ENG 2 _____REV FAULT
System Data Acquisition Computer. (EIVMU)
— RESET PROCEDURE—
- Reset breaker EVIMU 2 on the RH reset panel.
MEL STATUS: MEL 78-30-01
Read me first
All instructions and limitations given in those documents that relate to the resetting of systems both on the ground and in the air must be respected. No reset should be attempted without a thorough appreciation of the technical ramifications. No more than one computer should be reset at any one time. No reset should be attempted in flight unless specifically permitted by the QRH. Maintenance messages remaining after a reset require engineering investigation.
Tags
ACARS (4) ACSC (18) ADIRU (19) AEVC (10) ANTI ICE SYSTEM (14) AOA (3) APU (4) ATC (1) ATSU (5) BAT (3) BCL (5) BMC (29) BSCU (12) BTC (3) CHC (1) CIDS (7) CPC (15) CZC (1) DFDR (4) DMC (8) ECB (1) ECMU (7) EFCS (18) EIVMU (20) ELAC (6) EMCU (1) ESS (5) FAC (8) FADEC (23) FCDC (4) FCMC (25) FCPC (21) FCSC (4) FCU (3) FDU (12) FM (2) FMGEC (5) FQI (3) FTIS (1) FWC (22) GCU (9) GPCU (2) GPS (1) GPWS (2) HF (1) HSMU (20) ICE DET (2) ILS (2) IR (1) LGCIU (21) MMR (2) PBC (2) PHC (36) PSCU (12) PWS (2) RAD ALT (2) RPCU (1) SATCOM (1) SDAC (9) SDCU (22) SEC (10) SFCC (15) TCAS/T2CAS (1) TR (3) VC (20) VHF (1) WHC (8)
If you encounter an ECAM warning or caution that is not available on our website, please take a photo and send it to our Telegram.
Likewise, if you detect any discrepancies on the site, you can report them directly in our Telegram.
- A320F (0)
- A330 (0)
- A330 AMM TESTS (0)
- ECAM Warnings A330 (0)
- MMEL A330 (0)
- TSM A330 (0)
- Uncategorized (6)
Recent Posts
- AMM 26-12-00-710-002-A — Operational Test of the Engine Fire and Overheat Detection with CFDS A320
- TSM 26-21-00-810-819-A — Possible Engine 1 Fire or Detection System Failure A320
- AMM 73-25-34-710-043-A — Operational Test of the Engine Interface Unit A320
- TSM 73-25-00-810-853-A — Failure of the EIU on Engine 1 A320
- AMM 71-00-00-710-006-B — Minimum Idle Check A320
Social Icons
Gallery
