Limitations Flashcards

(33 cards)

1
Q

Max pressure altitude

A

41,000

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2
Q

Max takeoff and Landing tailwind

A

15 kts

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3
Q

Gear retraction

A

235 kts

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4
Q

Gear extension

A

270/.82

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5
Q

Gear operating

A

320/.82

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6
Q

Turbulence penetration cruise

A

Turbulence N1 from cruise page

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7
Q

Turbulence climb and descent

A

280 / .76

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8
Q

Severe turbulence below 15,000’

A

gross weight less than max landing weight and clean the aircraft may be slowed to 250 kts

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9
Q

Crosswind Component

A

Condition Code. Takeoff. Landing

6. dry * 33 37
5 wet * 25 37
4. comp snow. 22. 35
3 slippery dry/wet snow 20 25
2. water/slush >1/8" 15 17
1. wet ice/ water on top snow. 13 15
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10
Q

Max cabin differential pressure

A

9.1 psi

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11
Q

Max Differential Pressure

A

.125 psi

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12
Q

Duct pressure max cooling

A

20-25 psi

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13
Q

Icing conditions exist on the ground

A

10 C or less
visible moisture
vis less than 1 mile
ramp, taxiway, runway snow standing water or slush

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14
Q

Icing conditions exist in flight

A

10 C
visible moisture
visibility less than 1 mile

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15
Q

Moderate / Heavy freezing rain or Hail

A

Takeoff is prohibited

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16
Q

Minimum Autopilot engagement

17
Q

Autoland wind limits

A
Headwind 25 kts
Crosswind 15 kts
Tailwind 10 kts
900 Flaps 30
elevation less than 4000' 10 kts
elevation 4001-6000' 5 kts
elevation 6001 and greater 0 kts
18
Q

Minimum use for autopilot ILS/GLS no autoland

19
Q

Minimum use for autopilot non precision

A

50” below MDA/DA

20
Q

Autoland shall not be used for

A

overweight landings

21
Q

Autothrottle must be disconnected by

A

50’ AGL unless Autoland

22
Q

Starter Duty Cycle

A

Multiple attempts permits
limited to 2 minutes
limited to 3 minutes on the MAX
minimum of 10 seconds between start attempts

23
Q

Reduced thrust limits

A

not authorized with anti skid inoperative

not permitted on runway contaminated with standing water, ice, slush, or snow

24
Q

APU starter duty cycle

A

15 minutes cooling required after 3rd start attempt

25
APU shutdown
wait for a minimum of 120 seconds / 2 minutes for the shutdown cycle to complete before turning the battery off
26
Engine fire extinguisher bottle pressure
800 psi @ 70 F
27
Speed brake lever operation
Do not extend beyond the flight detent In-flight do not extend beyond armed w/ flaps 40 Do not use below 1000' RA
28
Fuel Loading
Main tanks must be scheduled full if the center tank contains more than 1000'
29
Fuel imbalance must not exceed
1000 lbs
30
Perform an operational check of the crossed valve during
the last hour of extended range operations
31
On the ground center, tank fuel pumps must not be turned on unless
there is greater than 1000 lbs in the center tank
32
Defueling with passengers on board is prohibited if:
main tank fuel pumps are powered
33
Minimum fuel for electric hydraulic pumps on the ground
1675 lbs in the related tank