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时间:2011-03-27 16:58来源:蓝天飞行翻译 作者:航空
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R (4) TORQUE self locking borescope cap assemblies to between 50 and 55 R lbf.in (0.56 and 0.62 m.daN).

R NOTE : To achieve the correct installation of the self locking
____ R borescope cap assembly, the slot of its ring must be R positioned on the borescope boss lug at the final tightening.
R END OF SB CFMI 72-0376
R 5. Close-up
________
R Subtask 72-54-00-410-096
R A. Close Access
R (1) Make sure that the work area is clean and clear of tool(s) and other R items.
R (2) Close the thrust reverser cowl doors (Ref. TASK 78-36-00-410-040): R FOR 1000EM1 R 451AL, 452AR R FOR 1000EM2 R 461AL, 462AR
R Subtask 72-54-00-440-066
R B. Make the thrust reverser serviceable (Ref. TASK 78-30-00-081-041).
R Subtask 72-54-00-410-097
R C. Close Access
R (1) Close the fan cowl doors (Ref. TASK 71-13-00-410-040): R FOR 1000EM1 R 437AL, 438AR R FOR 1000EM2 R 447AL, 448AR
R (2) Remove the warning notice(s).
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 E E TASK 72-54-00-290-008

 Inspection of the Stage 1-4 Stationary Air Seals
 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 No specific Torque Wrench : range 36.00 to 220.00 lbf.in
 (0.40 to 2.60 m.daN) 856A1320 1 BORESCOPE KIT 856A1322 1 BORESCOPE - LIGHT SOURCE SET
 B. Consumable Materials
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. CP2101 USA MIL-T-5544
 graphite grease (Ref. 70-30-00) Material No. CP2619 *
 Never Seez-Pure Nickel, Special (Ref. 70-30-00) Material No. CP8001 *
 lockwire 0.032 in. (0.8 mm) dia. (Ref. 70-30-00) Material No. CP8002 *
 lockwire 0.032 in. (0.8 mm) dia. (Ref. 70-30-00)
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 C. Referenced Information

 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
71-13-00-010-040 Opening of the Fan Cowl Doors 71-13-00-410-040 Closing of the Fan Cowl Doors 72-00-00-200-025 Over-Serviceable-Limit Extensions 78-30-00-081-041 Make the Thrust Reverser Serviceable after
 Maintenance 78-30-00-481-041 Make the Thrust Reverser Unserviceable for
 Maintenance 78-36-00-010-040 Opening of the Thrust Reverser Doors 78-36-00-410-040 Closing of the Thrust Reverser Doors 72-54-00-991-300 Fig. 601 72-54-00-991-301 Fig. 602 72-54-00-991-302 Fig. 603
 3. Job Set-up
__________
 Subtask 72-54-00-941-059
 A. 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).

 


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 B. Get Access
 (1) Open the fan cowl doors (Ref. TASK 71-13-00-010-040):
 FOR 1000EM1
 437AL, 438AR
 FOR 1000EM2
 447AL, 448AR

 (2) Allow parts, to return to ambient temperature. Subtask 72-54-00-040-059

 C. Make the thrust reverser unserviceable (Ref. TASK 78-30-00-481-041). Subtask 72-54-00-010-078


 D. Open the thrust reverser doors (Ref. TASK 78-36-00-010-040):
 FOR 1000EM1
 451AL, 452AR
 FOR 1000EM2
 461AL, 462AR
 
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