N265AV
Registered owner: BANK OF UTAH TRUSTEE, UT (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| PREMIER AIR CHARTER INC (QJOA) | Certificate holder | — | Matched by certificate designator |
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
SDR WRITTEN TO CLOSE SDR U30A200600003, WHICH READ: FLT 1013 CUN-STL; SHORTLY AFTER T/O, CREW REPORTED VIBRATION, POPPING SOUNDS COMING FROM NR 2 ENG. ENGINE ROLLED BACK TO IDLE. CREW MANINTAINED IDLE CONDITION (ENGINE PARAMETERS WERE NORMAL AND OIL QUANTITY GOOD). CREW DECLARED AN EMERGENCY, RETURNED AND LANDED W/O FURTHER INCIDENT. AFTER TOUCHDOWN. NR 2 ENG. WAS SHUTDOWN, TAXIED SINGLE ENG TO PARKING. MAINT WAS DISPATCHED WITH BOROSCOPE EQUIPMENT TO DETERMINE ENG CONDITION. TROUBLESHOOTING SUGGESTS NR 4 BEARING FAILURE. ENGINE CHANGE IS LIKELY. ENGINE WAS REMOVED, REPLACED. ENGINE WAS REPAIRED, DUE TO NR 4 BRG DETERIORATION. ENG HAS BEEN RETURNED TO SERVICE. SDR U30A200600008 CLOSES SDR U30A200600003.
SHORTLY AFTER TAKE OFF, CREW REPORTED VIBRATION AND POPPING SOUNDS COMING FROM NR 2 ENGINE. ENGINE ROLLED BACK TO IDLE. CREW MAINTAINED IDLE CONDITION (ENGINE PARAMETERS WERE NORMAL & OIL QUANTITY GOOD). CREW DECLARED AN EMERGENCY & RETURNED TO CUN, AND LANDED W/O FURTHER INCIDENT. AFTER TOUCHDOWN, THE NR 2 SHUTDOWN & TAXIED SINGLE ENGINE TO PARKING. MAINTENANCE PERSONNEL WERE DISPATCHED, WITH BOROSCOPE EQUIPMENT TO DETERMINE ENGINE CONDITION. TROUBLESHOOTING SUGGESTS NR 4 BEARING FAILURE. ENGINE CHANGE IS LIKELY. (OPEN)
PERMANENT REPAIR TO THE 1R PAX/CREW DOOR SKIN DENT AT FORWARD LOWER CORNER. REPAIRED UNDER EO 05-52-008, DATED 7 OCT 2005. WHICH INCORPORATES THE PERMANENT REPAIR DEFINITION PER AIRBUS SRM 52-10-00, PARA 5E ,FIG 205. REMOVED DAMAGED SKIN, FABRICATED EXTERNAL DOUBLER & SHIM (2024T3, 0.098 ALUMINUM). APPLIED PROTECTIVE TREATMENT PER SRM 51-23-00. APPLIED SEALANTS PER SRM 51-76-11. FAA FORM 337 HAS BEEN SUBMITTED.
AFTER LANDING, DURING TURNOFF FROM RUNWAY, CREW NOTED LIGHT SMOKE IN COCKPIT AND CABIN WITH NO DISTINCT ODOR OR ANY ECAM MESSAGE OR ABNORMAL INDICATION, EXCEPT ALL BRAKE TEMP SENSORS ON WHEEL PAGE SHOWED AMBER(XX). MAINT INSP AC AND FOUND WATER ON BELLY OF AC AROUND AIR COND PACK INLETS AND NR 2 ENG. FLIGHT CREW NOTED WATER PUDDLE ON TURN OFF WITH THRUST REVERSERS ACTIVATED. MAINT RAN AIR COND PACKS AND NO SMOKE OR ODOR NOTED THROUGHOUT AC. SUSPECT WATER INGESTION INTO AIR CONDITIONING PACK SYS AND RESULTING MIST/VAPOR ENTERED AC. PERFORMED BSCU (BRAKE STEERING CONTROL UNIT) TEST IAW AMM 32-46-00 AND BRAKE TEMP INDICATIONS ARE NORMAL. VISUALLY INSPECTED BSCU WITH NO DEFECTS NOTED. AC RETURNED TO SERVICE.
CORROSION WAS FOUND AT FRAME 16, RT (R1 PAX/CREW DOOR FWD FRAME) UNDER SAFETY BARRIER ATTACH POINT. CORROSION WAS REMOVED IAW SRM 51-74-00. HFEC AND A ROTO TEST INSPECTION TO ENSURE NIL CRACKS.REWORK AREA WAS REPROTECTED IW SRM, CORROSION PREVENTATIVE COMPOUND WAS APPLIED. NEW NUTPLATES WERE INSTALLED. E.O.03-53-006 HAS BEEN CREATED TO ACCOMPLISH THIS DVI AT 5 YR INTERVALS, AND THEREBY INCORPORATES IT INTO THE CONTINUOUS AIRWORTHINESS MAINTENANCE REQUIREMENTS OF THIS AIRCRAFT. THE REWORK AND REINSPECTION DATA REQUIREMENTS ARE DGAC APPROVED IAW MFG RAS (REPAIR DESIGN APPROVAL SHEET) 026456/009/2003 AND THEREFORE FAA APPROVED.
DURING CRUISE ON FLT 143 PUJ-BWI, THE LT AFT EMERGENCY WINDOW EXIT SHOWED ARMED ON ECAM (ABOVE FL 250). NO CHANGE IN CABIN ALTITUDE. ON GROUND, MAINTENANCE VERIFIED THAT THE PROX SENSOR AT THE LT AFT EMERGENCY EXIT HATCH ACCESS COVER TO BE OPERATIONAL IAW AMM 52-70-00-040-007. INDICATION OK AT THIS TIME. NO FAULT FOUND. AIRCRAFT RETURNED TO SERVICE.
AFTER MAINTENANCE ACCEPTANCE FLIGHT ASSOCIATED WITH AN 8C CK & 10 YR INSP., ON FLT 9265 YWG-YWG, THE L2 PAX/CREW DOOR DAMPER & EMERGENCY OPERATION CYLINDER PRESSURE WAS LOW (LEAKING NITROGEN).REPLACED THE L2 PAX/CREW DOOR DAMPER I/A/W AMM 52-13-14-401. AIRCRAFT RETURNED TO SERVICE.
AIRCRAFT IN C CHECK AT YWG. DURING AN INTENTIONAL DEPLOYMENT OF THE R2 PAX/CREW DOOR SLIDE/RAFT, THE SLIDE/RAFT FAILED TO DEPLOY PROPERLY. THE DISCHARGE RIPCORD HAD TO BE PULLED MANUALLY. ONCE THE RIPCORD WAS MANUALLY PULLED, THE SLIDE/RAFT INFLATED IN NORMAL TIME. AWAITING TEAR DOWN REPORT FROM VENDOR.
AFTER PUSHBACK FOR FLT 326 IN BWI, CREW RECEIVED ECAM MESSAGE FOR AUTO FLT YAW DAMPER FAULT, AFTER ENGINE START. AIRCRAFT RETURNED TO GATE. MAINTENANCE RESET THE NR 2 FAC (FLIGHT AUGMENTATION COMPUTER) IAW CAATS TASK 22-63-00-810-815. SYSTEM OPS CK'D OK. AIRCRAFT RETURNED TO SERVICE
ON THE GROUND AFTER FLT 304, BWI- PUJ, THE CREW RECEIVED AN ECAM MESSAGE " F/CTL SYS NR 2 SLAT FAULT". MAINTENANCE ACCOMPLISHED TASK PER AMM 27-80-00-869-004. RECYCLED FLAPS A COUPLE OF TIMES AND SYSTEM PERFORMED NORMAL, WITH NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE.
ON GROUND IN CUN AFTER FLT 306 PIT-CUN, SLATS LOCKED AND WTB (WING TIP BRAKES) MESSAGE ON ECAM. CUN MAINTENANCE RESET THE WTB OF THE SLAT SYSTEM ON GROUND IAW AMM TASK 27-80-00-869-060 AND SYSTEM RESET AND OPS CK'D NORMAL. AIRCRAFT RETURNED TO SERVICE. UPON RETURN TO BWI, DURING A "DAILY" CK IN BWI, A BITE CHECK WAS PERFORMED OF THE SFCC (SLAT FLAP CONTROL COMPUTER) & HAD NO FAULTS BUT INDICATED THE RT WTB SOLENOID HAD A SHORT CIRCUIT. MAINTENANCE REPLACED THE RT WTB SOLENOID PER AMM TASK 27-81-51-401 AND OPS CK'D THE SLATS WTB PER AMM TASK 27-81-00-710-001. OPS CK AND LEAK CK OK.
ON FLT 300, BWI-CUN, DURING TAXI IN, ECAM MESSAGE FOR SMOKE LAV AND CARGO DETECTOR FAULTED. MAINTENANCE IN CUN RESET CIRCUIT BREAKER AND PERFORMED OPS CHECK IAW AMM 26-17-00-710-01 WITH NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. UPON RETURN TO BWI, MAINTENANCE INSPECTED LAV"D" SMOKE DETECTOR DUCTING AND FOUND BLOCKAGE REMOVED BLOCKAGE FROM VACUUM RESTRICTOR AND VACUUM WAS RESTORED. OPS CHECKED OK.
ON GROUND AFTER FLT 326 BWI-PUJ, LAV-D SHOWS SMOKE DETECTOR FAULT. DEFERRED LAV-D PER MEL 26-17-01. ON RETURN TO BWI (7/28/03) AFTER FLT 327, BWI MAINTENANCE OPERATIONALLY TESTED THE SMOKE DETECTOR SYSTEM IAW AMM 26-17-00-501, WITH NO FAULTS FOUND. THIS CLEARED THE MEL AND THE AIRCRAFT WAS RETURNED TO SERVICE. ADDITIONAL WIRE TOUBLESHOOTING OF THE SMOKE DETECTOR SYSTEM PER SRTC 26-03-005 WAS ACCOMPLISHED WITH NO FAULTS FOUND.
AFTER FLT 319 CUN-BWI, DURING "DAILY CHECK", ECAM MESSAGE SHOWED SMOKE DETECTOR IN LAV D WAS FAULTED. REMOVED AND REPLACED LAV D SMOKE DETECTOR IAW AMM 27-17-15-401. OPS CK'D IAW AMM 26-17-00-710-001 WITH NO FAULTS. AIRCRAFT RETURNED TO SERVICE.
DURING DAILY CHECK, AFTER FLT 329 IN BWI, MAINTENANCE PERSONNEL DISCOVERED THAT ROWS 21, 25 & 27 ON LT SIDE OF AIRCRAFT AND THE L2 & R2 (LT AND RT REAR DOORS) EMERGENCY LIGHTS DID NOT ILLUMINATE WHEN TESTED. THE EPSU (EMERGENCY POWER SUPPLY UNIT) BATTERY PACK AT THE L2 DOOR WAS REPLACED AND TESTED I/A/W AMM 33-51-38-401. THE AIRCRAFT WAS RETURNED TO SERVICE.
DURING MAINTENANCE INSPECTION, DURING ENGINE RUN, AN ECAM MESSAGE FOR THE RT FUEL TANK PUMP NR 2, LOW PRESSURE. FURTHER TROUBLESHOOTING REVEALED ELECTRICAL ARCING AT THE RT WING FUEL PUMP WIRE HARNESS CONNECTOR. RELATED CIRCUIT BREAKER DID NOT TRIP. REPLACED FUEL PUMP IAW AMM. REPLACED FUEL PUMP CONNECTOR. INSPECTED ALL REMAINING WING (RT & LT) AND CENTER SECTION FUEL PUMPS & WIRING WITH NO OTHER DEFECTS NOTED. RELACED CIRCUIT BREAKER FOR PRECAUTIONARY REASONS. OPERATIONALLY CHECKED THE FUEL PUMP SYSTEM IAW AMM, NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE.
DURING DAILY INSPECTION AFTER FLT 313 IN BWI, THE L2 CREW PASSENGER DOOR EMERGENCY OPERATION CYLINDER PRESSURE WAS LOW. REPLACED DIAPHRAM PN FE240-221-001 AND ASSOCIATED PACKINGS & SERVICED CYLINDER IAW AMM 52-10-00-610-001. AIRCRAFT RETURNED TO SERVICE.
DURING CRUISE ON FLT 313 CUN-BWI, THE EMERGENCY EXIT LIGHTS IN THE CENTER OF AIRCRAFT FLASH SPORADICALLY. ON GROUND IN BWI, PERFORMED OPERATIONAL TEST OF EMERGENCY LIGHTS PER AMM TASK 33-51-00-710-001, OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. SDR UPDATED 12 JUNE 2003. AIR CARRIER HAS SUBMITTED TWO PREVIOUS SDR'S U30A200300007 & U30A200300009 ON SAME SYSTEM WITH SIMILAR PROBLEMS. A SUBSEQUENT INVESTIGATION REVEALED THAT AIRBUS S/B A320-33-1018 IDENTIFIES THESE PROBLEMS AND THIS S/B WAS NOT EMBODIED AT THE TIME. CARRIER GENERATED AN EO WHICH MODIFIES EPSU FROM P/N 3214-52 TO 3214-54. MODS TO FOUR EPSU'S COMPLETED ON 6/5/03. EMER EXIT LIGHT SYS HAS NOT FAULTED SINCE 3/31/03. THIS SDR U30A200300011 IS CLOSED.
AFTER FLT 306 BWI-CUN, IN CUN AT GATE, THE NR 1 FLIGHT MANAGEMENT GUIDANCE COMPUTER (FMGC) FAILED. DEFERRED PER MEL 22-83-01. IN BWI ON 3/25/03, RESET NR 1 FMGC IAW AMM AFS OPER TEST 22-96-00-710-001 AND SYSTEM OPS CHECKED OK. ON 3/25/03, NR 1 FMGC FAILED AGAIN. SWAPPED NR 1 & 2 FMGC'S AND OPS CHECKED BOTH FMGC NR 1 & 2 OK. C/W RVSM RETURN TO SERVICE REQUIREMENTS. ON 3/26/2003, FMGC NR 2 FAILED. REMOVED AND REPLACED NR 2 FMGC IAW 22-83-34-400-001 AND OPS CK'D OK. C/W RVSM RETURN TO SERVICE REQUIREMENTS.
IN CRUISE DURING FLT 315 RSW-BWI AND THEN ON DESCENT, THE EMERGENCY EXIT LIGHTS IN REAR OF AIRCRAFT AND ON AFT DOORS NOT LIGHT, INOPERATIVE. OTHERS AT MID CABIN AND FWD WORK. PERFORMED BITE TEST ON THE CABIN INTERCOMMUNICATIONS DATA SYSTEM (CIDS) PER TASK 23-73-00-740-003 (EMERGENCY BATTERY CAPACITY TEST). RECYCLED EMERGENCY EXIT LIGHT SWITCH IN COCKPIT. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE.
DURING CRUISE ON FLT 307 CUN-PIT, THE LEFT MID CABIN & AFT EMERGENCY EXIT LIGHTS (OVER EXITS) WENT INOP. ON GROUND IN PIT RECYCLED EMERGENCY LIGHT ARM SWITCH & CIRCUIT BREAKER. OPERATIONALLY CHECKED ALL EMERGENCY LIGHTS GOOD PER TASK 33-51-00-710-060 AND AMM 33-51-00-401.
DURING CRUISE ON FLT 304 BWI-PUJ, ECAM MESSAGE APPEARED "SMOKE-LAVATORY DET FAULT". ON GROUND IN PUJ TESTED SYSTEM & FOUND FWD LAV DETECTOR FAULT. DEFERRED PER MEL 26-17-01 (LAV "A"). UPON RETURN TO BWI, T/S SYSTEM PER TASK 26-17-00-810-801 WITH NO FAULT CONFIRMATION. SYSTEM OPERATIONALLY TESTED OK. A/C RETURNED TO SERVICE.
DURING WEEKLY INSPECTION AFTER FLT 315 IN BWI, THE R2 CREW PASSENGER DOOR EMERGENCY OPERATION CYLINDER PRESSURE WAS LOW. REPLACED SEAL P/N FE240-221-001 AND ASSOCIATED PACKINGS I/A W AMM 52-10-000-610. SERVICED TO CORRECT PRESSURE I/A/W AMM 52-10-00-614-001.
DURING INSPECTION AFTER FLT 314 AT BWI, INTERROGATED CFDS & FOUND MESSAGE: "SEC 1 OR INPUT OF CAPT ROLL CTL SSTU 4CE1". CAATS RECOMMENDS REPLACEMENT OF SEC NR 1 (SPOILER AND ELEVATOR COMPUTER). REPLACED SEC NR 1 I/A/W AMM 27-94-34-000-001. PERFORMED OPS CK WITH NO DEFECT. THIS SDR AMMENDED ON 2/25/2003 TO DOCUMENT ADDITIONAL MAINTENANCE ACTIVITY. THE # 1 SEC (P/N B372BAM0508, MFG BY THALES, S/N 5894 DID NOT CORRECT ORIGINAL DISCEPANCY. DUE TO REPEAT CFDS MESSAGE "SEC 1 OR INPUT OF CAPT ROLL CTL SSTU 4CE1", THE SSTU (SIDE STICK TRANSDUCER UNIT) 4CE1 WAS REPLACED I/A/W AMM TASK 27-92-41-000-002 AND OPERATIONALLY CHECKED I/A/W AMM 27-92-41-710-001. THE SSTU REPLACEMENT TOOK PLACE AT TAT 33661.8 AND TAC 13328 ON
DURING DAILY INSPECTION AFTER FLT 305 IN BWI, THE L1 CREW/PASSENGER DOOR EMERGENCY OPERATION CYLINDER PRESSURE WAS LOW. SERVICED THE EMERGENCY OPERATION CYLINDER WITH NITROGEN I/A W AMM 52-10-00-614-001. AIRCRAFT RETURNED TO SERVICE. ON JAN 8, REPLACED SEAL P/N, FE240-221-001 AND ASSOCIATED PACKINGS. SERVICED WWITH NITROGEN AND LEAK CK OK.