Limitations Flashcards

(52 cards)

1
Q

Maximum Ramp/Taxi Weight

A

768,000 lbs

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2
Q

Maximum Takeoff Weight

A

766,000

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3
Q

Maximum Landing Weight

A

575,000

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4
Q

Max Normal Taxi Speed

A

20 knots

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5
Q

Max Long, Straight Taxi Speed

A

30kts

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6
Q

Max Taxi Speed for Turn, Dry Surface

A

10kts

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7
Q

Severe Turbulent Air Penetration Speed Below 25,000’

A

270kts

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8
Q

Severe Turbulent Air Penetration Speed 25,000’ and Above

A

280 or .82M, whichever is lower

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9
Q

Maintain a minimum speed of ____kts above the minimum maneuver speed at all altitude when airspeed is below .82M

A

15kts

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10
Q

VFE Flaps 1

A

265kts

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11
Q

VFE Flaps 5

A

245kts

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12
Q

VFE Flaps 15

A

230kts

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13
Q

VFE Flaps 20

A

225kts

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14
Q

VFE Flaps 25

A

200kts

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15
Q

VFE Flaps 30

A

180kts

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16
Q

Landing Gear Operating Speed

A

270kts/.82M

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17
Q

Landing Gear Extended Speed

A

270kts/.82M

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18
Q

Max Tailwind for Takeoff, Landing, and Autoland

A

15kts

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19
Q

Max Headwind for Autoland

A

25kts

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20
Q

Max Crosswind for Takeoff

A

38kts (24) Dependent of TOGW & CG for Takeoff

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21
Q

Max Crosswind for Landing

A

38kts Sideslip Only are not recommended with landing Crosswind components in excess of 28kts

22
Q

Max Crosswind for Landing
Good to Medium

23
Q

Max Crosswind for Landing Medium

24
Q

Max Crosswind for Landing
Medium to Poor

25
Max Crosswind for Landing Poor
10kts
26
Max Crosswind for Landing Nil Braking
Operations Prohibited
27
Maximum Operating Altitude
43,100’ feet pressure altitude
28
Maximum Takeoff and Landing Altitude
9,800’ pressure altitude
29
30
APU to pack takeoffs are prohibited at airport pressure altitudes above
6,900’
31
Icing Conditions Exist when
OAT on the ground and for takeoff or TAT in flight is 10° or below and visible moisture in any form is present. Visible moisture is a form of precipitation such as clouds, fog with visibility of one mile or less, rain, snow, sleet or ice crystals. When operating on ramps, taxiways or runways where surface snow, ice, standing water or slush may be infested by the engines or freeze on engines, nacelles or engine sensors probes. Indicated in-flight by the primary ice detection system.
32
Do not use the autopilot below 100’ RA at airport field elevations above
8,500’
33
The autopilot must not be engaged below, a minimum engage altitude of ______ ‘ AGL after takeoff
500’
34
If autoland status annunciation does not display LAND 2 or LAND 3, the autopilot must be disengaged below ______ AGL
200’
35
For flaps 25 approach, the autopilot must be disengaged below _____’ AGL
100’
36
Do not use FLCH on final approach below ______ feet airport field elevation
1,000’
37
Autoland is approved with:
Flaps 20 or 30 Both engines operative, or one engine operative. Land two or land three displayed on the AFDS status annunciation
38
Autoland is not approved with: Flaps _______ __________ EICAS message displayed
Flaps 25 and/or Slats Drive EICAS Message
39
Autoland is required for:
CAT 3 & CAT 2 (FX) Approaches
40
CAT 3 & CAT 2 Approaches are not authorized with any of the following EICAS messages displayed:
SGL Source Displays SGL Source RAD ALT Single Source ILS
41
Do not operate HF radios during:
Refueling operations
42
Engine EGT Limitation: Ground Start
750°C
43
Full rated takeoff and go around thrust ratings are limited to:
5 minutes, or 10 minutes in the event of loos of thrust on one engine
44
Derated Takeoff and Reduced Takeoff thrust is not allow for:
Alternate EEC Mode Operation
45
Use of reduced thrust is not allowed when the runway is:
Contaminated
46
Position reverse thrust levels, full down (forward thrust) only after engines have:
Decelerated to reverse idle
47
Engine Oil - Minimum Oil Pressure
10PSI
48
When OAT is 3° or below during ground operations, (including taxi-in and taxi-out) the engine must be run up momentarily to a minimum of:
50% N1 at intervals not to exceed 60 minutes
49
APU starter motors duty cycle for the electric starter motor and air turbine starter is:
3 Start Attempts in a 60 minute period each.
50
Do not extend flaps above ________ feet
20,000’
51
Prior to takeoff the maximum allowable difference between Captains or First Officers altitude, display, and field elevation is:
75’
52
For Low Visibility Takeoffs requiring the use of HUD takeoff guidance mode(RVR < 500 feet/150 m actual or report visibility
The FPV must be caged The maximum crosswind is 15kts