Service difficulty reports · 8
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR MU1Z2011020200002Angle · crackedDURING HFEC INSPECTION CLOSE OUT ANGLE OF THE RT PYLON WAS FOUND CRACKED.SDR ANCF2010100900068Engine · leakingRIGHT PACK INOP LIGHT ILLUMINATED EICAS MESSAGE RT PACK TEMP DISPLAYED. LIGHT DID NOT EXTINGUISH WHEN STBY SELECTED. RESET PUSHED, LIGHT EXTINGUISHED THEN RE-ILLUMINATED. LIGHT SMOKE COMING FROM THE GASPERS IN BOTH CABIN SECTIONS. LIGHT SMOKE STOPS FLOWING SDR ANCF2009051500043Module · faultyAFTER LIFT OFF FIRE AURAL WARNING SOUND CONTINUOSLY WITHOUT ANY INDICATION UNTIL ON GROUND, C/B H35 WAS PULLED IAW FIM 31-51-00 FIG 103 BLOCKS 1 TO 6 AND 50 AND IAW AMM 31-51-04 PAGE 401. THE BELL CHIME AURAL WARNING MODULE (M1000) WAS REPLACED, PERFORMED OPSDR 2008FA0000466Computer · failedAIR TURNBACK DUE PILOT REPORT 4273256-1; EICAS MSG L FMC FAIL DISPLAYED. FIM 34-61-00 FOLLOWED L FMC PWR RESET ALL INDICATIONS NORMAL. PLS MONITOR FURTHER. AS A PREVENTIVE ACTION DURING OVERNIGHT; IAW AMM 34-61-01/401 WAS REMOVED AND REPLACED THE FLIGHT MANASDR ANCF200400051Heater · defectiveELECTRICAL SMOKE OF UNKNOW ORIGIN FROM THE CAPTAIN'S SIDE, BETWEEN THE LIGHT CONTROL PANEL AND THE GLARESHIELD PANEL, ACCORDING TO THE ABNORMAL CHECKLIST THE RECIRCULATION FANS AND THE UTILITY BUSES WERE SWITCHED OFF AND THE EQUIPMENT COOLING SELECTOR WAS SELESDR ANCF200300027Apu · leakingSMOKE ODOR THROUGH THE PASSENGER CABIN WITH NO SMOKE EVIDENCE. SMOKE DETECTORS ACTIVATED ON THE AFT AND FORWARD LAVATORIES. UTILITY BUSES WERE TURNED OFF WITH NO HELP ON THE SITUATION. LT AND RT RECIRCULATING FANS WERE TURNED OFF AS WELL AS THE RIGHT HAND. SDR ANCF200200015Coupling · damagedTRANSMISSION ON BOTH HF INOPERATIVE AT ALL STATIONS.CORRECTIVE ACTION:PERFORMED FIM 23-11-00 OPERATION FOUND NORMAL ON LH HF, ON RH SYSTEM WAS REPLACED HF COUPLER AND HF TRANCEIVER AS PER AMM 23-11-03 ANS 23-11-01, ACCOMPLISHED OPERATIONAL TEST ON BOTH SYSTEM SDR ANCF200000002Controller · malfunctionedDURING CRUISE, LT ENGINE BLEED OFF DISPLAYED AND ENGINE BLEED AIR VALVE OFF LIGHT ILLUMINATED, WITH SWITCH ON. DUCT PRESS WAS ZERO PSI, NACELLE ANTI-ICE OPERATION NOT CHECKED. DURING GROUND CHECK FAIL HPSOV AND EICAS MESSAGE. IAW AMM 36-11-07 PAGE 401, THE