Limitations Flashcards

1
Q

Runway slope

A

+ / - 2%

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2
Q

Max. T/O and Landing Tailwind component

A

10 knots

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3
Q

Maximum speeds

A

Observe Vmo pointed and gear / flaps placards

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4
Q

Maximum flight operational latitude

A

73 North / 60 South

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5
Q

Maximum operating altitude

A

37000 ft

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6
Q

Maximum T/O and landing altitude

A

8400 ft

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7
Q

Severe turbulent air penetration speed

A

280 KIAS / .73M Applicable to Climb and Descent only

During Cruise, refer to SP.16, Severe Turbulence Supplementary Procedure

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8
Q

Standby altimeters do not meet altimeter accuracy requirements of RVSM airspace.

True or false?

A

True

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9
Q

The maximum allowable in-flight difference between Captain and First Officer altitude displays for RVSM operations

A

200 ft

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10
Q

The maximum allowable on-the-ground altitude display differences for RVSM operations are

A

Memory

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11
Q

Possible conflicts between the AFM and the FCOM may occur due to separate publication release dates. In the event of a conflict between the FCOM and the AFM

A

the AFM shall govern

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12
Q

Maximum Taxi Weight

A

29337 & 29341 :
128,500 lbs (58,286 kgs)

28558 :
140,000 lbs (63,502 kgs)

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13
Q

Maximum Takeoff Weight

A

29337 & 29341:

128,000 lbs (58,059)

28558:

139,500 lbs (63,276 kgs)

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14
Q

Maximum Landing Weight

A

29337 & 29341:

114,000 lbs (51,709 kgs)

28558:

114,000 lbs (51,709 kgs)

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15
Q

Maximum zero fuel weight

A

29337 & 29341:
105,000 lbs (47,627kgs)

28558:

105,000 lbs (47,627 kgs)

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16
Q

The maximum cabin differential pressure (relief valves) is:

Air system

A

8.65 psi

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17
Q

Do not use aileron trim with:

A

autopilot engaged.

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18
Q

Maximum and minimum glideslope angles for autoland

A

3.25 degrees and 2.5 degrees respectively.

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19
Q

Do not use LVL CHG on final approach below

A

1000 ft AFE

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20
Q

Maximum generator drive oil temperature

A

157° C

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21
Q

Maximum and minimum limits are

A

Red

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22
Q

Caution limits are

A

Amber

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23
Q

Maximum time limit for takeoff thrust

A

5 minutes

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24
Q

Maximum N1 RPM

25
Maximum N2 RPM
105%
26
Maximum Takeoff EGT
930
27
Maximum Continuous EGT
895
28
Maximum Start EGT
725
29
Minimum Oil Pressure
13 psi
30
Maximum Oil Temperature
165° C maximum 160° C – 165° C allowable for 15 minutes 160° C maximum continuous
31
Continuous ignition must be on (ENGINE START switch in the CONT position) during
takeoff and landing and during engine anti–ice operations
32
When flight in moderate or heavy rain, hail, or sleet is encountered or anticipated, engine start switches must be set to
FLT and a minimum of 45% N1 must be maintained except on short final when landing is assured
33
Both PMCs must be either
OFF or ON for takeoff
34
Intentional selection of reverse thrust in flight is...
Prohibited
35
APU Maximum start EGT is
760° C
36
APU Maximum continuous EGT is
710° C
37
With APU bleed + electrical load, maximum altitude is
10,000 ft
38
With APU bleed, maximum altitude is
17,000 ft
39
APU can operate up to
37,000 ft
40
With APU electrical load, maximum altitude is...
35,000 ft
41
Pneumatic pressure (prior to starter engagement)
minimum 30 psig at sea level, decreasing 1/2 psig per 1,000 ft. above sea level.
42
APU bleed valve must be closed when:
* ground air connected and isolation valve open •engine no. 1 bleed valve open * isolation valve and engine no. 2 bleed valve open.
43
APU bleed valve may be open during engine start, but ...
avoid engine power above idle
44
APU If there are multiple aborted start attempts ... minutes of cooling is required between the second and third start attempt.
5
45
APU | A wait of... is required after the third start attempt.
One hour
46
The maximum altitude with flaps extended is
20,000 ft
47
In flight, do not extend the SPEED BRAKE lever beyond the...
FLIGHT DETEND
48
Do not deploy the speedbrakes in flight at radio altitudes less than...
1000 ft
49
When extending or retracting flaps with the ALTERNATE FLAPS position switch, allow ... after releasing the ALTERNATE FLAPS position switch before moving the switch again to avoid damage to the alternate flap motor clutch
15 minutes
50
After a completed extend/retract cycle, i.e., 0 to 15 and back to 0, allow ... cooling before attempting another extension.
5 minutes
51
Avoid weather radar operation in ..., or within ... of fueling operations or a fuel spill.
A hangar - 50 feet (15.25 meters)
52
The hangar recommendation does not apply to... .
the weather radar test mode.
53
Do not reset a tripped ... circuit breaker
Fuel pump
54
Maximum fuel temperature is... .
49°C.
55
Inflight tank fuel temperature must be maintained at least ... or ... , whichever is higher.
3°C above the freezing point of the fuel being used / –45°C
56
Lateral imbalance between main tanks 1 and 2 must be scheduled to be ...
Zero
57
Random fuel imbalance must not exceed ... for taxi, takeoff, flight, or landing.
1,000 lbs (453 kgs)
58
Main tanks 1 and 2 must be scheduled to be full if center tank contains more than ... of fuel.
1,000 lbs (453 kgs)
59
Do not apply brakes until ...
after touchdown