Limitations Flashcards

1
Q

Max Altitude for Operation of APU

A

41,000’

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2
Q

Max Altitude for Electric Only for APU

A

41,000’

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3
Q

Max Altitude Bleed Air Only for APU

A

17,000’

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4
Q

Max Altitude for Bleed and Electric from APU

A

10,000’

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5
Q

Max Operating Altitude

A

41,000’

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6
Q

Max EGT for Ground Start

A

725 degrees for NG

753 degrees for Max

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7
Q

Operate engines at or near idle for a minimum of ____ minutes prior to applying take off thrust

A

2 minutes for NG

3 minutes for Max

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8
Q

Operate engines at or near idle for a minimum of _____ minutes prior to shutdown.

A

One minute for NG

Three minutes for MAX

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9
Q

With engine bleed air switches ON, do not operate the air conditioning packs in______

A

High for takeoff, approach and landing

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10
Q

Do not remove AC power from the aircraft for at least ______ after IRS shutdown

A

30 seconds

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11
Q

On the ground, limit one generator operation to a maximum of

A

215 amps

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12
Q

Limit one generator operation for MAX on the ground and in the air to

A

215 amps

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13
Q

Do not extend the flaps above

A

20,000’

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14
Q

Do not use speed brakes below

A

1000’ AGL

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15
Q

In flight, do not use speed brakes with flaps

A

Greater than flaps 10

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16
Q

Max fuel tank temperature

A

+49 degrees

17
Q

Minimum fuel tank temperature

A

-37 degrees

18
Q

Circle to Land Minimums

A

1000’ and 3 miles or the published circling minima, whichever is higher

19
Q

Circle to Land MDA

A

1000 above airport altitude unless restricted to a higher minima on the approach chart

20
Q

Anti Ice Limitations

A
  • Holding in icing with flaps extended is prohibited
  • Do not operate wing anti-ice in the ground when the OAT is above 10 degrees C
  • Do not use wing anti ice as a substitute for ground deicing/anti-icing and inspection procedures
21
Q

Do not operate weather radar during

A

Fueling, near fuel spills, or near people

22
Q

In flight reset of circuit breakers should only be accomplished when

A

Directed by QRH. Allow approximately two minutes for cooling before resetting.

23
Q

Intentional selection of reverse thrust in flight is

A

Prohibited

24
Q

Do not operate the aircraft (700) at speeds in excess of 320 knots at weights over

A

143,000lbs if the speed brake wing load alleviation system is inoperative

25
Main tanks must be _______ if the center tank quantity is greater than _______ lbs
Full, 1000
26
Center fuel pumps must be _____ for all operations with more than ________ lbs of fuel in the center tank
ON, 1000
27
1000lbs may be retained in the center tank provided
The effects of balance have been considered
28
For ground operation, center tank fuel switches must not be positioned to ON unless
The center tank fuel quantity exceeds 1000lbs, except when defueling or transferring fuel
29
Flight crews must not reset tripped
Fuel quantity indicator, fuel pump, or fuel pump control circuit breakers
30
Aircraft must land within ____ minutes (MAX ____ minutes) of initial discharge of the cargo bay fire suppression system
60, 180
31
Pilots are authorized to deviate from an ATC clearance to the extent necessary to comply with
The TCAS II RA
32
Center fuel pumps must _____ be on unless personnel are available on the flight deck to monitor the pressure lights
Not
33
Corresponding center tank fuel pump switch must be positioned to _____ when a center tank LOW PRESSURE light illuminates
OFF
34
A tripped circuit breaker may only be reset ______. Allow approximately two minutes for cooling before resetting. An in-flight reset should only be accomplished if, in the judgment of the Captain, regaining use of that system is ______ to the safe conduct of flight.
Once, Critical
35
Alternate flap duty cycle in flight is one complete cycle, then ____ __________ off. A complete cycle is movement from position 0° to 15° and back to 0°. The ALTERNATE FLAPS position switch must be in the OFF position for ____ seconds before reversing the direction of flap movement.
5 minutes, 15
36
Flight Crews must immediately respond to TCAS information (both TAs and RAs) by using the TCAS (traffic avoidance) guidelines.
37
Fuel may be transferred from tank to tank or the aircraft may be refueled with passengers aboard provided:
The fuel quantity in the tank from which the fuel is being taken is maintained at not less than 2000 lbs
38