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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?

A

NO

48
Q

The Use of what Fuel is prohibited

A

JP-4 and JET B

49
Q

Maximum Tank fuel Temp

A

49C

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?

A

0

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?

A

45kts

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)

A

78,000lbs

63
Q

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

A

VHF-3

64
Q

Use what VHF # for primary communications the ground

A

VHF-1

65
Q

Maximum generator drive oil temp

A

157C

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)

A

YUP

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)

A

YUP

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)`

A

YUP

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

Initial (23 decks)

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