Limitations Flashcards
Runway slope
+/- 2%
Maximum takeoff and landing tailwinds component
10 knots
(A series G series,BXI, BXJ 15 knots FAA approved This finding does not constitute operational approval to conduct takeoffs or landings with tailwind components greater than 10 knots.)
Maximum Operating Altitude
41000 ft
Maximum Takeoff and Landing Altitude
8,400 feet pressure altitude
ONLY B737 MAX
Ground Wind Operating Envelope
• For crosswinds greater than 43 knots, limit thrust to a setting normally used for taxi.
• Except when setting takeoff thrust on the runway, limit engine thrust to idle for winds greater than 58 knots.
Severe Turbulent Air Penetration speed
280 KIAS / .76M
whichever is lower. Applicable to Climb and Descent only
For cruise use supplementary procedures
Non–AFM Operational Information
Refueling
Revenue flights
Do not operate HF radios during refueling operations.
On revenue flights, the escape slide retention bar (girt bar) must be installed during taxi, takeoff and landing.
Altitude Display Limits for RVSM Operations
Standby altimeters do not meet altimeter accuracy requirements of RVSM airspace.
The maximum allowable in-flight difference between Captain and First Officer altitude displays for RVSM operations is
200 feet
The maximum allowable on-the-ground altitude display differences for RVSM operations are:
Difference between capt and FO upto 5000ft 50 feet
Difference between capt and FO Above 5000 upto 10000 60 feet
Difference between crew and field elevation 75 feet
Possible conflicts between the AFM and the FCOM
conflict between the FCOM and the AFM, the AFM shall govern
737NG Weight Limitations Taxi, takeoff, landing, zero fuel.
Maximum Taxi Weight 79,242 Kilograms
Maximum Takeoff Weight 79,015 Kilograms
Maximum Landing Weight 66,360 Kilograms
Maximum Zero Fuel Weight 62,731 Kilograms
737 MAX Weight Limitations Taxi, takeoff, landing, zero fuel.
Maximum Taxi Weight 82,871 Kilograms
Maximum Takeoff Weight 82,644 Kilograms
Maximum Landing Weight 69,308 Kilograms
Maximum Zero Fuel Weight 65,952 Kilograms
The maximum cabin differential pressure (relief valves) is
9.1 psi
the air conditioning packs in HIGH With either one or both engine bleed air switches ON
DO NOT operate the air conditioning packs in HIGH for takeoff, approach or landing.( does not apply for NON NORMALS)