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时间:2011-03-24 08:39来源:蓝天飞行翻译 作者:admin
曝光台 注意防骗 网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者

R  (35) when you loosen the hose/tube coupling nut. 
R  (7) Remove the union/reducer (65) and the packing (60) from the pressure 
R  port on the pump (35) and discard the packing (60). 
R  (8) Remove the pump (35) as follows:
 (a) Loosen the four mount nuts (50). 
R  (b) Turn the pump (35) in a clockwise direction so that the nut goes 
R  through the large part of the hole in the pump flange. 
R  (c) Move the pump (35) forward and remove it from the engine.

 

R  Yellow Engine Pump (Vickers) Figure 401/TASK 29-13-51-991-300
 1EFF : 1 1 1CES  ALL  1 111 29-13-51 Page 405 May 01/05

 

R  (9) Remove and discard the gasket (45) from the mount pad. 
R  (10) Remove the packing (40) from the pump input splined-shaft and discard 
R  the packing (40). 
R  (11) Put protective covers on the end of the hose/tube assemblies, the 
R  unions, the unions/reducers, the pump and the electrical connector. 
R  (12) Put blanking plugs on the open end of the pump and on the gearbox 
R  mount pad.

 

 TASK 29-13-51-400-004
 Installation of the Yellow Engine Pump (3030GD)
 WARNING : OBEY THE HYDRAULIC SAFETY PROCEDURES._______
 WARNING : DO NOT TOUCH THE HYDRAULIC SYSTEM COMPONENTS FOR A SHORT TIME AFTER_______ THE ENGINE IS SHUTDOWN. THE ENGINE COMPONENTS STAY HOT FOR SOME TIME AND CAN CAUSE INJURY.
 CAUTION : DO NOT LET HYDRAULIC FLUID FALL ON THE ENGINE. UNWANTED HYDRAULIC_______ FLUID MUST BE REMOVED IMMEDIATELY WITH A CLEAN LINT FREE CLOTH. THE FLUID CAN CAUSE DAMAGE TO THE SURFACE PROTECTION AND TO SOME PARTS.
 1. Reason for the Job__________________
 Self Explanatory
 2. Job Set-up Information______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R R R R R  No specific No specific No specific No specific No specific No specific No specific  warning notice(s)access platform 1.50 m (4 ft. 11 in.)container 5 l (1.3208 USgal)container 8 l (2.1133 USgal) Torque Wrench : range 96.00 to 900.00 lbf.in (1.00 to 10.00 m.daN) Torque Wrench : range 180.00 to 1800.00 lbf.in (2.00 to 20.00 m.daN)Torque Wrench : range 0.20 to 3.60 m.daN (2.00 to 26.00 lbf.ft) 
B. Consumable Materials
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 02-003  F NSA 307110 TYPE 4 HYDRAULIC FLUID (PHOSPHATE ESTER BASE) (Ref. 20-31-00)

 

 C. Expendable Parts
 -------------------------------------------------------------------------------
FIG.ITEM |DESIGNATION  |IPC-CSN
 -------------------------------------------------------------------------------
30 packing  29-13-51 02A-040
R  40 packing 29-13-51 01 -140 45 gasket 29-13-51 02A-020 55 packing 29-13-51 02A-060 60 packing 29-13-51 02A-090
 D. Referenced Information
 -------------------------------------------------------------------------------
REFERENCE  DESIGNATION
 -------------------------------------------------------------------------------
12-12-29-611-001  Fill the Hydraulic Fluid Reservoir with a Hand Pump
 24-41-00-861-002  Energize the Aircraft Electrical Circuits from the
 External Power
 24-41-00-862-002  De-energize the Aircraft Electrical Circuits Supplied
 from the External Power
 29-10-00-710-001  Operational Check of Hydraulic Fire Shut Off Valves
 and Associated Indicating System
 29-13-00-710-002  Operational Test of the Yellow Hydraulic System
 29-14-00-614-001  Depressurization of the Hydraulic Reservoirs
 29-14-00-614-002  Pressurization of the Hydraulic Reservoirs through
 the Ground Connector
 29-23-00-863-002  Pressurize the Yellow Hydraulic System from the Green
 Hydraulic System through the PTU with the Ground
 Service Cart
 29-24-00-864-001  Depressurize the Yellow Hydraulic System
 31-60-00-860-001  EIS Start Procedure
 31-60-00-860-002  EIS Stop Procedure
 71-13-00-010-040  Opening of the Fan Cowl Doors
 71-13-00-410-040  Closing of the Fan Cowl Doors
 78-31-00-710-042  Operational Test of the Thrust Reverser System
 
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