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时间:2011-03-24 08:43来源:蓝天飞行翻译 作者:admin
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 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
29-00-00-864-001 29-00-00-910-002 29-14-00-614-001 29-23-00-860-001 32-12-00-010-001 29-32-11-991-001  Put the Related Hydraulic System in the Depressurized Configuration before Maintenance ActionSafety Procedures of the Hydraulic SystemDepressurization of the Hydraulic ReservoirsDisconnection of the Isolation Coupling of the Power Transfer Unit (PTU)Open the Main Gear Doors for AccessFig. 401

 

 3. Job Set-up__________
 Subtask 29-32-11-010-052
 A. Get Access
 (1) Open one main door of the main gear (Ref. TASK 32-12-00-010-001).
 (2) Open the access panel 196BB.
 Subtask 29-32-11-865-052
 B. Open, safety and tag this(these) circuit breaker(s):
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU HYD/HYD/PRESS/XMTR 1841GN C11
 Subtask 29-32-11-860-053
 C. Aircraft Maintenance Configuration
 WARNING : OBEY THE HYDRAULIC SAFETY PROCEDURES._______
 (1) Obey the hydraulic safety procedures (Ref. TASK 29-00-00-910-002).
 (2) Make sure that the Yellow hydraulic system is depressurized and put it in the maintenance configuration. (Ref. TASK 29-00-00-864-001).
 (3) Depressurize the reservoir of the Yellow hydraulic system (Ref. TASK 29-14-00-614-001). 
R R R R  (4) Put a WARNING NOTICE in position to tell persons not to pressurize the Yellow hydraulic system: - in the cockpit on the hydraulic section 40VU of the overhead panel - on the ground service panel of the Yellow hydraulic system.
 (5) Disconnect the isolation coupling of the Power Transfer Unit (PTU) (Ref. TASK 29-23-00-860-001). 
R R  (6) Put the CONTAINER 3 L(3/4 USGAL) in position below the hydraulic pressure transducer to collect hydraulic fluid.

 

 4. Procedure_________
 (Ref. Fig. 401/TASK 29-32-11-991-001)
 Subtask 29-32-11-020-055 
R  A. Removal of the Hydraulic Pressure Transducer
 (1) Disconnect the electrical connector (1). 
R  (2) Put the CAP - BLANKING on the disconnected electrical connector (1).
R R  (3) Remove the nut (7), the washer (8), the screw (10), the bonding jumper (9) and the clamp (11) from the hydraulic pressure transducer (2).
 (4) Remove the two bolts (3) and the two washers (4). 
R R  (5) Loosen the hydraulic pressure transducer (2) and remove it at the same time with the O-ring (5) from the manifold (6).
 (6) Discard the O-ring. 
R  (7) Install the PLUG - BLANKING in the open ports.

 

 TASK 29-32-11-400-003 Installation of the Hydraulic Pressure Transducer (3065GN) 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 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  1 CONTAINER 3 L(3/4 USGAL)
 No specific 2 WARNING NOTICE R No specific Torque Wrench : range 0.00 to 1.20 m.daN R (0.00 to 9.00 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 -------------------------------------------------------------------------------
O-ring  32-44-18 01A-010 D. Referenced Information


 -------------------------------------------------------------------------------
REFERENCE DESIGNATION
 -------------------------------------------------------------------------------
20-28-00-912-004 Electrical Bonding of Components With Conductive Bolts and Screws and Bonding Straps in the Fuselage R and in the Wings (this does not include the tanks)-29-00-00-864-001 Put the Related Hydraulic System in the Depressurized
 
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