# Service difficulty reports: N14056, cancelled Sep 15, 2011 A list on [N14056, cancelled Sep 15, 2011](https://openairdocs.org/deregistered/N14056-2011-09-15.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. Page 1 of 2 · 83 reports - [SDR AALA2009061300002](https://openairdocs.org/sdr/AALA2009061300002.md): Connector · loose · Jun 13, 2009 · N14056 · Airbus A300B4605R · Light System Wiring > MIA - EMERGENCY PATH LIGHT AT SEAT 10G INOPERATIVE. SECURED CONNECTION AT SEAT 10G. - [SDR AALA200800674](https://openairdocs.org/sdr/AALA200800674.md): Pressure Switch · inoperative · Mar 19, 2008 · N14056 · Airbus A300B4605R · Fuel Pressure Indicating > MIA INFLIGHT T588/19MAR - LEFT ENGINE FUEL CLOG LIGHT ILLUMINATED WITH ALERT. RETURNED TO MIA AND LANDED WITHOUT INCIDENT. REPLACED NUMBER ONE ENGINE FUEL PRESSURE SWITCH. SYSTEM GROUND CHECKED NORMAL OPERATION. - [SDR AALA20072439](https://openairdocs.org/sdr/AALA20072439.md): Battery Pack · inoperative · Dec 13, 2007 · N14056 · Airbus A300B4605R · Emergency Lighting > JFK - SEAT MOUNTED EMERGENCY LIGHT AT LEFT NUMBER TWO DOOR INOPERATIVE. REPLACED BATTERY PACK FOR SEAT MOUNTED EMERGENCY LIGHT AT LEFT NUMBER TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. - [SDR AALA20072438](https://openairdocs.org/sdr/AALA20072438.md): Lamp · inoperative · Dec 13, 2007 · N14056 · Airbus A300B4605R · Emergency Lighting > JFK - EMERGENCY EXIT SIGN LIGHT AT LEFT NUMBER TWO DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY EXIT SIGN LIGHT AT LEFT NUMBER TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. - [SDR AALA20072437](https://openairdocs.org/sdr/AALA20072437.md): Lamp · inoperative · Dec 13, 2007 · N14056 · Airbus A300B4605R · Emergency Lighting > JFK - EMERGENCY EXIT SIGN LIGHT AT LEFT NUMBER THREE DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY EXIT SIGN LIGHT AT LEFT NUMBER THREE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. - [SDR AALA20072436](https://openairdocs.org/sdr/AALA20072436.md): Lamp · inoperative · Dec 13, 2007 · N14056 · Airbus A300B4605R · Emergency Lighting > JFK - EMERGENCY EXIT SIGN LIGHT AT RIGHT NUMBER TWO DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY EXIT SIGN LIGHT AT RIGHT NUMBER TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. - [SDR AALA20072435](https://openairdocs.org/sdr/AALA20072435.md): Lamp · inoperative · Dec 13, 2007 · N14056 · Airbus A300B4605R · Emergency Lighting > JFK - EMERGENCY EXIT SIGN LIGHT AT RIGHT NUMBER FOUR DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY EXIT SIGN LIGHT AT RIGHT NUMBER FOUR DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. - [SDR AALA20072440](https://openairdocs.org/sdr/AALA20072440.md): Battery Pack · inoperative · Dec 13, 2007 · N14056 · Airbus A300B4605R · Emergency Lighting > JFK - SEAT MOUNTED EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR INOPERATIVE. REPLACED BATTERY PACK FOR SEAT MOUNTED EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. - [SDR AALA20072366](https://openairdocs.org/sdr/AALA20072366.md): Sensor · inoperative · Dec 3, 2007 · N14056 · Airbus A300B4605R · Landing Gear Position and Warning > JFK INFLIGHT T635/03DEC - LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. RETURNED TO JFK AND LANDED WITHOUT INCIDENT. REPLACED RIGHT STRUT SENSORS 64GB AND 62GB. SYSTEM GROUND CHECKED NORMAL OPERATION. - [SDR AALA20071917](https://openairdocs.org/sdr/AALA20071917.md): Slat System · jammed · Oct 10, 2007 · N14056 · Airbus A300B4605R · Leading Edge Slat Control System > BOG INFLIGHT T915/10OCT - ZERO SLAT LOCKOUT ON LANDING. LANDED BOG WITHOUT INCIDENT. ACCOMPLISHED BITE TO SLAT FLAT CONTROL COMPUTERS ONE AND TWO. FAULTS SLAT JAM AND FLAP SUPPLY RESET AND CLEARED. UNABLE TO DUPLICATE. SYSTEM GROUND CHECKED NORMAL OPERATI - [SDR AALA20070136](https://openairdocs.org/sdr/AALA20070136.md): Seal · leaking · Jan 18, 2007 · N14056 · Airbus A300B4605R · Hydraulic System, Main > JFK INFLIGHT - DURING DESCENT GREEN PUMP LOW PRESSURE LIGHT FOR BOTH PUMPS ILLUMINATED. MANUALLY EXTENDED LANDING GEAR DURING APPROACH. FLUID CYCLED FROM ZERO TO MID RANGE. LANDED JFK WITHOUT INCIDENT AND AIRCRAFT WAS TOWED TO HANGAR. FOUND GREEN SYSTEM H - [SDR AALA20060046](https://openairdocs.org/sdr/AALA20060046.md): Control Unit · inoperative · Jan 28, 2006 · N14056 · Airbus A300B4605R · Emergency Lighting > MEX - EMERGENCY EXIT LIGHT AT 1L DOOR INOPERATIVE. REPLACED POWER SUPPLY CONTROL UNIT 29WL1 FOR EMERGENCY EXIT LIGHT AT 1L DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. - [SDR AALA20060051](https://openairdocs.org/sdr/AALA20060051.md): Power Unit · inoperative · Jan 28, 2006 · N14056 · Airbus A300B4605R · Emergency Lighting > MEX - EMERGENCY LIGHT AT 1L DOOR INOPERATIVE. REPLACED POWER SUPPLY UNIT FOR EMERGENCY LIGHT AT 1L DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. - [SDR AALA20050713](https://openairdocs.org/sdr/AALA20050713.md): Light · inoperative · Oct 29, 2005 · N14056 · Airbus A300B4605R · Emergency Lighting > JFK - FORWARD BULKHEAD RIGHT HAND FLOOR EMERGENCY LIGHT INOPERATIVE. REPLACED FORWARD BULKHEAD RIGHT HAND FLOOR EMERGENCY LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. - [SDR AALA20050675](https://openairdocs.org/sdr/AALA20050675.md): Slide · deployed · Oct 10, 2005 · N14056 · Airbus A300B4605R · Escape Slide > JFK - L3 DOOR SLIDE INADVERTANTLY DEPLOYED UNSUCCESSFULLY. REPLACED L3 DOOR SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. - [SDR AALA20050376](https://openairdocs.org/sdr/AALA20050376.md): Pin · damaged · Jun 2, 2005 · N14056 · Airbus A300B4605R · Emergency Lighting > MIA - EMERGENCY LIGHT AT SEAT 24G INOPERATIVE. REPLACED PINS IN CONNECTION FOR EMERGENCY LIGHT AT SEAT 24G. SYSTEM GROUND CHECKED NORMAL OPERATION. - [SDR AALA20041213](https://openairdocs.org/sdr/AALA20041213.md): Battery Pack · discharged · Dec 10, 2004 · N14056 · Airbus A300B4605R · Emergency Lighting > JFK - EMERGENCY LIGHT AT DOOR 1L INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT DOOR 1L. SYSTEM GROUND CHECKED NORMAL OPERATION. - [SDR AALA20040361](https://openairdocs.org/sdr/AALA20040361.md): Beam · cracked · Mar 12, 2004 · N14056 · Airbus A300B4605R · Fuselage Main, Structure > TUL CRACK IN LOWER OUTBOARD FLANGE OF THE LEFT HAND GANTRY BEAM NR 4 AT FRAME 53. CRACK LENGTH IS 1.500 INCH. REPAIRED ACCORDING TO AIRBUS REPAIR TD 942.029285.004.2004, ISSUE B, DATED 10 MAR 2004 AND ESO 30595 DATED 12 MAR 2004. - [SDR AALA20040221](https://openairdocs.org/sdr/AALA20040221.md): Filter · clogged · Feb 11, 2004 · N14056 · Airbus A300B4605R · Aircraft Fuel Filter/Strainer > JFK INFLIGHT T837/11 AT FLIGHT LEVEL 270 NUMBER 2 ENGINE FUEL CLOG LIGHT CAME ON WITH ECAM MESSAGE. REDUCED POWER TWO TO THREE KNOBS AND LIGHT WENT OUT. RETURNED TO STATION AND LANDED WITHOUT INCIDENT. FOUND FUEL FILTER CLOGGED. REPLACED FUEL FILTER AND A - [SDR AALA20040102](https://openairdocs.org/sdr/AALA20040102.md): Pump · inoperative · Jan 21, 2004 · N14056 · Airbus A300B4605R · Hydraulic Pump (Electric/Engine), Main > JFK INFLIGHT T0635/21, YELLOW SYSTEM HYDRAULIC WENT TO 50 PSI SHORTLY AFTER TAKEOFF WITH ECAM MESSAGE. SYSTEM WENT TO 3300 PSI AFTER PTU PRESSED ON. RETURNED TO JFK. LANDED WITHOUT INCIDENT. REPLACED RIGHT HAND ENGINE YELLOW SYSTEM PUMP. SYSTEM GROUND CHE - [SDR AALA20040053](https://openairdocs.org/sdr/AALA20040053.md): Pump · inoperative · Jan 9, 2004 · N14056 · Airbus A300B4605R · Hydraulic Pump (Electric/Engine), Main > EWR INFLIGHT/T881/09 YELLOW HYDRAULIC SYSTEM LOW PRESSURE ECAM WARNING. RETURNED TO EWR AND LANDED WITHOUT INCIDENT. REPLACED ENGINE DRIVEN HYDRAULIC PUMP. SYSTEM GROUND CHECKED NORMAL OPERATION. - [SDR AALA20021210](https://openairdocs.org/sdr/AALA20021210.md): Connector · loose · Aug 22, 2002 · N14056 · Airbus A300B4605R · Emergency Lighting > MIA - FOUND EMERGENCY LIGHT AT 35G INOPERATIVE. RESECURED ATTACHING CONNECTOR AT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) - [SDR AALA20020510](https://openairdocs.org/sdr/AALA20020510.md): Power Supply · discharged · Apr 22, 2002 · N14056 · Airbus A300B4605R · Emergency Lighting > MIA - FOUND MID AND AFT CABIN EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLIES AT 4R AND 4L. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) - [SDR AALA20011673](https://openairdocs.org/sdr/AALA20011673.md): Door Frame · corroded · Aug 22, 2001 · N14056 · Airbus A300B4605R · Fuselage Main, Structure > TUL - FOUND CORROSION AT AFT LOWER DOOR FRAME CUT OUT. INSTALLED TRACK SPLICE PER SRM 53-10-15. (M) - [SDR ALA20011672](https://openairdocs.org/sdr/ALA20011672.md): Stringer · corroded · Aug 22, 2001 · N14056 · Airbus A300B4605R · Fuselage Main, Longeron/Stringer > TUL - FOUND CORROSION ON STRINGER 46R FROM STATION FRAME 65, FRAME 70. REPLACED CORRODED STRINGER SPLICES AND STRINGER SEGMENTS PER SRM 51-75-10. (M) - [SDR AALA20011613](https://openairdocs.org/sdr/AALA20011613.md): Seat Track · corroded · Aug 13, 2001 · N14056 · Airbus A300B4605R · Fuselage, Seat/Cargo Attach Fittings > TUL - FOUND RIGHT SEAT TRACK C (3RD FROM R-2 DOOR) HAS CORROSION TOP SIDE, FRAME 30 TO FRAME 33. REPLACED RIGHT SEAT TRACK C PER SRM 51-72-10-0. (M) - [SDR AALA20011646](https://openairdocs.org/sdr/AALA20011646.md): Splice · cracked · Aug 9, 2001 · N14056 · Airbus A300B4605R · Fuselage Miscellaneous Structure > TUL - FOUND CRACK FOUND ON ATTACHMENT ANGLE ABOVE WINDOW STRINGER CROSS OVER POINT AND FRAME 47 RIGHT. INSTALLED NEW MANUFACTURED STRINGER SPLICE ANGLE, WET WITH NEW FASTENERS AT FRAME 47 RIGHT, AND STRINGER 18R. (M) - [SDR AALA20011612](https://openairdocs.org/sdr/AALA20011612.md): Fitting · corroded · Aug 9, 2001 · N14056 · Airbus A300B4605R · Fuselage Miscellaneous Structure > TUL - FOUND LAV TIE DOWN PITTING, CORRODED AT LAV M BETWEEN FRAME 32 AND 33. INSTALLED LAV TIE DOWN FRAME 32-33 PER SRM 51-72-10. (M) - [SDR AALA20011555](https://openairdocs.org/sdr/AALA20011555.md): Warning System · false indication · Aug 3, 2001 · N14056 · Airbus A300B4605R · Landing Gear Position and Warning > MIA - FLT 2111 - EN ROUTE LIM NOSE GEAR INDICATION MESSAGE AFTER TAKEOFF. LANDED MIA WITHOUT INCIDENT. PERFORMED OVERWEIGHT LANDING INSPECTION. NO DISCREPANCIES NOTED. (M) - [SDR AALA20002021](https://openairdocs.org/sdr/AALA20002021.md): Shear Tie · bent · Dec 4, 2000 · N14056 · Airbus A300B4605R · Fuselage Main, Structure > TUL - FOUND SHEAR TIE WEB BETWEEN FRAMES 12A/14 IS BENT AT OPENINGS ON FRAME 14 SIDE FROM FLOOR TO 52 INCHES ABOVE FLOOR AT L-1 DOOR OPENING. ACCOMPLISHED REPAIR TO FORWARD TORQUE BOX VERTICAL WEB AT L1 DOOR CUTOUT AT 13A PER ESO 30595, DATED 1 DEC 00. (M) - [SDR AALA991666](https://openairdocs.org/sdr/AALA991666.md): Wire · shorted · Nov 7, 1999 · N14056 · Airbus A300B4605R · Light System Wiring > SJU - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING INOPERATIVE FROM ROWS 29 TO 37. REPAIRED WIRE TO EMERGENCY EXIT FLOOR PATH LIGHTS FROM ROWS 29 TO 37. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) - [SDR AALA990971](https://openairdocs.org/sdr/AALA990971.md): Prox Unit · not seated · Jun 28, 1999 · N14056 · Airbus A300B4605R · Landing Gear Position and Warning > TUL - FOUND LANDING GEAR WOULD NOT RETRACT ON TAKEOFF. ON TOUCH DOWN, AUTO BRAKES GRABBED THEN RELEASED BRAKE PEDALS GAVE NO BRAKING FORCE. ALT BRAKE WAS SELECTED TO STOP. (M) - [SDR AALA990920](https://openairdocs.org/sdr/AALA990920.md): Support · corroded · Jun 19, 1999 · N14056 · Airbus A300B4605R · Fuselage Miscellaneous Structure > TUL - FOUND CORROSION ON F/B SUPPORT BETWEEN FRAMES 75-76 AT AFT END R-4 DOOR. INSTALLED NEW F/B SUPPORT PER SRM 51-72-10-0. (M) - [SDR AALA990910](https://openairdocs.org/sdr/AALA990910.md): Longeron · corroded · Jun 19, 1999 · N14056 · Airbus A300B4605R · Fuselage Main, Longeron/Stringer > TUL - FOUND CORROSION ON LONGERON 58 FORWARD OF FRAME 57.1. REPAIRED PER 53-10-14-2. (M) - [SDR AALA990929](https://openairdocs.org/sdr/AALA990929.md): Support · corroded · Jun 18, 1999 · N14056 · Airbus A300B4605R · Fuselage Miscellaneous Structure > TUL - FOUND CORROSION ON F/B SUPPORT OUTBOARD OF LAV V TIE DOWN BETWEEN FRAMES 71-74. INSTALLED F/B SUPPORT OUTBOARD OF LAV V TIE DOWN FROM FRAME 71 TO 74 PER SRM 51-72-10. (M) - [SDR AALA990928](https://openairdocs.org/sdr/AALA990928.md): Support · corroded · Jun 18, 1999 · N14056 · Airbus A300B4605R · Fuselage Miscellaneous Structure > TUL - FOUND CORROSION ON F/B SUPPORT BETWEEN FRAME 75-80 IN CENTER OF CABIN. REPLACED F/B SUPPORT PER SRM 51-72-10-0. (M) - [SDR AALA990927](https://openairdocs.org/sdr/AALA990927.md): Support · corroded · Jun 18, 1999 · N14056 · Airbus A300B4605R · Fuselage Miscellaneous Structure > TUL - FOUND CORROSION ON F/B SUPPORT BETWEEN FRAMES 73-76 LEFT CENTER OF CABIN. REPLACED F/B SUPPORT PER SRM 51-72-10-0. (M) - [SDR AALA990926](https://openairdocs.org/sdr/AALA990926.md): Support · corroded · Jun 18, 1999 · N14056 · Airbus A300B4605R · Fuselage Miscellaneous Structure > TUL - FOUND CORROSION ON F/B SUPPORT BETWEEN FRAMES 74-76 AFT NR 3 SEAT TRACK. REPLACED F/B SUPPORT PER SRM 51-72-10-0 FROM FRAME 74 TO 76. (M) - [SDR AALA990919](https://openairdocs.org/sdr/AALA990919.md): Support · corroded · Jun 18, 1999 · N14056 · Airbus A300B4605R · Fuselage Miscellaneous Structure > TUL - FOUND FLOORBOARD 'D' LEFT CORRODED SEVERAL AREAS. INSTALLED NEW FLOOR SUPPORT PER SRM 51-70-00. (M) - [SDR AALA990900](https://openairdocs.org/sdr/AALA990900.md): Support · corroded · Jun 17, 1999 · N14056 · Airbus A300B4605R · Fuselage Miscellaneous Structure > TUL - FOUND CORROSION ON SUPPORT ANGLE AT AFT END OF L-4 DOOR OPENING BETWEEN FRAME 75-76. INSTALLED ANGLE AFT END OF L-4 DOOR PER SRM 51-72-10. (M) - [SDR AALA990899](https://openairdocs.org/sdr/AALA990899.md): Tie Down · corroded · Jun 17, 1999 · N14056 · Airbus A300B4605R · Fuselage Miscellaneous Structure > TUL - FOUND CORROSION ON LAV TIE DOWN ON AFT SIDE OF FRAME 74 OUTBOARD OF NR 5 SEAT TRACK. REPLACED TIE DOWN AFT SIDE OF FRAME 74 OUTBOARD OF NR 5 SEAT TRACK PER SRM 51-72-10-0. (M) - [SDR AALA990898](https://openairdocs.org/sdr/AALA990898.md): Angle · corroded · Jun 17, 1999 · N14056 · Airbus A300B4605R · Fuselage Miscellaneous Structure > TUL - Z-ANGLE CORRODED AT AFT JAMB OF L-4 DOOR SILL PLATE AT FLOOR LINE. INSTALLED 'Z' ANGLE LEFT DOOR AND AFT OF DOOR FRAME 75A PER SRM 51-72-10. (M) - [SDR AALA990897](https://openairdocs.org/sdr/AALA990897.md): Support · corroded · Jun 16, 1999 · N14056 · Airbus A300B4605R · Fuselage Miscellaneous Structure > TUL - F/B SUPPORT CORRODED FROM FRAME 74 TO FRAME 80 ON LEFT SIDE OF CABIN. REMOVED AND REPLACED F/B SUPPORT FROM FRAME 74 TO FRAME 80 PER SRM 51-72-10-0. (M) - [SDR AALA990896](https://openairdocs.org/sdr/AALA990896.md): Support · corroded · Jun 16, 1999 · N14056 · Airbus A300B4605R · Fuselage Miscellaneous Structure > TUL - FOUND CORROSION ON F/B SUPPORT IN CENTER OF CABIN FROM FRAME 74 TO 75. INSTALLED NEW F/B SUPPORT FROM FRAME 74 TO 75 IN CENTER CABIN PER SRM 51-14-10-2. (M) - [SDR AALA990893](https://openairdocs.org/sdr/AALA990893.md): Seat Track · corroded · Jun 16, 1999 · N14056 · Airbus A300B4605R · Fuselage, Seat/Cargo Attach Fittings > TUL - FOUND CORROSION ON SEAT TRACK AT STATION 58 LEFT. REMOVED AND REPLACED SEAT TRACK IN ACCORDANCE WITH SRM 51-72-10-0. (M) - [SDR AALA990895](https://openairdocs.org/sdr/AALA990895.md): Support · corroded · Jun 15, 1999 · N14056 · Airbus A300B4605R · Fuselage Miscellaneous Structure > TUL - FOUND CORROSION ON F/B SUPPORT ON SIDE OF FRAME 74 IN CENTER OF CABIN. REPLACED FLOORBOARD SUPPORT ON AFT SIDE OF FRAME 74 IN CENTER OF CABIN PER SRM 51-72-10-0. (M) - [SDR AALA990894](https://openairdocs.org/sdr/AALA990894.md): Support · corroded · Jun 15, 1999 · N14056 · Airbus A300B4605R · Fuselage Miscellaneous Structure > TUL - FOUND CORROSION ON FLOORBOARD SUPPORT 'F' BETWEEN FRAME 75 AND 76. REPLACED FLOORBOARD SUPPORT 'F' BETWEEN FRAME 75 AND 76 PER SRM 51-72-10-0. (M) - [SDR AALA990892](https://openairdocs.org/sdr/AALA990892.md): Support · corroded · Jun 15, 1999 · N14056 · Airbus A300B4605R · Fuselage Miscellaneous Structure > TUL - F/B SUPPORT CORRODED 3 PLACES RIGHT SIDE OF CABIN BETWEEN FRAMES 77-80. INSTALLED SERVICEABLE BEAM P/N A532-79224-001-0019 PER SRM 51-72-10-0. (M) - [SDR AALA990880](https://openairdocs.org/sdr/AALA990880.md): Support · corroded · Jun 15, 1999 · N14056 · Airbus A300B4605R · Fuselage Miscellaneous Structure > TUL - FOUND CORROSION ON F/B SUPPORT LEFT FROM FRAME 75 TO 80. INSTALLED LEFT F/B SUPPORT FROM FRAME 74 TO 80, 3RD F/B SUPPORT FROM LEFT SIDE PER SRM 51-72-10-0. (M) - [SDR AALA990879](https://openairdocs.org/sdr/AALA990879.md): Support · corroded · Jun 14, 1999 · N14056 · Airbus A300B4605R · Fuselage Miscellaneous Structure > TUL - FOUND CORROSION ON F/B SUPPORT FROM FRAME 79-80 ON RIGHT SIDE OF CABIN. REMOVED AND REPLACED F/B SUPPORT FROM FRAME 74 TO 80 PER SRM 51-72-10-0. (M) Next page: https://openairdocs.org/deregistered/N14056-2011-09-15/reports.md?page=2 ## 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 = 'N14056' AND deregistration_id = 'N14056-2011-09-15' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N14056-2011-09-15/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.