F 『
E C F M E
E E
E 56 E
E E
TASK 77-00-00-810-890
Type Disagree between Engine 1 and Engine 2
1. Possible Causes
_______________
- Identification Connector
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 31-32-00-860-012 Procedure to Get Access to the SYSTEM REPORT/TEST/ENG Page AMM 73-21-60-400-001 Installation of the Electronic Control Unit
(ECU)(4000KS) AMM 73-21-90-000-002 Removal of the Engine Identification Connector AMM 73-21-90-400-002 Installation of the Engine Identification Connector
3. Fault Confirmation
__________________
A. Test
NOTE : This fault is generated if the installed engine thrust and/or bump
____
rating is not correct.
(1) On the MCDU, get the SYSTEM REPORT/TEST page (Ref. AMM TASK 31-32-00-860-012).
(a) Push the line key adjacent to the FADEC 1A(1B) for engine 1 or 2.
(b) Push the line key adjacent to the LRU identification.
(c) Check that both engines have the same thrust and bump rating (Ref. AMM TASK 73-21-60-400-001).
4. Fault Isolation
_______________
A. Do this procedure:
(1) If engines have not the same thrust and bump rating:
- check engine configuration table to determine which rating is correct, and replace the Identification Connector (Ref. AMM TASK 73-21-90-000-002) and (Ref. AMM TASK 73-21-90-400-002).
(2) If both engines thrust and bump rating are the same:
- check that both engines match the A/C type configuration:
F 『 EEFF : ALL E ∞∞77-00-00∞∞∞∞∞∞∞∞∞∞Page A202
E E Nov 01/04 ERE ECES
F 『
E C F M E
E E
E 56 E
E E
----------------------------------------------------------------------
| ----- A/C MODEL -------------------- | -------------- ENGINE MODEL ------------------------ |-------
| A318-121 | CFM56-5B8/P |
| A318-122 | CFM56-5B9/P |
----------------------------------------------------------------------| A319-111 | CFM56-5B5 | | A319-111 | CFM56-5B5/P | |------------------------------------------------------------------- | | A319-112 | CFM56-5B6 | | A319-112 | CFM56-5B6/P | | A319-112 | CFM56-5B6/2 | | A319-112 | CFM56-5B6/2P | |------------------------------------------------------------------- | | A319-115 | CFM56-5B7/P | |------------------------------------------------------------------- | | A320-214 | CFM56-5B4 | | A320-214 | CFM56-5B4/P | | A320-214 | CFM56-5B4/2 | | A320-214 | CFM56-5B4/2P | |------------------------------------------------------------------- | | A321-111 | CFM56-5B1 | | A321-111 | CFM56-5B1/P | | A321-111 | CFM56-5B1/2 | | A321-111 | CFM56-5B1/2P | |------------------------------------------------------------------- | | A321-112 | CFM56-5B2 | | A321-112 | CFM56-5B2/P | | A321-112 | CFM56-5B2/2 | | A321-112 | CFM56-5B2/2P | |------------------------------------------------------------------- | | A321-211 | CFM56-5B3/P | | A321-211 | CFM56-5B3/2P | ----------------------------------------------------------------------
F 『 EEFF : ALL E ∞∞77-00-00∞∞∞∞∞∞∞∞∞∞Page A203
E E Nov 01/04 ERE
ECES
F 『
E C F M E
E E
E 56 E
E E
TASK 77-00-00-810-903
Core Vibration Higher than 3.2 Units (1.3 Ips) and Lower than 4.1 Units (1.64 Ips) on the Engine 1 or 2
1. Possible Causes
_______________
- wiring, connectors and receptacles
- Engine
- No. 1 bearing vibration sensor (4002EV)
- TRF vibration sensor (4003EV)
- EVMU (2EV)
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific bristle brush
No specific megohmeter
No specific soft nose pliers
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320 Trouble Shooting Manual 排故手冊 發動機指示(107)
