# Service difficulty reports: N50051, cancelled Aug 19, 2011 A list on [N50051, cancelled Aug 19, 2011](https://openairdocs.org/deregistered/N50051-2011-08-19.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 · 62 reports - [SDR AALA200802730](https://openairdocs.org/sdr/AALA200802730.md): Battery Pack · discharged · Oct 12, 2008 · N50051 · Airbus A300B4605R · Emergency Lighting > MIA - EMERGENCY LIGHTS AT SEAT ROWS 1G TO 5G INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT ROWS 1G TO 5G. SYSTEM GROUND CHECKED NORMAL OPERATION. - [SDR AALA2008022979](https://openairdocs.org/sdr/AALA2008022979.md): Adc · failed · Sep 7, 2008 · N50051 · Airbus A300B4605R · Air Data Computer > MIA INFLIGHT T937/07SEP. CREW REPORTED FIRST OFFICERS AIRSPEED STOPPED ACCELERATING AFTER TAKE OFF. BOTH CAPTAIN AND FIRST OFFICERS AIRSPEED FAILED TO ACCELERATE IN STANDBY. RETURNED TO MIA AND LANDED WITHOUT INCIDENT. REPLACED NR 2 AIR DATA COMPUTER. SYS - [SDR AALA200801411](https://openairdocs.org/sdr/AALA200801411.md): Connector · loose · May 27, 2008 · N50051 · Airbus A300B4605R · Light System Wiring > SDQ - EMERGENCY LIGHTS AT LEFT HAND FIRST CLASS INOPERATIVE. REPAIRED LOOSE CONNECTION AFT OF ROW 2 FOR EMERGENCY LIGHTS AT LEFT HAND FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) - [SDR AALA20072450](https://openairdocs.org/sdr/AALA20072450.md): Sign · inoperative · Dec 15, 2007 · N50051 · Airbus A300B4605R · Emergency Lighting > JFK - EMERGENCY EXIT SIGN AT OVERHEAD RIGHT NUMBER TWO DOOR INOPERATIVE. REPLACED EXIT SIGN ASSEMBLY FOR EMERGENCY EXIT SIGN AT OVERHEAD RIGHT NUMBER TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. - [SDR AALA20070931](https://openairdocs.org/sdr/AALA20070931.md): Connector · loose · May 20, 2007 · N50051 · Airbus A300B4605R · Light System Wiring > MIA - EMERGENCY LIGHT AT SEAT 18G INOPERATIVE. SECURED LOOSE CONNECTOR FOR EMERGENCY LIGHT AT SEAT 18G. SYSTEM GROUND CHECKED NORMAL OPERATION. - [SDR AALA20070930](https://openairdocs.org/sdr/AALA20070930.md): Connector · loose · May 20, 2007 · N50051 · Airbus A300B4605R · Light System Wiring > MIA - EMERGENCY LIGHT AT SEAT 11G INOPERATIVE. SECURED LOOSE CONNECTOR FOR EMERGENCY LIGHT AT SEAT 11G. SYSTEM GROUND CHECKED NORMAL OPERATION. - [SDR AALA20070899](https://openairdocs.org/sdr/AALA20070899.md): Bulb · burned out · May 20, 2007 · N50051 · Airbus A300B4605R · Emergency Lighting > MIA - EMERGENCY LIGHT AT SEAT 31G INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 31G. SYSTEM GROUND CHECKED NORMAL OPERATION. - [SDR AALA20070901](https://openairdocs.org/sdr/AALA20070901.md): Bulb · burned out · May 20, 2007 · N50051 · Airbus A300B4605R · Emergency Lighting > MIA- EMERGENCY LIGHT AT SEAT 18G INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 18G. SYSTEM GROUND CHECKED NORMAL OPERATION. - [SDR AALA20070900](https://openairdocs.org/sdr/AALA20070900.md): Bulb · burned out · May 20, 2007 · N50051 · Airbus A300B4605R · Emergency Lighting > MIA - EMERGENCY LIGHT AT SEAT 11G INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 11G. SYSTEM GROUND CHECKED NORMAL OPERATION. - [SDR AALA20060693](https://openairdocs.org/sdr/AALA20060693.md): Connector · loose · Sep 13, 2006 · N50051 · Airbus A300B4605R · Light System Wiring > JFK - EMERGENCY LIGHT AT SEAT 15G INOPERATIVE. RESECURED SEAT CONNECTOR FOR EMERGENCY LIGHT AT SEAT 15G. SYSTEM GROUND CHECKED NORMAL OPERATION. - [SDR AALA20060175](https://openairdocs.org/sdr/AALA20060175.md): Landing Gear · unknown · Mar 16, 2006 · N50051 · Airbus A300B4605R · Landing Gear Retraction/Extension System > JFK - INFLIGHT RIGHT LANDING GEAR WOULD NOT EXTEND. EXTENDED RIGHT LANDING GEAR MANUALLY. LANDED JFK WITHOUT INCIDENT. REPLACED RIGHT HAND MAIN LANDING GEAR DOWN (RETURN) LINE RESTRICTOR. REPLACED RIGHT HAND GEAR SEQUENCE VALVE AND UPLOCK ACTUATOR. SYSTEM - [SDR AALA20050681](https://openairdocs.org/sdr/AALA20050681.md): Actuator · inoperative · Oct 14, 2005 · N50051 · Airbus A300B4605R · Landing Gear Door Actuator > INFLIGHT UPON RETRACTION OF GEAR ON TAKEOFF GOT ECAM LANDING GEAR SYSTEM FAULT. EXCESSIVE NOISE, ELECTED TO PUT GEAR DOWN AND GOT THREE GREEN. NO DOOR LIGHTS. ELECTED TO ONCE AGAIN RETRACT GEAR RESULTING IN GEAR UP NO FAULT OR DOOR LIGHTS UNTIL GEAR HANDLE - [SDR AALA20050629](https://openairdocs.org/sdr/AALA20050629.md): Actuator · inoperative · Sep 27, 2005 · N50051 · Airbus A300B4605R · Landing Gear Door Actuator > JFK INFLIGHT T1683/27SEPTEMBER, NOSE GEAR UNSAFE LIGHTS ILLUMINATED. RETURNED TO JFK AND LANDED WITHOUT INCIDENT. REPLACED RIGHT HAND NOSE LANDING GEAR UPLOCK ACTUATOR AND DOOR CYLINDER. SYSTEM GROUND CHECKED NORMAL OPERATION. - [SDR AALA20040752](https://openairdocs.org/sdr/AALA20040752.md): Beam · cracked · Jul 1, 2004 · N50051 · Airbus A300B4605R · Fuselage Main, Structure > TUL - FRAME 51 LEFT HAND GANTRY BEAM NUMBER 4 CRACKED AT LOWER OUTBOARD FLANGE AT STATION 3195. CRACK IS 2 INCHES IN LENGTH. REPAIRED PER ESO 30595 DATED 2004 JULY 01 REPAIR NUMBER 40 531500 3505. - [SDR AALA20030907](https://openairdocs.org/sdr/AALA20030907.md): Clamp · loose · Aug 27, 2003 · N50051 · Airbus A300B4605R · Pneumatic Distribution System > AFTER TAKEOFF SMOKE OR BURNING SMELL IN CABIN DETECTED. CREW DECLARED AN EMERGENCY AND RETURNED TO BOG WITHOUT FURTHER INCIDENT. TIGHTENED SEVERAL PNEUMATIC DUCT CLAMPS. SWAPPED MINIMUM EQUIPMENT BAY DETECTOR WITH ZONE 125 DETECTOR. HISTORY OF HOT FLOORS AN - [SDR AALA20030117](https://openairdocs.org/sdr/AALA20030117.md): Indicator · faulty · Jan 27, 2003 · N50051 · Airbus A300B4605R · Fuel Quantity Indicator > BOS - FLT 989 - EN ROUTE BOS-MIA, LEFT OUTER FUEL QUANTITY STARTED DROPPING AFTER TAKEOFF ON ECAM AND FUEL QUANTITY PANEL. RETURNED BOS AND LANDED WITHOUT INCIDENT. REPLACED FUEL QUANTITY INDICATOR. SUMPED LEFT OUTER FUEL TANK. SUMP OF FUEL QUANTITY BITE S - [SDR AALA20030116](https://openairdocs.org/sdr/AALA20030116.md): Connector · contaminated · Jan 25, 2003 · N50051 · Airbus A300B4605R · Fuel Quantity Indicator > JFK - FLT 1270 - EN ROUTE SJU-EWR, LEFT ENGINE WAS SHUTDOWN FOR APPROXIMATELY 10 MINUTES DUE TO LEFT WING OUTER TANK INDICATION SHOWING FUEL QUANTITY GOING UP AND DOWN. LANDED JFK WITHOUT INCIDENT. AFTER AIRCRAFT LANDED INSPECTED LEFT WING WITH NO FUEL LEAKS - [SDR AALA20021688](https://openairdocs.org/sdr/AALA20021688.md): Wire · broken · Nov 24, 2002 · N50051 · Airbus A300B4605R · Light System Wiring > MIA - DURING OVERNIGHT MAINTENANCE, SEAT MOUNTED EMERGENCY LIGHT WIRE AT SEAT 30G BROKEN. REPLACED SEAT MOUNTED EMERGENCY LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) - [SDR AALA20020060](https://openairdocs.org/sdr/AALA20020060.md): Dampener · broken · Jan 17, 2002 · N50051 · Airbus A300B4605R · Autopilot System > MIA - FLT 2139 - EN ROUTE MIA-CCS - UNCOMMANDED RUDDER MOVEMENT DURING CLIMB-OUT. ISOLATING A/P SYSTEM DID NOT HELP. NO AIRFRAME VIBRATION NOTICES. RETURNED AND LANDED MIA WITHOUT INCIDENT. REPLACED NR 1 AND NR 2 FLIGHT AUGMENTATION COMPUTERS. DID NOT RES - [SDR AALA20011795](https://openairdocs.org/sdr/AALA20011795.md): Splice · corroded · Sep 17, 2001 · N50051 · Airbus A300B4605R · Fuselage Miscellaneous Structure > TUL - FOUND CORROSION OF SPLICE ANGLE. REPLACED SPLICE ANGLE. (M) - [SDR AALA20011794](https://openairdocs.org/sdr/AALA20011794.md): Splice · corroded · Sep 17, 2001 · N50051 · Airbus A300B4605R · Fuselage Miscellaneous Structure > TUL - FOUND CORROSION ON STRINGER SPLICE ANGLE. REPLACED SPLICE ANGLE. (M) - [SDR AALA20011793](https://openairdocs.org/sdr/AALA20011793.md): Splice · corroded · Sep 17, 2001 · N50051 · Airbus A300B4605R · Fuselage Miscellaneous Structure > TUL - FOUND CORRODED SPLICE ANGLE. REPLACED SPLICE ANGLE. (M) - [SDR AALA20011791](https://openairdocs.org/sdr/AALA20011791.md): Splice · corroded · Sep 17, 2001 · N50051 · Airbus A300B4605R · Fuselage Miscellaneous Structure > TUL - FOUND SPLICE ANGLE CORRODED. REPLACED SPLICE ANGLE. (M) - [SDR AALA20011792](https://openairdocs.org/sdr/AALA20011792.md): Splice · corroded · Sep 17, 2001 · N50051 · Airbus A300B4605R · Fuselage Miscellaneous Structure > TUL - FOUND CORRODED STRINGER SPLICE ANGLE. REPLACED STRINGER SPLICE. (M) - [SDR AALA20011790](https://openairdocs.org/sdr/AALA20011790.md): Splice · corroded · Sep 17, 2001 · N50051 · Airbus A300B4605R · Fuselage Miscellaneous Structure > TUL - FOUND SPLICE ANGLE CORRODED. REPLACED SPLICE ANGLE. (M) - [SDR AALA20011789](https://openairdocs.org/sdr/AALA20011789.md): Stringer · corroded · Sep 17, 2001 · N50051 · Airbus A300B4605R · Fuselage Main, Longeron/Stringer > TUL - FOUND STRINGER CORRODED FS 69-70. REPLACED STRINGER. (M) - [SDR AALA20011796](https://openairdocs.org/sdr/AALA20011796.md): Splice · corroded · Sep 14, 2001 · N50051 · Airbus A300B4605R · Fuselage Miscellaneous Structure > TUL - FOUND CORRODED STRINGER SPLICE ANGLE AT FRAME 65. REPLACED SPLICE ANGLE. (M) - [SDR AALA20001755](https://openairdocs.org/sdr/AALA20001755.md): Hose · leaking · Oct 25, 2000 · N50051 · Airbus A300B4605R · Hydraulic System, Main > FLT 1416 - EN ROUTE SJU-JFK, GREEN HYDRAULIC SYSTEM RESERVOIR QUANITITY SLOWLY DECREASED TO ZERO. AIR INTERRUPTED, RETURNED SJU AND LANDED WITHOUT FURTHER INCIDENT. REPLACED LEFT MAIN GEAR LOCK ACTUATOR FLEXIBLE HOSE. SERVICED HYDRAULIC SYSTEM. NO LEAKS NO - [SDR AALA20000093](https://openairdocs.org/sdr/AALA20000093.md): Light · inoperative · Jan 15, 2000 · N50051 · Airbus A300B4605R · Emergency Lighting > JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SIGN AT DOOR 3L INOPERATIVE. REPLACED EMERGENCY EXIT SIGN AT DOOR 3L. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) - [SDR AALA991153](https://openairdocs.org/sdr/AALA991153.md): Stringer · corroded · Aug 6, 1999 · N50051 · Airbus A300B4605R · Fuselage Main, Longeron/Stringer > TUL - FOUND CORROSION ON STRINGER 48L 2 PLACES BETWEEN FRAME 70 AND 71 BELOW THE WASTE WATER TANK JUNCTION BOX. REMOVED AND REPLACED SECTION OF STRINGER 48L PER SRM 51-72-10. (M) - [SDR AALA991152](https://openairdocs.org/sdr/AALA991152.md): Stringer · corroded · Aug 5, 1999 · N50051 · Airbus A300B4605R · Fuselage Main, Longeron/Stringer > TUL - FOUND CORROSION ON AFT SIDE OF FRAME C-20 ON STRINGER. STRINGER 53L IS CORRODED FROM FRAME 20 FORWARD ABOUT 8 INCHES TO 10 INCHES. REPLACED SECTION OF STRINGER AND SPLICED PER SRM 53-00-00. (M) - [SDR AALA991140](https://openairdocs.org/sdr/AALA991140.md): Angle · corroded · Aug 3, 1999 · N50051 · Airbus A300B4605R · Fuselage Miscellaneous Structure > TUL - FOUND CORROSION ON NUT PLATE AT POWER ROLLER TRAY 4TH FROM AFT, RT SIDE, OUTBOARD OF NR 5 TRAY. REMOVED AND REPLACED FLOOR ANGLE PER MM 53-10-15-2. (M) - [SDR AALA991114](https://openairdocs.org/sdr/AALA991114.md): Seat Track · corroded · Jul 29, 1999 · N50051 · Airbus A300B4605R · Fuselage, Seat/Cargo Attach Fittings > TUL - FOUND CORROSION IN SEAT TRACK AND NR 10 RIGHT SIDE OF AIRCRAFT. REMOVED AND REPLACED RT SIDE NR 10 SEAT TRACK PER SRM 51-72-10-8. (M) - [SDR AALA991127](https://openairdocs.org/sdr/AALA991127.md): Support · corroded · Jul 28, 1999 · N50051 · Airbus A300B4605R · Fuselage Miscellaneous Structure > TUL - FOUND CORROSION ON FLOORBOARD SUPPORT AT FRAME 26 BELOW CENTER SCISSOR. REPAIRED PER SRM 53-10-15, BY REPLACING SECTION OF SUPPORT ANGLE. (M) - [SDR AALA991116](https://openairdocs.org/sdr/AALA991116.md): Fitting · corroded · Jul 28, 1999 · N50051 · Airbus A300B4605R · Fuselage Miscellaneous Structure > TUL - FOUND AFT LEFT GALLEY ON TRACK B HAS CORROSION AROUND TWO ATTACH FITTING. REMOVED DAMAGED TRACK SECTION AND INSTALLED NEW ONE OF SAME P/N USING HI-LOCKS AND PRO BR870 RAF A300 SRM 51-72-10. (M) - [SDR AALA991115](https://openairdocs.org/sdr/AALA991115.md): Support · corroded · Jul 28, 1999 · N50051 · Airbus A300B4605R · Fuselage Miscellaneous Structure > TUL - FOUND CORROSION AT LAV TIE DOWN AF TOF FRAME C79 ON FLOOR SUPPORT 59 INCHES LEFT OF AIRCRAFT CENTER LINE. REMOVED DAMAGE TRACK SECTION AND INSTALLED NEW ONE OF SAME P/N USING HI-LOCKS AND PRO PR870 REF A300 SRM 51-72-10. (M) - [SDR AALA981896](https://openairdocs.org/sdr/AALA981896.md): Angle · cracked · Oct 7, 1998 · N50051 · Airbus A300B4605R · Wing Miscellaneous Structure > TUL - FOUND LEFT WING ROOT ANGLE CRACKED. REPLACED LEFT PICK UP ANGLE PER ESO 3095, DATED 10-7-98. (M) - [SDR AALA980395](https://openairdocs.org/sdr/AALA980395.md): Valve · defective · Feb 22, 1998 · N50051 · Airbus A300B4605R · Cabin Cooling System > SJU - FLT 1915 - DURING CLIMB-OUT, NR 2 PACK FAILED AT 25,000 FEET AND CABIN ALTITUDE CONTINUED TO CLIMB AT 1,000 FEET PER MINUTE. NR 1 PACK FAILED AND BOTH PACKS UNABLE TO BE RESET. OXYGEN MASKS DEPLOYED AT 14,000 CABIN ALTITUDE DURING EMERGENCY DESCENT. A - [SDR AALA972129](https://openairdocs.org/sdr/AALA972129.md): Packing · leaking · Nov 9, 1997 · N50051 · Airbus A300B4605R · Hydraulic System, Main > BOS - FLT 1096 - DURING DESCENT INTO BOS, ECAM MESSAGE HYDRAULIC RESERVOIR GREEN SYSTEM LOW. TURNED OFF GREEN SYSTEM HYDRAULIC PUMPS AND MANUALLY EXTENDED LANDING GEAR. AIRCRAFT LANDED BOS WITHOUT INCIDENT. REPLACED PACKING AT GREEN HYDRAULIC MANIFOLD ELBOW - [SDR AALA971304](https://openairdocs.org/sdr/AALA971304.md): Stringer · corroded · Jul 15, 1997 · N50051 · Airbus A300B4605R · Fuselage Main, Frame > TUL - CORROSION ON S56R BETWEEN FRAMES 57.2 AND 57.3. SPLICED NEW SECTION OF STRINGER PER SRM 53-10-4. TST: 25,726:17 HOURS, CYCLES 10,398. (X) - [SDR AALA971303](https://openairdocs.org/sdr/AALA971303.md): Frame · corroded · Jul 15, 1997 · N50051 · Airbus A300B4605R · Fuselage Main, Frame > TUL - CORROSION ON AFT SIDE OF FR 57.2 BETWEEN S55L AND S55R. INSTALLED NEW SECTION OF FRAME PER SRM 53-10-3. TST: 25,726.17 HOURS. CYCLES: 10,398. (X) - [SDR AALA971273](https://openairdocs.org/sdr/AALA971273.md): Seat Track · corroded · Jul 15, 1997 · N50051 · Airbus A300B4605R · Fuselage, Seat/Cargo Attach Fittings > TUL - NR 8 SEAT TRACK HAS SEVERAL AREAS OF CORROSION BETWEEN FRAMES 30 TO 33. INSTALLED NEW SEAT TRACK, NR 8, FROM FRAMES 30 TO 33 PER SRM 51-72-10-0. ALODINED, PRIMED AND PAINTED PER SRM 51-21-00-0. TST: 25,729.17 HOURS. CYCLES: 10,398. (X) - [SDR AALA971302](https://openairdocs.org/sdr/AALA971302.md): Seat Track · corroded · Jul 14, 1997 · N50051 · Airbus A300B4605R · Fuselage, Seat/Cargo Attach Fittings > TUL - SEAT TRACK AND FLOOR BOARD SUPPORT FROM FRAME 26 TO FRAME 29 HAS SEVERAL AREAS OF INTERGRANULAR CORROSION. INSTALLED NEW SEAT TRACK, NR 10, FROM FRAMES 26 TO 30 PER SRM 51-72-10-0. ALODINED, PRIMED AND PAINTED PER SRM 51-21-00-0. TST: 25,726.17 HOURS - [SDR AALA971301](https://openairdocs.org/sdr/AALA971301.md): Support · corroded · Jul 14, 1997 · N50051 · Airbus A300B4605R · Fuselage Miscellaneous Structure > TUL - FLOOR BOARD SUPPORT AT SEAT TRACK NR 9 BETWEEN FRAMES 26-29 HAVE INTERGRANULAR CORROSION. REMOVED DAMAGED SUPPORT, ALODINED, RPIMED AND PAINTED SERVICEABLE REPLACEMENT SUPPORT. INSTALLED WET USING PR-870 PER A-300-600 SRM'S 51-72-10-0 AND 51-21-00. TS - [SDR AALA971269](https://openairdocs.org/sdr/AALA971269.md): Angle · corroded · Jul 14, 1997 · N50051 · Airbus A300B4605R · Fuselage Miscellaneous Structure > TUL - CORROSION ON ANGLE AT LEFT CENTER ROLLER TRACK, FRAME 58. SPLICED IN NEW SECTION OF FLOOR ANGLE SUPPORT PER SRM 53-10-13. TST: 25,726.17 HOURS. CYCLES: 10,398. (X) - [SDR AALA971265](https://openairdocs.org/sdr/AALA971265.md): Support · corroded · Jul 14, 1997 · N50051 · Airbus A300B4605R · Fuselage Miscellaneous Structure > TUL - CORROSION ON LAVATORY-V FLOOR SUPPORT BEAM AT FRAME C-73. INSTALLED FLOOR BEAM UNDER LAV-V PER SRM 51-72-10-0. TST: 25,726.17 HOURS. CYCLES: 10,398. (X) - [SDR AALA971257](https://openairdocs.org/sdr/AALA971257.md): Seat Track · corroded · Jul 12, 1997 · N50051 · Airbus A300B4605R · Fuselage, Seat/Cargo Attach Fittings > TUL - CORROSION ON SEAT TRACK NR 8 BETWEEN FRAME 26 - FRAME 29, BOTH SIDES OF FLANGE. INSTALLED NEW SEAT TRACK NR 8 BETWEEN FRAME 26 - FRAME 29 PER SRM 51-72-10-0. TST: 25,726. CYCLES: 10,398. (X) - [SDR AALA971259](https://openairdocs.org/sdr/AALA971259.md): Frame · cracked · Jul 11, 1997 · N50051 · Airbus A300B4605R · Fuselage Main, Frame > TUL - FRAME 45, LEFT, HAS CRACK BELOW ANGLE FITTING. INSTALLED FRAME DOUBLER REPAIR PER AARD 53-00-00-5, REPAIR 5. TST: 25,726. CYCLES: 10,398. (X) - [SDR AALA971220](https://openairdocs.org/sdr/AALA971220.md): Seat Track · corroded · Jul 11, 1997 · N50051 · Airbus A300B4605R · Fuselage, Seat/Cargo Attach Fittings > TUL - CORROSION AROUND LAVATORY 'L' MOUNT, OUTBOARD. INSTALLED DOUBLER AFTER CORROSION REMOVAL PER AARD 53-20-00-2. (X) - [SDR AALA971219](https://openairdocs.org/sdr/AALA971219.md): Seat Track · corroded · Jul 11, 1997 · N50051 · Airbus A300B4605R · Fuselage, Seat/Cargo Attach Fittings > TUL - CORROSION AROUND LAVATORY L-MOUNT, INBOARD. INSTALLED DOUBLER AFTER CORROSION REMOVAL PER AARD 53-20-00-2. TST: 25,726. CYCLES: 10,398. (X) Next page: https://openairdocs.org/deregistered/N50051-2011-08-19/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 = 'N50051' AND deregistration_id = 'N50051-2011-08-19' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N50051-2011-08-19/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.