Maintenance
78-36-00-010-040 Opening of the Thrust Reverser Doors
78-36-00-410-040 Closing of the Thrust Reverser Doors
R 77-21-10-991-308 Fig. 406
3. Job Set-up
__________
Subtask 77-21-10-860-062
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 77-21-10-010-091
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
F 『 EEFF : ALL E Page 46377-21-10
E E Aug 01/04 E E ECES E
F 『
E C F M E
E E
E 56-5B E
E E
(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 77-21-10-040-075
C. Make sure that the thrust reverser is unserviceable (Ref. TASK 78-30-00-481-041).
4. Procedure
_________
R (Ref. Fig. 406/TASK 77-21-10-991-308)
Subtask 77-21-10-420-062
R A. Installation of the Upper Left Thermocouple Lead Assembly (Upper Left R 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 (50), (70), (110) with graphite grease (Material No. CP2101).
R (4) Carefully install the upper left T495 sector (20) in position on the R engine, and engage the upper left T495 sector probes in the LPT case.
R (5) Install the parts which attach the upper left T495 sector as follows:
F 『 EEFF : ALL E Page 46477-21-10
E E Aug 01/04 E E ECES E
F 『
E C F M E
E E
E 56-5B E
E E
R -------------------------------------------------------------------------------R INSTALL | ON | NOTE R | | R Nuts (10) | Studs (30) | On LPT case, at the 9:30 and the 10:30 R | | o'clock positions (Detail B) R | | R Clamp (60) | Bracket (40) | On flange S, at the 10:15 o'clock position R | | (Detail C) R | | R Bolt (50) | | R Bolts (70) | Flange S | At the 10:30 o'clock position (Detail D) R | | R Nuts (80) | | R Clamp (120) | Bracket (100) | On flange S, at the 11 o'clock position R | | (Detail E) R Bolt (110) | |
R (6) TORQUE the nuts (10), (80) to between 100 and 110 lbf.in (1.13 and
1.24 m.daN).
R (7) TORQUE the bolts (50), (110) to between 47 and 53 lbf.in (0.53 and R 0.59 m.daN).
R (8) Make sure that the connectors and receptacles are clean and clear of R unwanted materials.
R (9) Connect the main junction box lead connector (130) to the upper left R T495 sector junction box (parallel junction box) (20).
R (10) TORQUE the connecting nut to between 168 and 186 lbf.in (1.89 and R 2.10 m.daN) and safety with lockwire 0.032 in (0.8 mm) dia (Material R No. CP8001) or lockwire 0.032 in (0.8 mm) dia (Material No. CP8002). R
R Subtask 77-21-10-710-062
R B. Do an Operational Test of the FADEC Ground (with engine non motoring) R (Ref. TASK 73-29-00-710-040).
F 『 EEFF : ALL E Page 46577-21-10
E E Aug 01/04 E E ECES E
F 『
E C F M E
E E
E 56-5B E
E E
5. Close-up
________
Subtask 77-21-10-410-075
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other items.
(2) Close the thrust reverser doors: (Ref. TASK 78-36-00-410-040). FOR 1000EM1 451AL, 452AR. FOR 1000EM2 461AL, 462AR.
(3) Remove the warning notice(s).
Subtask 77-21-10-440-062
B. Make the thrust reverser serviceable (Ref. TASK 78-30-00-081-041). R
Subtask 77-21-10-410-076
R C. Close Access
R (1) Close the fan cowl doors (Ref. TASK 71-13-00-410-040).
R FOR 1000EM1 437AL, 438AR. FOR 1000EM2 447AL, 448AR.
R (2) Remove the warning notice(s).
F 『 EEFF : ALL E Page 46677-21-10
E E Aug 01/04 E E ECES E
R
R
R
F 『
E C F M E
E E
E 56-5B E
E E
TASK 77-21-10-000-029
Removal of the Lower Right Thermocouple Lead Assembly
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 ENGINE INDICATING 发动机指示(29)