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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
Vfe/Vfo - flaps 15 deg.
220 KIAS
25
Vfe/Vfo - flaps 25 deg
175 KIAS
26
Vfe/Vfo - flaps 45 deg.
165 KIAS
27
Max operating speed for air brakes - flaps 0
No limit
28
Vlo/Vle
220 KIAS
29
Bird strike - normal conditions
280 KIAS to 8,000ft
30
Bird strike | Heat off <-10deg C
257 KIAS to 8,000ft
31
Max tailwind component for takeoff and landing
10 KIAS
32
Max ramp weight
28,120 lbs
33
Max takeoff weight
28,000 lbs
34
Max landing weight
23,350 lbs
35
Min operating weight
16,100 lbs
36
Max zero fuel weight
18,450 lbs
37
Min zero fuel weight
14,120 lbs
38
Max wing fuel out of balance
500 lbs
39
Wing fuel contents fuel ventral fuel transfer
3,300 lbs/side
40
Max operating altitude
41,000 ft
41
Max altitude flaps or gear extended
20,000 ft
42
Max altitude - flaps 15 | Descent and holding
15,000 ft
43
Min field PA for takeoff or landing
-2,000
44
Max field PA for takeoff or landing
13,000 ft
45
Max battery amps before takeoff | B1 and B2
20 amps
46
Max continuous generator load
300 amps
47
Max transient generator load
400 amps for up to 2 mins
48
Starter limits
30 secs/1 min - 30 secs/1 min - 30 secs/30 mins
49
Takeoff - N1
100% RPM
50
Takeoff - N2
100% rpm
51
Takeoff - ITT | APR not operating
999 deg C | 5 min
52
Takeoff (APR operating) - N1
100% rpm
53
Takeoff (APR operating) - N2
101% rpm
54
Takeoff (APR operating) - ITT
1022 C | 5 mins
55
Max continuous N1
100% rpm
56
Max continuous N2
100% rpm
57
Max continuous ITT
991 C
58
Max cruise ITT
974 C | Not a limitation, but will extend engine life
59
Max overspeed N1
100.5% rpm | 10 sec
60
Max overspeed N2
102.5% | 10 secs
61
Starting ITT | Unrestricted
994 C
62
Max oil temp | Surface to 30,500 ft
127 C
63
Max oil temp above 30,500 ft
140 C
64
Max transient oil temp
149C | 2 mins
65
Min oil temp | Starting
-40 C
66
Min oil temp | Takeoff
30 C
67
Oil pressure limit | Takeoff, Max continuous and climb
65-80 psi
68
Min oil pressure | Idle
49 psi
69
Max transient oil pressure
100 psi
70
Oil consumption rate
0.01 Gal per hour/15 hours
71
Digital Electric Engine Computer (DEEC)
Required for flight
72
Engine synchronizer switch
Off for takeoff
73
Automatic performance reserve (APR)
Must be armed for takeoff | Except for crew training
74
Wing fuel quantity
8,500 lbs
75
Ventral fuel quantity
1,500 lbs
76
Total fuel quantity
10,000 lbs
77
Min fuel required with fuel in the ventral tank
3450 lbs/side
78
Ventral fuel restriction before flight
Completely full or empty
79
Wing fuel contents for ventral transfer
3,300 / side
80
Max fuel temp
57C
81
Airframe icing requirements
Must be clear of slush, ice, frost or snow before takeoff
82
Approved de-ice fluids
TKS80, R328, to fluid spec DTD 406B
83
Ice detection lights requirements
Must be operational before FIKI at night
84
Max temp for all regimes
ISA +35 Surface to 25,000ft ISA +30 25,000 to 35,000ft ISA +25 35,000+
85
Min temp | Takeoff and landing
-40 C
86
Min temp | Enroute
-75 C
87
Max runway slope | Takeoff
+\- 2%
88
Air brake usage
Flaps 0 only
89
Cabin high datum selection
Limited to Airfields higher than 9,000 ft
90
Inter-compartment door position
Open for takeoff and landing
91
Lift dump use
Only when the aircraft is on the ground
92
Max load factor | Flaps extended
2.0G
93
Max load factor | Flaps retracted
2.73G
94
Minimum flight crew requirement
2 pilots
95
Max pressure differential
8.55 psi
96
Rejected takeoff <=90 KIAS Waiting period, 1st rejection
25 mins
97
Rejected takeoff waiting period 2nd or further attempt <= 90 KIAS
45 mins
98
Rejected takeoff >90 KIAS | Requirement
Brake inspection
99
Garrett GTCP36-150W APU | Normal operation
100%
100
APU Max operating temp
1350 F
101
APU Max operating altitude
30,000ft
102
APU Max starting altitude
20,000ft
103
APU Max transient Egt
1400-1500 F | 15 secs max
104
APU starting cycle limits before shutdown
Between 50-95% rpm - 10 secs max | Shut down APU if "ready to load" light doesn't illuminate within 60 seconds of start
105
APU starter cycle multi-attempt time limits
30 secs ON, 3 mins off 30 secs on, 3 mins off 30 secs on, 30 minutes off
106
APU Max generator limits for continuous operation
.80
107
APU generator limit for transient operation
1.2 < 10 secs
108
Combined bleed time limit
Shall not exceed 60 secs
109
APU use in icing conditions
Not authorized
110
APU ground deicing procedure
APU must be shut down for ground deicing
111
APU operating restrictions during ground refueling
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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