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Delta 737 Study Info > Delta B737 Limitations > Flashcards

Delta B737 Limitations Flashcards

1
Q

Maximum Takeoff and Landing Tailwind Component?

A

10 knots, or as permitted by company pages

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2
Q

Maximum Operating Altitude?

A

41,000 feet pressure altitude.

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3
Q

Maximum Takeoff and Landing Altitude?

A

8,400 feet pressure altitude

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4
Q

Maximum crosswind limit for takeoff or landing, including gusts?

A

33 knots

Note: The crosswind component may be further limited by low visibility takeoffs, low visibility approaches, autolands, contamination, or runway width.

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5
Q

Severe turbulent air penetration speed?

A

280 KIAS/.76M (whichever is lower)

Note: applicable to climb and descent only.

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6
Q

Maximum Cabin deferential pressure?

A

9.1 PSI

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7
Q

Maximum differential pressure for takeoff and landing?

A

0.125 PSI

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8
Q

With engine bleed air switches ON, do not operate the air conditioning packs in ______________ for takeoff, approach, and landing.

A

HIGH

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9
Q

When must engine Anti-ice be on?

A

Engine TAI must be on when icing conditions exist or are anticipated, except during climb and Cruise below -40C SAT

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10
Q

Do not operate wing anti-ice on the ground when OAT is above ____________?

A

10 degrees C (50 degrees F)

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11
Q

Use of aileron trim with the autopilot engaged is ________________?

A

Prohibited

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12
Q

Do not engage the autopilot for takeoff below _____________?

A

400 feet AGL

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13
Q

For single channel operation during approach, the autopilot shall not remain engaged below ____________?

A

50 feet AGL

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14
Q

Autoland maximum headwind?

A

25 Knots

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15
Q

Autoland maximum crosswind?

A

20 knots

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16
Q

Autoland maximum tailwind?

A

10 knots

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17
Q

The Autoland capability may only be used with flaps __________ or __________ and both engines operating.

A

Flaps 30 or 40

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18
Q

Autoland capability may not be used to runways above ______________ feet pressure altitude?

A

8,400

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19
Q

Do not use LVL CHG on final approach below ________________ feet AFE?

A

1,000 feet AFE

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20
Q

Electrical- on the ground limit one generator (engine driven) operation to a maximum of __________________?

A

75 KVA (215 amps)

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21
Q

EGT Limits-

Takeoff?

A

Top of the amber arc 5 minutes

(10 minutes allowed in the event of loss of thrust on one engine during takeoff.

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22
Q

EGT Limits-

Maximum Continuous?

A

Top of the white arc

23
Q

EGT Limits-

Starting- ground/flight

A

EGT start limit line

24
Q

Engine ignition must be on for?

A
  • takeoff
  • landing
  • operation in heavy rain
  • anti-ice operation
25
Q

Engine oil-

If engine oil is in the yellow band with takeoff thrust set, ________________?

A

Do not Takeoff

26
Q

Limit each start attempt to a maximum of _______________ minutes?

A

2 minutes

27
Q

A minimum on of _______________ seconds is required between start attempts?

A

10 seconds

28
Q

APU maximum inflight altitude with APU bleed + Electrical load?

A

10,000 feet

29
Q

APU maximum inflight altitude with APU bleed only?

A

17,000 feet

30
Q

APU start duty cycle:

Maximum of _____________ per 15 minute interval?

A

3 starts

31
Q

APU start duty cycle:

Wait time after 3 (successful or unsuccessful) starts is ____________ minutes?

A

15 minutes

32
Q

APU-

Run the APU for ______________ minutes before using it as a bleed source?

A

2 minutes

33
Q

Maximum altitude with flaps extended?

A

20,000 feet

34
Q

Holding in icing conditions with the flaps extended is ______________?

A

Prohibited

35
Q

Do not use the speed brakes in flight at radio altitudes less than ____________ feet?

A

1,000 feet

36
Q

In flight, do not extend the speed brake lever beyond __________________?

A

FLIGHT DETENT

37
Q

Full application of pitch, roll, or yaw controls should be confined to speeds below the _________________ speed?

A

Maneuvering Speed

38
Q

Alternate flaps-
When extending or retracting flaps with the ALTERNATE FLAPS switch, allow ________ seconds before moving the switch again?

A

15 seconds

39
Q

Maximum allowable crosswind for HUD takeoffs?

A

10 knots

40
Q

Maximum allowable headwind speed for HUD AIII operation?

A

25 knots

41
Q

Maximum allowable crosswind speed for HUD AIII operation?

A

15 knots

42
Q

Maximum allowable tailwind speed for HUD AIII operation?

A

10 knots

43
Q

For HUD AIII approach to manual landing, AIII mode must be selected and the autopilot (A/P) & auto throttle (A/T) must be disengaged prior to __________ feet above TDZE?

A

500 feet above TDZE

44
Q

Use if HUD AIII for landing must be done with flaps _________ or _________ with both engines operating

A

Flaps 30 or Flaps 40

45
Q

Use if HUD AIII for landing must be done with flaps _________ with one engine operating?

A

Flaps 15

46
Q

On the ground, the standby altimeter must be within +/-__________ feet of the captain and first officers altimeters.

A

+/- 75 feet

47
Q

The maximum allowable in-flight difference between captain and first officers altitude displays is __________ feet?

A

200 feet

48
Q

Maximum fuel tank temperature?

A

49 degrees C

49
Q

Minimum inflight fuel temperature?

A

3 degrees C above the freezing point of the fuel being used or -43 degrees C, whichever is higher.

50
Q

Maximum fuel imbalance for taxi, takeoff, flight or landing?

A

1,000 lbs

51
Q

Ensure the center tank fuel pump switches are selected ____________ before any planned power transfer.

A

OFF

52
Q

Maximum & Minimum glide slope angles for Autoland?

A

3.25 & 2.5 degrees

53
Q

Alternate flaps-
After a complete extend/retract cycle, I.e., 0 to 15 and back to 0, allow _________ minutes cooling before attempting another extension.

A
  • 5 minutes

Delta 737 Study Info (6 decks)

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