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Aircraft Communications Addressing and Reporting System (As installed) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . L.10.11 Electrical Power . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . L.10.11 Engines and APU . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . L.10.11 Engine Limit Display Markings . . . . . . . . . . . . . . . . . . . . . . L.10.11 General Engine Limitations  . . . . . . . . . . . . . . . . . . . . . . . . . L.10.12 Engine Ignition . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . L.10.12 PMC  . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . L.10.12 Reverse Thrust . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . L.10.12 APU  . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . L.10.13 Flight Controls . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . L.10.13 Flight Management, Navigation  . . . . . . . . . . . . . . . . . . . . . . . . L.10.14 Look-Ahead Terrain Alerting (EGPWS) (As Installed)  . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . L.10.14 Non–AFM Flight Management, Navigation Operational Information  . . . . . . . . . . . . . . . . . . . . . . . . . . . L.10.14 Fuel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . L.10.14 Fuel Balance . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . L.10.14 Landing Gear  . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . L.10.15
Limitations -Table of Contents 737 Operations Manual

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Copyright . The Boeing Company. See title page for details.
L.TOC.0.2  December 3, 2004

737 Operations Manual

General
This chapter contains Airplane Flight Manual (AFM) limitations and Boeing recommended operating information. 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 (15 knots: Serial No. 24364) 
Maximum speeds  Observe Vmo pointer and gear/ flap placards 
Turbulent airspeed  280 KIAS/.73M 
Maximum flight operational latitude  73° North and 60° South (For operation beyond these latitudes, see Ch. 11 for Serial No. 26318, 27635 and 28085) 
Maximum Operating Altitude  37,000 feet 
Maximum Takeoff and Landing Altitude  8,400 feet 14,000 feet – Serial No. 26318 

Verify that an operational check of the flight deck door access system (as installed) has been accomplished according to approved procedures once each flight day.
For Airplanes Operated Under British CAA Rules, Maximum Precipitation Depth for Takeoff:
Dry snow  6 cm 
Water, slush, or wet snow  15 mm 

Non–AFM Operational Information
Note:  The following items are not AFM limitations but are provided for flight crew information.
Limitations -Operating Limitations 737 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 35 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  40 feet  75 feet 
5,000 feet  45 feet  75 feet 
10,000 feet  50 feet  75 feet 

Weight Limitations 737–300 Airplanes Serial No. 24403, 24963, 24701 & 24702
Maximum Taxi Weight  125,000 lbs (56,699 kgs) 
Maximum Takeoff Weight (1)  124,500 lbs (56,472 kgs) 
Maximum Landing Weight (2)  114,000 lbs (51,709 kgs) 
Maximum Zero Fuel Weight  105,000 lbs (47,627 kgs) 

Copyright . The Boeing Company. See title page for details.
L.10.2  June 4, 2004

Limitations -Operating Limitations 737 Operations Manual
Serial No. 24698
Maximum Taxi Weight  128,368 lbs (58,227 kgs) 
Maximum Takeoff Weight (1)  127,868 lbs (58,000 kgs) 
Maximum Landing Weight (2)  114,000 lbs (51,709 kgs) 
　
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