737-300 400 500 AMM 飞机维护手册 飞行操纵 FLIGHT CONTROLS 1(44)

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 NOTE:____ This is the trim for the flaps 1-unit condition.
 (l) (m) (n)  Reduce the airspeed to flaps 15 maneuvering speed, 150 KIAS, and extend the flaps to the 15-unit position, and extend the landing gear.Apply aileron trim to keep the wings level and maintain zero heading change.Write down the amount and direction of aileron trim necessary to maintain straight and level flight.
 NOTE:____ This is the trim for the flaps 15-unit condition.
 (o) (p) (q)  Reduce the airspeed to flaps 40 maneuvering speed, 130 KIAS, and extend the flaps to the 40-unit position.Apply aileron trim to keep the wings level and maintain zero heading change.Write down the amount and direction of aileron trim necessary to maintain straight and level flight.
 NOTE:____ This is the trim for the flaps 40-unit condition.

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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
 (3)  
If the aileron trim necessary to maintain level flight is not in the limits shown in Fig. 501A for the flaps up cruise condition, then do the steps in Trailing Edge Flaps for FLAPS UP Discrepancy Adjustment below.

 (4)  
If the aileron trim necessary to maintain level flight is not in the limits shown in Fig. 501A for the flaps extended to the 40-unit condition, then do the steps in Trailing Edge Flaps Adjustment for 40-Unit Discrepancy below.

 (5)  
If the aileron trim necessary to maintain level flight is not in the limits shown in Fig. 501A for the flaps extended to the 15-unit condition, then do the steps in Trailing Edge Flaps Adjustment for 15-Unit Discrepancy below.

 (6)  
If the aileron trim necessary to maintain level flight is not in the limits shown in Fig. 501A for multiple flight conditions, then do the steps in Trailing Edge Flaps for FLAPS UP and 15-Unit Discrepancy Adjustment below.

 TASK 27-09-71-825-037
 2. Trailing Edge Flaps for FLAPS UP Discrepancy Adjustment
_______________________________________________________
 A. General
 (1)  
This procedure contains instructions for the adjustment of the trailing edge flaps to keep a straight and level flight without high aileron trim. All lateral control surfaces, flaps, and rudder are correctly adjusted for this adjustment.

 (2)  
You can do more than one of the adjustments to correct for lateral trim problems. The charts shown in these tasks are for single adjustments. The results shown in the charts can be added together if you do multiple adjustments.

 B.
References

 (1)  
AMM 27-51-00/201, Trailing Edge Flap System

 (2)  
AMM 27-51-34/501, Outboard Trailing Edge Flap

 (3)  
AMM 27-51-52/501, Outboard Flap Track Fairings

 (4)  
AMM 27-61-00/501, Spoiler Control System

 (5)  
AMM 27-62-00/501, Speed Brake Control System

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A 737-300/400/500MAINTENANCE MANUAL

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A
737-300/400/500MAINTENANCE MANUAL
737-300/400/500 WING AND RUDDER SURFACE MISMATCH RECORD
NOTES:
THE CLEARANCES AT THE LEFT AND RIGHT OUTBOARD FLAPS 1. THE INBD FLAP TE WILL BE SYMMETRICAL WILL BE EQUAL IN 0.12 INCH (3.05 mm) OR LESS. THE WITH THE OPPOSITE INBD CLEARANCES AT THE LEFT AND RIGHT INBOARD FLAPS WILL FLAP TE IN 0.10 INCH (2.54 mm) OR LESS. BE EQUAL IN 0.12 INCH (3.05 mm) OR LESS. MANUALLY 2. THE OUTBD FLAP TE WILL BE PULL DOWN ON THE AFT FLAP WITH APPROXIMATELY SYMMETRICAL WITH THE OPPOSITE OUTBD 100 LBS (45.36 Kg) BEFORE YOU MEASURE THE DISTANCES. FLAP TE IN 0.10 INCH (2.54 mm) OR LESS.
　
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