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B737 > Limitations > Flashcards

Limitations Flashcards

1
Q

Max Tailwind Component TAKE OFF and LANDING

A

-300 and -700 Pax - 10 KTS
-800 - 15 KTS
-All Freighters - 15KTS

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2
Q

Severe Turbulent Air Penetration Speed - Climb and Descent

A

Classic - 280 Knots / 0.73M
Classic Freighter - 264 Knots / 0.65M
All NG’s - 280 Knots / 0.76M

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3
Q

Can HF Radio be operated during refuelling?

A

No

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4
Q

Is aileron trim allowed with autopilot engaged?

A

No

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5
Q

After take off, at what Altitude can the autopilot be engaged?

A

Classic - 1000 feet AGL
NG - 400 feet AGL

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6
Q

For single channel autopilot operation during approach, at what height must the autopilot be disconnected for landing?

A

50 feet AGL

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7
Q

Max glideslope angle for autoland?

A

3.25 degrees

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8
Q

Min glideslope angle for autoland?

A

2.5 degrees

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9
Q

Restrictions on autoland?

A
  • Flaps must be 30 or 40 degrees
  • Both engines must be operative
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10
Q

Level Change mode restriction on approach?

A

Do not use below 1000 feet above field elevation

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11
Q

Max N1 RPM

A

Classic - 106%
NG - Red Line

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12
Q

Max N2 RPM

A

Classic - 105%
NG - Red Line

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13
Q

Max Take Off EGT

A

Classic - 930º
NG - Red Line

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14
Q

Max Continuous EGT

A

Classic - 895º
NG - Red Line

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15
Q

Max Start EGT

A

Classic - 725º
NG - Red Line

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16
Q

Min Oil Pressure

A

13PSI

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17
Q

Max Oil Temperatures

A

Classic - 160º continuous
160-165º for up to 15 Minutes
165º Max

NG - Red Line

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18
Q

When must continuous ignition be used? (Engine start switch in the CONT position)

A

During take off, landing and engine anti-ice procedures

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19
Q

Reverse Thrust Limitation

A

Intentional selection of reverse thrust during flight is prohibited

20
Q

APU Altitude Limitations

A

Max operating - Classic - 37000 feet, NG - 41000 feet

With electrical load - Classic - 35000 feet, NG - 41000 feet

With Bleed Load - 17000 feet

With bleed and electrical load - 10000 feet

21
Q

Max Altitude with flaps extended

A

20000 feet

22
Q

Control input limitation

A

Avoid rapid control inputs at any speed

23
Q

Lowest Altitude for speed brake deployment?

A

1000 feet

24
Q

Weather radar operation distance limits

A
  • Not within 50 feet (16m) of refuelling, or spilt fuel
  • Not inside a hangar other than test mode
25
Q

Max fuel imbalance

A

453Kgs

26
Q

Max cabin pressure differential

A

Classic - 8.65 PSI

NG - 9.1 PSI

27
Q

Max main fuel tank imbalance ….?

A

453Kgs

28
Q

Max fuel temp

A

49°C

29
Q

Can a fuel pump circuit breaker be reset?

A

No

30
Q

Time required between movements of the alternate flap position switch?

A

15 seconds

31
Q

Min pneumatic pressure req for Engine start ?

A

30PSI at Sea Level

32
Q

Max APU start EGT ?

A

Classic - 760°

33
Q

Max continuous EGT APU ?

A

Classic - 710°

34
Q

Max take off thrust time limit ?

A

5 minutes or 10 minutes if an engine failure has occurred and there are obstacles in net flight path

35
Q

Max generator drive oil temp ?

A

Classic - 157°C

36
Q

Min N1 for anti ice operation

A

40%

37
Q

Max CSD oil temp rise ?

A

20°

38
Q

Minimum duct pressure for dual pack operation from one source

A

20PSI

39
Q

Minimum Fuel Temp

A

-43º

40
Q

Minimum time between complete flap retraction cycles?

A

5 min

41
Q

Max Operating Altitude

A

Classic - 37000 feet
NG - 41000 feet

42
Q

Max Take-Off and Landing Altitude

A

8400 feet

43
Q

Max allowable in flight difference between captain and FO altimeters for RVSM

A

200 feet

44
Q

Max allowable difference on ground between captain and FO altimeters for RVSM

A

Classic
Sea level - 40 feet
5000 feet - 45 feet
10000 feet - 50 feet

NG
Sea Level - 5000 - 50 feet
5000 - 10000 - 60 feet

45
Q

Max X-Wind Component TO and Landing

A

Classic - Dry 35 KTS (30KTS - Narrow Runway)

NG - Dry 34 KTS (30KTS - Narrow Runway)

Wet 25 KTS (20KTS - Narrow Runway)

Standing water/slush 15 KTS

Snow/Ice 15KTS

46
Q

Is Holding with flaps extended in icing conditions allowed?

A

No

B737 (9 decks)

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