(3) Lubricate the thermocouple probe bolts (80) with graphite grease (Material No. CP2101).

 (4) Install the four bolts (80) in the thermocouple probe flange. TORQUE the bolts (80) to between 55 and 70 lbf.in (0.62 and 0.79 m.daN). Wirelock the bolts (80) with lockwire 0.8 mm dia (Material No. CP8001) or lockwire 0.8 mm dia (Material No. CP8002).

 (5) Lubricate the electrical cable connector unit bolts (20) with graphite grease (Material No. CP2101).

 (6) Attach the electrical cable connector unit to the forward bracket with bolts (20) and nuts (10). TORQUE the nuts (10) to between 55 and 70 lbf.in (0.62 and 0.79 m.daN).

 (7) Lubricate the mid-conduit bracket bolt (50) with graphite grease (Material No. CP2101).

 F 『 EEFF : ALL E Page 40777-23-10
 E E Feb 01/00 E E ECES E

 F  『
 E  C F M  E
 E  E
 E  56-5B  E
 E  E

 (8) Install the bolt (50), washer (60) and nut (70) at the mid-conduit bracket. TORQUE the nut (70) to between 55 and 70 lbf.in (0.62 and

 0.79 m.daN).

 (9) Remove the blanking caps from the electrical connectors.

 (10) Make sure that the electrical connectors are clean and in the correct condition.

 (11) Connect the 2 electrical cable connectors (30, 40). Tighten the connectors by hand. If necessary, use soft-jawed pliers to fully seat the connectors.

 5. Close-up
________
 Subtask 77-23-10-410-052

 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

 Subtask 77-23-10-440-050
 B. Make the thrust reverser serviceable (Ref. TASK 78-30-00-081-041).
 Subtask 77-23-10-710-051

 C. Do a FADEC ground test (Ref. TASK 73-29-00-710-040).
 Subtask 77-23-10-410-053

 D. Close Access
 (1) Close the fan cowl doors (Ref. TASK 71-13-00-410-040):
 FOR 1000EM1
 437AL, 438AR
 FOR 1000EM2
 447AL, 448AR

 (2) Remove the warning notice(s).

 F 『 EEFF : ALL E Page 40877-23-10
 E E Feb 01/98 E E ECES E F 『 E C F M E E E E 56-5B E E E

 (3) Remove the access platform(s).
 F 『 EEFF : ALL E Page 40977-23-10
 E E Feb 01/98 E E ECES E

 F  『
 E  C F M  E
 E  E

 E 56-5B E
 E E
 ANALYZERS - DESCRIPTION AND OPERATION

_____________________________________
 1. General
_______
R **ON A/C 001-049, 052-099, 101-149, 151-199, 201-299, 301-399, 401-499,
 The engine vibration measurement channel comprises :
 - two transducers (piezoelectric accelerometers)

 - an Engine Vibration Monitoring Unit

 - two vibration indications N1 and N2.
 They appear on the lower display unit of the ECAM, on the engine and cruise
 page.
 The engine vibration system provides the following functions :

 - vibration indication due to rotor unbalance via N1 and N2 slaved tracking filters

 - excess vibration (above advisory levels)

 - fan trim balancing

 - shaft speed (N1 and N2)

 - storage of balancing data

 - BITE and MCDU communication

 - accelerometer selection

 - frequency analysis when the printer is available (option).

 **ON A/C 051-051,
 The engine vibration measurement channel comprises :
 - two transducers (piezoelectric accelerometers)

 - an Engine Vibration Monitoring Unit

 - two vibration indications N1 and N2.
 They appear on the lower display unit of the ECAM, on the engine and cruise
 page.
 The engine vibration system provides the following functions :

 - vibration indication due to rotor unbalance via N1 and N2 slaved tracking filters

 - excess vibration (above advisory levels)

 - fan balancing (phase and displacement)

 - shaft speed (N1 and N2)

 - storage of balancing data

 - initial values acquisition on request

 - BITE and MCDU communication

 - accelerometer selection

 - frequency analysis when the printer is available (option).

 F 『 EEFF : ALL E Page 177-30-00
 E E Aug 01/05 E E ECES ER **ON A/C ALL

 F  『
 E  C F M  E
 E  E
　
中國航空網 m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機維護手冊 AMM ENGINE INDICATING 發動機指示(43)