Limitations Flashcards
Max Operating Alt
41,000ft
Max T/O & Landing Runway Alt
8,400ft
12,000ft (high alt sys)
Runway slope
+/- 2%
Max T/O & Landing tailwind component
(FAA) 10kts: T/O
(FCOM)15kts: Landing
Turbulence air penetration speed
Above FL200: 280kts/0.76M
Below FL200: 250kts
Alt display limits: RVSM OPS
• Stdby Alt: do not meet alt accuracy requirements
PFD 1&2
• Max in-flight diff: +-200ft
• Max on-the-ground:
SL - 5,000ft = +-50ft
5,001 - 10,000 = +-60ft
PFD1/2 & Field elevation
SL - 10,000ft = +-75ft
Min Oil Quantity
12 quarts
Max Weights 737-800
MZFW: 136,000Lbs / 61,688kg
MRW: 156,000Lbs / 70,760kg
MTOW: 155,500Lbs / 70,533kg
MLW: 144,000Lbs / 65,317kg
Fuel Quantity
Tank 1 - 8630Lbs/3915kg
Tank 2 - 8630 Lbs/3915kg
Center - 28,803Lbs/13,066kg
Total quantity: 46,063Lbs/20,896kg
Max Start EGT (QRH in-flight start)
725 deg cel
Max diff press
9.1psi (2relief valves)
Fuel Imbalance
Must not exceed 1000Lbs/453kg
Tanks 1&2 - MUST be scheduled to be 0
NB: tank 1&2 must be full if centre tank is more than 1000Lbs
Fuel Loading
Main tanks 1 & 2 must be full if center tank contains more than 1000Lbs/453kg
Fuel Tank Temp
Max: +49 deg cel
Min: - 43 deg cel / 3 deg cel above the fuel freezing point temp whichever is higher.
Max Alt with flaps extended
20,000ft
AP engage after T/O
Not below 400ft AGL
AP on approach
Not below:
SC Ops: 50ft AGL
High alt landing sys (above 8,400ft): 100ft RA
Auto land capability
Flaps 30 / 40 and both engines operative
Runways at or below 8,400ft press alt
Dual AP engaged
Max & min GS angles: 3.25 and 2.5 deg resp.
Glide slope angles for auto land
Max: 3.25 deg
Min: 2.5 deg
Max landing gear speeds
Extend : 270kts/.82m
Retract : 235kts
Extended 320kts / .82m