Limitations (Other) Flashcards

To assess general knowledge of limitations and operational information that need NOT be memorised.

1
Q

Maximum runway slope?

A

+/-2%

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2
Q

Maximum Operating Altitude?

A

43,100 feet pressure altitude

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3
Q

Maximum Takeoff and Landing Altitude?

A

8,400 feet pressure altitude

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4
Q

Maximum “demonstrated” takeoff and landing crosswind from the AFM?

A

38 knots

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5
Q

Maximum allowable difference between Captain’s or First Officer’s altitude display and field elevation for RVSM operation?

A

75 feet

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6
Q

Does the standby altimeter meet the accuracy requirements for RVSM operation?

A

No

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7
Q

Takeoff crosswind limit on a DRY runway?

A

40 knots

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8
Q

Takeoff crosswind limit on a WET runway?

A

34 knots

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9
Q

Takeoff crosswind limit on a CONTAMINATED runway?

A

24 knots

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10
Q

Do gusts need to be considered for crosswind limitations?

A

Yes. The Emirates policy is to include the gust as part of the limit.

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11
Q

Below what weight must takeoff crosswind limits be reduced?

A

250,000 kg

Reduce crosswind limit by 1 knot for every 5,000 kg below 250,000 kg.

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12
Q

Greater than what CG must takeoff crosswind limits be reduced?

A

39% MAC

Reduce crosswind limit by 10 knots for CG greater than 39% MAC.

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13
Q

Landing crosswind limits are based on a runway of what width?

A

45 meters

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14
Q

Landing crosswind limit on a DRY runway?

A

45 knots

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15
Q

Landing crosswind limit on a WET runway?

A

40 knots

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16
Q

Landing crosswind limit on a runway CONTAMINATED with compact snow, dry snow or wet snow?

A

25 knots

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17
Q

Landing crosswind limit on a runway CONTAMINATED with slush or water?

A

17 knots

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18
Q

Landing crosswind limit on a runway CONTAMINATED with ice?

A

15 knots

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19
Q

Landing crosswind limit correction wherever asymmetric reverse thrust is used?

A

Reduce crosswind limit by 5 knots on wet and contaminated runways.

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20
Q

When is landing on untreated snow or ice to be attempted?

A

Only when no melting is present.

21
Q

Sideslip only (zero crab) landings are not recommended above what crosswind component?

A

28 knots

22
Q

What is the -200LR MTOW?

A

343,369 kg

23
Q

What is the -200LR MLW?

A

223,167 kg

24
Q

What is the -300ER MTOW?

A

340,194 kg

25
Q

What is the -300ER MLW?

A

251,290 kg

26
Q

What are the -300ER/ULR MTOWs? (2)

A

349,266 kg

351,534 kg

27
Q

What is the -300ER/ULR MLW?

A

251,290 kg

28
Q

The Flight Deck Access System needs to have an operational check once each flight day. How is compliance achieved?

A

Daily check by the engineer.

29
Q

Maximum cabin differential pressure (relief valves)?

A

9.1 psi

30
Q

Maximum allowable cabin pressure differential for takeoff and landing?

A

0.11 psi

31
Q

What flap setting(s) may be used for automatic landings during normal operations? (200LR, 300ER, 300 ER/ULR)

A

Flaps 30

32
Q

What flap setting(s) may be used for automatic landings during normal operations? (777F)

A

Flaps 30 or 25

33
Q

In what circumstances are automatic landings permitted using Flaps 20?

A

Only under certain non-normal conditions where flaps 20 is specified or recommended.

34
Q

What approach type(s) require the use of autothrottle?

A

Cat IIIB

35
Q

Can the Autoland System be used during overweight landings?

A

No. The Autoland System should not be used for landings above certified Maximum Landing Weight (MLW).

36
Q

What is the policy on electrical supply during ground operations?

A

Use dual electrical sources to power the aircraft during ground operations as much as possible.

If conditions permit, and two independent ground power sources are available, the APU should be switched off to conserve fuel.

37
Q

What are the limitations on the use of the COMPANY datalink format?

A

The datalink from the COMPANY format is limited to the transmission and receipt of messages, which will not create an unsafe condition if the message is improperly received, such as the following conditions:

  • the message or parts of the message are delayed or not received,
  • the message is delivered to the wrong recipient, or
  • the message content may be frequently corrupted.
38
Q

When must the handset on the aisle stand be used for normal cabin interphone and PA system communications?

A

Whenever the flight deck speakers are in use.

39
Q

On the 777F what must the Swift Broadband service not be used for?

A

ATC communications

40
Q

Maximum fuel tank temperature?

A

+49 degree C

41
Q

Minimum fuel tank temperature for takeoff?

A

-40 degrees C

or

3 degrees C above freezing point

42
Q

Minimum fuel tank temperature in flight?

A

In-flight tank fuel temperature must be maintained at least 3 degrees C above the freezing point of the fuel being used.

The use of Fuel System Icing Inhibitor additives does not change the minimum fuel tank temperature limit.

43
Q

Ground operation engine power limitations in tailwinds and crosswinds?

A

For ground operation (exclusive of takeoff) in tailwinds and crosswinds between 30 and 45 knots, engine power should be limited to a maximum of 70% N1.

Avoid thrust levels above that required for normal taxi operation in all tailwinds and crosswinds greater than 45 knots.

44
Q

Maximum number of APU start attempts?

A

3 starts attempts in a 60 minute period each.

45
Q

Wait time between APU start attempts?

A

1 minute

46
Q

When must the ground maneuver cameras not be used?

A

The ground maneuver cameras should not be used during takeoff, approach, and landing.

47
Q

ADIRU alignment must not be attempted above at latitudes greater than..

A

78 degrees 14.75 minutes

48
Q

When may the center fuel tank be loaded with fuel?

A

Main tanks must be scheduled to be full if center tank fuel is loaded.

Note: The center tank may contain up to 1360 kilograms of fuel with less than full main tanks provided center tank fuel weight plus actual zero fuel weight does not exceed the maximum zero fuel weight, and center of gravity limits are observed.

49
Q

Limitations on the use of terrain display?

A

Not to be used for navigation.