LIMITATIONS Flashcards

1
Q

The maximum allowable in flight difference between captain and first officer
altitude displays for RVSM operations?

A

200 ft

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2
Q

The maximum allowable on-the-ground difference between captain and first
officer altitude displays for RVSM operations is?

A
  • 50 feet (from sea level to 5000 feet).

* 60 feet (from 5001 feet to 10,000 feet)

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3
Q

The maximum allowable on-the-ground difference between captain or first officer
altitude displays and field elevation for RVSM operations is?

A

75 feet

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4
Q

Should you trim the ailerons with autopilot engaged?

A

No

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5
Q

Lowest altitude to disconnect autopilot?

A

50 ft agl

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6
Q

Max tailwind for cat 2 or 3 approach?

A

10 kts

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7
Q

Max headwind for cat 2 or 3 approach?

A

25 kts

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8
Q

Max crosswind for cat 2 or 3 approach?

A

15 kts

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9
Q

Engine cooldown time?

A

Cooldown period is three minutes. Begin timing after clearing the landing runway.
Otherwise use OOOI ON event with four minutes to allow for transition to ground idle after reverse thrust usage.

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10
Q

Turbulence penetration airspeed?

A

280/M0.76

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11
Q

Takeoff with CSFF on upper wing surfaces is allowed. True or False?

A

True. Provided all conditions are met

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12
Q

Maximum operating altitude with flaps and/or slats

extended

A

20000 ft

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13
Q

Maximum takeoff and landing altitude

A

8400 ft

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14
Q

Maximum operating altitude

A

41000 ft

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15
Q

The maximum allowable in flight difference between captain and first officer
altitude displays for RVSM operations

A

200 ft

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16
Q

The maximum allowable on-the-ground difference between captain and first
officer altitude displays for RVSM operations is

A
50 feet (from sea level to 5000 feet).
60 feet (from 5001 feet to 10,000 feet)
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17
Q

The maximum allowable on-the-ground difference between captain or first officer
altitude displays and field elevation for RVSM operations is

A

75 ft

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18
Q

Severe turbulence air penetration airspeed

A

280 kts / M0.76

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19
Q

Vlo

A

275 kts

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20
Q

Vle

A

320 kts

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21
Q

Vmo / Mmo

A

340 Kts / 0.82M

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22
Q

Maximum gear retraction speed (VLO)

A

235 kts

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23
Q

Maximum takeoff weight NG

A

174200 lb

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24
Q

Maximum takeoff weight MAX

25
Maximum landing weight NG
146300 lbs
26
Maximum taxi weight NG
174700 lb
27
Maximum taxi weight MAX
181700 lbs
28
Maximum landing weight NG
146300 lbs
29
Maximum landing weight MAX
152800 lbs
30
Live animals will only be carried in the forward cargo compartment. True or False?
True
31
With either one or both engine bleed air switches ON, do not operate the air conditioning packs in HIGH for takeoff, approach or landing. True or False?
True
32
Maximum altitude when aircraft is dispatched for unpressurized flight
10000 ft
33
Maximum altitude for unpressurized flight, following an inflight depressurization
14,000 feet. This altitude may be exceeded when terrain clearance requirements dictate.
34
Maximum cabin pressure differential | safety relief valve setting
9.1 psi
35
Engine ignition must be on when operating in icing conditions. True or False?
True
36
Engine anti-ice must be on during all ground and flight operations when icing conditions exist or are anticipated, except during climb and cruise when the temperature is below - 40°C SAT. True or False?
True
37
Engine anti-ice must be on prior to and during descent in icing conditions, including temperatures below - 40°C SAT. True or False?
True
38
Should you use level change below 1000 ft?
No
39
Should you use aileron trim with autopilot on?
No
40
Does AA allow auto lands or dual autopilot operations?
No
41
APU starter limit?
After three consecutive aborted start attempts, a fifteen minute cooling period is required.
42
APU bleed + electrical load: max altitude?
10000 ft
43
APU bleed: max altitude?
17000 ft
44
APU electrical load: max altitude?
41000 ft
45
Do not operate HF radios during refueling operations. True or False?
True
46
Operation with assumed temperature reduced takeoff thrust is not permitted with antiskid inoperative. True or False?
True
47
Lowest altitude you can extend speed brakes?
1000 ft
48
In flight, do not extend the speed brake lever beyond the FLIGHT detent. True or False?
True
49
Conduct an operational check of the fuel crossflow valve prior to each ETOPS flight. True or False?
True
50
Maximum tank fuel temperature
49 C
51
Minimum fuel temprature
Tank fuel temperature prior to takeoff must not be less than -43°C or 3°C above the fuel freeze point, whichever is higher.
52
Is ballast fuel authorized?
No
53
Minimum amount of fuel in wing tanks if center tank has more than 1000 lb of fuel?
Wing tanks have to be full
54
Random or transient fuel imbalance must not exceed 1000 lbs for taxi, takeoff, flight or landing. True or False?
True
55
The maximum allowable difference between the captain’s and first officer’s PFD AOA indication is?
0.5 degrees
56
Recommend full IRS alignment before each flight. True or False?
True
57
Do not operate the entry or service doors with winds at the door of more than how many knots?
40 kts
58
Do not keep the entry or service doors open when wind gusts are more than how many knots?
65 kts