Landing Gear . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . L.10.8 Non–AFM Operational Information . . . . . . . . . . . . . . . . . . . . L.10.8
Copyright . The Boeing Company. See title page for details.
737 Flight Crew Operations Manual
General
This chapter contains Airplane Flight Manual (AFM) limitations and Boeing recommended operating limitations. Limitations that are obvious, shown on displays or placards, or incorporated within an operating procedure are not contained in this chapter.
Airplane General Operational Limitations
Runway slope +/– 2%
Maximum Takeoff and Landing Tailwind Component 10 knots
Maximum speeds Observe gear and flap placards
Maximum Operating Altitude 41,000 ft
Maximum Takeoff and Landing Altitude YA613 - YA687, YA803 - YK104 8,400 ft YA721 - YA802 13,500 ft
Maximum flight operating latitude – 82° North and 82° South, except for the region between 80° West and 130 ° West longitude, the maximum flight operating latitude is 70° North, and the region between 120° East and 160° East longitude, the maximum flight operating latitude is 60° South.
Installation of handle covers on the overwing exits must be verified prior to departure whenever passengers are carried.
YA809, YD651 - YK104 Photoluminescent Floor Emergency Lighting must be charged in accordance with approved procedures.
Verify that an operational check of the flight deck door access system has been accomplished according to approved procedures once each flight day.
Non–AFM Operational Information
Note: The following items are not AFM limitations, but are provided for flight crew information.
Copyright . The Boeing Company. See title page for details.
Limitations -Operating Limitations 737 Flight Crew Operations Manual
On revenue flights, the escape slide retention bar (girt bar) must be installed
during taxi, takeoff and landing.
The maximum demonstrated takeoff and landing crosswind is 36 knots.
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:
Field Elevation Max Difference Between Captain & F/O Max Difference Between Captain or F/O & Field Elevation
Sea Level to 5,000 feet 50 feet 75 feet
5,001 to 10,000 feet 60 feet 75 feet
Weight Limitations
YA721, YA722
Weights Kilograms
Maximum Taxi Weight 67,358
Maximum Takeoff Weight 67,131
Maximum Landing Weight 58,059
Maximum Zero Fuel Weight 54,657
YA801 - YA809
Weights Kilograms
Maximum Taxi Weight 69,626
Maximum Takeoff Weight 69,399
Maximum Landing Weight 58,059
Maximum Zero Fuel Weight 54,657
Copyright . The Boeing Company. See title page for details.
L.10.2 March 29, 2004
Limitations -Operating Limitations 737 Flight Crew Operations Manual
YA613 - YA687
Weights Kilograms
Maximum Taxi Weight 70,306
Maximum Takeoff Weight 70,080
Maximum Landing Weight 58,604
Maximum Zero Fuel Weight 54,657
YC411, YC413
Weights Kilograms
Maximum Taxi Weight 79,227
Maximum Takeoff Weight 79,000
Maximum Landing Weight 65,317
Maximum Zero Fuel Weight 61,688
YC153, YC154, YK101 - YK104
Weights Kilograms
Maximum Taxi Weight 79,242
Maximum Takeoff Weight 79,015
Maximum Landing Weight 66,224
Maximum Zero Fuel Weight 61,688
YD651 - YD655
Weights Kilograms
Maximum Taxi Weight 79,242
Maximum Takeoff Weight 79,015
Maximum Landing Weight Max Landing Weight (Flaps 15*) 66,814 65,408
Maximum Zero Fuel Weight 63,639
YD651 - YD655
* This maximum weight applies when landing with Flaps 15 under normal conditions.
It does not apply when Flaps 15 is required during a Non-Normal Checklist.
Copyright . The Boeing Company. See title page for details.
Limitations -Operating Limitations 737 Flight Crew Operations Manual
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