff

67
Q

Oil pressure limit

Takeoff, Max continuous and climb

68
Q

Min oil pressure

Idle

69
Q

Max transient oil pressure

70
Q

Oil consumption rate

A

0.01 Gal per hour/15 hours

71
Q

Digital Electric Engine Computer (DEEC)

A

Required for flight

72
Q

Engine synchronizer switch

A

Off for takeoff

73
Q

Automatic performance reserve (APR)

A

Must be armed for takeoff

Except for crew training

74
Q

Wing fuel quantity

75
Q

Ventral fuel quantity

76
Q

Total fuel quantity

A

10,000 lbs

77
Q

Min fuel required with fuel in the ventral tank

A

3450 lbs/side

78
Q

Ventral fuel restriction before flight

A

Completely full or empty

79
Q

Wing fuel contents for ventral transfer

A

3,300 / side

80
Q

Max fuel temp

81
Q

Airframe icing requirements

A

Must be clear of slush, ice, frost or snow before takeoff

82
Q

Approved de-ice fluids

A

TKS80, R328, to fluid spec DTD 406B

83
Q

Ice detection lights requirements

A

Must be operational before FIKI at night

84
Q

Max temp for all regimes

A

ISA +35 Surface to 25,000ft
ISA +30 25,000 to 35,000ft
ISA +25 35,000+

85
Q

Min temp

Takeoff and landing

86
Q

Min temp

Enroute

87
Q

Max runway slope

Takeoff

88
Q

Air brake usage

A

Flaps 0 only

89
Q

Cabin high datum selection

A

Limited to Airfields higher than 9,000 ft

90
Q

Inter-compartment door position

A

Open for takeoff and landing

91
Q

Lift dump use

A

Only when the aircraft is on the ground

92
Q

Max load factor

Flaps extended

93
Q

Max load factor

Flaps retracted

94
Q

Minimum flight crew requirement

95
Q

Max pressure differential

96
Q

Rejected takeoff
<=90 KIAS
Waiting period, 1st rejection

97
Q

Rejected takeoff waiting period
2nd or further attempt
<= 90 KIAS

98
Q

Rejected takeoff >90 KIAS

Requirement

A

Brake inspection

99
Q

Garrett GTCP36-150W APU

Normal operation

100
Q

APU Max operating temp

101
Q

APU Max operating altitude

102
Q

APU Max starting altitude

103
Q

APU Max transient Egt

A

1400-1500 F

15 secs max

104
Q

APU starting cycle limits before shutdown

A

Between 50-95% rpm - 10 secs max

Shut down APU if “ready to load” light doesn’t illuminate within 60 seconds of start

105
Q

APU starter cycle multi-attempt time limits

A

30 secs ON, 3 mins off
30 secs on, 3 mins off
30 secs on, 30 minutes off

106
Q

APU Max generator limits for continuous operation

107
Q

APU generator limit for transient operation

A

1.2 < 10 secs

108
Q

Combined bleed time limit

A

Shall not exceed 60 secs

109
Q

APU use in icing conditions

A

Not authorized

110
Q

APU ground deicing procedure

A

APU must be shut down for ground deicing

111
Q

APU operating restrictions during ground refueling

A

Center point refueling only
May not start APU during refueling
APU may not be running if using JP4 or if temp >40C
Boost pumps must be off

Hawker (8 decks)

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