N264AV, cancelled Jun 19, 2012

Service difficulty reports · 20

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. 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 = 'N264AV' AND deregistration_id = 'N264AV-2012-06-19'
  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 EE4Y201205240215Panel · crackedFOUND LT HORIZONTAL STAB PANEL ASSY CRACKED.May 15, 2012 · N264AV · Airbus A320214 · Horizontal Stabilizer, Plate/SkinSDR EE4Y201205060182Frame · corrodedENGINE NR 1 INBD THRUST REVERSER LOWER ACTUATOR, FWD FRAME BORE WAS FOUND WITH CORROSION.May 6, 2012 · N264AV · Airbus A320214 · Engine Thrust ReverserSDR EE4Y201205060183Frame · corrodedENGINE NR 2 OTBD THRUST REVERSER UPPER ACTUATOR, FWD FRAME BORE WAS FOUND WITH CORROSION.May 6, 2012 · N264AV · Airbus A320214 · Engine Thrust ReverserSDR EE4Y201205060184Frame · corrodedENGINE NR 2 INBD THRUST REVERSER LOWER AND UPPER ACTUATORS, FWD FRAME BORES WERE FOUND CORRODED.May 6, 2012 · N264AV · Airbus A320214 · Engine Thrust ReverserSDR EE4Y201205060185Frame · corrodedNR 1 ENGINE OTBD THRUST REVERSER UPPER ACTUATOR FWD FRAME BORE WAS FOUND CORRODED.May 6, 2012 · N264AV · Airbus A320214 · Engine Thrust ReverserSDR EE4Y201204240191Skin · corrodedLT WING T/E TOP SKIN PANEL 2 OVERHANG LOWER SURFACE WAS FOUND WITH CORROSION AT RIB 14 LOCATION.Apr 24, 2012 · N264AV · Airbus A320214 · Wing, Plate/SkinSDR EE4Y201204240190Skin · corrodedLT WING T/E AREA TOP SKIN PANEL 2 OVERHANG LOWER SURFACE WAS FOUND CORRODED AT RIB 10 LOCATION.Apr 24, 2012 · N264AV · Airbus A320214 · Wing, Plate/SkinSDR EE4Y201204240189Skin · corrodedLT WING T/E AREA, TOP SKIN PANEL 2 OVERHANG LOWER SURFACE WAS FOUND CORRODED AT RIB 7 LOCATION.Apr 24, 2012 · N264AV · Airbus A320214 · Wing, Plate/SkinSDR EE4Y201204200192Skin · corrodedRT WING T/E AREA TOP SKIN PANEL 2 OVERHANG LOWER SURFACE WAS FOUND WITH CORROSION BETWEEN RIBS 15 AND RIB 16.Apr 20, 2012 · N264AV · Airbus A320214 · Wing, Plate/SkinSDR EE4Y201204180188Trunnion · wornLT WING INBD FLAP INBD TRACK, TRUNNION FITTING WAS FOUND WITH WEAR.Apr 18, 2012 · N264AV · Airbus A320214 · Trailing Edge FlapsSDR EE4Y201204170187Anchor Fitting · corrodedLOWER FUSELAGE RT MLG RETRACTION JACK ANCHORAGE FITTING WAS FOUND WITH CORROSION.Apr 17, 2012 · N264AV · Airbus A320214 · Wing, Landing Gear Attach FittingsSDR EE4Y201204170186Anchor Fitting · corrodedLOWER FUSELAGE LT MAIN LANDING GEAR RETRACTION JACK ANCHORAGE FITTING WAS FOUND WITH CORROSION.Apr 17, 2012 · N264AV · Airbus A320214 · Wing, Landing Gear Attach FittingsSDR U30A2011113000005O-Ring · damagedDURING CRUISE ON SCHEDULED FLIGHT, EXPERIENCED LOSS OF GREEN HYD SYS-SYS INDICATED TOTAL LOSS OF FLUID. ECAM HYD G RSVR LO LVL, LANDING GEAR MANUAL EXTENSION ACCOMPLISHED. DIVERTED AND LANDED WITHOUT INCIDENT. MX CONTACTED AND FOUND HYD LEAK AT ENGINE NR 1 Nov 27, 2011 · N264AV · Airbus A320214 · Hydraulic System, MainSDR U30A2011111500004Slide · dislodgedUPON ARRIVAL AND AT THE GATE AFTER FLIGHT, ESCAPE SLIDE AT L2 DOOR FELL OFF POUCH HOLDING IT AND SLIGHTLY UNFOLDED . NO BOTTLE DISCHARGED.Nov 12, 2011 · N264AV · Airbus A320214 · Escape SlideSDR U30A2008121100006Skin · damagedAFTER FLT 599, ACFT PARKED ON GATE IN ORD FOR OVERNIGHT. ACFT WAS STRUCK BY GROUND EQUIPMENT (ASIG) TUG, CAUSING DAMAGE TO THE FWD EXTERNAL GROUND POWER RECEPTACLE DOOR, THE FWD DME ATC ANTENNA & LOWER FUSELAGE SKIN ADJACENT TO THE DME ANTENNA INSTALLATION. TDec 8, 2008 · N264AV · Airbus A320214 · Fuselage Main, Plate/SkinSDR U30A200500006Glowstrip · crackedAFTER FLT 631 IN ORD, MAINTENANCE WAS PERFORMING A "DAILY INSP." AND FOUND THE PHOTOLUMINESCENT EMERGENCY FLOOR PATH LIGHTING STRIP BROKEN (CRACKED). THE CRACK WAS APPROXIMATELY 6" FROM THE END OF THE STRIP IN THE AFT OF THE AIRCRAFT BY LAV "D". (NOTE: THE PHOJul 20, 2005 · N264AV · Airbus A320214 · Emergency EquipmentSDR U30A200500002Pipe · leakingCREW RECEIVED AN ECAM MESSAGE, GREEN HYD LOW PRESS. TURNED OFF PUMP & PTU. STATUS PG INDICATED LOW PRESS & NIL QTY. DIVERTED, DECLARED AN EMERGENCY. ECAM GENERATED APPROACH LIST INSTRUCTS TO TURN PTU BACK ON TO TRY TO RESTORE PRESSURE, PRESSURE RESTORED. Mar 12, 2005 · N264AV · Airbus A320214 · Hydraulic System, MainSDR U30A200300028Computer · inoperativeDURING DESCENT ON FLT 581 ATL-CUN, NR 1 FCU (FLIGHT CONTROL UNIT) WENT INOP.UNIT WAS DEFERRED PER MEL 22-81-01 ON GND IN CUN. IN ORD ON 5 AUG 03, REPLACED FCU IAW AMM 22-81-12-401 AND ALL SYSTEM CHECKS PERFORMED GOOD. AIRCRAFT RETUNED TO SERVICE. NOTE REVISED Aug 5, 2003 · N264AV · Airbus A320214 · Autopilot ComputerSDR U30A200300025Bottle · dischargedDURING "DAILY" CHECK, IN ORD, THE R2 CREW/PAX DOOR EMERGENCY OPERATION ASSIST/DAMPER BOTTLE HAD LOW PRESURE. MAINTENANCE SERVICED THE R2 EMERGENCY OPERATION ASSIST/DAMPER BOTTLE IAW AMM 52-10-00-614. ON 8/4/03 DURING THE NEXT "DAILY CHECK, SRTC (SPECIAL REQUESAug 3, 2003 · N264AV · Airbus A320214 · Passenger/Crew DoorsSDR U30A200200033Computer · malfunctionedDURING CRUISE ON FLT 9518, ORD-CUN, AUTO PILOT NR 2 (AP2) FAULTED. UPON ARRIVAL IN CUN, DEFERRED PER MEL 22-83-01. REPLACED FMGC NR 2 IN ORD ON DEC. 9, 2002 IAW AMM 22-83-34-400-001. AFS TEST OK PER AMM 22-96-00-710-001. AIRCRAFT RETURNED TO SERVICE.Dec 8, 2002 · N264AV · Airbus A320214 · Autopilot Computer
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