EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 12-33-02
 ALL  ú ú 01A Page 301 ú Feb 18/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL

 CAUTION: IF YOU CAN DRAIN THE FUEL FROM THE DRAIN VALVE AFTER YOU
_______ APPLIED HOT AIR TO THE EXTERIOR FOR 3 TO 5 MINUTES, DO NOT THINK THAT ALL THE ICE IS MELTED. THE ICE ADJACENT TO THE DRAIN VALVE UNIT CAN MELT AND LET SOME WATER AND FUEL FLOW FROM THE DRAIN. BUT, A PIECE OF ICE CAN STAY BEHIND. IF THE FUEL DOES NOT FLOW FROM THE DRAIN, CONTINUE TO APPLY HOT AIR FOR A SHORT TIME, AND FREQUENTLY DO A CHECK OF THE FLOW FROM THE DRAIN. CATCH THE FUEL IN A CONTAINER AND MAKE SURE ALL OF THE WATER IS REMOVED.
 THE HEAT APPLIED TO THE SUMP DRAIN VALVES FOR THE OUTBOARD MAIN AND RESERVE THANKS WILL NOT REMOVE THE ICE WHICH HAS COLLECTED IN THE TANK SUMP OR IN THE DRAIN LINE BETWEEN THE TANK SUMP AND VALVE. TO REMOVE THIS ICE, YOU MUST PUT THE AIRPLANE IN A WARM HANGAR FOR SUFFICIENT TIME TO MELT THE ICE. THEN DRAIN THE SUMPS UNTIL THE WATER IS REMOVED.
 (3)  
In cold weather it is necessary to drain the fuel tank sumps prior to refueling to remove water from the fuel tanks if the airplane has been idle for more then 45 minutes prior to refueling. Drain the fuel tanks sumps again after refueling if the airplane has been idle for 2 hours or more after refueling, prior to departure (AMM 12-11-03/301).

 (4)  
When adding fuel, you must use these requirements:

 (a)  Make sure the fuel temperature is at least 6°F (3°C) above the fuel freeze point or -45.4°F (-43°C), whichever is higher. Use the ASTM method to determine the freeze point.
 NOTE: The Fuel Quantity Indicator on the wing fuel station can
____ indicate slowly or not show numbers in extreme cold conditions. Use an external fuel flow meter to show the amount of fuel added to the airplane.
 (b)  
Use fuels that meet specification ASTM D1655; or

 (c)  
Use fuels that meet specification GOST 10227:
 1) RT (PT, Russian spelling)
 2) TS-1 (TC-1, Russian spelling)

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 12-33-02
 ALL  ú ú 02A Page 302 ú Jun 18/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
 B.
C.
D.
A
747-400 MAINTENANCE MANUAL
 (d)  Approved fuel additives are:
 NOTE: Adding an anti-icing fuel additive may help in the
____
 sumping of the fuel tanks.

 1)  Fuel Additive, specification GOST 8313, Fluid I (also known as Fluid E) a) Fluid I may be used at a mixture of no more than 0.15
 percent by volume.
 2)  Fuel Additive, specification TU-6-10-1458, Fluid I-M (also known as Fluid E- Methanol) a) Fluid I-M may be used at a mixture of no more than 0.15
 percent each, by volume. 3) Fuel Additive, specification GOST 17477, Fluid TGF a) Fluid TGF may be used at a mixture of no more than 0.15 percent by volume.
 4)  Fuel Additive, specification TU-6-10-1457, Fluid TGF-M (also known as Fluid TGF- Methanol) a) Fluid TGF-M may be used at a mixture of no more than
 0.15 percent each, by volume.References
 (1)  
AMM 10-11-01/201, Park the Airplane (Normal Parking)

 (2)  
AMM 12-13-07/301, IDG Oil Fill

 (3)  
AMM 12-15-03/301, Wing Landing Gear Shock Strut Fluid Check

 (4)  
AMM 12-15-04/301, Body Landing Gear Shock Strut Fluid Check

 (5)  
AMM 12-15-05/301, Nose Landing Gear Shock Strut Fluid Check

 (6)  
AMM 12-15-06/301, Landing Gear Tire Pressure Check

 (7)  
AMM 12-33-01/301, Cold Weather Maintenance Procedure

 (8)  
AMM 12-33-02/301, Interior Ice Removal

 (9)  
AMM 21-00-00/201, Supply Conditioned Air to the Airplane

 (10)
 AMM 24-22-00/201, Supply Electrical Power

 (11)
 29-11-00/201, Main Hydraulic Systems

 (12)
 AMM 32-41-17/401, Brake Disconnect Removal/Installation

 (13)
 AMM 32-42-00/501, Antiskid/Autobrake System - Functional Check
　
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 SERVICING 2(117)