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
Engine oil- | If engine oil is in the yellow band with takeoff thrust set, ________________?
Do not Takeoff
26
Limit each start attempt to a maximum of _______________ minutes?
2 minutes
27
A minimum on of _______________ seconds is required between start attempts?
10 seconds
28
#APU maximum inflight altitude with APU bleed + Electrical load?
10,000 feet
29
#APU maximum inflight altitude with APU bleed only?
17,000 feet
30
APU start duty cycle: | Maximum of _____________ per 15 minute interval?
3 starts
31
APU start duty cycle: | Wait time after 3 (successful or unsuccessful) starts is ____________ minutes?
15 minutes
32
APU- | Run the APU for ______________ minutes before using it as a bleed source?
2 minutes
33
#Maximum altitude with flaps extended?
20,000 feet
34
Holding in icing conditions with the flaps extended is ______________?
Prohibited
35
Do not use the speed brakes in flight at radio altitudes less than ____________ feet?
1,000 feet
36
In flight, do not extend the speed brake lever beyond __________________?
FLIGHT DETENT
37
Full application of pitch, roll, or yaw controls should be confined to speeds below the _________________ speed?
Maneuvering Speed
38
Alternate flaps- When extending or retracting flaps with the ALTERNATE FLAPS switch, allow ________ seconds before moving the switch again?
15 seconds
39
Maximum allowable crosswind for HUD takeoffs?
10 knots
40
#Maximum allowable headwind speed for HUD AIII operation?
25 knots
41
#Maximum allowable crosswind speed for HUD AIII operation?
15 knots
42
#Maximum allowable tailwind speed for HUD AIII operation?
10 knots
43
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?
500 feet above TDZE
44
#Use if HUD AIII for landing must be done with flaps _________ or _________ with both engines operating
Flaps 30 or Flaps 40
45
#Use if HUD AIII for landing must be done with flaps _________ with one engine operating?
Flaps 15
46
On the ground, the standby altimeter must be within +/-__________ feet of the captain and first officers altimeters.
+/- 75 feet
47
The maximum allowable in-flight difference between captain and first officers altitude displays is __________ feet?
200 feet
48
Maximum fuel tank temperature?
49 degrees C
49
Minimum inflight fuel temperature?
3 degrees C above the freezing point of the fuel being used or -43 degrees C, whichever is higher.
50
Maximum fuel imbalance for taxi, takeoff, flight or landing?
1,000 lbs
51
Ensure the center tank fuel pump switches are selected ____________ before any planned power transfer.
OFF
52
Maximum & Minimum glide slope angles for Autoland?
3.25 & 2.5 degrees
53
Alternate flaps- After a complete extend/retract cycle, I.e., 0 to 15 and back to 0, allow _________ minutes cooling before attempting another extension.
* 5 minutes