Limitations Flashcards

1
Q

Max Runway Slope

A

+/- 2% -

FCOM Vol. 1 L.10.2

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2
Q

Maximum takeoff and landing tailwind component

A

10 knots

FCOM Vol. 1 L.10.2

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3
Q

Maximum demonstrated T/O and Landing crosswind

A
  • 400 = 35kts
  • 800 = 33kts

FCOM Vol. 1 L.10.2

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4
Q

Maximum Speeds

A

Observer VMO Pointer and gear / flap placards

FCOM Vol. 1 L.10.2

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5
Q

Maximum flight operational latitude

A
  • 400 = 73N and 60S
  • 800 = 82N and 82S

FCOM Vol. 1 L.10.2

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6
Q

Maximum operating altitude

A
  • 400 = 37000ft
  • 800 = 41000ft

FCOM Vol. 1 L.10.2

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7
Q

Severe Turbulent Air Penetration Speed (whatever is lower)

A
  • 400 = 264KIAS or .65M
  • 800 = 280KIAS or .76M

In cruise: SP.16 Supplementary Chart
FCOM Vol. 1 L.10.2

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8
Q

On revenue flights what must be installed regarding L1 Door

A

The escape slide retention bar (grit bar), taxi, takeoff, landing

FCOM Vol 1 L.10.3

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9
Q

What must not be operated during refueling operations

A

HF Radios

FCOM Vol 1 L.10.3

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10
Q

Max allowable in-flight difference between captain and FO altitude display for RVSM

A

200ft

FCOM Vol 1 L.10.3

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11
Q

Maximum allowable on the ground altitude display differences for RVSM operations

A

-400:
Sea level = 40ft for Captain/FO
5000ft = 45ft for Captain/FO
10000ft = 50ft for Captain/FO

-800:
Sea level to 5000ft = 50ft
5000ft to 10,000ft = 60ft

Maximum difference between Capt/FO/Ground for all = 75ft

FCOM Vol 1 L.10.3

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12
Q

Weight Limitations (800) Max Taxi

A

174,700lbs

AFM or FCOM Vol 1 L.10.4

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13
Q

Weight Limitations (800) Max Takeoff

A

174,200lbs

AFM or FCOM Vol 1 L.10.4

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14
Q

Weight Limitations (800) Max Landing

A

146,300lbs

AFM or FCOM Vol 1 L.10.4

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15
Q

Weight Limitations (800) Max Zero Fuel

A

138,300lbs

AFM or FCOM Vol 1 L.10.4

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16
Q

Weight Limitations (800) Min Operating

A

80,800lbs

AFM or FCOM Vol 1 L.10.4

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17
Q

Max differential pressure (400)

A

8.65 PSI

AFM or FCOM Vol 1 L.10.4

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18
Q

Max differential pressure (800)

A

9.1 PSI

AFM or FCOM Vol 1 L.10.4

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19
Q

Flight with freight in the Main Deck Cargo Compartment without at least one air conditioning pack is ? (400)

A

Prohibited

AFM or FCOM Vol 1 L.10.4

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20
Q

Use of Aileron trim with the autopilot engaged is

A

Prohibited

AFM or FCOM Vol 1 L.10.5

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21
Q

(400) Do not engage the autopilot below what ALT

A

1000ft AGL

AFM or FCOM Vol 1 L.10.5

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22
Q

(800) Do not engage the autopilot below what ALT

A

400ft AGL

AFM or FCOM Vol 1 L.10.5

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23
Q

For single channel operating during approach, when shall the autopilot be disengaged

A

50ft AGL

AFM or FCOM Vol 1 L.10.5

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24
Q

MAX Wind Component for Autoland (400)

A

Headwind: 25kts
Tailwind: 10kts
Crosswind: 15kts
Crosswind CAT2/3: 15kts

AFM or FCOM Vol 1 L.10.5

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25
Q

MAX Wind Component for Autoland (800)

A

Headwind: 25kts
Tailwind: 10kts
Crosswind: 20kts
Crosswind CAT2/3: 15kts

AFM or FCOM Vol 1 L.10.5

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26
Q

MAX and MIN glideslope angle for for autoland

A

2.5 to 3.25 degrees

AFM or FCOM Vol 1 L.10.5

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27
Q

Autoland flap and engine requirements

A

Flaps 30 or 40 // both engines operative

AFM or FCOM Vol 1 L.10.5

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28
Q

Are autolands authorized on the 400LF? What about the normal 400?

A

NOPE

YUP

AFM or FCOM Vol 1 L.10.5

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29
Q

When can you not use LVL Change on approach?

A

Do not use below 1000 AFE

AFM or FCOM Vol 1 L.10.5

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30
Q

Engine limit display markings (What colors)

A
Red = max and min limits
Amber = caution limits

AFM or FCOM Vol 1 L.10.7

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31
Q

Maximum time limit for takeoff thrust

A

5 mins

AFM or FCOM Vol 1 L.10.7

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32
Q

Engine Ignition must on AUTO/CONT for what phases

A

T/O
Landing
Anti-ice operation and
(800) operation in heavy rain

AFM or FCOM Vol 1 L.10.8

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33
Q

Operation with Assumed temperature reduced takeoff is not permitted with what INOP

A

Anti-skid inoperative

AFM or FCOM Vol 1 L.10.8

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34
Q

Reverse Thrust is not permitted when

A

in-flight

AFM or FCOM Vol 1 L.10.8

35
Q

APU Max config ALT’s

A
APU bleed + electric load = 10,000ft
APU bleed = 17,000ft
APU Electrical Load = 
400 - 35000ft
 800 - 41000ft

AFM or FCOM Vol 1 L.10.9

36
Q

(800) Normal Starter duty cycle

A

Multiple consecutive start attempts are permitted, each start attempt limited to 2 minutes of starter usage

minimum of 10 seconds is needed between start attempts

(400)
minimum of 20 seconds in between start attempts

3 minutes needed between second and subsequent attempts

AFM or FCOM Vol 1 L.10.9

37
Q

(800) Extended Engine Motoring

A

Starter usage is limited to 15 mins for the first two extended engine motorings. a minimum of 2 mins is needed between each attempt.

For the third and subsequent extended motorings, starter usage is limited to 5 mins. a minimum of 10 mins is needed between each attempt

AFM or FCOM Vol 1 L.10.9

38
Q

APU bleed valve must be closed when?

Can APU bleed valve be open during engine start?

A
  • Ground air connected and isolation valve is open
  • engine no.1 bleed valve open
  • isolation and engine no.2 bleed valve open

APU bleed valve may be open during engine start, but avoid engine power above idle

AFM or FCOM Vol 1 L.10.10

39
Q

After 3 consecutive APU aborted start attempts, how long is the cooling period required (800)

A

15 mins

AFM or FCOM Vol 1 L.10.10

40
Q

The max alt for flaps extended is ?

A

20,000ft

AFM or FCOM Vol 1 L.10.10

41
Q

Holding in ICE conditions with flaps extended is ?

A

Prohibited

AFM or FCOM Vol 1 L.10.10

42
Q

In flight do not extended the speed brakes past what point?

A

Flight Detent

AFM or FCOM Vol 1 L.10.10

43
Q

Rapid and large alternating control inputs may result in what?

A

Structural failure at any speed, including below VA

AFM or FCOM Vol 1 L.10.10

44
Q

Do not deploy speedbreaks below what ALT ?

A

1000ft RA

AFM or FCOM Vol 1 L.10.11

45
Q

Alternate Flap Duty Cycle

A

when extending or retracting flaps, allow 15 seconds after releasing the ALTERNATE FLAPS position switch before moving the switch again to avoid damage to ALTERNATE FLAP motor clutch

After a complete extend and retract cycle 0-15 and back to 0 allow 5 mins for cooling before trying again

46
Q

Avoid WX radar operation in what or around what

A

In a hanger / within 50ft of fueling operations or fuel spill

47
Q

If a fuel pump circuit break trips, can you reset it?

48
Q

The Use of what Fuel is prohibited

A

JP-4 and JET B

49
Q

Maximum Tank fuel Temp

50
Q

inflight tank fuel temp must be what in flight?

A

3C must be maintained above the freezing point of the fuel used or -43C (800) -45C (400) whichever is higher

51
Q

What fuel is allowed

A

JET A, JET A-1, JP-5, JP-8

52
Q

Intentionally dry running the center tank fuel pump (low pressure light illuminated) is?

A

prohibited

53
Q

Maximum scheduled lateral fuel imbalance is?

54
Q

Random later fuel imbalance is ? Taxi, T/O, Flight, Landing

A

1000lbs / 453KGs

55
Q

Main tanks must have how much fuel if the center tank contains more than ?

A

full / 1000lbs

56
Q

Do not open the main deck cargo door in actual or anticipated winds exceeding?

57
Q

MAX start EGT

A

(400) 725C
(800) red line but equates to 725C

AFM or FCOM Vol 1 L.10.8

58
Q

MAX Taxi weight (-400 except 311GT)

A

144,000lbs

59
Q

MAX takeoff weight (-400 except 311GT)

A

143,500lbs

60
Q

MAX landing weight (-400 except 311GT)

A

121,000lbs

61
Q

MAX zero fuel weight (-400 except 311GT)

A

113,000lbs

62
Q

Minimum Operating Weight (-400 except 311GT)

63
Q

Do not use what VHF # for ATC communications with ACARS operational

64
Q

Use what VHF # for primary communications the ground

65
Q

Maximum generator drive oil temp

66
Q

MAX N1 RPM (400)

A

106%

AFM or FCOM Vol 1 L.10.8

67
Q

MAX N2 RPM (400)

A

105%

AFM or FCOM Vol 1 L.10.8

68
Q

MAX T/O EGT (400)

A

930°

AFM or FCOM Vol 1 L.10.8

69
Q

MAX Continuous EGT (400)

A

895°C

AFM or FCOM Vol 1 L.10.8

70
Q

Minimum Oil Pressure

A

13 psi

AFM or FCOM Vol 1 L.10.8

71
Q

MAX Oil Temp

A

165C

160C-165 Allowable for 15 mins

160C maximum continuous

AFM or FCOM Vol 1 L.10.8

72
Q

Both PMC/s must be either (Blank) or (blank) for takeoff (400)

A

OFF or On

AFM or FCOM Vol 1 L.10.8

73
Q

APU MAX start EGT (400)

A

760C

AFM or FCOM Vol 1 L.10.9

74
Q

APU Max continuous EGT (400)

A

710C

AFM or FCOM Vol 1 L.10.9

75
Q

APU can operate up to ? (400)

A

37000ft

AFM or FCOM Vol 1 L.10.9

76
Q

Pneumatic pressure for start PSI (400)

A

30PSI at sea level, decreasing 1/2 PSI per 1000ft

AFM or FCOM Vol 1 L.10.9

77
Q

If there are multiple aborted start attempts of the APU, (blank) mins cooling is required between the 2nd and 3rd attempt. how many is needed after the 3rd failed attempt (400)

A

5 mins // 1 hour

AFM or FCOM Vol 1 L.10.10

78
Q

Should you Functionally operate the Main Cargo Compartment Air Supply Shutoff vale prior to each flight or each series of flights by the same crew on the same day? (400)

79
Q

Should the Main Deck Cargo compartment Smoke Detector System be inspected prior to each flight or each series of flights by the same crew on the same day? (400)

80
Q

Should you do a preflight inspection of the Secondary Main Landing Gear Position Indicating System prior to each flight or series of flights by the same crew on the same day (400)`

81
Q

Maximum T/O and LDG Altitude

A

8,400

FCOM Vol. 1 L.10.2

Also, -400F aircraft with CABIN ALTITUDE and TAKEOFF config lights, as well as a High Altitude Landing Switch have a maximum of 9,000 feet pressure altitude.

FCOM Vol 1 L.10.3

82
Q

-400LF and -800 what operational check must be done once each flight day?

A

Flight Deck Door Access System Check

FCOM Vol. 1 L.10.2

83
Q

When can yo not operate one or both engine bleed air switch on HIGH

A

Takeoff, Approach, Landing

AFM or FCOM Vol 1 L.10.5