Memory Flash Cards

Question 0

Engine fire, engine failure, or inadvertent thrust reverser deployment

After V1 - Takeoff continued

Answer 0

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

Question 1

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

Below V1 - takeoff aborted

Answer 1

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

Question 2

Engine fire in flight

Answer 2

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

Question 3

Engine fire on ground

Answer 3

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

Question 4

Enine computer failure

Answer 4

ENG CMPTR - off

Question 5

Oil low pressure

Answer 5

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

Question 6

Inadvertent thrust reverser deployment in flight

Answer 6

1. HP COCK - close

Question 7

Double engine failure in flight

Answer 7

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

Question 8

Depressurization

Answer 8

1. Crew oxygen - don masks

2. MIC selector - OXY-MIC

Question 9

Rear equipment bay overheat

Answer 9

1. MAIN AIR VLV 1 & 2 - close

2. F/DK VLV - open fully

Question 10

High pressure air overheat

Answer 10

1. MAIN AIR VLV (affected engine) - close

2. F/DK VLV - close

Question 11

Emergency descent

Answer 11

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

Question 12

Electrical fire or smoke

Answer 12

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

Question 13

Fuselage fire or smoke

Fire or smoke from any source other than avionics/electronics

Answer 13

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

Question 14

Smoke from air conditioning ducts

Answer 14

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

Question 15

Brake failure

Answer 15

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

Question 16

EGPWS warning

Answer 16

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

Question 17

Windshear warning

Answer 17

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

Question 18

Emergency evacuation

Answer 18

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

Question 19

Vmo, ventral fuel tanks empty, flaps 0

Answer 19

335 KIAS (sfc - 12,000ft)

Question 20

Vmo

Ventral tanks not empty, flaps 0

Answer 20

280 KIAS

Question 21

Mmo

Answer 21

Mach .80

Question 22

Mmo

Mach trim system Inop and autopilot disengaged

Answer 22

Mach .73

Question 23

Va

Answer 23

196 KIAS

Question 24

Vfe/Vfo - flaps 15 deg.

Answer 24

220 KIAS

Question 25

Vfe/Vfo - flaps 25 deg

Answer 25

175 KIAS

Question 26

Vfe/Vfo - flaps 45 deg.

Answer 26

165 KIAS

Question 27

Max operating speed for air brakes - flaps 0

Answer 27

No limit

Question 28

Vlo/Vle

Answer 28

220 KIAS

Question 29

Bird strike - normal conditions

Answer 29

280 KIAS to 8,000ft

Question 30

Bird strike | Heat off <-10deg C

Answer 30

257 KIAS to 8,000ft

Question 31

Max tailwind component for takeoff and landing

Answer 31

10 KIAS

Question 32

Max ramp weight

Answer 32

28,120 lbs

Question 33

Max takeoff weight

Answer 33

28,000 lbs

Question 34

Max landing weight

Answer 34

23,350 lbs

Question 35

Min operating weight

Answer 35

16,100 lbs

Question 36

Max zero fuel weight

Answer 36

18,450 lbs

Question 37

Min zero fuel weight

Answer 37

14,120 lbs

Question 38

Max wing fuel out of balance

Answer 38

500 lbs

Question 39

Wing fuel contents fuel ventral fuel transfer

Answer 39

3,300 lbs/side

Question 40

Max operating altitude

Answer 40

41,000 ft

Question 41

Max altitude flaps or gear extended

Answer 41

20,000 ft

Question 42

Max altitude - flaps 15 | Descent and holding

Answer 42

15,000 ft

Question 43

Min field PA for takeoff or landing

Answer 43

-2,000

Question 44

Max field PA for takeoff or landing

Answer 44

13,000 ft

Question 45

Max battery amps before takeoff | B1 and B2

Answer 45

20 amps

Question 46

Max continuous generator load

Answer 46

300 amps

Question 47

Max transient generator load

Answer 47

400 amps for up to 2 mins

Question 48

Starter limits

Answer 48

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

Question 49

Takeoff - N1

Answer 49

100% RPM

Question 50

Takeoff - N2

Answer 50

100% rpm

Question 51

Takeoff - ITT | APR not operating

Answer 51

999 deg C | 5 min

Question 52

Takeoff (APR operating) - N1

Answer 52

100% rpm

Question 53

Takeoff (APR operating) - N2

Answer 53

101% rpm

Question 54

Takeoff (APR operating) - ITT

Answer 54

1022 C | 5 mins

Question 55

Max continuous N1

Answer 55

100% rpm

Question 56

Max continuous N2

Answer 56

100% rpm

Question 57

Max continuous ITT

Answer 57

991 C

Question 58

Max cruise ITT

Answer 58

974 C | Not a limitation, but will extend engine life

Question 59

Max overspeed N1

Answer 59

100.5% rpm | 10 sec

Question 60

Max overspeed N2

Answer 60

102.5% | 10 secs

Question 61

Starting ITT | Unrestricted

Answer 61

994 C

Question 62

Max oil temp | Surface to 30,500 ft

Answer 62

127 C

Question 63

Max oil temp above 30,500 ft

Answer 63

140 C

Question 64

Max transient oil temp

Answer 64

149C | 2 mins

Question 65

Min oil temp | Starting

Answer 65

-40 C

Question 66

Min oil temp | Takeoff

Answer 66

30 C

Question 67

Oil pressure limit | Takeoff, Max continuous and climb

Answer 67

65-80 psi

Question 68

Min oil pressure | Idle

Answer 68

49 psi

Question 69

Max transient oil pressure

Answer 69

100 psi

Question 70

Oil consumption rate

Answer 70

0.01 Gal per hour/15 hours

Question 71

Digital Electric Engine Computer (DEEC)

Answer 71

Required for flight

Question 72

Engine synchronizer switch

Answer 72

Off for takeoff

Question 73

Automatic performance reserve (APR)

Answer 73

Must be armed for takeoff | Except for crew training

Question 74

Wing fuel quantity

Answer 74

8,500 lbs

Question 75

Ventral fuel quantity

Answer 75

1,500 lbs

Question 76

Total fuel quantity

Answer 76

10,000 lbs

Question 77

Min fuel required with fuel in the ventral tank

Answer 77

3450 lbs/side

Question 78

Ventral fuel restriction before flight

Answer 78

Completely full or empty

Question 79

Wing fuel contents for ventral transfer

Answer 79

3,300 / side

Question 80

Max fuel temp

Answer 80

57C

Question 81

Airframe icing requirements

Answer 81

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

Question 82

Approved de-ice fluids

Answer 82

TKS80, R328, to fluid spec DTD 406B

Question 83

Ice detection lights requirements

Answer 83

Must be operational before FIKI at night

Question 84

Max temp for all regimes

Answer 84

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

Question 85

Min temp | Takeoff and landing

Answer 85

-40 C

Question 86

Min temp | Enroute

Answer 86

-75 C

Question 87

Max runway slope | Takeoff

Answer 87

+\- 2%

Question 88

Air brake usage

Answer 88

Flaps 0 only

Question 89

Cabin high datum selection

Answer 89

Limited to Airfields higher than 9,000 ft

Question 90

Inter-compartment door position

Answer 90

Open for takeoff and landing

Question 91

Lift dump use

Answer 91

Only when the aircraft is on the ground

Question 92

Max load factor | Flaps extended

Answer 92

2.0G

Question 93

Max load factor | Flaps retracted

Answer 93

2.73G

Question 94

Minimum flight crew requirement

Answer 94

2 pilots

Question 95

Max pressure differential

Answer 95

8.55 psi

Question 96

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

Answer 96

25 mins

Question 97

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

Answer 97

45 mins

Question 98

Rejected takeoff >90 KIAS | Requirement

Answer 98

Brake inspection

Question 99

Garrett GTCP36-150W APU | Normal operation

Answer 99

100%

Question 100

APU Max operating temp

Answer 100

1350 F

Question 101

APU Max operating altitude

Answer 101

30,000ft

Question 102

APU Max starting altitude

Answer 102

20,000ft

Question 103

APU Max transient Egt

Answer 103

1400-1500 F | 15 secs max

Question 104

APU starting cycle limits before shutdown

Answer 104

Between 50-95% rpm - 10 secs max | Shut down APU if "ready to load" light doesn't illuminate within 60 seconds of start

Question 105

APU starter cycle multi-attempt time limits

Answer 105

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

Question 106

APU Max generator limits for continuous operation

Answer 106

.80

Question 107

APU generator limit for transient operation

Answer 107

1.2 < 10 secs

Question 108

Combined bleed time limit

Answer 108

Shall not exceed 60 secs

Question 109

APU use in icing conditions

Answer 109

Not authorized

Question 110

APU ground deicing procedure

Answer 110

APU must be shut down for ground deicing

Question 111

APU operating restrictions during ground refueling

Answer 111

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