Delta B737 Limitations Flashcards
Maximum Takeoff and Landing Tailwind Component?
10 knots, or as permitted by company pages
Maximum Operating Altitude?
41,000 feet pressure altitude.
Maximum Takeoff and Landing Altitude?
8,400 feet pressure altitude
Maximum crosswind limit for takeoff or landing, including gusts?
33 knots
Note: The crosswind component may be further limited by low visibility takeoffs, low visibility approaches, autolands, contamination, or runway width.
Severe turbulent air penetration speed?
280 KIAS/.76M (whichever is lower)
Note: applicable to climb and descent only.
Maximum Cabin deferential pressure?
9.1 PSI
Maximum differential pressure for takeoff and landing?
0.125 PSI
With engine bleed air switches ON, do not operate the air conditioning packs in ______________ for takeoff, approach, and landing.
HIGH
When must engine Anti-ice be on?
Engine TAI must be on when icing conditions exist or are anticipated, except during climb and Cruise below -40C SAT
Do not operate wing anti-ice on the ground when OAT is above ____________?
10 degrees C (50 degrees F)
Use of aileron trim with the autopilot engaged is ________________?
Prohibited
Do not engage the autopilot for takeoff below _____________?
400 feet AGL
For single channel operation during approach, the autopilot shall not remain engaged below ____________?
50 feet AGL
Autoland maximum headwind?
25 Knots
Autoland maximum crosswind?
20 knots
Autoland maximum tailwind?
10 knots
The Autoland capability may only be used with flaps __________ or __________ and both engines operating.
Flaps 30 or 40
Autoland capability may not be used to runways above ______________ feet pressure altitude?
8,400
Do not use LVL CHG on final approach below ________________ feet AFE?
1,000 feet AFE
Electrical- on the ground limit one generator (engine driven) operation to a maximum of __________________?
75 KVA (215 amps)
EGT Limits-
Takeoff?
Top of the amber arc 5 minutes
(10 minutes allowed in the event of loss of thrust on one engine during takeoff.
EGT Limits-
Maximum Continuous?
Top of the white arc
EGT Limits-
Starting- ground/flight
EGT start limit line
Engine ignition must be on for?
- takeoff
- landing
- operation in heavy rain
- anti-ice operation
Engine oil-
If engine oil is in the yellow band with takeoff thrust set, ________________?
Do not Takeoff
Limit each start attempt to a maximum of _______________ minutes?
2 minutes
A minimum on of _______________ seconds is required between start attempts?
10 seconds
APU maximum inflight altitude with APU bleed + Electrical load?
10,000 feet
APU maximum inflight altitude with APU bleed only?
17,000 feet
APU start duty cycle:
Maximum of _____________ per 15 minute interval?
3 starts
APU start duty cycle:
Wait time after 3 (successful or unsuccessful) starts is ____________ minutes?
15 minutes
APU-
Run the APU for ______________ minutes before using it as a bleed source?
2 minutes
Maximum altitude with flaps extended?
20,000 feet
Holding in icing conditions with the flaps extended is ______________?
Prohibited
Do not use the speed brakes in flight at radio altitudes less than ____________ feet?
1,000 feet
In flight, do not extend the speed brake lever beyond __________________?
FLIGHT DETENT
Full application of pitch, roll, or yaw controls should be confined to speeds below the _________________ speed?
Maneuvering Speed
Alternate flaps-
When extending or retracting flaps with the ALTERNATE FLAPS switch, allow ________ seconds before moving the switch again?
15 seconds
Maximum allowable crosswind for HUD takeoffs?
10 knots
Maximum allowable headwind speed for HUD AIII operation?
25 knots
Maximum allowable crosswind speed for HUD AIII operation?
15 knots
Maximum allowable tailwind speed for HUD AIII operation?
10 knots
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
Use if HUD AIII for landing must be done with flaps _________ or _________ with both engines operating
Flaps 30 or Flaps 40
Use if HUD AIII for landing must be done with flaps _________ with one engine operating?
Flaps 15
On the ground, the standby altimeter must be within +/-__________ feet of the captain and first officers altimeters.
+/- 75 feet
The maximum allowable in-flight difference between captain and first officers altitude displays is __________ feet?
200 feet
Maximum fuel tank temperature?
49 degrees C
Minimum inflight fuel temperature?
3 degrees C above the freezing point of the fuel being used or -43 degrees C, whichever is higher.
Maximum fuel imbalance for taxi, takeoff, flight or landing?
1,000 lbs
Ensure the center tank fuel pump switches are selected ____________ before any planned power transfer.
OFF
Maximum & Minimum glide slope angles for Autoland?
3.25 & 2.5 degrees
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
