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时间:2011-04-02 05:47来源:蓝天飞行翻译 作者:航空
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 28-10-00
 ALL  ú ú 04 Page 252 ú Mar 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 S 092-414
 (11) FOR AIR BLOWER TYPE VENTILATION EQUIPMENT; Do these steps to remove the air blower equipment:
 (a)  
For the main tanks do these steps: 1) Remove the ground from the airplane to the ventilation blower.

 2)  Install the applicable wing tank access doors (AMM 28-11-11/401).

 (b)  
For the surge tank access doors, do these steps: 1) Remove the ground from the airplane to the ventilation

 blower. 2) Install the surge tank access doors (AMM 28-11-11/401).

 (c)  
For the center tank, do these steps: 1) Remove the ground from the airplane to the ventilation


 blower. 2) Install the center tank access doors (AMM 28-11-31/401).
 S 092-415
 (12) Follow approved procedures to clean and return all respiratory equipment.
 S 092-416
 WARNING: CAREFULLY DO THE APPLICABLE PROCEDURE TO REMOVE THE GROUND LOCK
_______ ASSEMBLIES FROM THE LANDING GEAR. INJURY TO PERSONS OR DAMAGE TO EQUIPMENT.
 (13) Remove the ground lock assemblies from the landing gear (AMM 32-00-01/201).
 S 092-417
 WARNING: DO THE ACTIVATION PROCEDURE FOR THE TRAILING EDGE FLAPS.
_______ ACCIDENTAL OPERATION OF THE TRAILING EDGE FLAPS COULD CAUSE INJURY TO PERSONS.
 (14) Do the activation procedure for the trailing edge flaps (AMM 27-51-00/201).
 S 092-418
 WARNING: MAKE SURE NO PERSONS ARE IN THE SLAT AREA WHEN YOU DO THE
_______ ACTIVATION OF THE LEADING EDGE SLAT PROCEDURE. IF PERSONS ARE IN THE SLAT AREA, INJURY CAN OCCUR.
 (15) Do the activation of the leading edge slat procedure (AMM 27-81-00/201).
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 28-10-00
 ALL  ú ú 04 Page 253 ú Mar 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 S 862-419
 (16) Close these circuit breakers and remove DO-NOT-CLOSE tags:
 (a)  P6 Main Power Distribution Panel
 1) TANK-1 FWD BOOST PUMP
 2) TANK-2 FWD BOOST PUMP
 3) TANK-1 AFT BOOST PUMP
 4) TANK-2 AFT BOOST PUMP
 5) CENTER TANK BOOST PUMP LEFT
 6) CENTER TANK BOOST PUMP RIGHT

 S 412-421
 (17)
 Connect the storage battery (AMM 24-31-11/201).

 S 942-422

 (18)
 Remove all precautionary signs.


 S 652-507
 WARNING:_______DO THE FUEL TRANSFER PROCEDURE TO REMOVE AIR POCKETS. AIR POCKETS CAN CAUSE THE ENGINE TO STOP IN FLIGHT.
 (19) If the fuel feed line in the No. 2 tank was disconnected, do these steps before the airplane is put back into service:
 (a)  
Put fuel into the fuel tanks (AMM 12-11-00/301).

 (b)  
Do this task: Fuel Transfer to Remove Air Pockets from the Engine Fuel Feed Line Adjacent to the Defueling Valve (AMM 28-23-00/201).


 TASK 28-10-00-102-149
 4.  Apply the Biocide to the Fuel Tanks___________________________________
 A. General
 (1)  Microbes or fungus are the usual cause of structural corrosion of the fuel tank. They also cause deterioration of the components in the fuel tank. The microbes and fungus increase in number at the interface of the fuel and the water. To prevent this problem, decrease the quantity or remove all of the water kept in the tanks. If you find microbes or fungus in the tank, refer to 28-11-00/701 to clean the tank.
 B. Equipment
 (1)  Cart - Hydrant, Portable, Biocide Injection, Model 800 or equivalent Hammonds Technical Services 15740 West Hardy Road Houston, Texas 77060-3147 Phone: (800)582-4224
 C. Consumable Materials
 (1)  One of these two biocides:
 (a)  
G00452 - Biobor JF, Biocide

 (b)  
G02347 - Kathon FP 1.5 biocide, Rohm and Haas Company, Philadelphia, PA, (215) 592-3000


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