# Service difficulty reports: N15841, cancelled Jul 16, 2008 A list on [N15841, cancelled Jul 16, 2008](https://openairdocs.org/deregistered/N15841-2008-07-16.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 · 95 reports - [SDR CALA0400410](https://openairdocs.org/sdr/CALA0400410.md): Web · cracked · Apr 23, 2004 · N15841 · Doug DC982 · Fuselage Miscellaneous Structure > WEB CRACKED AT FWD LWR SIDE OF BAG BIN DOOR AT STA 636, LONG 27 LEFT. REMOVED AND REPLACED WEB PER ECRA 5310-04416. - [SDR CALA0400404](https://openairdocs.org/sdr/CALA0400404.md): Shear Tie · corroded · Apr 20, 2004 · N15841 · Doug DC982 · Fuselage Main, Longeron/Stringer > A/B/B SHEAR TIE CORRODED AT LONGERON 30 AND 28 RIGHT AT STATION 1193. FABRICATED AND INSTALLED SHEAR TIE REPAIR SPLICE BETWEEN LONG 30 AND 29 RIGHT PER SRM 53-03 FIG 3. - [SDR CALA0300053](https://openairdocs.org/sdr/CALA0300053.md): Longeron · cracked · Feb 17, 2003 · N15841 · Doug DC982 · Fuselage Main, Longeron/Stringer > INSPECTION FOUND LONGERON 2L CRACKED AT STA 1418. REPAIRED IAW ECRA 5311-01132. - [SDR CALA0300048](https://openairdocs.org/sdr/CALA0300048.md): Longeron · cracked · Feb 15, 2003 · N15841 · Doug DC982 · Fuselage Main, Longeron/Stringer > INSPECTION FOUND A 2" CRACK IN LONGERON 2R AT STA 1418. A SECTION OF LONGERON WAS SPLICED IN IAW ECRA 5311-01132. - [SDR CALA0001412](https://openairdocs.org/sdr/CALA0001412.md): Skin · cracked · Sep 12, 2000 · N15841 · Doug DC982 · Wing, Plate/Skin > INSPECTION FOUND LT WING LEADING EDGE SKIN CRACKED AT APPROXIMATELY STA XIS 60. REPAIR DOUBLERS, SHIMS, ANGLES, AND NUT PLATE STRIPS WERE INSTALLED IAW EA 9-5721-2-AD760 AND ECRA 5721-01057. - [SDR CALA0001411](https://openairdocs.org/sdr/CALA0001411.md): Frame · corroded · Sep 12, 2000 · N15841 · Doug DC982 · Fuselage Main, Frame > INSPECTION FOUND AFT CARGO FRAME AFT SIDE CORRODED UNDER PAINT AT FS 1309, L24R-24L. THE CORRODED SECTION WAS CUT OUT AND A FRAME REPAIR SPLICE WAS INSTALLED IAW SRM 53-03, FIGURE 2A. - [SDR CALA0001410](https://openairdocs.org/sdr/CALA0001410.md): Cargo Track · corroded · Sep 11, 2000 · N15841 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings > INSPECTION FOUND MID CARGO RT CARGO TIE DOWN TRACK CORRODED AT FS 532 - 625 AND FS 693 - 807. THE TIE DOWN TRACK SECTIONS WERE REMOVED AND NEW TRACK SECTIONS WERE INSTALLED IAW SRM 53-05, FIGURE 4. - [SDR CALA0001409](https://openairdocs.org/sdr/CALA0001409.md): Skin · cracked · Sep 11, 2000 · N15841 · Doug DC982 · Wing, Plate/Skin > AN INTERIM REPAIR WAS REMOVED AND A PERMANENT REPAIR WAS INSTALLED WHERE A 1 INCH CRACK EXISTED ON L/E LOWER SURFACE OF LT WING SKIN AT NR 2 SLAT CENTER TRACK CUTOUT, XFS 206. THE INTERIM REPAIR WAS REMOVED IAW SRM 51-10-4. EXTERNAL AND INTERNAL DOUBLERS AND - [SDR CALA0001408](https://openairdocs.org/sdr/CALA0001408.md): Fairing · cracked · Sep 11, 2000 · N15841 · Doug DC982 · Wing Miscellaneous Structure > INSPECTION FOUND A 1 INCH CRACK IN RT WING FLAP HINGE FAIRING NR 3 AFT. THE CRACK WAS STOP DRILLED AND A DOUBLER REPAIR WAS INSTALLED IAW SRM 57-01, FIGURE 3, SHEET 2, 51-10-4, AND 51-10-3. - [SDR CALA0001403](https://openairdocs.org/sdr/CALA0001403.md): Floor Support · corroded · Sep 8, 2000 · N15841 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND MID CARGO RT TRACK FLOOR SUPPORT CORRODED AT FS 598 - 636. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-01, 51-10-04, 51-30-02, AND 51-30-01. - [SDR CALA0001402](https://openairdocs.org/sdr/CALA0001402.md): Seat Track · corroded · Sep 7, 2000 · N15841 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings > INSPECTION FOUND LEFT I/B CABIN SEAT TRACK CORRODED AT FS 1117 - 1309. THE CORROSION WAS REMOVED IAW SRM 53-05, FIGURE 4. CORROSION REMOVAL WAS WITHIN LIMITS FROM FS 1212 - 1309. THE SEAT TRACK SECTION FROM FS 1117 - 1212 WAS REPLACED IAW SRM 51-30-1, 53-05 - [SDR CALA0001400](https://openairdocs.org/sdr/CALA0001400.md): Skin · dented · Sep 5, 2000 · N15841 · Doug DC982 · Trailing Edge Flaps > INSPECTION FOUND NR 2 LEFT T/E FLAP DENTED ON LOWER SIDE. THE DENTED AREA WAS TRIMMED OUT AND A REPAIR DOUBLER WAS INSTALLED IAW SRM 57-01, FIGURE 5 AND FIGURE 3. - [SDR CALA0001399](https://openairdocs.org/sdr/CALA0001399.md): Angle · cracked · Sep 5, 2000 · N15841 · Doug DC982 · Vertical Stabilizer > INSPECTION FOUND FOUR VERTICAL STABILIZER DOGHOUSE ANGLES CRACKED. LOCATIONS WERE RT AND LT FWD LOWER AND RT AND LT AFT LOWER AREA. THE CRACKS WERE.5 INCH LONG. THE ANGLES WERE REPAIRED IAW SRM 55-01, FIGURE 2, 55-10-4, 51-10-3, AND 51-30-2. - [SDR CALA0001398](https://openairdocs.org/sdr/CALA0001398.md): Door Frame · corroded · Sep 5, 2000 · N15841 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND AFT CARGO DOOR CUTOUT LOWER JAMB CORRODED. A DOUBLER AND STRAP WERE INSTALLED IAW SRM 51-10-4 AND ECRA 5310-03027. - [SDR CALA0001397](https://openairdocs.org/sdr/CALA0001397.md): Doubler · corroded · Sep 5, 2000 · N15841 · Doug DC982 · Fuselage Main, Plate/Skin > INSPECTION FOUND ANTENNA DOUBLER CORRODED ON MOUNTING FLANGE AT FS 700, LONGERON 30. THE ANTENNA DOUBLER WAS REMOVED AND A NEW DOUBLER WAS INSTALLED IAW SRM 51-30-2 AND 51-30-5. - [SDR CALA0001389](https://openairdocs.org/sdr/CALA0001389.md): Pan · cracked · Sep 3, 2000 · N15841 · Doug DC982 · Cargo/Baggage Doors > INSPECTION FOUND A 1.9 INCH CRACK AT CAM LATCH OF FWD CARGO DOOR FWD EDGE OF INNER PAN. THE CRACKED SECTION WAS REMOVED IAW EA 9-5231-2-A0749. A REPAIR ANGLE AND FILLER WERE INSTALLED IAW SRM 52-05, FIGURE 26A, 51-10-3, 51-30-2, AND 51-30-5. - [SDR CALA0001388](https://openairdocs.org/sdr/CALA0001388.md): Angle · corroded · Sep 3, 2000 · N15841 · Doug DC982 · Cargo/Baggage Doors > INSPECTION FOUND UPPER AND LOWER SURFACE OF DOOR Z-ANGLE CORRODED AT RT SIDE OF AFT PIT. THE Z-ANGLE WAS REMOVED AND A NEW Z-ANGLE WAS INSTALLED IAW SRM 51-30-1, 51-10-3, AND 51-30-2. - [SDR CALA0001387](https://openairdocs.org/sdr/CALA0001387.md): Bracket · corroded · Sep 3, 2000 · N15841 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND L-2 DOOR THRESHOLD SUPPORT BRACKETS CORRODED. THE BRACKETS WERE REMOVED AND NEW BRACKETS WERE INSTALLED IAW SRM 51-30-5. - [SDR CALA0001386](https://openairdocs.org/sdr/CALA0001386.md): Cargo Track · corroded · Sep 3, 2000 · N15841 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings > INSPECTION FOUND RT TIEDOWN TRACK CORRODED FROM STA 1211 - 1309 AND LT TIEDOWN TRACK CORRODED FROM STA 1007 - 1309 IN AFT PIT. THE TRACKS WERE REMOVED AND NEW TRACKS WERE INSTALLED IAW SRM 53-05, FIGURE 5, 51-10-3, 51-10-4, AND 51-30-5. - [SDR CALA0001385](https://openairdocs.org/sdr/CALA0001385.md): Seat Track · corroded · Sep 3, 2000 · N15841 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings > INSPECTION FOUND LEFT I/B SEAT TRACK CORRODED AT FS 936 - 1212. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED IAW SRM 51-30-1 AND 53-05, FIGURE 1. - [SDR CALA0001383](https://openairdocs.org/sdr/CALA0001383.md): Fairing · cracked · Sep 3, 2000 · N15841 · Doug DC982 · Horizontal Stabilizer Structure > INSPECTION FOUND A 1 INCH CRACK IN RT UPPER HORIZONTAL STABILIZER BANANA FAIRING ON FORWARD END. A REPAIR DOUBLER WAS INSTALLED IAW SRM 55-01, FIGURE 2, 55-10-0, FIGURE 7, AND 51-30-02. - [SDR CALA0001382](https://openairdocs.org/sdr/CALA0001382.md): Frame · cracked · Sep 3, 2000 · N15841 · Doug DC982 · Landing Gear Doors > INSPECTION FOUND A 3 INCH CRACK IN LT MLG WHEEL WELL DOOR FRAME AT O/B FORWARD CORNER. THE FRAME WAS REMOVED AND REPLACED IAW SRM 51-30-2, 51-30-1, AND 51-30-8. - [SDR CALA0001381](https://openairdocs.org/sdr/CALA0001381.md): Cargo Track · corroded · Sep 3, 2000 · N15841 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings > INSPECTION FOUND LT CARGO TIE DOWN TRACK CORRODED IN MID CARGO COMPARTMENT AT FS 522. THE TIE DOWN TRACK WAS REMOVED AND A REPLACEMENT TRACK WAS INSTALLED IAW SRM 53-05, FIGURE 4G. - [SDR CALA0001380](https://openairdocs.org/sdr/CALA0001380.md): Seat Track · corroded · Sep 3, 2000 · N15841 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings > INSPECTION FOUND LT CENTER SEAT TRACK CORRODED AT STA 1126 - 1240. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-1, 51-30-2, AND 53-05, FIGURE 4. - [SDR CALA0001379](https://openairdocs.org/sdr/CALA0001379.md): Skin · dented · Sep 3, 2000 · N15841 · Doug DC982 · Fuselage Main, Plate/Skin > INSPECTION FOUND LOWER FUSELAGE SKIN DENTED AT STA 294, LONGERON 22L. THE SKIN WAS REPAIRED IAW SRM 53-04, FIGURE 38G. - [SDR CALA0001378](https://openairdocs.org/sdr/CALA0001378.md): Structure · corroded · Sep 3, 2000 · N15841 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND CABIN AREA SUPPORT CORRODED AT STA 200, LBL 10. THE SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-30-2, 53-14-1, 51-10-4, 51-10-3, AND 51-30-5. - [SDR CALA0001377](https://openairdocs.org/sdr/CALA0001377.md): Doubler · gouged · Sep 3, 2000 · N15841 · Doug DC982 · Cargo/Baggage Doors > INSPECTION FOUND FORWARD CARGO DOOR FORWARD LOWER OUTER SKIN DOUBLER LOWER EDGE GOUGED. THE DOUBLER WAS REMOVED AND A NEW DOUBLER WAS INSTALLED IAW SRM 51-30-2. - [SDR CALA0001376](https://openairdocs.org/sdr/CALA0001376.md): Web · bent · Sep 3, 2000 · N15841 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND CABIN SUBFLOOR LIGHTENING HOLE DOUBLER BENT AND TORN AT STA 160, LBL 12. THE DOUBLER WAS REMOVED AND A NEW DOUBLER WAS INSTALLED IAW SRM 51-30-2, 51-10-4, AND 51-10-3. - [SDR CALA0001375](https://openairdocs.org/sdr/CALA0001375.md): Structure · cracked · Sep 3, 2000 · N15841 · Doug DC982 · Wing Miscellaneous Structure > INSPECTION FOUND A 1 INCH CRACK IN RT WING LEADING EDGE I/B SUPPORT. THE SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-30-2, 51-10-4, AND 51-10-3. - [SDR CALA0001373](https://openairdocs.org/sdr/CALA0001373.md): Floor Panel · corroded · Sep 3, 2000 · N15841 · Doug DC982 · Fuselage Floor Panel > INSPECTION FOUND COCKPIT RT METAL FLOOR PANEL CORRODED AND DENTED. THE FLOOR PANEL WAS REMOVED AND REPLACED IAW SRM 51-30-1 AND 53-24-0. - [SDR CALA0001367](https://openairdocs.org/sdr/CALA0001367.md): Floor Support · corroded · Sep 2, 2000 · N15841 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 160, BL 0. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW 51-30-02, 51-10-04, AND 51-30-05. - [SDR CALA0001366](https://openairdocs.org/sdr/CALA0001366.md): Floor Support · corroded · Sep 2, 2000 · N15841 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND CABIN FLOOR SUPPORTS CORRODED AT STA 160, RBL 45 AND AT STA 200, RBL 51. THE FLOOR SUPPORTS WERE REMOVED AND NEW SUPPORTS WERE INSTALLED IAW SRM 51-30-05, 51-10-04, 51-10-2, AND 51-30-1. - [SDR CALA0001365](https://openairdocs.org/sdr/CALA0001365.md): Bracket · cracked · Sep 2, 2000 · N15841 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND A 1 INCH CRACK IN TWO AFT CARGO PIT L BRACKETS AT FORWARD AND AFT END OF OVERHEAD CARGO DOOR LATCH SUPPORT. THE BRACKETS WERE REMOVED AND REPLACED IAW SRM 51-10-2, 51-10-3, AND 51-30-2. - [SDR CALA0001364](https://openairdocs.org/sdr/CALA0001364.md): Bracket · cracked · Sep 2, 2000 · N15841 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND TWO L BRACKETS CRACKED IN FORWARD CARGO PIT AT FORWARD AND AFT END OF CARGO DOOR LATCH SUPPORT. THE CRACKS WERE.25 INCH LONG. THE BRACKETS WERE REMOVED AND NEW BRACKETS WERE INSTALLED IAW SRM 51-30-2 AND 51-10-4. - [SDR CALA0001363](https://openairdocs.org/sdr/CALA0001363.md): Panel · cracked · Sep 2, 2000 · N15841 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND A 1 INCH CRACK IN AFT CARGO CENTER FLOOR TRANSITION PANEL AT STA 1212 - 1231. THE CRACKED AREA WAS TRIMMED OUT IAW SRM 53-01, FIGURE 4, SHEET 3. DOUBLER AND FILLER WERE INSTALLED IAW SRM 53-01, 51-10-4, 51-10-3, AND 51-30-2. - [SDR CALA0001361](https://openairdocs.org/sdr/CALA0001361.md): Floor Support · corroded · Sep 2, 2000 · N15841 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND CABIN AREA FLOOR SUPPORTS CORRODED AT STA 200, BL 0 AND AT STA 140 - 200, RBL 7. THE FLOOR SUPPORTS WERE REMOVED AND NEW SUPPORTS WERE INSTALLED IAW SRM 51-30-02, 51-10-03, 51-10-04, AND 51-30-1. - [SDR CALA0001360](https://openairdocs.org/sdr/CALA0001360.md): Angle · cracked · Sep 2, 2000 · N15841 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND A 1 INCH CRACK IN LT MLG FORWARD KEELBEAM ANGLE. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-10-4, 51-10-03, 51-30-05, AND 51-30-01. - [SDR CALA0001359](https://openairdocs.org/sdr/CALA0001359.md): Skin · dented · Sep 2, 2000 · N15841 · Doug DC982 · Passenger/Crew Doors > INSPECTION FOUND L-1 DOOR UPPER AFT I/B EDGE DENTED. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 38. - [SDR CALA0001354](https://openairdocs.org/sdr/CALA0001354.md): Skin · dented · Aug 31, 2000 · N15841 · Doug DC982 · Fuselage Main, Plate/Skin > INSPECTION FOUND LOWER FUSELAGE SKIN DENTED AT STA 294, LONGERON 21L. THE SKIN WAS REPAIRED IAW SRM 53-04, FIGURE 38, VIEW G. - [SDR CALA0001353](https://openairdocs.org/sdr/CALA0001353.md): Seat Track · corroded · Aug 31, 2000 · N15841 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings > INSPECTION FOUND LEFT O/B SEAT TRACK AFT OF L-2 DOOR CORRODED AT FS 1174. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED IAW SRM 51-30-1, 51-10-4, AND 51-10-3. - [SDR CALA0001352](https://openairdocs.org/sdr/CALA0001352.md): Floor Support · cracked · Aug 31, 2000 · N15841 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND A 1 INCH CRACK IN LOWER FLOOR PANEL SUPPORT IN FORWARD CARGO AREA AT FS 522. THE FLOOR PANEL SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-30-02 AND 51-10-03. - [SDR CALA0001351](https://openairdocs.org/sdr/CALA0001351.md): Web · corroded · Aug 31, 2000 · N15841 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND LOWER SURFACE OF CABIN SUBFLOOR CORRODED AT FS 200 BETWEEN BL 0 AND RT SIDE OF AIRCRAFT. THE SUBFLOOR WAS REMOVED AND REPLACED IAW SRM 53-14-01, FIGURE 11, 51-10-3, AND ECRA 5100-01844. - [SDR CALA0001348](https://openairdocs.org/sdr/CALA0001348.md): Skin · dented · Aug 29, 2000 · N15841 · Doug DC982 · Fuselage Main, Plate/Skin > INSPECTION FOUND LOWER FUSELAGE SKIN DENTED AT FS 465, LONGERON 23R - 24R. THE SKIN WAS REPAIRED IAW SRM 53-04, FIGURE 38, VIEW G. - [SDR CALA0001347](https://openairdocs.org/sdr/CALA0001347.md): Floor Support · corroded · Aug 29, 2000 · N15841 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND CABIN FLOOR SUPPORT CORRODED AT FS 168, RBL 28. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-30-2. - [SDR CALA0001346](https://openairdocs.org/sdr/CALA0001346.md): Floor Support · corroded · Aug 29, 2000 · N15841 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND CABIN FLOOR SUPPORT CORRODED AT FS 200, RBL 29. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-2, 53-14-1, AND 51-10-4. - [SDR CALA0001345](https://openairdocs.org/sdr/CALA0001345.md): Skin · dented · Aug 29, 2000 · N15841 · Doug DC982 · Cargo/Baggage Doors > INSPECTION FOUND AFT CARGO DOOR EXTERIOR SKIN DENTED. REPAIRED SKIN IAW SRM 52-05, FIGURE 1 AND 51-10-3. - [SDR CALA0001344](https://openairdocs.org/sdr/CALA0001344.md): Fitting · corroded · Aug 29, 2000 · N15841 · Doug DC982 · Entrance Stairs > INSPECTION FOUND FORWARD AIRSTAIRS DOOR MOUNT BASE FITTING CORRODED AT STA 180. THE FITTING WAS REMOVED AND A NEW FITTING WAS INSTALLED IAW SRM 51-10-4, 51-10-3, AND 51-30-1. - [SDR CALA0001340](https://openairdocs.org/sdr/CALA0001340.md): Web · cracked · Aug 28, 2000 · N15841 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND TWO 1 INCH CRACKS IN RT CUSP WEB AT FS 218 - 237. THE CUSP WEB WAS REMOVED AND A NEW PART WAS INSTALLED IAW SRM 51-10-4, 51-10-3, AND 51-30-2. - [SDR CALA0001339](https://openairdocs.org/sdr/CALA0001339.md): Floor Support · corroded · Aug 28, 2000 · N15841 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND CABIN FLOOR SUPPORT CORRODED AT STA 160, LBL 52. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-5, 51-10-4, AND 51-30-2. - [SDR CALA0001338](https://openairdocs.org/sdr/CALA0001338.md): Cover · corroded · Aug 28, 2000 · N15841 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND CABIN FLOOR SUPPORT COVER PLATE CORRODED AT FS 160 - 200, RBL 54. THE COVER PLATE WAS REMOVED AND A NEW COVER PLATE WAS INSTALLED IAW SRM 51-30-1. Next page: https://openairdocs.org/deregistered/N15841-2008-07-16/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 = 'N15841' AND deregistration_id = 'N15841-2008-07-16' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N15841-2008-07-16/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.