N265AV

Service difficulty reports not matched to an aircraft · 25

They name N265AV, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. Newest first.

Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE n_number = 'N265AV' AND registry_match IS NULL
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR U30A200600008Bearing · spalledSDR 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 GMar 11, 2006 · N265AV · Airbus A320212 · Engine (Turbine/Turboprop)SDR U30A200600003Engine · malfunctionedSHORTLY 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 LANDEDMar 11, 2006 · N265AV · Airbus A320212 · Engine (Turbine/Turboprop)SDR U30A200600004Skin · dentedPERMANENT 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 EXTERNALNov 29, 2005 · N265AV · Airbus A320212 · Passenger/Crew DoorsSDR U30A200300039A/C Pack · contaminatedAFTER 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 ACDec 26, 2003 · N265AV · Airbus A320212 · Cabin Cooling SystemSDR U30A200300037Frame · corrodedCORROSION 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 COMPOUNDNov 11, 2003 · N265AV · Airbus A320212 · Fuselage Main, FrameSDR U30A200300036Warning Light · false activationDURING 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 Oct 18, 2003 · N265AV · Airbus A320212 · Emergency ExitsSDR U30A200300035Cylinder · dischargedAFTER 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. AIRCRAFOct 17, 2003 · N265AV · Airbus A320212 · Passenger/Crew DoorsSDR U30A20030034Slide · malfunctionedAIRCRAFT 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 Sep 17, 2003 · N265AV · Airbus A320212 · Escape SlideSDR U30A200300033Computer · malfunctionedAFTER 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. AIRCRAug 11, 2003 · N265AV · Airbus A320212 · Flight ControllerSDR U30A200300032Warning Light · illuminatedON 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 RETURNEAug 8, 2003 · N265AV · Airbus A320212 · Trailing Flap Position Indicating SystemSDR U30A200300024Solenoid · intermittentON 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 REJul 31, 2003 · N265AV · Airbus A320212 · Drag Control SystemSDR U30A200300023Smoke Detector · faultyON 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, MAINTEJul 31, 2003 · N265AV · Airbus A320212 · Smoke DetectionSDR U30A200300022Smoke Detector · malfunctionedON 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 CLEJul 28, 2003 · N265AV · Airbus A320212 · Smoke DetectionSDR U30A200300021Smoke Detector · faultyAFTER 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.Jul 16, 2003 · N265AV · Airbus A320212 · Smoke DetectionSDR U30A200300019Battery Pack · dischargedDURING 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 PACKJun 30, 2003 · N265AV · Airbus A320212 · Emergency LightingSDR U30A200300015Connector · arcedDURING 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 FMay 8, 2003 · N265AV · Airbus A320212 · Fuel System WiringSDR U30A200300014Reservoir · lowDURING 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.May 2, 2003 · N265AV · Airbus A320212 · Passenger/Crew DoorsSDR U30A200300011Light · intermittentDURING 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 Mar 26, 2003 · N265AV · Airbus A320212 · Emergency LightingSDR U30A200300010Computer · faultyAFTER 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 AMar 23, 2003 · N265AV · Airbus A320212 · Flight Management Computing Hardware SystemSDR U30A200300009Light · malfunctionedIN 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 23Mar 12, 2003 · N265AV · Airbus A320212 · Emergency LightingSDR U30A200300007Light · malfunctionedDURING 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 3Mar 2, 2003 · N265AV · Airbus A320212 · Emergency LightingSDR U30A200300005Smoke Detector · faultyDURING 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 CONFIFeb 9, 2003 · N265AV · Airbus A320212 · Smoke DetectionSDR U30A200300003Seal · damagedDURING 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.Jan 29, 2003 · N265AV · Airbus A320212 · Passenger/Crew DoorsSDR U30A200300002Computer · intermittentDURING 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 WITJan 9, 2003 · N265AV · Airbus A320212 · Drag Control SystemSDR U30A200300001Seal · damagedDURING 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/Jan 5, 2003 · N265AV · Airbus A320212 · Passenger/Crew Doors
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