Copyright . The Boeing Company. See title page for details.
December 3, 2004 L.10.7
Limitations -Operating Limitations 737 Operations Manual
Serial No. 26309
Maximum Taxi Weight 139,392 lbs (63,227 kgs)
Maximum Takeoff Weight (1) 138,892 lbs (63,000 kgs)
Maximum Landing Weight (2) 114,000 lbs (51,709 kgs)
Maximum Zero Fuel Weight 106,500 lbs (48,307 kgs)
Serial No. 26283
Maximum Taxi Weight 140,000 lbs (63,502 kgs)
Maximum Takeoff Weight (1) 139,500 lbs (63,276 kgs)
Maximum Landing Weight (2) 114,000 lbs (51,709 kgs)
Maximum Zero Fuel Weight 105,000 lbs (47,627 kgs)
Serial No. 25162
Maximum Taxi Weight 140,000 lbs (63,502 kgs)
Maximum Takeoff Weight (1) 139,500 lbs (63,276 kgs)
Maximum Landing Weight (2) 114,000 lbs (51,709 kgs)
Maximum Zero Fuel Weight 106,500 lbs (48,307 kgs)
Copyright . The Boeing Company. See title page for details.
L.10.8 December 3, 2004
Limitations -Operating Limitations 737 Operations Manual
Serial No. 26307, 26333 & 28200
Maximum Taxi Weight 140,000 lbs (63,502 kgs)
Maximum Takeoff Weight (1) 139,500 lbs (63,276 kgs)
Maximum Landing Weight (2) 116,600 lbs (52,888 kgs)
Maximum Zero Fuel Weight 106,500 lbs (48,307 kgs)
Serial No. 23788, 26282, 26286, 26293, & 26301
Maximum Taxi Weight 140,000 lbs (63,502 kgs)
Maximum Takeoff Weight (1) 139,500 lbs (63,276 kgs)
Maximum Landing Weight (2) 116,600 lbs (52,888 kgs)
Maximum Zero Fuel Weight 109,600 lbs (49,713 kgs)
All Airplanes
C. G. Limits Use approved weight and
balance system
(1)
May be further restricted by takeoff, enroute, and landing performance.
(2)
May be further restricted by field length or climb limit.
Air Systems
The maximum cabin differential pressure (relief valves) is 8.65 psi.
Non–AFM Air Systems Operational Information
Note: The following items are not AFM limitations but are provided for flight crew information.
With engine bleed air switches ON, do not operate the air conditioning packs in HIGH for takeoff, approach or landing.
Limitations -Operating Limitations 737 Operations Manual
Anti–Ice, Rain
Engine TAI must be on when icing conditions exist or are anticipated, except during climb and cruise below –40°C SAT.
Autopilot/Flight Director System
Do not use aileron trim with autopilot engaged.
For airplanes operated under FAA rules:
.
Do not engage the autopilot for takeoff below 1000 feet AGL
.
For single channel operation, the autopilot shall not be engaged below 50 feet AGL.
.
See AFM limitations on automatic landing.
For airplanes operated under CAA rules:
.
Do not engage the autopilot for takeoff or during climb below 1000 feet AGL
.
The autopilot must be disengaged descending below 1000 feet ARTE
unless coupled to an ILS glide slope and localizer or in the V/S mode
.
In a single channel ILS approach, the autopilot must be disengaged at or below 140 feet ARTE
.
In an approach using V/S mode, the autopilot must be disengaged at or
above 300 feet ARTE.
.
See AFM limitations on automatic landing.
Communications
Do not use VHF–3 for ATC Communications with ACARS (as installed) operational.
Note: The following limitation is applicable to airplanes which have not incorporated the effects of Honeywell service bulletin 4051600–22–0023 which installs a Honeywell flight control computer to correct the VHF-2 squelch break anomoly.
Because of unacceptable electromagnetic interference between the flight control computer, the EFIS symbol generator, and the VHF–2 antenna, do not use VHF–2 on 120.000 MHz or 120.005 MHz as a primary means of communication. If frequency 120.000 MHz or 120.005 MHz is required, use VHF–1.
On airplanes equipped with Rockwell/Collins Model HFS–700 and/or HFS–900 communication transceivers, flights predicated on the use of the following HF frequencies are prohibited:
.
11.133 MHz
.
22.434 MHz
Copyright . The Boeing Company. See title page for details.
L.10.10 December 3, 2004
Limitations -Operating Limitations 737 Operations Manual
.
22.683 MHz
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