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Automatic Flight Control System. This system meets the applicable
airworthiness and performance reliability requirements for auto coupled
approaches and landings.
Auxiliary Power Unit (APU)
Limitations
1. >>@ Max EGT: 760°C BCD - N/A
2. >>@ Max Cont: 710°C BCD - N/A
3. APU bleed and electrical maximum altitude: 10,000 ft.
4. APU bleed maximum altitude: 17,000 ft.
5. APU electrical load maximum
altitude:
>>@ BCD
35,000 ft. 41,000 ft.
Operating Parameters
1. >>@ Do not operate APU above FL 350.
2. Operate one minute before using pneumatic air. Operate one minute with
pneumatics off prior to shutdown.
3. Aborted Starts: Ground - Allow 4 minutes between starts
- Maximum 2 start attempts
Air - Allow 4 minutes between starts
- Maximum 4 start attempts
737
Flight Manual Continental
Sec. 1 Page 9
Rev. 11/15/02 #41
4. >>@ Successful starts not assured above FL 250.
5. After shutdown, wait 20 seconds for inlet door to close before turning
battery switch to OFF.
Enhanced Ground Proximity Warning System
Limitations
1. Do not use the terrain display for navigation.
2. The uses of terrain awareness alerting and terrain display functions are
prohibited within 15 nm and approaching to land at an airport not contained
in the GPWS terrain database.
Note: ALL CAL Ops Spec Authorized Airports have been verified to
be included in the EGPWS terrain database.
3. The use of Terrain Awareness and Terrain Display functions are prohibited
when the FMC is in IRS only operation.
4. For takeoff, the use of Terrain Awareness and Terrain Display functions are
prohibited until position verification has been accomplished.
5. For ditching, or other off-airport landings, the terrain awareness alerting
and terrain display functions should be inhibited by selecting the TERR
INHIBIT switch in INHIBIT.
Sec. 1 Page 10
Rev. 11/15/02 #41 Continental
737
Flight Manual
Communication
Limitations
The Aircraft Communications And Reporting System (ACARS) is limited to
transmission and receipt of messages that will not create an unsafe condition if
the message is improperly received, such as the following conditions:
· The message or parts of the message are delayed or not received,
· The message is delivered to the wrong recipient, or
· The message content may be frequently corrupted.
1. Do not use VHF-3 for ATC communications with ACARS operational, or
if audio entertainment system is in use.
2. Do not use VHF COMM #2 or VHF COMM #3 on 120.00 MHZ as a
primary means of communication. If frequency 120.00 MHZ is required
use VHF COMM #1.
3. When placard installed use VHF-2 for primary ATC COMM on ground.
4. BCD The following HF frequencies are prohibited:
Listed in MHZ: 11.133 22.434 22.683 22.766
Operating Parameters
BCD Use the VHF radio connected to the top of the fuselage antenna
for primary ATC communications on the ground.
737
Flight Manual Continental
Sec. 1 Page 11
Rev. 11/15/02 #41
Electrical Power
Limitations
1. BCD Maximum single engine drive generator load: 75KVA –
215 amps (ground operations).
Operating Parameters
1. Minimum battery voltage for APU start: 23 volts
2. >>@ Maximum engine driven generator load: 125 amps
3. >>@ Maximum TR load: 65 amps
50 amps (ground operation without
cooling)
4. TR voltage range: 24 - 30 volts
5. Battery bus voltage range: 22 - 30 volts
Fire Protection
Limitations
1. >>@ Smoke Detection & Fire Suppression System (Ref. STC
ST01674AT):
A. The cargo compartment smoke detector and fire suppression system
must be verified to be serviced and operational before cargo can be
carried in the cargo compartments.
B. The aircraft must land at the nearest suitable airport within 60 minutes
after the activation of the suppression system.
Operating Parameters
1. Lavatory fire extinguishing: If evidence of overtemperature as indicated by
black placard dot(s) or nozzle discharge (nozzle tip turns aluminum color),
maintenance action required.
2. Engine fire extinguisher bottle pressure: 800 psi @ 70°F.
Sec. 1 Page 12
Rev. 11/15/02 #41 Continental
737
Flight Manual
Flight Controls
Limitations
1. Maximum flap extension altitude: 20,000 ft.
2. BCD Holding in icing conditions with flaps extended is
prohibited.
3. BC Per Airworthiness Directives 2001-12-51 and 2002-08-52, “Do
not operate the airplane at speeds in excess of 300 KIAS with speedbrakes
　
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