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Limitations (FCOM and Policy) Flashcards

1
Q

Runway Slope

A

+- 2%

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2
Q

Maximum T/O & Ldg Tailwind Component

A

15 Knots

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3
Q

Maximum T/O & Ldg Altitude

A

8400 feet

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4
Q

Ground Wind Operating Envelope (MAX)

A

Crosswinds > 43kt - Limit thrust to normal taxi
Winds > 58kt - Limit thrust to idle except when
setting T/O thrust

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5
Q

Runway < 45m wide- dispatch not allowed for

A

Nose gear Steering inop
One thrust reverser inop

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6
Q

If possible, don`t divert to an alternate <45m wide in case of which of the following?

A
  • Jammed or restricted flight controls
  • Trailing edge flap asymmetry
  • LE flap/slat asymmetry
  • Loss of system A or B hydraulics
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7
Q

Severe turbulent air penetration speed

A

Climb: 280 knots/ .76M, whichever is lower

Cruise: Use FMC recommended thrust​ settings. If​ the FMC ​is inoperative, refer to the Unreliable Airspeed​ page ​in the Performance–Inflight section of the QRH for ​approximate​ N1​ settings that maintain​ near optimum ​penetration airspeed

Descend: .76 Mach/280/250 knots, whichever is lower. If ​severe turbulence is encountered​ at altitudes below ​15,000 feet​ and the airplane gross weight​ is less than ​the maximum landing weight, the airplane may be​ ​slowed​ to 250​ knots in the clean​ configuration.

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8
Q

Operation of radios during refueling

A

Do not operate HF Radios during refueling

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9
Q

Altitude display limits for RVSM in-flight

A

200 feet between Captain and FO

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10
Q

Altitude display limits for RVSM on ground

A

Both altimeters and Field Elevation- 75 feet

Difference between CA and FO altimeters

Sea level to 5000 feet: 50ft
5001 feet to 10 000 feet: 60ft

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11
Q

Maximum cabin differential press (relief valves)

A

9.1 psi

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12
Q

With either one or both engine bleed air switches ON-

A

Don`t operate the packs in HIGH for T/O, app or Ldg

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13
Q

A/P Minimum altitude use T/O and Ldg

A

Do not engage below 400ft AGL on T/O
Disengage before 50ft AGL on Ldg (single channel)

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14
Q

LVL CHG restriction

A

Do not use on final app below 1000` AFE

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15
Q

Engine Ignition must be on for:

A
  • T/O
  • Ldg
  • operation in heavy rain
  • anti-ice operation
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16
Q

APU Max Alt: Inflight Bleed+ Electrical

A

10 000 feet

17
Q

APU Max Alt: Bleed

A

17 000 feet

18
Q

APU Max Alt: Electrical

A

41 000 feet

19
Q

APU Aborted Start cooling period

A

15 minutes following 3 consecutive aborted start attempts

20
Q

Speed Brakes

A

Do not extend beyond FLIGHT detent in flight

Do not use speed brake below 1000 feet Above the Surface

Do not use speed brake below 1000 feet Radar altitude

Do not extend beyond ARMED with F40
(Flydubai this limit is flap greater than 10)

21
Q

Alternate Flap Duty Cycle

A

Allow 15 seconds after releasing the switch

Allow 5 minutes cooling after a complete extend/retract cycle

22
Q

GPWS- when not to use

A

Don`t use within 15nm of T/O, App or Ldg at any airport not in the database

23
Q

Overrun Warning (ORW) inhibit when:

A
  • Ldg OAT on the ground is below - 40º C or
    greater than 50º C
  • GW is greater than MLW

Check, there is a bulletin for this as well

24
Q

Max and min tank fuel temp

A
  • Maximum 49º C
  • Minimum - 43º C or 3º C above fuel freezing
    point temp
25
Q

Is intentional dry running of a center tank fuel pump allowed?

A

No

26
Q

Fuel imbalance between main wing tanks for taxi, takeoff, flight or landing must ​not​ exceed _____

A

453 kg

27
Q

Main tanks must be full if center tank contains more than-

A

453kg

28
Q

Landing gear only lim

A

Don`t apply brakes until after touchdown

29
Q

No Assumed Temp 9 reasons

A

Antiskid Inop
EEC in alternate mode
Contaminated runway
Low vis T/O
Windshear
Gusty Crosswind conditions
De-icing/Anti-icing Performed
Temperature inversion
Rough or poor rwy conditions(not
recommended)

30
Q

Derate 2 restrictions

A

EEC in Alternate mode
Windshear

31
Q

IAN maximum GP angle

A

3.77 º

32
Q

Required Visibility/RVR for T/O (Non LVTO)

A

Table in OM-A 8.1.3.2.1. Day and night with facilities is 400m but 500m in day only with nil facilities

33
Q

Use VHF 1 (antenna on top of fuselage) when?

A

For primary ATC comms on the ground

34
Q

Flight Manoeuvring Load Acceleration Limits (AFM)- not mem item

A

Flaps Up: +2.5g to -1.0g
Flaps Down: +2.0g to 0.0g

35
Q

Minimum fuel for​ ground operation of hyd electric motor-driven ​pumps is?

A

760 Kgs in​ the related main tank

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