Limitations Flashcards

1
Q

Reinforced cockpit door

A

A check of the remote access system must be performed once each flight day.

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2
Q

Reduced Thrust Operation

Not authorized on…

A

The operator must have a means to verify availability of takeoff thrust to ensure engine does not exceed authorized limits

Not authorized on runaways with standing water, slush, loose or compact snow or wet ice, can do it on a wet runway with wet runway numbers

Not permitted if items affecting performance cause a significant increase in crew workload, line inop engine guages, anti-skid inop, or non standard takeoff technique is required.

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3
Q

Evac system

A

Slide girt bars must be inserted into the floor fittings prior to departure, and until arrival at the passenger loading ramp.

The emergency handle on the aft pressure bulkhead must be exposed, and the normal handle covered, prior to departure from the pax loading ramp until arrival at pax offloading ramp

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4
Q

Circuit breakers

A
Do not reset:
Hydraulic auxillary pump
Fuel pump
Fuel qty indicating system
Lav flush motor
Galley power
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5
Q

Emergency lights

A

Must be armed for all flight operations

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6
Q

Wing landing lights
Cycles
Ambient

A

Cool did 1.5 minutes after initial extension or retraction, and 3.5 minutes after each subsequent one.

Do not have lamps on in ambient air for periods over 10 minutes.

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7
Q
Max weights
Taxi
Takeoff
Landing
ZFW
A

115,000(119,000)
114,000(118,000)
110,000
100,500

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8
Q

Maneuvering limit load Factors

A

Flaps/slats retracted 2.5 to -1.0 G

Either extended 2.0 to 0.0G

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9
Q

Runway slope
Tailwind
Vmo
Mmo

A

1.7 to -2.0%
10kts
340kts up to 26,000ft
.82 above 26,000ft

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10
Q

Engine crosswind minutes

A

40 kts

For tailwinds > 10kts or crosswinds >40kts limited to 50% N1 and taxi and ground handling only

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11
Q

Max altitude

A

37,000ft

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12
Q

ACARS

A

Limited to messages which do not create unsafe conditions if;

  1. Message is delayed or not received
  2. Message is delivered to wrong recipient
  3. Message content may be frequently corrupt
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13
Q

Windshield heat

A

Windshield anti ice must be on for all flight operations except:
1. Do not operate on a cracked windshield
2. Do not exceed 315kts below 10,000ft if windshield heat is inop on any window
Cracked window limits below 10,000ft are
315kts outer glass
235kts inner glass

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14
Q

Cabin pressurization

A

Max cabin diff 7.86
Max emergency relief is 8.27
If manual mode takeoff and land unpressurized

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15
Q

Air conditioning

A

FLOW switch must be in NORM for takeoff if air conditioning is used

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