Limitations Flashcards

1
Q

Maximum Taxi Weight

A

79,242kg
VYA - VZE
75,296kg

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2
Q

Maximum Takeoff Weight

A

79,015kg
VYE - VZE
75,069kg

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3
Q

Maximum Landing Weight

A

66,360kg

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4
Q

Maximum Zero Fuel Weight

A

61,688kg
VZF - XZP
62,731kg

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6
Q

Runway slope

A

+/- 2%

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7
Q

Maximum tailwind component for takeoff and landing

A

15kt

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8
Q

Maximum operating altitude

A

41,000ft

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9
Q

Maximum takeoff and landing altitude

A

8,400ft

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10
Q

Operations on Narrow Runways
No dispatch
Diversion required

A
No dispatch
- nose wheel steering inoperative
- one reverser inoperative
Diversion required
- jammed or restricted flight controls
- trailing/leading edge flap or slat asymmetry
- loss of system A or B hydraulics
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11
Q

HF radios

A

Do not operate HF radios during refuelling operations

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12
Q

RVSM Altimetry
Max inflight difference

Max on ground difference

A

Max inflight difference
200ft

Max on ground difference
Sea level to 5000ft - 50ft/75ft
5001ft to 10000ft - 60ft/75ft

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13
Q

Air conditioning pack restrictions

A

With one or both engine bleed switches ON do not operating the air conditioning packs in HIGH for takeoff, approach or landing.

Non-normal procedures take precedence

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14
Q

Maximum cabin differential pressure

A

9.1 psi

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15
Q

Autopilot/Flight director
Aileron trim
Minimum autopilot engagement takeoff
Single channel operations

A

Use of aileron trim with autopilot engaged is prohibited
Minimum - 400ft
Single channel operation autopilot shall not remain engaged below 50ft AGL

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16
Q

Autoland operations
Maximum HW
Maximum XW
Maximum TW

Landing flaps

A

Headwind - 25kt
Crosswind - 20kt
Tailwind - 15kt

Autoland capability may only be used with flaps 30 or 40 with both engine operating

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17
Q

Maximum and minimum glideslope angles

A
  1. 25 degrees

2. 5 degrees

18
Q

LVL CHG

A

Do not use LVL CHG on final approach below 1000ft AFE

19
Q

Engine Ignition must be on

A

Engine ignition must be on for

  • takeoff
  • landing
  • operation in heavy rain
  • anti-ice operation
20
Q

Reverse Thrust

A

Intentional selection of reverse thrust in flight is prohibited

21
Q

APU bleed valve must be closed

A
  • ground air connected and isolation valve open
  • engine no 1 bleed valve open
  • isolation and engine no 2 bleed valve open
    Except during engine start, but avoid engine power above idle
22
Q
APU limitations
APU bleed and electrical
APU bleed and electrical on ground
APU bleed
APU electrical
A

Bleed & elec (in air) - 10,000ft
Bleed & elec (on ground) - 15,000ft
Bleed only - 17,000ft
Electrical - 41,000ft

23
Q

APU start limitation

A

3 consecutive attempts 15 min cooling period required

24
Q

Flight controls
Max alt with flaps extended
Holding in icing
Speed brake

A

Max alt with flaps extended - 20,000ft
Holding in icing - not permitted
Speed brake - not beyond FLIGHT DETENT in flight, not extended below 1,000ft RA

25
Q

Alternate flap extension
Time between moving switch
Cooling time

A

Time between moving switch - 15s

Cooling time extend/retract cycle 0-15-0 5 minutes

26
Q

Weather Radar

A

Avoid operation in hanger or within 50ft fuelling operations or fuel spill
Or when personnel are within the area normally enclosed by the radome

27
Q

Maximum fuel temperature

A

49 degrees Celsius

28
Q

Minimum fuel temperature

A

-43 degrees or 3 degrees above the fuel freezing point whichever is greater

29
Q

Maximum fuel imbalance

A

Must be scheduled to zero

Maximum 453kg for taxi, takeoff, flight or landing

30
Q

Fuel loading

A

Main tanks must be full of centre tank contains more than 453kg

31
Q

Anti skid inop

A

Assumed temperature takeoffs not permitted

32
Q

Brakes

A

Do not apply until after touchdown

33
Q
Wind limitations
Dry
Wet
Asymmetric reverse thrust
RVR
A

Dry - 33kt
Wet - 25kt
Asymmetric reverse thrust, reduce by 5kt on wet/contaminated

34
Q

Flight manoeuvring loads
Flaps up
Flaps down

A

Flaps up +2.5g to -1.0g

Flaps down +2.0g to 0.0g

35
Q

Max fuel:
Main tank
Centre tank

A

Main tank - 4147kg

Centre tank - 13843kg

36
Q

Engine RPM
Maximum N1
Maximum N2

A

Maximum N1 - 104%

Maximum N2 - 105%

37
Q

Maximum EGT
Takeoff
Maximum continuous
Starting

A

Takeoff - 950 degrees maximum 5 minutes/10 minutes EOI
Maximum continuous - 925 degrees
Starting - 725 degrees

38
Q

Severe Turbulence Air Penetration speed

A

280KIAS/.76 Mach

39
Q
HGS Wind Limitations
HW
XW
TW
Field Elevation
A
HGS Wind Limitations
HW - 25kt
XW - 15kt
TX - 10kt
Field Elevation - 5,500ft