(9)
Put blanking caps on the ports of the ejection jack (10).
(10)
Remove the nut (13), the washers (12) and the bolt (14) which attaches the ejection jack (10) to the leg assembly (11).
(11)
Remove and discard the cotter pins (4).
(12)
Remove the nuts (5) and the washers (6). The bolts (24) can not be removed at this time.
(13)
Support the ejection jack (10).
(14)
Remove the nuts (23), the washers (2) and the bolts (1).
(15)
Carefully remove the gimbal halves (3) from the ejection jack (10). NOTE : Retain the gimbal halves for the replacement component.
____
(16)
Lift the ejection jack (10) out of its stowage compartment.
(17)
Remove the bolts (24) out of the holes in the structure.
R 1EFF : 001-049, 051-061, 101-105, 201-203, 1 29-22-53Page 405 1 1 Config-1 May 01/05 1 1 1CES 1
TASK 29-22-53-400-001 Installation of the RAT Ejection Jack (2454GE) WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______ START A TASK ON OR NEAR:
-
THE FLIGHT CONTROLS
-
THE FLIGHT CONTROL SURFACES
-
THE LANDING GEAR AND THE RELATED DOORS
-COMPONENTS THAT MOVE. WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROL SURFACES ARE
_______ CLEAR BEFORE YOU PRESSURIZE/DEPRESSURIZE A HYDRAULIC SYSTEM.
WARNING : MAKE SURE THAT THE RAT TRAVEL RANGE IS CLEAR BEFORE YOU
_______ EXTEND/RETRACT THE RAT.
WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______ GEAR.
1. Reason for the Job__________________ Self Explanatory
2. Job Set-up Information______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
No specific warning notice(s)
No specific 1 ACCESS PLATFORM 2M (6 FT)
No specific 1 CONTAINER 1 L (1/4 USGAL)
No specific Torque Wrench : range 0.20 to 3.60 m.daN
(2.00 to 26.00 lbf.ft)
R 1EFF : 001-049, 051-061, 101-105, 201-203, 1 29-22-53Page 406 1 1 Config-1 May 01/05 1 1 1CES 1
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
No specific lockwire 0.4 mm (0.015 in.)
Material No. 02-003 F NSA 307110 TYPE 4 HYDRAULIC FLUID (PHOSPHATE ESTER BASE) (Ref. 20-31-00)
Material No. 04-011 USA MIL-G-4343 SILICONE GREASE PNEUMATIC SYST AND SEALS (Ref. 20-31-00)
Material No. 05-002 USA MIL-P-8116 PUTTY, ZINC CHROMATE GENERAL PURPOSE (Ref. 20-31-00)
C. Expendable Parts
-------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN -------------------------------------------------------------------------------
4 cotter pins 29-22-03 03 -050 4 cotter pins 29-22-03 03A-050
D. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
12-12-29-611-001 Fill the Hydraulic Fluid Reservoir with a Hand Pump 12-12-29-611-002 Fill the Hydraulic Fluid Reservoir with a Hydraulic Service Cart
20-28-00-912-004 Electrical Bonding of Components With Conductive Bolts and Screws and Bonding Straps in the Fuselage and in the Wings (this does not include the tanks)-
29-00-00-864-001 Put the Related Hydraulic System in the Depressurized
Configuration before Maintenance Action 29-00-00-910-002 Safety Procedures of the Hydraulic System 29-10-00-863-003 Pressurize the Blue Hydraulic System with a Ground
Power Supply 29-10-00-864-003 Depressurize the Blue 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
R 1EFF : 001-049, 051-061, 101-105, 201-203, 1 29-22-53Page 407 1 1 Config-1 May 01/05 1 1 1CES 1 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
29-22-00-710-003 Operational Test of the Manual Deployment and the
Retraction of the Ram Air Turbine 29-22-00-820-001 Adjustment of the RAT Doors 29-22-51-000-001 Removal of the Ram Air Turbine 2140GE 29-22-51-400-001 Installation of the Ram Air Turbine 2140GE 32-12-00-010-001 Open the Main Gear Doors for Access 29-22-53-991-001 Fig. 401
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：A320飞机维护手册 AMM HYDRAULIC POWER 液压6(45)
