# Service difficulty reports: N810US, cancelled Oct 1, 2003 A list on [N810US, cancelled Oct 1, 2003](https://openairdocs.org/deregistered/N810US-2003-10-01.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 · 54 reports - [SDR USAAD01108](https://openairdocs.org/sdr/USAAD01108.md): Light · inoperative · May 16, 2001 · N810US · Doug DC981 · Emergency Lighting > PHL - THE LOW LEVEL EMERGENCY LIGHT AT SEAT ROW 25 WAS INOPERATIVE. MAINTENANCE REPLACED THE LIGHT AND TRANSMITTER ASSEMBLY. (M) - [SDR USAAD01100](https://openairdocs.org/sdr/USAAD01100.md): Module · failed · May 10, 2001 · N810US · Doug DC981 · Emergency Lighting > CLT - THE EMERGENCY LIGHTS IN THE AFT PASSENGER CABIN WOULD NOT OPERATE CORRECTLY. MAINTENANCE REPLACED THE AFT EMERGENCY LIGHT CONTROL MODULE. (M) - [SDR USAA010550](https://openairdocs.org/sdr/USAA010550.md): Skin · cracked · Apr 20, 2001 · N810US · Doug DC981 · Fuselage Main, Plate/Skin > PIT - FOUND SKIN CRACKED.25 INCH, STATION 1418 LONGERON 2 RT. CUT OUT DAMAGE, INSTALLED FILLER AND DOUBLER PER SRM 53-04 FIG 40. (M) - [SDR USAA010420](https://openairdocs.org/sdr/USAA010420.md): Skin · cracked · Apr 18, 2001 · N810US · Doug DC981 · Fuselage Main, Plate/Skin > PIT - FOUND SKIN CRACKED 1 INCH, STATION 1474 CANTED AT 9 OCLOCK POSITION ON FUSELAGE. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 53-01 FIG 2. (M) - [SDR USAAD01071](https://openairdocs.org/sdr/USAAD01071.md): Battery · discharged · Mar 30, 2001 · N810US · Doug DC981 · Emergency Lighting > BOS - THE SEAT MOUNTED EMERGENCY LIGHT BATTERIES WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. (M) - [SDR USAAD01029](https://openairdocs.org/sdr/USAAD01029.md): Light · misinstalled · Feb 11, 2001 · N810US · Doug DC981 · Emergency Lighting > MCO - WHILE COMPLETING AND ''A'' CHECK INSPECTION, THE LOWER LEVEL EMERGENCY LIGHTS WERE FOUND TO BE INSTALLED AT SEAT ROWS OTHER THEN THOSE INDICATED BY THE PAPERWORK. THE LOW LEVEL EMERGENCY LIGHTS WERE INSTALLED IN THE PROPER POSITIONS. (M) - [SDR USAAD00144](https://openairdocs.org/sdr/USAAD00144.md): Sensor · failed · Sep 10, 2000 · N810US · Doug DC981 · Detection System > ROC-BOS - FLT 392 - AFTER TAKEOFF, THE LEFT AIR CONDITIONING SUPPLY HIGH TEMP LIGHT WOULD NOT EXTINGUISH, EVEN IN THE HP BLEED OFF POSITION. THE FLIGHT ATTENDANTS ALSO REPORTED A SMOKE SMELL. MAINTENANCE REPLACED THE AIR CONDITIONING HIGH SUPPLY SENSOR. (M) - [SDR USAAD00112](https://openairdocs.org/sdr/USAAD00112.md): Light · failed · Jul 6, 2000 · N810US · Doug DC981 · Emergency Lighting > BOS - THE AFT GALLEY EMERGENCY EXIT IDENTIFIER LIGHT LED LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EXIT IDENTIFIER LIGHT. (M) - [SDR USAAD00067](https://openairdocs.org/sdr/USAAD00067.md): Battery · discharged · May 4, 2000 · N810US · Doug DC981 · Emergency Lighting > LGA - THE FORWARD EMERGENCY EXIT WINDOW LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY. (X) - [SDR USAAD00036](https://openairdocs.org/sdr/USAAD00036.md): Battery · discharged · Feb 27, 2000 · N810US · Doug DC981 · Emergency Lighting > PIT - THE RIGHT AFT OVERWING EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE RIGHT AFT OVERWING EMERGENCY LIGHT BATTERY. (M) - [SDR USAAD99180](https://openairdocs.org/sdr/USAAD99180.md): Battery · discharged · Dec 21, 1999 · N810US · Doug DC981 · Emergency Lighting > PHL - THE GALLEY SERVICE DOOR AND RIGHT AFT EMERGENCY WINDOW EMERGENCY LIGHTS WERE INOPERATIVE. REPLACED THE GALLEY SERVICE DOOR AND EMERGENCY WINDOW EMERGENCY LIGHT BATTERIES. (M) - [SDR 2000ZZZM226](https://openairdocs.org/sdr/2000ZZZM226.md): Battery · discharged · Dec 21, 1999 · N810US · Doug DC981 · Emergency Lighting > THE LOW LEVEL EMERGENCY LIGHTS WERE INOPERATIVE. REPLACED 7 LOW LEVEL EMERGENCY LIGHT BATTERIES. (M) - [SDR 2000ZZZM225](https://openairdocs.org/sdr/2000ZZZM225.md): Battery · discharged · Dec 21, 1999 · N810US · Doug DC981 · Emergency Lighting > THE AFT AIRSTAIR EXIT IDENTIFIER LIGHT WAS INOPERATIVE. REPLACED THE AFT AIRSTAIR EXIT IDENTIFIER BATTERY. (M) - [SDR USAA991111](https://openairdocs.org/sdr/USAA991111.md): Floor · corroded · Oct 8, 1999 · N810US · Doug DC981 · Fuselage Floor Panel > PIT - DURING Q2 CHECK, FOUND 2 FOOT BY 3 FOOT CORRODED AREA AT SUB-FLOOR AT STA 160 - STA 200 AND BETWEEN CENTERLINE OF AIRCRAFT AND RT INBOARD SEAT TRACK. CORROSION TASK NR C46-53303 CORROSION LEVEL 1. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER PER SRM 53-0 - [SDR USAA991110](https://openairdocs.org/sdr/USAA991110.md): Frame · corroded · Oct 8, 1999 · N810US · Doug DC981 · Fuselage Main, Frame > PIT - DURING Q2 CHECK, FOUND 1 INCH CRACK AT FRAME STA 160 LONGERON 2 LEFT. INSTALLED SPLICES PER SRM 53-02 FIG 18. (X) - [SDR USAA991109](https://openairdocs.org/sdr/USAA991109.md): Frame · corroded · Oct 8, 1999 · N810US · Doug DC981 · Fuselage Main, Frame > PIT - DURING Q2 CHECK, FOUND.50 INCH LONG CRACK AT FRAME ATTACH POINT AT STA 160. INSTALLED SPLICES PER SRM 53-02 FIG 18. (X) - [SDR USAA991108](https://openairdocs.org/sdr/USAA991108.md): Frame · corroded · Oct 8, 1999 · N810US · Doug DC981 · Fuselage Main, Frame > PIT - DURING Q2 CHECK, FOUND.50 INCH CRACK AT FRAME ATTACH POINT AT STA 160 LONGERON 3 LEFT. INSTALLED SPLICE PER SRM 53-02, FIG 18. (X) - [SDR USAA991107](https://openairdocs.org/sdr/USAA991107.md): Bulkhead · corroded · Oct 8, 1999 · N810US · Doug DC981 · Fuselage Main, Bulkhead > PIT - DURING Q2 CHECK, FOUND UPPER LEFT CUSP HANDLE 2 INCH BY 3 INCH CORRODED AT STA 160 AT AIRSTAIRS FORWARD BULKHEAD LEFT CORNER. INSTALLED DOUBLER PER EA 52924. (X) - [SDR USAA991106](https://openairdocs.org/sdr/USAA991106.md): Web · corroded · Oct 8, 1999 · N810US · Doug DC981 · Fuselage Miscellaneous Structure > PIT - DURING Q2 CHECK, FOUND 6 INCH BY 1 INCH AREA OF CORROSION AT WEB AT STA 1338 AT LONGERON 18R (RT AFT LAVATORY). CORROSION TASK NR C58-53300. CORROSION LEVEL: 1. CUT OUT DAMAGED AREA OF THE WEB AND SPLICED IN NEW SECTION PER SRM 53-01, FIG 2, AND SRM - [SDR USAA991105](https://openairdocs.org/sdr/USAA991105.md): Service Door · corroded · Oct 8, 1999 · N810US · Doug DC981 · Service Doors > PIT - DURING Q2 CHECK, FOUND CORROSION AT STATION 205 AT AFT SIDE OF SERVICE DOOR 2 INCH BY 3 INCH AT STATION 205 LONG 18 CUSP AREA. CORROSION LEVEL 1, CORROSION TASK NR C46-53301. INSTALLED NEW CUSP MEMBRANE AND SPLICED DOOR PAN PER SRM 53-05 SIG 55 AND EA - [SDR USAA991088](https://openairdocs.org/sdr/USAA991088.md): Support · corroded · Oct 8, 1999 · N810US · Doug DC981 · Fuselage Miscellaneous Structure > PIT - DURING Q2 CHECK, FOUND 1 INCH BY 1 INCH CORROSION ON AND AROUND FASTENER HOLES, QTY 4, AT FLOOR SUPPORT STATION 636 BETWEEN LONGS 28L AND 29R. CORROSION TASK NR C51-53300, CORROSION LEVEL 2. REPLACED FLOOR SUPPORT PER EA 53012. (M) - [SDR USAA991087](https://openairdocs.org/sdr/USAA991087.md): Skin · cracked · Oct 8, 1999 · N810US · Doug DC981 · Fuselage Main, Plate/Skin > PIT - DURING Q2 CHECK, FOUND 1.5 INCH CRACK IN SKIN AT FORWARD UPPER CORNER MED DOORWAY. DOUBLERS INSTALLED PER SRM 53-05, FIG 26. (M) - [SDR USAAD99095](https://openairdocs.org/sdr/USAAD99095.md): Coalescer Bag · contaminated · Jul 13, 1999 · N810US · Doug DC981 · Humidity Control System > PHL-PIT - FLT 656 - AFTER TAKEOFF, BOTH AFT LAVATORY SMOKE DETECTORS ACTIVATED. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED BOTH WATER SEPARATOR COALESCER BAGS. (M) - [SDR USAAD98115](https://openairdocs.org/sdr/USAAD98115.md): Batteries · discharged · Jun 25, 1998 · N810US · Doug DC981 · Emergency Lighting > IND - FIRST CLASS CEILING EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. (M) - [SDR USAAD98114](https://openairdocs.org/sdr/USAAD98114.md): Battery Pack · discharged · Jun 25, 1998 · N810US · Doug DC981 · Emergency Lighting > IND - EXTERIOR EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK. (M) - [SDR USAAD98064](https://openairdocs.org/sdr/USAAD98064.md): Connector · corroded · Apr 6, 1998 · N810US · Doug DC981 · Autopilot System > MCO - FLT 1826 - ON CLIMB-OUT, AIRCRAFT BEGAN TO YAW AT AROUND 3,000 FEET. CAPTAIN TURNED YAW DAMPER OFF AND RUDDER UNRESTRICTED LIGHT CAME ON. CAPTAIN SWITCHED TO RUDDER POWER CONTROL TO MANUAL AND YAW STOPPED. TURNED AUTOPILOT ON AND YAW BEGAN AGAIN. TUR - [SDR 98ZZZX2258](https://openairdocs.org/sdr/98ZZZX2258.md): Sensor · intermittent · Apr 6, 1998 · N810US · Doug DC981 · Autopilot System > MCO - FLT 1826 - ON CLIMB-OUT, AIRCRAFT BEGAN TO YAW AT AROUND 3,000 FEET. CAPTAIN TURNED YAW DAMPER OFF AND RUDDER UNRESTRICTED LIGHT CAME ON. CAPTAIN SWITCHED TO RUDDER POWER CONTROL TO MANUAL AND YAW STOPPED. TURNED AUTOPILOT ON AND YAW BEGAN AGAIN. TUR - [SDR 98ZZZX2257](https://openairdocs.org/sdr/98ZZZX2257.md): Actuator · malfunctioned · Apr 6, 1998 · N810US · Doug DC981 · Autopilot System > MCO - FLT 1826 - ON CLIMB-OUT, AIRCRAFT BEGAN TO YAW AT AROUND 3,000 FEET. CAPTAIN TURNED YAW DAMPER OFF AND RUDDER UNRESTRICTED LIGHT CAME ON. CAPTAIN SWITCHED TO RUDDER POWER CONTROL TO MANUAL AND YAW STOPPED. TURNED AUTOPILOT ON AND YAW BEGAN AGAIN. TUR - [SDR USAAD97214](https://openairdocs.org/sdr/USAAD97214.md): Engine · failed · Nov 23, 1997 · N810US · Doug DC981 · Engine (Turbine/Turboprop) > MCO - FLT 1554 - AFTER TAKEOFF, THE TOWER ADVISED THE CREW THAT SPARKS WERE OBSERVED COMING FROM THE RIGHT ENGINE. THE FLGIHT DIVERTED TO MCO, LANDED AND TAXIED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE ENGINE. (M) - [SDR USAAD97129](https://openairdocs.org/sdr/USAAD97129.md): O-Ring · cut · Jul 29, 1997 · N810US · Doug DC981 · Engine Oil Cooler > PIT - FL541 - CAPTAIN ADVISED THAT CLIMBING THROUGH 10, 000 FT, THE NR 1 ENGINE OILQTY INDICATED A STEADY LOSS OF OIL. CREW SHUT DOWN THE NR 1 ENGINE WITH 5 QUARTS OF OIL REMAINING AND DECLARED AN EMERGENCY. FLIGHT RETURNED TO FIELD AT PIT AND LANDED WITHOUT - [SDR USAAD97085](https://openairdocs.org/sdr/USAAD97085.md): Engine · failed · May 12, 1997 · N810US · Doug DC981 · Engine (Turbine/Turboprop) > FLT 2260 - DCA-FLL - AFTER TAKEOFF, AT ABOUT 500-600 FEET, THE CREW HEARD A LOUD BANG AND THE NR 1 ENGINE SHUTDOWN. DIVERTED TO IAD. REPLACED NR 1 ENGINE. (M) - [SDR USAA960776](https://openairdocs.org/sdr/USAA960776.md): Skin · cracked · Dec 6, 1996 · N810US · Doug DC981 · Fuselage Main, Plate/Skin > PIT - DURING C-2 CHECK, FOUND 1 INCH CRACK IN SKIN AT STATION 1437, 3RT. REMOVED DAMAGE AND INSTALLED DOUBLER PER SRM 53-04 FIG 27. (M) - [SDR USAAD955004](https://openairdocs.org/sdr/USAAD955004.md): Fuel Control · failed · Oct 21, 1995 · N810US · Doug DC981 · Fuel Control/Turbine Engines > IND - FLT NR 987 - AT CRUISE, NR 2 ENGINE ADVANCED TO FULL THROTTLE AND WOULD NOT RESPOND TO CONTROLS. THE CAPTAIN SHUT DOWN NR 2 ENGINE DIVERTED TO IND. THE FLT LANDED WITHOUT FURTHER INCIDENT. REMOVED AND REPLACED RIGHT FUEL CONTROL. RAN ENGINE. OPS CHEC - [SDR USAA950873](https://openairdocs.org/sdr/USAA950873.md): Skin · gouged · Jul 7, 1995 · N810US · Doug DC981 · Fuselage Main, Plate/Skin > PIT - DURING Q-1/CX-6 CHECK INSPECTION, FOUND GOUGE.014 INCH DEEP AT STATION 1309-1322 ABOVE LONGERON 20R. BLENDED GOUGE TO.016 INCH AND INSTALLED DOUBLER PER SRM 53-04 FIG 38 VIEW G. (M) - [SDR USAA950872](https://openairdocs.org/sdr/USAA950872.md): Bulkhead · hole · Jul 7, 1995 · N810US · Doug DC981 · Fuselage Main, Bulkhead > PIT - DURING Q-1/CX-6 CHECK INSPECTION, FOUND.5 INCH DIAMETER HOLE AT STATION 1380 LONGERON 6L IN TAIL INTERIOR BULKHEAD. REMOVED DAMAGED AREA AND INSTALLED DOUBLER REPAIR PER SRM 53-01 FIG 3. (M) - [SDR USAA950871](https://openairdocs.org/sdr/USAA950871.md): Fitting · cracked · Jul 7, 1995 · N810US · Doug DC981 · Fuselage Miscellaneous Structure > PIT - DURING Q-1/CX-6 CHECK INSPECTION, FOUND 1 INCH AND 1.5 INCH CRACK IN LEFT AND RIGHT SADDLE SUPPORT FITTING FORWARD END OF KEEL STRUCTURE, STATION 940. FABRICATED AND INSTALLED KEEL SADDLE SUPPORT FITTING PER SRM 53-05 FIG 81. (M) - [SDR USAA950870](https://openairdocs.org/sdr/USAA950870.md): Support · cracked · Jul 7, 1995 · N810US · Doug DC981 · Fuselage Miscellaneous Structure > PIT - DURING Q-1/CX-6 CHECK INSPECTION, FOUND 1 INCH CRACK STATION 937 LEFT AT KEEL TO SADDLE SUPPORT. FABRICATED SUPPORT CHANNEL AND INSTALLED PER SRM 53-05 FIG 81. (M) - [SDR USAA950869](https://openairdocs.org/sdr/USAA950869.md): Skin · gouged · Jul 7, 1995 · N810US · Doug DC981 · Fuselage Main, Plate/Skin > PIT - DURING Q-1/CX-6 CHECK INSPECTION, FOUND GOUGE.065 BY 1 INCH LONG STATION 1309 LONGERON 29L. NDT CHECK FOR CRACKS AND INSTALLED REPAIR DOUBLER PER SRM 53-04 FIG 38. (M) - [SDR USAA950868](https://openairdocs.org/sdr/USAA950868.md): Skin · cracked · Jul 7, 1995 · N810US · Doug DC981 · Fuselage Main, Plate/Skin > PIT - DURING Q-1/CX-6 CHECK INSPECTION, FOUND.5 INCH CRACK IN SKIN AT STATION 1380 RIGHT SIDE BETWEEN LONGERON 13R AND 14R. CUT OUT CRACK AND INSTALLED REPAIR DOUBLER AND FILLER PER SRM 53-04 FIG 18. (M) - [SDR USAA950867](https://openairdocs.org/sdr/USAA950867.md): Clip · cracked · Jul 7, 1995 · N810US · Doug DC981 · Fuselage Miscellaneous Structure > PIT - DURING Q-1/CX-6 CHECK INSPECTION, FOUND ONE.5 INCH LONG CRACK IN SKIN CLIP STATION 1307 LONGERON 16R. SPLICED IN NEW SKIN CLIP PER SRM 53-03. (M) - [SDR USAA950866](https://openairdocs.org/sdr/USAA950866.md): Clip · cracked · Jul 7, 1995 · N810US · Doug DC981 · Fuselage Miscellaneous Structure > PIT - DURING Q-1/CX-6 CHECK INSPECTION, FOUND 1 INCH LONG CRACK STATION 1307 SKIN CLIP LONGERON 16L. SPLICED IN NEW SECTION OF SKIN CLIP PER SRM 53-03. (M) - [SDR USAA950865](https://openairdocs.org/sdr/USAA950865.md): Skin · cracked · Jul 7, 1995 · N810US · Doug DC981 · Fuselage Main, Plate/Skin > PIT - DURING Q-1/CX-6 CHECK INSPECTION, FOUND CRACK.125 INCH LONG IN SKIN AT STATION 1437 LONGERON 2L. STOP DRILLED CRACK AND INSTALLED REPAIR DOUBLER PER US AIR EA NR 30625. (M) - [SDR USAA950864](https://openairdocs.org/sdr/USAA950864.md): Skin · dented · Jul 7, 1995 · N810US · Doug DC981 · Fuselage Main, Plate/Skin > PIT - DURING Q-1/CX-6 CHECK INSPECTION, FOUND DENT IN SKIN 1.25 INCH BY 1.25 INCH BY.108 DEEP AT STATION 221 BETWEEN LONGERON 15L AND 16L. CUT OUT DAMAGE AND INSTALLED CLASS 1 REPAIR DOUBLER PER SRM 53-04 FIG 38 SHEET NR 21 VIEW 1. (M) - [SDR USAA950863](https://openairdocs.org/sdr/USAA950863.md): Clip · cracked · Jul 7, 1995 · N810US · Doug DC981 · Fuselage Miscellaneous Structure > PIT -DURING Q-1/CX-6 CHECK INSPECTION, FOUND 1.5 INCH CRACK IN SKIN CLIP STATION 1307 LONGERON 16R. MANUFACTURED SKIN SLIP AND INSTALLED PER SRM 51-01. (M) - [SDR USAA950862](https://openairdocs.org/sdr/USAA950862.md): Longeron · cracked · Jul 7, 1995 · N810US · Doug DC981 · Fuselage Main, Longeron/Stringer > PIT - DURING Q-1/CX-6 CHECK INSPECTION, FOUND TWO.75 INCH LONGERON CRACKS AT STATION 237 AND 256 LONGERON 17L. INSTALLED SPLICE REPAIR PER SRM 53-02 FIG 2. (M) - [SDR USAA950861](https://openairdocs.org/sdr/USAA950861.md): Skin · puncture · Jul 7, 1995 · N810US · Doug DC981 · Fuselage Main, Plate/Skin > PIT - DURING Q-1/CX-6 CHECK INSPECTION, FOUND PUNCTURE IN APU SHROUD ENCLOSURE SKIN. MFG AND INSTALLED REPAIR DOUBLER PER SRM 53-01 PG 2. (M) - [SDR USAA950860](https://openairdocs.org/sdr/USAA950860.md): Longeron · corroded · Jul 7, 1995 · N810US · Doug DC981 · Fuselage Main, Longeron/Stringer > PIT - DURING Q-1/CX-6 CHECK INSPECTION, FOUND LEVEL 1 CORROSION PREVIOUSLY REWORKED STATION 1300 TO 1338 LONGERON 29L. INSTALLED LONGERON SPLICE REPAIR PER SRM 53-02 FIG 14. (M) - [SDR USAA950859](https://openairdocs.org/sdr/USAA950859.md): Longeron · corroded · Jul 7, 1995 · N810US · Doug DC981 · Fuselage Main, Longeron/Stringer > PIT - DURING Q-1/CX-6 CHECK INSPECTION, FOUND LEVEL 1 CORROSION PREVIOUSLY REWORKED STATION 1282 TO 1300 LONGERON 30. SPLICED IN NEW SECTION OF LONGERON PER SRM 53-02 FIG 14. (M) - [SDR USAA950858](https://openairdocs.org/sdr/USAA950858.md): Skin · gouge · Jul 7, 1995 · N810US · Doug DC981 · Fuselage Main, Plate/Skin > PIT - DURING Q-1/CD-6 CHECK INSPECTION, FOUND GOUGE.015 BY 1.75 INCHES LONG AT STATION 755 LONGERON 15R. BLENDED GOUGE, DYE CHECKED AND INSTALLED INTERNAL DOUBLER PER SRM 53-04 FIG 38 VIEW E. (M) - [SDR USAA950857](https://openairdocs.org/sdr/USAA950857.md): Skin · cracked · Jul 7, 1995 · N810US · Doug DC981 · Fuselage Main, Plate/Skin > PIT - DURING Q-1/CX-6 CHECK INSPECTION, FOUND CRACK.75 INCHES LONG AND CREASE.055 DEEP AT STATION 522 BETWEEN LONGERON 21R AND 22R FUSELAGE SKIN. CUT OUT DAMAGED AREA AND INSTALLED EXTERIOR DOUBLER AND INTERIOR FINGER DOUBLER PER SRM 53-04 FIG 12B. (M) Next page: https://openairdocs.org/deregistered/N810US-2003-10-01/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 = 'N810US' AND deregistration_id = 'N810US-2003-10-01' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N810US-2003-10-01/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.