OWNER/EXT S. GESBERT Tel : +33 561932841 Fax : +33 561934425 | Reporting A/L : FFT, EZY, AFR A/C affected : A318, A319 Engine affected : | TFU ISSUE DATE : Mar 2004 TFU FIRST ISSUE DATE : Jul 2003 TFU NEXT ISSUE DATE : ISSUE NB : 07 | IMPACT ON : EFFECT ON FLIGHT : NO CATEGORY : VISIBILITY ON PAX : NO |
DESCRIPTION : Prior to the entry into service of the new A318, the laboratory and flight test have allowed Airbus to identify a deviation related to the new enhanced CIDS (OBRM PN Z064H000030B/Z064H000030C). In case of CIDS short power interrupts caused by power transfers, the warning "CIDS 1+2 fault" might be triggered briefly (Approximately 1s) on the upper ECAM. CONSEQUENCES : N/A INVESTIGATION STATUS : N/A INTERIM SOLUTION : N/A MAINTENANCE ADVICE : In case of ECAM Warning "CIDS 1+2 Fault" or Warning message "23-00: COM CIDS 1 +2 Fault" inside the PFR, please perform a CIDS Interface and Power Up Test (AMM Task 23.73.00.740.010), before any other maintenance actions, to confirm the failure. This spurious ECAM warning is referenced in the last revision of SIL 00-028 "Centralized Fault Display System (CFDS) Anomalies" (Dated July 2003). OPS ADVICE : The temporary spurious upper ECAM warning must be disregarded by the cockpit crew. Reset procedure for permanent ECAM CIDS 1+2 fault is already referenced in the FCOM (Chapter 3-04-24). REPERCUSSION ON A/C DISPATCH : N/A PERMANENT OR FINAL SOLUTION : R This deviation is corrected with introduction of CIDS OBRM software PN Z064H000030D (AI R SB23-1239) and CIDS hardware PN Z014H000030C (AI SB23-1241). | SERVICE BULLETIN Airbus Ref. Rev. Date AIB Mod 23-1239 (A318) 00 Iss 15-Mar-2004 33976 Emb. Point : 2170 23-1239 (A319) 00 Iss 15-Mar-2004 33976 Emb. Point : 2170 23-1239 (A319) 00 Iss 15-Mar-2004 34071 Emb. Point : 2188 23-1239 (A318) 00 Iss 15-Mar-2004 34072 Emb. Point : 2109 23-1239 (A319) 00 Iss 15-Mar-2004 34073 Emb. Point : 2170 23-1239 (A318) 00 Iss 15-Mar-2004 34074 Emb. Point : 1660 23-1241 (A318) 00 Iss 15-Mar-2004 33976 Emb. Point : 2170 23-1241 (A319) 00 Iss 15-Mar-2004 33976 Emb. Point : 2170 Vendor Ref. Rev. Date Z014H-23-002 (A318) 00 Z014H-23-002 (A319) 00 Z064H-23-002 (A318) 00 Z064H-23-002 (A319) 00 RELEVANT DOCUMENTATION Airbus OPS documentation Doc. Ref. Rev. Date FCOM 3.04.24 Airbus Maintenance documentation Doc. Ref. Rev. Date AMM 23.73.00.740.010 Other documentation VENDOR and P/N affected Kid-Systeme Z064H000030B Kid-systeme Z064H000030C |