Limitations Flashcards

1
Q

Runway Slope limit

A

+/-2%

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2
Q

Max tailwind

A

15kts

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3
Q

Max operating altitude

A

43100ft (-300 & -200)

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4
Q

Max T/O and Landing altitude

A

8400ft (-300 & -200)

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5
Q

Turbulent Air Penetration Speed (severe turbulence)

A

-270kts below 25000ft
-280/0.82 (lower of) at 25000ft or above
(Maintain min 15kts above min manoeuvre speed when airspeed below 0.82

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6
Q

Max demonstrated crosswind limit for takeoff and landing

A

38kts

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7
Q

Limit on using HF radios

A

Do not operate during refuelling

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8
Q

Avoid weather radar operation in a hangar or within ___ ft of _____ or a ______ .

A
  • 50ft
  • Fueling operations
  • Fuel spill
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9
Q

Avoid weather radar operation when personnel are within area normally enclosed by _____

A

The aircraft nose radome

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10
Q

Max difference between altimeters and airfield elevation?

A

75ft

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11
Q

Does the standby altimeter meet RVSM criteria?

A

No

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12
Q

Main door emergency power assists and evacuation slide systems must be armed prior to ____, _____ and ______ whenever passengers are carried.

A
  • Taxi
  • Takeoff
  • Landing
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13
Q

How often does flight deck door access system need to be checked?

A
  • Once a day
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14
Q

Max taxi weight

A

352,441kgs (-300)

298,463kgs (-200)

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15
Q

Max takeoff weight

A

351,534kgs (-300)

297,556kgs (-200)

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16
Q

Max landing weight

A

251,290kgs (-300)

213,188kgs (-200)

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17
Q

Max ZFW

A

237,682kgs (-300)

199,580kgs (-200)

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18
Q

Which two 300s have a higher max ZFW and what is it?

A
  • ZK-OKR and ZK-OKS

- 239,950kgs

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19
Q

Min height for autopilot engagement

A

200ft AGL after takeoff

20
Q

Without LAND2 or LAND3 annunciated the autopilot must be disengaged below?

A

200ft AGL

21
Q

Do not use _____ on final approach below _____ feet AAL.

A
  • FLCH

- 1000ft

22
Q

Autoland maximum headwind, tailwind and crosswind

A
  • 25kts headwind
  • 15kts tailwind
  • 25kts crosswind (15kts company limit)
23
Q

Max glideslope angle

A

3.25deg

24
Q

Min glideslope angle

A

2.5deg

25
Q

Can autolands be made single engine?

A

Yes, with flaps 20 or 30

26
Q

What operational DATALINK messages are acceptable to be transmitted using the ‘COMPANY’ messages format?

A

Pre departure clearance, D-ATIS, TAF, Oceanic clearances, Weight and Balance, Take Off Data

27
Q

Max fuel tank temperature (-300 & -200)

A

49 deg C

28
Q

(-300) Fuel tank temp must not be lower than ____ deg C or ____ deg C above the fuel freeze point prior to takeoff, whichever is higher

A

-40 deg C

3 deg C above

29
Q

In flight fuel temperature must be maintained at least ___ deg C above the fuel freeze point of the fuel being used

A

3 deg C

30
Q

Does FSII change the min fuel tank temperature limit?

A

No

31
Q

(-200) Fuel tank temp must not be lower than ____ deg C or ____ deg C above the fuel freeze point prior to takeoff, whichever is higher

A

-37 deg C

3 deg C

32
Q

What are the engine oil temperature limits?

A

-200 only (RR) - min 40 deg C for engine starting and 50 deg C before advancing thrust levers to take off power

33
Q

Intentional selection of reverse thrust in flight is ______

A

Prohibited

34
Q

Backing the aircraft with the use of reverse thrust is ______

A

Prohibited

35
Q

(-300 only) For ground operation (exclusive of take off) in tailwinds and crosswinds between ____ and _____ kts engine power should be limited to a maximum of ____ .

A

Between 30-45kts

Maximum of 70% N1

36
Q

(-300 only) Avoid thrust levels above that required for normal taxi operation in all tailwinds and crosswinds greater than ____ kts

A

45kts

37
Q

APU starter cycle limit (electric starter and air turbine starter) is _ starte attempts in a __ minute period

A

3 attempts in a 60 minute period

38
Q

Must wait how many minutes between any electric or air turbine APU start attempt

A

1 minute

39
Q

Avoid ________ , especially in combination with large changes in _______ as they may result in structural failure at any speed, including below VA

A
  • large alternating control inputs

- changes in pitch, roll or yaw (e.g. large side slip angles)

40
Q

Maximum altitude with flaps extended

A

20000ft

41
Q

Ground wind limit for all doors

A
  • 40kts opening/closing

- 65kts open

42
Q

The ground maneuver cameras should not be used for ______, ________ and ________ .

A

Takeoff, approach and landing

43
Q

Should main tanks be full if centre tank fuel is loaded?`

A

Yes

44
Q

The centre tank may contain up to _____ kgs of fuel with less than full main tanks provided centre tank fuel weight plus ____ does not exceed ______ and ________ limits are observed.

A
  • 1360kgs
  • centre tank fuel plus actual ZFW does not exceed maximum ZFW
  • centre of gravity limits
45
Q

Runway width for 180deg turn?

A
(-300) = 56.1m
(-200) = 47.5m
46
Q

Where are crosswind limits annotated?

A

FCOM PD