737 Limitations Flashcards
Max operating altitude?
41,000 ft
Max takeoff and landing altitude?
8,400 ft
Max demonstrated crosswind takeoff and landing?
33 knots
36 knots EKD & EKE
HF
Do not operate during refueling operations
RVSM
In flight max difference between CAP & F/O 200 feet.
On the ground:
Sea level to 5,000 ft-50 feet CAP & F/O, 75 feet from field elevation.
5,001 to 10,000 ft-60 feet CAP & F/O, 75 feet from field elevation.
Max taxi weight
737-800: 79,242
737-900: 85,366
Max takeoff weight
737-800: 79,015
737-900: 85,139
Max landing weight
737-800: 66,360
737-900: 71,350
Max zero fuel weight
737-800: 62,731 ***EKP 62,142
737-900: 67,721
Max cabin diff
9.1 PSI
When engine bleed air switches ON for takeoff approach and landing
Do not operate packs in HIGH
Note: fire protection non-normal procedures take precedence over that statement (CARGO FIRE or SMOKE/FUMES REMOVAL)
Autopilot/flight director system
Use of Aileron trim with auto pilot is prohibited.
Do not engage autopilot for takeoff below 400 feet.
Single channel operation during approach- not below 50 feet.
Max speed when wether minima predicated on autoland operation:
Headwind 25 knots
Crosswind 20 knots
Tailwind 15 knots
Max & min glideslope angles
2.5 - 3.25
Autoland
Only using flaps 30 or 40 and both engines operative.
Engine ignition must be on
Takeoff
Landing
Operation in heavy rain
Anti ice operation
Intentional selection of the revers thrust in flight
Is prohibited
APU in flight
Bleed + electrical max 10,000 ft inflight & 15,000 ft ground only
Bleed only max 17,000 ft
Electrical only max 41,000 ft
APU bleed must be closed when
Ground air connected and isolation valve open
Engine no. 1 bleed valve open
Isolation and engine no. 2 bleed valve open
APU valve maybe open during engine start, but avoid above idle power
APU start
After three consecutive aborted start attempts, a 15 min cooling period is required
Max flap extension altitude
20,000 ft
Holding in icing conditions with flaps extended
Is prohibited
Flight controls operation
Avoid rapid and large alternating control inputs
Do not deploy speedbrakes inflight below radio altitude
Of 1000 ft
Alternate flap duty cycle
After moving the flaps in alternate allow 15 seconds to avoid damage to alternate flap motor clutch
After a complete cycle extend/retract allow 5 min cooling before attempting another try
ADIRU alignment
Should not be attempted at latitudes greater than 78 degrees
Look Ahead Terrain Alerting (GPWS)
Do not use terrain display for navigation
Do not use terrain alerting and terrain display for takeoff, approach and landing within 15 NM of airports not contained in database
Weather radar
Do not operate in a hangar or within 50 feet of a fuel spill.
Fuel tank limitations
Max temp 49
Min -43 or 3 above freezing point
Do not dry run center fuel tank (low pressure light illuminated)
Fuel balance
Lateral imbalance between tanks 1&2 must be scheduled to be zero
Random imbalance must not exceeds 453 kgs
Main tanks 1&2 must be full if center tank contains more than 453kgs
Takeoff using assume temperature trust reduction with the anti-skid inoperative
Prohibited
EGT limits
Engine start - 725
Caution range - 925
Max - 950
Cross wind limitation and guidelines
Talpa arc
Crab - on slippery runways
Side slip limits 15 flaps - 15 k, 30 flaps - 18 k, 40 flaps - 21 k
Asymmetric revers on wet or contaminated runways - reduce limit by 5 k
Takeoff - 33
Landing - 40
First officer - up to code 4, gust up to 10k, BA good to medium
Maximum takeoff and landing tailwind component?
15 knots
