S 822-027

 (2)  
Make sure all the fire extinguishers (Engine, APU, Portable) have been weighed within the 60 day period and are in the weight limits shown on the fire extinguisher nameplate.

 (a)  
Reference: 1) AMM 26-26-01/601, Halon fire extinguisher. 2) AMM 26-26-02/601, Water-type fire extinguisher.

 (b)  
If the weight is below the full weight shown on the nameplate, replace the fire extinguishers.

 S 612-028
 (3)  Make sure the fire extinguisher bottles in the cargo compartment are fully charged (AMM 26-23-01/601).
 NOTE: The fire extinguisher bottles and squibs
____ installed and connected when the airplane is parked.
 H. Flight Controls Deactivation
 S 862-029
 (1)  Move the trailing edge flaps until the flaps complete one full movement of travel.
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 10-11-02
 ALL  ú ú 02 Page 205 ú Oct 18/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL

 S 862-202
 (2)  
Move the leading edge flaps until the flaps complete one full movement of travel.

 S 862-030

 (3)  
Move the stabilizer trim until you complete one full movement of travel.

 S 862-203

 (4)  
Move the rudder trim until you complete one full movement of travel.

 S 862-204

 (5)  
Move the aileron trim until you complete one full movement of travel.

 S 862-205

 (6)  
Move the elevators until you complete three full movements of travel.

 S 862-206

 (7)
Move the rudder until you complete three full movements of travel.

 S 862-031

 (8)  
Move the ailerons until you complete three full movements of travel.

 S 862-032

 (9)  
Operate the rudder ratio changer actuators until you complete three full strokes and put the actuators to their initial position.

 S 642-033

 (10)
 Lubricate all the flight controls with MIL-G-23827 grease
 AMM 12-21-16/301 thru AMM 12-21-23/301).

 S 642-034

 (11)
 Lubricate the control cables which are external to the fuselage pressurize area (AMM 12-21-05/301).

 S 212-035

 (12)
 Make sure the drain holes for the flap and the flap fairing are open.

 S 862-036

 (13)
 Put all the flaps in the FULL UP position (AMM 27-51-00/201 and AMM 27-81-00/201).

 I. Fuel System Deactivation
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 10-11-02
 ALL  ú ú 02 Page 206 ú Oct 18/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 S 652-252
 WARNING:_______ BIOBOR JF IS POISONOUS.  DO NOT BREATH THE VAPOR AND AVOID
 CONTACT WITH THE SKIN.  IF YOU BREATH THE VAPOR OR TOUCH THE
 BIOBOR YOU CAN CAUSE INJURY TO YOURSELF.
 CAUTION:_______ DO NOT ADD CONCENTRATED BIOCIDE TO THE FUEL TANKS.  IF YOU
 ADD CONCENTRATED BIOCIDE TO THE FUEL TANKS, SALT DEPOSITS CAN
 FORM AND CAN CAUSE DAMAGE.  IF METERED INJECTION EQUIPMENT IS
 NOT AVAILABLE, REFER TO CPM 20-62-00, CORROSION PREVENTION
 MANUAL, PART I, FOR OTHER APPROVED PROCEDURES TO ADD BIOCIDE TO

 THE FUEL TANKS.
 (1)  Fill and keep all of the wing fuel and optional horizontal stabilizer fuel tanks at approximately 10 percent capacity (AMM 12-11-01/301).
 NOTE: The fuel should contain 135 to 270 parts per million
____ maximum by weight Biobor JF or 0.05 percent to 0.15 percent by volume PFA55MB (MIL-I-27686) additive to prevent micro-organisms in fuel tanks. The preferred procedure to mix the additive is by metered injection into the flowing stream of fuel. Do a check of the additive ratio each year by chemical test.
　
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：747-400 AMM 飛機維護手冊 PARKING AND MOORING(10)