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extended.
WARNING: Use of speedbrakes at speeds in excess of 320 KIAS
could result in a severe vibration which, in turn, could
cause extreme damage to the horizontal stabilizer.”
Note: Under the Captains Emergency Authority and after careful
consideration, speedbrake deployment above 300 KIAS may be
accomplished for emergency descent.
4. In flight, do not extend the speedbrake lever beyond the FLIGHT
DETENT.
5. Flap limit speeds (IAS):
>>@ :
1 - 230 knots 15 - 195 knots
2 - 230 knots 25 - 190 knots
5 - 225 knots 30 - 185 knots
10 - 210 knots 40 - 158 knots
B :
1 - 230 knots 15 - 195 knots
2 - 230 knots 25 - 170 knots
5 - 225 knots 30 - 165 knots
10 - 210 knots 40 - 156 knots
CD :
1 - 230 knots 15 - 200 knots
2 - 230 knots 25 - 190 knots
5 - 225 knots 30 - 175 knots
10 - 210 knots 40 - 162 knots
The label designates an AFM limitation which has been further restricted by
Company policy.
737
Flight Manual Continental
Sec. 1 Page 13
Rev. 11/15/02 #41
Operating Parameters
1. Alternate flap duty cycle (flight): One cycle:
Flaps 0-15 5 minutes off
Flaps greater than 15 25 minutes off
2. Alternate flap operation: Maximum airspeed - 230 knots to extend.
3. Speedbrake usage:
A. Should not be deployed in flight at radio altitudes less than 1000 ft.
B. Speedbrakes should not be deployed with flaps extended beyond flaps
15.
4. Mach Trim Fail (both channels):
>>@ BCD
280 KIAS / .74 Mach 280 KIAS / .82 Mach
Flight Management Computer
Operating Parameters
1. See MEL for restrictions.
2. Do not use the autopilot or the autothrottle for approach if the associated
radio altimeter is inoperative.
3. The Flight Management Computer has been demonstrated to meet the
requirement of FAA Advisory Circular 20-130A for a multi-sensor area
navigation system when operated with radio or Global Position System
(GPS) (if installed) updating. When operated in this configuration, the
FMCS may be used for enroute and terminal operations.
4. The FMCS with dual FMC installation may be used as primary means for
navigation for instrument approaches (excluding ILS, LOC, LOC-BC,
LDA, SDF, and MLS) with ACTUAL (ANP) less than RNP.
5. The FMCS with single FMC installation may be used as a supplement to
other primary means navigation for instrument approaches (with the
exception of specifically approved and identified RNAV approaches).
6. BCD ADIRU alignment must not be attempted at latitudes greater
than 78 degrees 15 minutes.
737
Flight Manual Continental
Sec. 1 Page 14
TR 03-01 01/01/03
Fuel
Limitations
1. BCD (ETOPS) Perform an operational check of the fuel crossfeed
valve during the last hour of cruise flight during each extended range
operation. Enter valve failure conditions resulting from the operational
check in the airplane log.
2. Maximum tank fuel temperature: 49°C.
3. Inflight tank fuel temperature must be maintained at least 3°C above the
freezing point of the fuel being used or -45°C, whichever is higher.
4. Lateral fuel imbalance between wing tanks 1 and 2 must be scheduled to be
zero. Random fuel imbalance must not exceed 1000 lbs.
5. Fuel Crossfeed valve must be closed for takeoff and landing.
6. Center tank fuel pump switches
Ground Operations (Per A.D. 2001-08-24)
· Center tank fuel pump switches must not be positioned to ON unless
the center tank fuel quantity exceeds 1000 pounds (453 kilograms),
except when defueling or transferring fuel.
· Center tank fuel pump switches must be positioned to OFF when both
center tank fuel pump low-pressure lights illuminate.
· Center tank fuel pump switches must not be positioned to ON unless
personnel are available on the flight deck to monitor low-pressure
lights.
Note: Once the center tank fuel pump switches are turned on, they do
not need to be turned off once the fuel quantity depletes to less
than 1000 lbs.
7. BCD Center tank fuel pump switches:
Per AD 2002-19-52, and AD 2002-24-51 with AMOC 140S-02-376:
“The center tank fuel pumps must be OFF for takeoff if center tank fuel is
less than 5,000 lbs. with the airplane readied for initial taxi.
Both center tank fuel pump switches must be selected OFF when center tank
fuel quantity reaches approximately 1,000 lbs. during climb and cruise or
3,000 lbs. during descent and landing. The fuel pumps must be positioned
OFF at the first indication of fuel pump low pressure.”
The center wing tank fuel quantity indication system must be operative to
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