FCOM Flashcards

1
Q

When is the probe heat required to function properly

A

For IFR flight and flight into known icing conditions

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2
Q

Autopilot minimum use heights
takeoff/climb
enroute
APV/ILS
Non-precision

A

400
1000
200
400

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3
Q

maximum approved glideslope angle for all coupled approaches

A

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4
Q

maximum approved VNAV/VPATH coupled descent angle

A

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5
Q

Minimum O2 supply for each occupant above FL250

A

10 minutes

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6
Q

To allow adequate cooling of the wheels and brakes the aircraft must remain on the ground for how long following what 2 events

A

45 minutes
- rejected takeoff with brake on speed greater than Vr -20 kts and heavy brake usage
- 0° flap full stop landing with heavy brake usage

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7
Q

deice boot temperature limitations

A

-40 to 40° C

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8
Q

flap limits with and without pneumatic boots

A

15° with
0° without

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9
Q

outside air temp limitations

A

-50 to 55° C

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10
Q

maximum cabin differential pressure and pressurized landing PSI limit

A

5.75 and .7

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11
Q

max operating altitude with 2 pilots

A

FL280

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12
Q

starter operating limitations

A

60 sec
60 sec
30 min

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13
Q

flight load limitations

A

flaps up +3.3, -1.32g
flaps down +2.0, -0.0g

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14
Q

max ramp weight
max takeoff weight
max landing weight
max zero fuel weight

A

10495
10450
9921
9039

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15
Q

max torque takeoff/climb

A

44.34

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16
Q

max torque cruise

A

36.95

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17
Q

max torque transient (limit)

A

61 limited to 20 sec

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18
Q

max torque reverse

A

34.25

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19
Q

max itt takeoff

A

850

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20
Q

max itt climb/cruise

A

820

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21
Q

max its starting

A

1000 limited to 5 sec

22
Q

max itt reverse

A

760° C

23
Q

max itt reverse

A

760

24
Q

max Ng takeoff/climb/cruise/transient

A

104%

25
Q

max Np transient

A

1870 limited to 20 sec

26
Q

max reverse Np

A

1650

27
Q

oil pressure takeoff/climb/cruise/reverse

A

90 to 135 PSI

28
Q

max oil pressure starting

A

200

29
Q

oil pressure transient

A

40 to 200 limited to 20 sec

30
Q

oil temp climb/cruise/reverse

A

10 to 105

31
Q

oil temp takeoff

A

10 to 110

32
Q

oil temp limit starting

A

-40

33
Q

gen 1/2 max continuous load/max load for 2 min

A

300 and 450

34
Q

oil capacity

A

3.6 gal

35
Q

oil operating range

A

1 gal

36
Q

approved fuel grades

A
37
Q

anti ice additive required below

A

0°C

38
Q

total fuel capacity

A

406.8

39
Q

total usable fuel

A

402

40
Q

total unusable fuel

A

4.8

41
Q

maximum fuel imbalance

A

26.4 gal / 3 segments / 178 pounds

42
Q

Vmo
Mmo
Vo
Vfe
Vlo
Vle

A
43
Q

cabin altitude`

A

oxygen lever on
oxygen masks on
go to QRH

44
Q

pitch trim runaway

A

Trim interrupt switch
go to QRH

45
Q

Fire, smoke or fumes in the cockpit

A

oxygen lever on
masks and smoke goggles on
crew oxygen to emgcy
vent valve open
go to QRH

46
Q

engine failure in flight total power loss

A

SPD (best glide)
HDG to airport
PCL idle
condition lever cutoff/feather
go to QRH

47
Q

engine failure after rotation gear down

A

land straight
flaps 40
DSB
PCL idle
condition lever cutoff
fuel emergency shutoff

48
Q

engine failure after rotation gear up

A

gear down if appropriate
flaps 40
DSB
PCL idle
condition lever cutoff
fuel emerg shutoff

49
Q

max rate descent

A

PCL idle
gear down
Mmo
go to QRH

50
Q

inadvertent pusher operation

A

hold against pusher action
pusher interrupt button
go to QRH