F 『
E C F M E
E E
E 56-5B E
E E
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
24-41-00-861-002 Energize the Aircraft Electrical Circuits from the External Power
24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied from the External Power
31-32-00-860-012 Procedure to Get Access to the SYSTEM REPORT/TEST/ENG Page
31-60-00-860-001 EIS Start Procedure
31-60-00-860-002 EIS Stop Procedure
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
77-22-10-991-301 Fig. 401
3. Job Set-up
__________
Subtask 77-22-10-860-052
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).
F 『 EEFF : ALL E Page 40977-22-10
E E Feb 01/98 E E ECES E Subtask 77-22-10-010-057
F 『
E C F M E
E E
E 56-5B E
E E
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
(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 77-22-10-040-053
C. Make sure that the thrust reverser is unserviceable (Ref. TASK 78-30-00-481-041).
4. Procedure
_________
(Ref. Fig. 401/TASK 77-22-10-991-301) Subtask 77-22-10-420-051
A. Installation of the T5 Sensor: CAUTION : THE DESIGN OF T5 SENSOR ASSEMBLY IS SUCH THAT IT CAN BE EASILY
_______ DAMAGED IF YOU HANDLE IT WITHOUT PRECAUTION. DO NOT USE FORCE AND PREVENT CONDITIONS WHICH PUT IT UNDER STRAINS AND STRESSES.
(1) Assemble the bracket (170) to the T5 sensor (10) connector as follows:
(a) Clean the component interface and/or the adjacent area.
(b) Do an inspection of the component interface and/or the adjacent area.
(c) Remove the blanking cap from the T5 sensor (10) connector.
(d) Apply a thin layer of graphite grease (Material No. CP2101) to the threads of the 4 screws (120).
F 『 EEFF : ALL E Page 41077-22-10
E E Feb 01/98 E E ECES E
F 『
E C F M E
E E
E 56-5B E
E E
(e) Engage the T5 sensor connector through bracket (170). Attach the bracket to the connector with screws (120) and half-plates (160).
(f) TORQUE the screws (120) to between 9.5 and 10.5 lbf.in (0.10 and
0.11 m.daN). Safety the screws in pairs with a lockwire 0.6 mm (0.0236 in.) dia. (Material No. CP8004) or lockwire 0.6 mm (0.0236 in.) dia. (Material No. CP8005).
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(38)
