# Service difficulty reports: N264AV, cancelled Jun 19, 2012 A list on [N264AV, cancelled Jun 19, 2012](https://openairdocs.org/deregistered/N264AV-2012-06-19.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR EE4Y201205240215](https://openairdocs.org/sdr/EE4Y201205240215.md): Panel · cracked · May 15, 2012 · N264AV · Airbus A320214 · Horizontal Stabilizer, Plate/Skin > FOUND LT HORIZONTAL STAB PANEL ASSY CRACKED. - [SDR EE4Y201205060182](https://openairdocs.org/sdr/EE4Y201205060182.md): Frame · corroded · May 6, 2012 · N264AV · Airbus A320214 · Engine Thrust Reverser > ENGINE NR 1 INBD THRUST REVERSER LOWER ACTUATOR, FWD FRAME BORE WAS FOUND WITH CORROSION. - [SDR EE4Y201205060183](https://openairdocs.org/sdr/EE4Y201205060183.md): Frame · corroded · May 6, 2012 · N264AV · Airbus A320214 · Engine Thrust Reverser > ENGINE NR 2 OTBD THRUST REVERSER UPPER ACTUATOR, FWD FRAME BORE WAS FOUND WITH CORROSION. - [SDR EE4Y201205060184](https://openairdocs.org/sdr/EE4Y201205060184.md): Frame · corroded · May 6, 2012 · N264AV · Airbus A320214 · Engine Thrust Reverser > ENGINE NR 2 INBD THRUST REVERSER LOWER AND UPPER ACTUATORS, FWD FRAME BORES WERE FOUND CORRODED. - [SDR EE4Y201205060185](https://openairdocs.org/sdr/EE4Y201205060185.md): Frame · corroded · May 6, 2012 · N264AV · Airbus A320214 · Engine Thrust Reverser > NR 1 ENGINE OTBD THRUST REVERSER UPPER ACTUATOR FWD FRAME BORE WAS FOUND CORRODED. - [SDR EE4Y201204240191](https://openairdocs.org/sdr/EE4Y201204240191.md): Skin · corroded · Apr 24, 2012 · N264AV · Airbus A320214 · Wing, Plate/Skin > LT WING T/E TOP SKIN PANEL 2 OVERHANG LOWER SURFACE WAS FOUND WITH CORROSION AT RIB 14 LOCATION. - [SDR EE4Y201204240190](https://openairdocs.org/sdr/EE4Y201204240190.md): Skin · corroded · Apr 24, 2012 · N264AV · Airbus A320214 · Wing, Plate/Skin > LT WING T/E AREA TOP SKIN PANEL 2 OVERHANG LOWER SURFACE WAS FOUND CORRODED AT RIB 10 LOCATION. - [SDR EE4Y201204240189](https://openairdocs.org/sdr/EE4Y201204240189.md): Skin · corroded · Apr 24, 2012 · N264AV · Airbus A320214 · Wing, Plate/Skin > LT WING T/E AREA, TOP SKIN PANEL 2 OVERHANG LOWER SURFACE WAS FOUND CORRODED AT RIB 7 LOCATION. - [SDR EE4Y201204200192](https://openairdocs.org/sdr/EE4Y201204200192.md): Skin · corroded · Apr 20, 2012 · N264AV · Airbus A320214 · Wing, Plate/Skin > RT WING T/E AREA TOP SKIN PANEL 2 OVERHANG LOWER SURFACE WAS FOUND WITH CORROSION BETWEEN RIBS 15 AND RIB 16. - [SDR EE4Y201204180188](https://openairdocs.org/sdr/EE4Y201204180188.md): Trunnion · worn · Apr 18, 2012 · N264AV · Airbus A320214 · Trailing Edge Flaps > LT WING INBD FLAP INBD TRACK, TRUNNION FITTING WAS FOUND WITH WEAR. - [SDR EE4Y201204170187](https://openairdocs.org/sdr/EE4Y201204170187.md): Anchor Fitting · corroded · Apr 17, 2012 · N264AV · Airbus A320214 · Wing, Landing Gear Attach Fittings > LOWER FUSELAGE RT MLG RETRACTION JACK ANCHORAGE FITTING WAS FOUND WITH CORROSION. - [SDR EE4Y201204170186](https://openairdocs.org/sdr/EE4Y201204170186.md): Anchor Fitting · corroded · Apr 17, 2012 · N264AV · Airbus A320214 · Wing, Landing Gear Attach Fittings > LOWER FUSELAGE LT MAIN LANDING GEAR RETRACTION JACK ANCHORAGE FITTING WAS FOUND WITH CORROSION. - [SDR U30A2011113000005](https://openairdocs.org/sdr/U30A2011113000005.md): O-Ring · damaged · Nov 27, 2011 · N264AV · Airbus A320214 · Hydraulic System, Main > DURING 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 - [SDR U30A2011111500004](https://openairdocs.org/sdr/U30A2011111500004.md): Slide · dislodged · Nov 12, 2011 · N264AV · Airbus A320214 · Escape Slide > UPON ARRIVAL AND AT THE GATE AFTER FLIGHT, ESCAPE SLIDE AT L2 DOOR FELL OFF POUCH HOLDING IT AND SLIGHTLY UNFOLDED. NO BOTTLE DISCHARGED. - [SDR U30A2008121100006](https://openairdocs.org/sdr/U30A2008121100006.md): Skin · damaged · Dec 8, 2008 · N264AV · Airbus A320214 · Fuselage Main, Plate/Skin > AFTER 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. T - [SDR U30A200500006](https://openairdocs.org/sdr/U30A200500006.md): Glowstrip · cracked · Jul 20, 2005 · N264AV · Airbus A320214 · Emergency Equipment > AFTER 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 PHO - [SDR U30A200500002](https://openairdocs.org/sdr/U30A200500002.md): Pipe · leaking · Mar 12, 2005 · N264AV · Airbus A320214 · Hydraulic System, Main > CREW 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. - [SDR U30A200300028](https://openairdocs.org/sdr/U30A200300028.md): Computer · inoperative · Aug 5, 2003 · N264AV · Airbus A320214 · Autopilot Computer > DURING 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 - [SDR U30A200300025](https://openairdocs.org/sdr/U30A200300025.md): Bottle · discharged · Aug 3, 2003 · N264AV · Airbus A320214 · Passenger/Crew Doors > DURING "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 REQUES - [SDR U30A200200033](https://openairdocs.org/sdr/U30A200200033.md): Computer · malfunctioned · Dec 8, 2002 · N264AV · Airbus A320214 · Autopilot Computer > DURING 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. ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 ``` This list as a web page: https://openairdocs.org/deregistered/N264AV-2012-06-19/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.