Limitations Flashcards

1
Q

Maximum Runway Slope

A

+/- 2%

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2
Q

Maximum Takeoff and Landing Tailwind Component

A

15 Knots

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3
Q

Maximum Operating Altitude

A

45,100 feet pressure altitude

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4
Q

Maximum Takeoff and Landing Altitude

A

10,000 feet pressure altitude

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5
Q

Maximum Field Elevation

A

9,500 feet pressure altitude

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6
Q

Maximum speed Operating in RVSM Airspace

A

0.90 Mach

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7
Q

Turbulent Air Penetrating Speed

A

290 KIAS to 310 KIAS or
0.82 Mach to 0.85 Mach
Whichever is LOWER

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8
Q

Maximum Takeoff and Landing Crosswind

A

30 KIAS (not limiting)

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9
Q

DO NOT USE H.F. Radio’s During _________

A

refueling

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10
Q

Avoid Weather Radar use within ___ of Fuel Spill

A

50’

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11
Q

Maximum in-flight Difference between Captain and F/O Altitudes for RVSM

A

200 feet

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12
Q

Maximum on-ground difference between Captain and F/O Altitudes for RVSM

A
Field Elevation  Max. Difference between 
Captain and F/O
Max Difference between Captain, F/O and Field Elevation
Sea Level to 5,000’
35 feet
75 feet
9,500 feet
40 feet
75 feet
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13
Q

Emergency evacuation slide must be in ________ mode and knob must be visible prior to Taxi, Takeoff and Landing

A

AUTOMATIC

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14
Q

Maximum Taxi Weight

A

395,986 Kilograms

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15
Q

Maximum Takeoff Weight

A

394,625 Kilograms

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16
Q

Maximum Landing Weight

A

295,742 Kilograms

17
Q

Maximum Zero Fuel Weight

A

276,691 Kilograms

18
Q

Maximum Differential Pressure

19
Q

Maximum Allowable Cabin Differential Pressure for Takeoff and Landing

20
Q

If Pack _ available, Do NOT move the Pack 3 Control Lever to ___ during normal ground operations unless Pack _ and _ are selected OFF

A

3, OFF, 1 and 2

21
Q

Use of aileron trim with autopilot engaged is ______

A

prohibited

22
Q

Autopilot must NOT be engaged below

A

250’ AGL after takeoff

23
Q

Autopilot must be disengaged before descending more than

A

50’ below MDA unless coupled to ILS glideslope or in GA mode

24
Q

For Single channel ILS approach, autopilot must be disengaged before descending below

A

100’ AGL

25
Do NOT use FLCH on Final Approach below
1000’ AFE
26
Maximum allowable wind speeds when weather minima are predicted on autoland operations:
Headwind 25 Knots Tailwind 15 Knots Crosswind 25 Knots
27
Maximum and Minimum Glideslope angles:
Maximum: 3.25 degrees Minimum: 2.5 degrees
28
Autoland with Flaps
25 or Flaps 30 ONLY
29
Maximum Fuel | Temperature: (Jet A, Jet A-1, JP-5 or JP-8)
54°C (130°F) | Must be maintained at least 3°C above Fuel Freezing point
30
Continuous Ignition must be ON for:
* Heavy Rain * Severe Turbulence • Volcanic Ash * Icing Conditions * Standing Water or Slush on Runway
31
Thrust Reversers in Flight is _________?
Prohibited
32
Backing airplane with use of Thrust Reversers is ____?
Prohibited
33
If leveling off within _____ after changing altimeter setting from QNE to QNH, or QNH to QNE, do NOT use _____ to execute level off if QNH is less than __.__ in / 1006 hPa.:
2,000’, VNAV, 29.70
34
Avoid rapid and large alternating control inputs, especially in combination with large changes in _____
pitch, roll or yaw
35
Maximum Flap extension:
20,000 '
36
Use of Speedbrakes in flight with flaps extended beyond ____ is NOT recommended
20
37
Do NOT use terrain display for
Navigation
38
The use of Look-ahead terrain alerting and terrain display function is prohibited within
15 nm of takeoff, approach or landing at airport or runway not contained in GPWS database.