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时间:2011-03-27 08:52来源:蓝天飞行翻译 作者:admin
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No specific circuit breaker(s) safety clip(s) No specific warning notice
 B. Consumable Materials
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 11-003 USA ASTM D 740
 METHYL-ETHYL-KETONE (Ref. 20-31-00) Material No. 19-003 USA AMS 3819
 LINT-FREE COTTON CLOTH (Ref. 20-31-00) C. Expendable Parts


 -------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN -------------------------------------------------------------------------------
1 seal 54-54-11 01B-180 1 seal 54-54-11 01B-180A 2 seal 54-54-11 01B-190 2 seal 54-54-11 01B-190A
 D. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
29-00-00-910-002 Safety Procedures of the Hydraulic System 54-54-00-000-001 Removal of the Aft Fixed Fairing 54-54-00-400-001 Installation of the Aft Fixed Fairing 78-30-00-081-041 Make the Thrust Reverser Serviceable after
 Maintenance 78-30-00-481-041 Make the Thrust Reverser Unserviceable for Maintenance 54-54-41-991-001 Fig. 801
 3. Job Set-up
__________
 Subtask 54-54-41-865-050
 A. Open, safety and tag this(these) circuit breaker(s):
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU HYD/HYD PWR/B WARN/& CTL 2702GJ C12 121VU HYDRAULIC/HYD POWER/Y 3803GX N30 123VU B HYD/ELEC PUMP 2701GJ AB09 123VU Y HYD/ELEC/PUMP 3802GX AB06 123VU Y HYD/ELEC/ELEC PUMP/NORM 3801GX AB03


 Subtask 54-54-41-941-050

 B. Safety Precautions
 (1)
 On the center pedestal, on the ENG panel 115VU:

 (a) Put a warning notice to tell persons not to start the engine.

 (2)
 Make sure that the engine 1(2) shutdown occurred not less than 5 minutes before you do this procedure.

 (3)
 On the overhead maintenance panel 50VU:

 (a)
 Make sure that the ON legend of the ENG/FADEC GND PWR/1(2) pushbutton switch is off.

 (b)
 Put a warning notice to tell persons not to energize the FADEC 1(2).

 

 (4)
 Obey the safety procedures of the hydraulic system (Ref. TASK 29-00-00-910-002)


 Subtask 54-54-41-040-050
 C. Aircraft Maintenance Configuration
 (1) Make the thrust reverser unserviceable (Ref. TASK 78-30-00-481-041). Subtask 54-54-41-020-050
 D. Removal of the Components
 (1) Remove the aft fixed fairing (Ref. TASK 54-54-00-000-001).

 4. Procedure
_________

 (Ref. Fig. 801/TASK 54-54-41-991-001) Subtask 54-54-41-010-051
 A. Removal of the Aft Fixed Fairing Seals
 WARNING : USE SOLVENTS/CLEANING AGENTS, SEALANTS AND OTHER SPECIAL

_______ MATERIALS ONLY WITH A GOOD SUPPLY OF AIR. OBEY THE MANUFACTURERS INSTRUCTIONS. PUT ON PROTECTIVE CLOTHING. DO NOT GET THEM IN YOUR MOUTH. DO NOT SMOKE. DO NOT BREATHE THE GAS. THESE MATERIALS ARE POISONOUS, FLAMMABLE AND SKIN IRRITANT. GET MEDICAL HELP IF YOUR SKIN OR EYES BECOME IRRITATED.
 (1)
 Remove and discard the seals (1) and (2) from the retainers.

 (2)
 Clean the retainers with CLEANING AGENTS (Material No. 11-003) and a MISCELLANEOUS (Material No. 19-003).


 Subtask 54-54-41-410-050
 B. Installation of the Aft Fixed Fairing Seals
 (1) Put the new seal (1) and the new seal (2) in position on the retainers.
 5. Close-up
________ Subtask 54-54-41-420-051
 A. Installation of the Components
 (1) Install the aft fixed fairing (Ref. TASK 54-54-00-400-001). Subtask 54-54-41-440-050
 B. Aircraft Maintenance Configuration
 (1) Make the thrust reverser serviceable (Ref. TASK 78-30-00-081-041).


 Aft Fixed Fairing Seal
 Figure 801/TASK 54-54-41-991-001
 1EFF :  ALL  1  54-54-41 Page 805 
1  1  May 01/05
 1  1
 1CES  1

 


 Subtask 54-54-41-865-051

 C. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 2701GJ, 2702GJ, 3801GX, 3802GX, 3803GX
 Subtask 54-54-41-942-050
 D. Put the aircraft back to its initial configuration.
 (1)
 Make sure that the work area is clean and clear of tool(s) and other items.

 (2)
 Remove the access platform(s).
 
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