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时间:2011-03-27 17:13来源:蓝天飞行翻译 作者:航空
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R (4) Carefully remove the lower left T495 sector (20) from the LPT holes R and from the engine.
R (5) Install the blanking plugs and caps on all disconnected parts. R
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R Lower Left Thermocouple Lead Assembly (Upper Left T495 Sector) R Figure 405/TASK 77-21-10-991-307- 13 (SHEET 1)
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R Lower Left Thermocouple Lead Assembly (Upper Left T495 Sector) R Figure 405/TASK 77-21-10-991-307- 23 (SHEET 2)
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R Lower Left Thermocouple Lead Assembly (Upper Left T495 Sector) R Figure 405/TASK 77-21-10-991-307- 33 (SHEET 3)
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 TASK 77-21-10-400-027
 Installation of the Lower Left Thermocouple Lead Assembly
 1. Reason for the Job
__________________
 Self Explanatory
 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R No specific blanking plugs
R  No specific caps No specific warning notice No specific Torque Wrench : range 36.00 to 220.00 lbf.in
 (0.40 to 2.60 m.daN)
 B. Consumable Materials
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. CP2101 USA MIL-T-5544
 graphite grease (Ref. 70-30-00) R Material No. CP2544 * R Molykote P37 (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 73-29-00-710-040 Operational Test of the FADEC on the Ground (with
 Engine Non motoring)
 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

R 77-21-10-991-307 Fig. 405
 3. Job Set-up
__________
 Subtask 77-21-10-860-061
 A. Aircraft Maintenance Configuration
 (1) On the center pedestal, on the ENG panel 115VU, make sure that a warning notice is in position to tell persons not to start the engine.

 (2) On the overhead maintenance panel 50VU, make sure that the ON legend of the ENG/FADEC GND PWR/1(2) pushbutton switch is off. Make sure that a warning notice is in position to tell persons not to energize the FADEC 1(2).


 Subtask 77-21-10-010-089
 B. Get Access
 (1) Make sure that the fan cowl doors are open: (Ref. TASK 71-13-00-010-040) FOR 1000EM1 437AL, 438AR FOR 1000EM2 447AL, 448AR
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 (2) Make sure that the thrust reverser doors are open: (Ref. TASK 78-36-00-010-040) FOR 1000EM1 451AL, 452AR FOR 1000EM2 461AL, 462AR

 Subtask 77-21-10-040-073
 C. Make sure that the thrust reverser is unserviceable (Ref. TASK 78-30-00-481-041).
 4. Procedure
_________
R (Ref. Fig. 405/TASK 77-21-10-991-307)
 Subtask 77-21-10-420-061
R A. Installation of the Lower Left (L/H) Thermocouple Lead Assembly (Lower R Left T495 Sector)
R (1) Remove blanking plugs and caps.
R (2) Lubricate the threads of the LPT case studs (30) with Molykote P37 R (Material No. CP2544).
R (3) Lubricate the threads of the bolts (60), (70), (120), (150) with R graphite grease (Material No. CP2101).
 
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