# Service difficulty reports: N809US, cancelled Nov 18, 2003 A list on [N809US, cancelled Nov 18, 2003](https://openairdocs.org/deregistered/N809US-2003-11-18.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 · 72 reports - [SDR USAA011137](https://openairdocs.org/sdr/USAA011137.md): Skin · cracked · Aug 21, 2001 · N809US · Doug DC981 · Passenger/Crew Doors > CLT - FOUND DOOR SKIN CRACKED 3 INCHES, AFT END OF DOOR HOLD OPEN HOOK/DOOR SKIN. INSTALLED DOUBLER PER SRM 52-05 FIG 20A. (M) - [SDR USAA011179](https://openairdocs.org/sdr/USAA011179.md): Skin · cracked · Aug 16, 2001 · N809US · Doug DC981 · Doors > TPA - FOUND SKIN CRACKED 3 INCHES, AFT END OF DOOR HOLD OPEN HOOK OPENING DOOR SKIN. INSTALLED DOUBLER PER SRM 52-05 FIG 20A. (M) - [SDR 2001F00176](https://openairdocs.org/sdr/2001F00176.md): Battery · discharged · Jul 9, 2001 · N809US · Doug DC981 · Emergency Lighting > IND - THE LOW LEVEL EMERGENCY LIGHTS AND THE LEFT AFT EXIT WINDOW SIDEWALL LIGHT FAILED TO TEST. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. REF USAAD01134. (M) - [SDR USAAD01134](https://openairdocs.org/sdr/USAAD01134.md): Battery · discharged · Jul 9, 2001 · N809US · Doug DC981 · Emergency Lighting > IND - THE LOW LEVEL EMERGENCY LIGHTS AND THE LEFT AFT EXIT WINDOW SIDEWALL LIGHT FAILED TO TEST. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. (M) - [SDR USAA010453](https://openairdocs.org/sdr/USAA010453.md): Skin · cracked · Apr 25, 2001 · N809US · Doug DC981 · Fuselage Main, Plate/Skin > CLT - FOUND 2 CRACKS IN FUSELAGE SKIN, BS 58.75, RIGHT SIDE APPROX 10 INCHES BELOW FLOORLINE. INSTALLED DOUBLER PER SRM 53-01, FIG 2. (M) - [SDR USAAD01083](https://openairdocs.org/sdr/USAAD01083.md): Light · inoperative · Apr 24, 2001 · N809US · Doug DC981 · Emergency Lighting > IND - THE LEFT AFT OVERWING EMERGENCY WINDOW EXIT IDENTIFIER LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE EXIT IDENTIFIER LIGHT ASSEMBLY. (M) - [SDR USAAD01064](https://openairdocs.org/sdr/USAAD01064.md): Warning Light · illuminated · Mar 26, 2001 · N809US · Doug DC981 · Landing Gear Position and Warning > PBI-PIT - FLT 1575 - THE NOSE LANDING GEAR UNSAFE LIGHT ILLUMINATED DURING GEAR RETRACTION. THE FLIGHT RETURNED TO PBI AND LANDED WITHOUT INCIDENT. S/D - MAINTENANCE SECURED THE NOSE LANDING GEAR DOORS AND PERFORMED AN OVERWEIGHT LANDING INSPECTION. (M) - [SDR USAAD00181](https://openairdocs.org/sdr/USAAD00181.md): Engine · seized · Nov 26, 2000 · N809US · Doug DC981 · Engine (Turbine/Turboprop) > PIT-PHL - FLT 523 - AFTER TAKEOFF AND CLIMBING THROUGH 2,000 FEET THE RIGHT ENGINE SEIZED. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. 15 MINUTES SINGLE ENGINE TIME. MAINTENANCE REPLACED THE RIGHT ENGINE. (M) - [SDR 20000428AP014](https://openairdocs.org/sdr/20000428AP014.md): Battery · discharged · Feb 23, 2000 · N809US · Doug DC981 · Emergency Lighting > PIT - THE LOW LEVEL EMERGENCY LIGHTING WAS INOPERATIVE. MAINTENANCE REPLACED DOOR EXIT IDENTIFER LIGHT ASSEMBLIES AND THE FLOOR LEVEL LIGHT BATTERIES. (M) - [SDR USAAD00038](https://openairdocs.org/sdr/USAAD00038.md): Light · failed · Feb 23, 2000 · N809US · Doug DC981 · Emergency Lighting > PIT - THE LOW LEVEL EMERGENCY LIGHTING WAS INOPERATIVE. MAINTENANCE REPLACED DOOR EXIT IDENTIFIER LIGHT ASSEMBLIES AND THE FLOOR LEVEL LIGHT BATTERIES. (M) - [SDR USAA991505](https://openairdocs.org/sdr/USAA991505.md): Beam · corroded · Jan 8, 2000 · N809US · Doug DC981 · Fuselage Miscellaneous Structure > PIT - DURNG Q-6, C-6 CHECK, FOUND 3 INCH BY 57 INCH CORRODED AREA AT BEAM, DOUBLER, PAN AT STATION 636 TO 693 MID CARGO DOOR JAMB LOWER EDGE. CORROSION LEVEL 1. CORROSION TASK NR C51-53300. SPLICED IN NEW PAN SECTION PER SRM 53-05 FIG 63. (M) - [SDR USAA991504](https://openairdocs.org/sdr/USAA991504.md): Longeron · corroded · Jan 8, 2000 · N809US · Doug DC981 · Fuselage Main, Longeron/Stringer > PIT - DURING Q-6, C-6 CHECK, FOUND 1 INCH BY 1 INCH CORRODED AREA AT STATION 636 LONG 30 CORROSION LEVEL 1, CORROSION TASK NR C51-53300. REMOVED CORROSION, TREATED, PRIMED, PAINTED AND INSTALLED FASTENER. (M) - [SDR USAA991503](https://openairdocs.org/sdr/USAA991503.md): Longeron · corroded · Jan 8, 2000 · N809US · Doug DC981 · Fuselage Main, Longeron/Stringer > PIT - DURING Q-6, C-6 CHECK, FOUND.5 INCH BY.5 INCH CORRODED AREA AT LONGERON 281 STATION 1060. CORROSION TASK NR C57-53300, CORROSION LEVEL 1. REMOVED CORROSION, TREATED, PRIMED, PAINTED AND INSTALLED FASTENER. (M) - [SDR USAAD99164](https://openairdocs.org/sdr/USAAD99164.md): Battery · discharged · Nov 12, 1999 · N809US · Doug DC981 · Emergency Lighting > THE NACELLE EMERGENCY LIGHTS WERE INOPERATIVE. REPLACED THE NACELLE EMERGENCY LIGHT BATTERY. (M) - [SDR 99ZZZM799](https://openairdocs.org/sdr/99ZZZM799.md): Battery · discharged · Nov 12, 1999 · N809US · Doug DC981 · Emergency Lighting > THE PASSENGER CABIN LOW LEVEL EMERGENCY LIGHTS WERE INOPERATIVE. REPLACED THE PASSENGER CABIN LOW LEVEL EMERGENCY LIGHT BATTERIES. (M) - [SDR USAA991178](https://openairdocs.org/sdr/USAA991178.md): Lasting · corroded · Oct 26, 1999 · N809US · Doug DC981 · Main Landing Gear > PIT - DURING RON AND EA 53181, FOUND 100 PERCENT CORROSION OF ALL BUSHING AREA OF BOTTLE PIN FOR THE RIGHT MLG. DEFECTIVE PART REPLACED WITH IDENTICAL PART NUMBER. (M) - [SDR USAA991177](https://openairdocs.org/sdr/USAA991177.md): Bottle Pin · sheared · Oct 26, 1999 · N809US · Doug DC981 · Main Landing Gear > PIT - PILOT REPORT INDICATED THREADS OF BOTTLE PIN FOR THE LEFT MAIN LANDING GEAR SHEARED 100 PERCENT. DEFECTIVE PART REPLACED WITH IDENTICAL PART NUMBER. (M) - [SDR USAAD99150](https://openairdocs.org/sdr/USAAD99150.md): Fitting · broken · Oct 21, 1999 · N809US · Doug DC981 · Landing Gear Retraction/Extension System > EWR-PIT - FLT 760 - DURING LANDING GEAR EXTENSION PRIOR TO LANDING THE RIGHT HYDRAULIC SYSTEM WENT TO ZERO. THERE GEAR INDICATION LIGHTS WERE GREEN, BUT THE CREW ELECTED TO FLYBY THE TOWER FOR CONFIRMATION. ALL APPEARED NORMAL AND THE AIRCRAFT LANDED WITHOUT - [SDR USAAD98195](https://openairdocs.org/sdr/USAAD98195.md): Battery · discharged · Nov 2, 1998 · N809US · Doug DC981 · Emergency Lighting > PHL - THE LOW LEVEL EMERGENCY LIGHT AT ROWS 16 WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY. (M) - [SDR USAAD98193](https://openairdocs.org/sdr/USAAD98193.md): Power Supply · inoperative · Oct 30, 1998 · N809US · Doug DC981 · Emergency Lighting > PIT - THE EMERGENCY LIGHTS STAYED ON ALL THE TIME. MAINTENANCE REPLACED THE FORWARD ENTRY AND COCKPIT EMERGENCY LIGHT POWER SUPPLY. (M) - [SDR USAAD98126](https://openairdocs.org/sdr/USAAD98126.md): Battery · discharged · Jul 18, 1998 · N809US · Doug DC981 · Emergency Lighting > PIT - THE EMERGENCY LIGHTS AT ROW 25 AND THE AFT TAIL COMPARTMENT LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. (M) - [SDR USAAD98085](https://openairdocs.org/sdr/USAAD98085.md): Power Supply · inoperative · May 13, 1998 · N809US · Doug DC981 · Emergency Lighting > MCO - THE EMERGENCY LIGHTS AT THE AFT OVERWING EXITS AND THE AFT FLIGHT ATTENDENT POSITION WERE INOPERATIVE. MAINTENANCE REPLACED THE AFT OVERWING EXIT LIGHT POWER SUPPLY AND THE AFT FLIGHT ATTENDANT POSITION LIGHT ASSEMBLY. (M) - [SDR 98ZZZM493](https://openairdocs.org/sdr/98ZZZM493.md): Light · inoperative · May 13, 1998 · N809US · Doug DC981 · Emergency Lighting > MCO - THE EMERGENCY LIGHTS AT THE AFT OVERWING EXITS AND THE AFT FLIGHT ATTENDENT POSITION WERE INOPERATIVE. MAINTENANCE REPLACED THE AFT OVERWING EXIT LIGHT POWER SUPPLY AND THE AFT FLIGHT ATTENDANT POSITION LIGHT ASSEMBLY. (M) - [SDR USAAD98037](https://openairdocs.org/sdr/USAAD98037.md): Control Module · failed · Feb 27, 1998 · N809US · Doug DC981 · Emergency Lighting > THE LOW LEVEL EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE LOW LEVEL EMERGENCY LIGHT CONTROL MODULE. (M) - [SDR USAAD97066](https://openairdocs.org/sdr/USAAD97066.md): Gearbox · failed · Apr 2, 1997 · N809US · Doug DC981 · Turbine Engine Accessory Drive > FLT 891 - CLT-RSW - LEFT ENGINE OIL STRAINER CLOGGING LIGHT CAME ON IN FLIGHT. DIVERTED TO TPA. REPLACED LEFT ENGINE GEARBOX ASSEMBLY. (M) - [SDR USAAD96168](https://openairdocs.org/sdr/USAAD96168.md): Bulb · failed · Nov 20, 1996 · N809US · Doug DC981 · Emergency Lighting > ROX - MX CHECK FOUND CEILING EMERGENCY LIGHTS OUT FROM ROWS 10-14. MAINTENANCE RELAMPED LIGHT. OPERATIONAL CHECK GOOD. (M) - [SDR USAAD96105](https://openairdocs.org/sdr/USAAD96105.md): T4 Blades · fractured · Jul 14, 1996 · N809US · Doug DC981 · Turbine Section > SDF/PIT - FLT 2288 - ON DESCENT, HEARD THUMP ON RIGHT FUSELAGE AREA. ON FINAL, AT 1,000 FEET, RIGHT ENGINE WOULD NOT RESPOND TO POWER INPUT. AIRCRAFT LANDED, AND CREW NOTED RIGHT ENGINE EGT WAS CLIMBING, AND SHUT DOWN THE ENGINE. REPLACED ENGINE. FOUND ALL - [SDR USAAD96084](https://openairdocs.org/sdr/USAAD96084.md): Engine · failed · Jun 23, 1996 · N809US · Doug DC981 · Engine (Turbine/Turboprop) > FLT 912 - FLL-CLT - DURING CLIMB, CREW HEARD A LOUD BANG AND NOTICED POWER LOSS FROM RIGHT ENGINE. SHUT DOWN ENGINE. REPLACED RIGHT ENGINE. (M) - [SDR USAAD96078](https://openairdocs.org/sdr/USAAD96078.md): Slide · malfunctioned · Jun 14, 1996 · N809US · Doug DC981 · Escape Slide > CLEANING DEPARTMENT AT SRQ DEPLOYED TAILCONE AND AFT SLIDE. SLIDE UNROLLED, BUT DID NOT INFLATE. REPLACED SLIDE ASSEMBLY. (M) - [SDR USAAD96056](https://openairdocs.org/sdr/USAAD96056.md): Transducer · failed · May 4, 1996 · N809US · Doug DC981 · Brake Anti-Skid Section > FLT NR 1846 - MCO-PIT - 'WHEEL NOT TURNING' LIGHT CAME ON AT 85 KNOTS. REPLACED OUTBOARD RIGHT WHEEL TRANSDUCER. (M) - [SDR USAA960248](https://openairdocs.org/sdr/USAA960248.md): Skin · cracked · Feb 15, 1996 · N809US · Doug DC981 · Fuselage Main, Plate/Skin > PIT - DURING C-1 CHECK INSPECTION, FOUND A 1 INCH CRACK IN STATION 1437 LONGERON 4R FUSELAGE SKIN. INSTALLED DOUBLER REPAIR PER SRM 53-04 FIG 27. (M) - [SDR USAA960247](https://openairdocs.org/sdr/USAA960247.md): Skin · cracked · Feb 15, 1996 · N809US · Doug DC981 · Fuselage Main, Plate/Skin > PIT - DURING C-1 CHECK INSPECTION, FOUND 1 INCH CRACK IN STATION 1437 LONGERON 4L FUSELAGE SKIN. INSTALLED DOUBLER REPAIR PER SRM 53-04 FIG 27. (M) - [SDR USAA960246](https://openairdocs.org/sdr/USAA960246.md): Skin · cracked · Feb 14, 1996 · N809US · Doug DC981 · Fuselage Main, Plate/Skin > PIT - DURING THE C-1 INSPECTION, FOUND TWO CRACKS, 1 INCH AND 2 INCHES AT STATION 1437 LONGERON 4L IN FUSELAGE SKIN. REMOVED CRACK AND INSTALLED FILLER AND DOUBLER SRM 53-04 FIG NR 27. (M) - [SDR USAAD9500C](https://openairdocs.org/sdr/USAAD9500C.md): Audio Select · intermittent · Dec 30, 1995 · N809US · Doug DC981 · Audio Integrating System > PIT - FLT 987 - AFTER TAKEOFF FROM PIT, CREW EXPERIENCED LOSS OF RADIO COMMUNCIATIONS. SHORTLY THEREAFTER, ONE RADIO BEGAN TO WORK. FLIGHT RETURNED TO PIT AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE CAPTAIN'S AUDIO SELECTOR PANEL AND MICRO - [SDR USAA950536](https://openairdocs.org/sdr/USAA950536.md): Pt2 Line · cracked · May 29, 1995 · N809US · Doug DC981 · Fuel Controlling System > MIA - FLT NR 1166 - THE EPR GAUGE FOR THE NR 2 ENGINE FAILED AFTER TAKEOFF. THE FLIGHT DIVERTED TO MIA. REPLACED PT2 LINE AND TIGHTENED PT7 LINE. (M) - [SDR USAA950733](https://openairdocs.org/sdr/USAA950733.md): Membrane · cracked · May 25, 1995 · N809US · Doug DC981 · Fuselage Miscellaneous Structure > PIT - DURING Q-5 CHECK INSPECTION, FOUND 2.50 INCH CRACK STA 1268 - STA 1307, LT SIDE CUSP MEMBRANE. CUT OUT SECTION OF CUSP MEMBRANE AND SPLICED IN REPAIR PER SRM 53-05, FIGURE 97. (X) - [SDR USAA950707](https://openairdocs.org/sdr/USAA950707.md): Pan · cracked · May 25, 1995 · N809US · Doug DC981 · Fuselage Miscellaneous Structure > PIT - DURING Q-5 CHECK INSPECTION, FOUND.50 INCH CRACK IN WINDOW PAN UPPER FWD CORNER AT STA 888 RT. STOP DRILLED CRACK AND INSTALLED DOUBLER REPAIR PER USAIR TYPICAL REPAIR 53-30-06. (X) - [SDR USAA950706](https://openairdocs.org/sdr/USAA950706.md): Pan · cracked · May 25, 1995 · N809US · Doug DC981 · Fuselage Miscellaneous Structure > PIT - DURING Q-5 CHECK INSPECTION, FOUND.50 INCH CRACK IN WINDOW PAN STA 929 UPPER FWD CORNER RT. STOP DRILLED CRACK AND INSTALLED DOUBLER REPAIR PER USAIR TYPICAL REPAIR 53-30-06. (X) - [SDR USAA950705](https://openairdocs.org/sdr/USAA950705.md): Pan · cracked · May 25, 1995 · N809US · Doug DC981 · Fuselage Miscellaneous Structure > PIT - DURING Q-5 CHECK INSPECTION, FOUND.50 INCH CRACK UPPER FORWARD CORNER STA 886, LT WINDOW PAN. STOP DRILLED CRACK AND INSTALLED DOUBLER REPAIR PER USAIR TYPICAL REPAIR 53-30-06. (X) - [SDR USAA950704](https://openairdocs.org/sdr/USAA950704.md): Pan · cracked · May 25, 1995 · N809US · Doug DC981 · Fuselage Miscellaneous Structure > PIT - DURING Q-5 CHECK INSPECTION, FOUND.50 INCH CRACK IN UPPER FWD CORNER OF WINDOW PAN AT STA 946 LT. STOP DRILLED CRACK AND INSTALLED DOUBLER REPAIR PER USAIR TYPICAL REPAIR 52-30-06. (X) - [SDR USAA950703](https://openairdocs.org/sdr/USAA950703.md): Longeron · cracked · May 25, 1995 · N809US · Doug DC981 · Fuselage Main, Longeron/Stringer > PIT - DURING Q-5 CHECK INSPECTION, FOUND.75 INCH CRACKS AT ATTACH POINTS IN LONGERON 17L AT STA 237, 256, 275, 294, 313, 332, 370, AND 427. SPLICED IN NEW SECTION OF LONGERON PER SRM 53-02, FIGURE 2A. (X) - [SDR USAA950702](https://openairdocs.org/sdr/USAA950702.md): Intercostal · misdrilled · May 25, 1995 · N809US · Doug DC981 · Fuselage Miscellaneous Structure > PIT - DURING Q-5 CHECK INSPECTION, FOUND INTERCOSTAL AND DOUBLER MISDRILLED AT STA 886 AND STA 905, LONGERON 16L. FABRICATED AND HEAT TREATED NEW SECTION OF INTERCOSTAL AND INSTALLED DOUBLERS PER SRM 53-01, SRM 51-10-2A. (X) - [SDR USAA950701](https://openairdocs.org/sdr/USAA950701.md): Skin · cracked · May 25, 1995 · N809US · Doug DC981 · Wing, Plate/Skin > PIT - DURING Q-5 CHECK INSPECTION, FOUND.6250 INCH CRACK IN RT WING LEADING EDGE OUTBOARD OF VORTILON. STOP DRILLED CRACK AND INSTALLED DOUBLER AND SUPPORT ANGLE REPAIR PER SRM 57-068, FIGURE 9. (X) - [SDR USAA950700](https://openairdocs.org/sdr/USAA950700.md): Skin · cracked · May 25, 1995 · N809US · Doug DC981 · Fuselage Main, Plate/Skin > PIT - DURING Q-5 CHECK INSPECTION, FOUND 1 INCH CRACK FWD UPPER CORNER OF M.E.D. IN FUSELAGE SKIN (X-RAY). INSTALLED EXTERNAL DOUBLER AND FILLER REPAIR PER SRM 53-05, FIGURE 25A AND USAIR, EA 30427. (X) - [SDR USAA950699](https://openairdocs.org/sdr/USAA950699.md): Skin · cracked · May 25, 1995 · N809US · Doug DC981 · Fuselage Main, Plate/Skin > PIT - DURING Q-5 CHECK INSPECTION, FOUND.3125 INCH CRACK STA 1380 LT SIDE ABOVE LONGERON 14L IN FUSELAGE SKIN. CUT OUT AREA AND INSTALLED FILLER AND DOUBLER PER SRM 53-04 FIG 18. (W) - [SDR USAA950698](https://openairdocs.org/sdr/USAA950698.md): Longeron · chafed · May 25, 1995 · N809US · Doug DC981 · Fuselage Main, Longeron/Stringer > PIT - DURING Q-5 CHECK INSPECTION, FOUND HOLE CHAFED IN LONGERON 8R AT STA 1401 AND 1418. CUT OUT CHAFED SECTION AND INSTALLED NEW SECTION OF LONGERON. SPLICED PER USAIR TYPICAL REPAIR 53-10-17. (W) - [SDR USAA950697](https://openairdocs.org/sdr/USAA950697.md): Blkhd Angle · cracked · May 25, 1995 · N809US · Doug DC981 · Fuselage Main, Bulkhead > PIT - DURING Q-5 CHECK INSPECTION, FOUND.25 INCH CRACK IN ANGLE AT STA 1338 TOP CENTER OF AFT PRESSURE BULKHEAD FWD SIDE. STOP DRILLED CRACK AND INSTALLED REPAIR DOUBLERS PER SRM 53-01 PG 9. (W) - [SDR USAA950696](https://openairdocs.org/sdr/USAA950696.md): Angle · cracked · May 25, 1995 · N809US · Doug DC981 · Fuselage Miscellaneous Structure > PIT - DURING Q-5 CHECK INSPECTION, FOUND 1.5 INCH CRACK AT STA 1463 LT SIDE VERTICAL STAB TO FUSELAGE ATTACH ANGLE. CUT OUT CRACKED SECTION OF ANGLE, INSTALLED FILLER AND REPAIR ANGLES PER SRM 53-05 FIG 23A AND USAIR EA NR 19449. (W) - [SDR USAA950695](https://openairdocs.org/sdr/USAA950695.md): Angle · cracked · May 25, 1995 · N809US · Doug DC981 · Nacelle/Pylon Structure > PIT - DURING Q-5 CHECK INSPECTION, FOUND 1 INCH CRACK IN THE STA 1480 UPPER PYLON ATTACH ANGLE RT SIDE. STOP DRILLED CRACK AND INSTALLED REPAIR DOUBLER TO ANGLE PER SRM 54-04 FIG 10 SHT 3. (W) - [SDR USAA950694](https://openairdocs.org/sdr/USAA950694.md): Skin · cracked · May 25, 1995 · N809US · Doug DC981 · Fuselage Main, Plate/Skin > PIT - DURING Q-5 CHECK INSPECTION, FOUND 1.25 INCH CRACK STA 1437 LT SIDE BELOW LONGERON 3L IN FUSELAGE SKIN. CUT OUT DAMAGED AREA AND INSTALLED FILLER AND EXTERNAL DOUBLER PER SRM 53-04 FIG 27. (W) Next page: https://openairdocs.org/deregistered/N809US-2003-11-18/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 = 'N809US' AND deregistration_id = 'N809US-2003-11-18' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N809US-2003-11-18/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.