# Service difficulty reports: N10834, cancelled Jun 1, 2007 A list on [N10834, cancelled Jun 1, 2007](https://openairdocs.org/deregistered/N10834-2007-06-01.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 · 66 reports - [SDR CALA0200495](https://openairdocs.org/sdr/CALA0200495.md): Longeron · cracked · Oct 12, 2002 · N10834 · Doug DC982 · Fuselage Main, Longeron/Stringer > INSPECTION FOUND A 1" CRACK IN TAIL COMPARTMENT LONGERON 2R AT STA 1418. REPAIRED LONGERON IAW SRM 53-02, FIGURE 18. - [SDR CALA0200494](https://openairdocs.org/sdr/CALA0200494.md): Frame · cracked · Oct 12, 2002 · N10834 · Doug DC982 · Fuselage Main, Frame > INSPECTION FOUND A 2" CRACK IN TAIL COMPARTMENT BELTFRAME AT STA 1418, L2R. REPAIRED FRAME IAW SRM 53-03, FIGURE 31A. - [SDR CALA0200490](https://openairdocs.org/sdr/CALA0200490.md): Skin · dented · Oct 9, 2002 · N10834 · Doug DC982 · Fuselage Main, Plate/Skin > INSPECTION FOUND A DENT IN L/H FUSELAGE SKIN AFT OF FORWARD ENTRY DOOR. THE DENTED SKIN WAS REMOVED AND NEW SKIN WAS INSTALLED IAW SRM 53-04. - [SDR CALA0000957](https://openairdocs.org/sdr/CALA0000957.md): Pan · gouged · Jun 21, 2000 · N10834 · Doug DC982 · Cargo/Baggage Doors > INSPECTION FOUND FORWARD CARGO DOOR TOP PAN FLANGE GOUGED AT STOP. THE GOUGED AREA WAS REMOVED AND A DOUBLER WAS INSTALLED IAW 51-10-02, 51-30-02, 51-10-03, AND ECRA 5330-02819. - [SDR CALA0000953](https://openairdocs.org/sdr/CALA0000953.md): Retainer · cracked · Jun 21, 2000 · N10834 · Doug DC982 · Engine Mount Section > INSPECTION FOUND NR 1 ENGINE APRON FORWARD UPPER SUPPORT (RETAINER) BENT WITH A SIX INCH CRACK. THE RETAINER WAS REMOVED AND REPLACED IAW SRM 51-30-2. - [SDR CALA0000952](https://openairdocs.org/sdr/CALA0000952.md): Stringer · cracked · Jun 21, 2000 · N10834 · Doug DC982 · Horizontal Stabilizer, Spar/Rib > INSPECTION FOUND A 2 INCH CRACK IN HORIZONTAL STABILIZER DOG HOUSE STRINGER. THE CRACKED AREA WAS REMOVED AND A NEW STRINGER WAS INSTALLED IAW SRM 51-30-2, 53-01, AND 55-01, FIGURE 2. - [SDR CALA0000949](https://openairdocs.org/sdr/CALA0000949.md): Seat Track · corroded · Jun 20, 2000 · N10834 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings > INSPECTION FOUND LEFT O/B SEAT TRACK CORRODED AT FS 1174 - 1207, LBL 54. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED IAW SRM 51-30-1, 53-05, FIGURE 4, AND 51-10-4. - [SDR CALA0000948](https://openairdocs.org/sdr/CALA0000948.md): Floor Support · corroded · Jun 20, 2000 · N10834 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 180, LBL 16 - 36. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-30-5. - [SDR CALA0000947](https://openairdocs.org/sdr/CALA0000947.md): Floor Support · corroded · Jun 20, 2000 · N10834 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND FLOOR SUPPORT CORRODED AT FS 180 - 208, LONGERON 18L. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-10-2, 51-10-4, AND 51-30-2. - [SDR CALA0000946](https://openairdocs.org/sdr/CALA0000946.md): Attach Angle · cracked · Jun 20, 2000 · N10834 · Doug DC982 · Passenger/Crew Doors > INSPECTION FOUND A 1 INCH CRACK IN L-1 DOOR UPPER AFT INNER ATTACH ANGLE. THE ATTACH ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-2. - [SDR CALA0000945](https://openairdocs.org/sdr/CALA0000945.md): Panel · corroded · Jun 20, 2000 · N10834 · Doug DC982 · Wing, Plate/Skin > INSPECTION FOUND LT LOWER FUEL PANEL NR 1363 CORRODED ON MOUNT FACE AND IN COUNTERSINK. THE PANEL WAS REMOVED AND A NEW PANEL WAS INSTALLED IAW MM 51-30-2. - [SDR CALA0000944](https://openairdocs.org/sdr/CALA0000944.md): Skin · cracked · Jun 20, 2000 · N10834 · Doug DC982 · Cargo/Baggage Doors > INSPECTION FOUND TWO 3 INCH CRACKS IN MID CARGO DOOR I/B SKIN. THE CRACKED AREA WAS REMOVED AND A DOUBLER REPAIR WAS INSTALLED IAW SRM 53-01, FIGURE 1 AND 51-10-4. - [SDR CALA0000942](https://openairdocs.org/sdr/CALA0000942.md): Nut Plate · corroded · Jun 20, 2000 · N10834 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND CORROSION AROUND AND UNDER NUT PLATES INSIDE AFT CARGO LOWER TORQUE BOX AT FS 1183, LONGERON 27R AND 28R. THE TORQUE BOX WAS REPAIRED IAW ECRA 5310-04023. - [SDR CALA0000929](https://openairdocs.org/sdr/CALA0000929.md): Shear Tie · corroded · Jun 20, 2000 · N10834 · Doug DC982 · Fuselage Main, Structure > INSPECTION FOUND SHEAR TIE CORRODED AT STA 1287, LONGERON 30 TO 29R. THE SHEAR TIE WAS REMOVED AND REPLACED IAW SRM 51-30-2. - [SDR CALA0000928](https://openairdocs.org/sdr/CALA0000928.md): Frame · corroded · Jun 20, 2000 · N10834 · Doug DC982 · Fuselage Main, Frame > INSPECTION FOUND AFT SIDE OF FRAME CORRODED AT STA 1309, LONGERON 30. THE CORRODED SECTION OF FRAME WAS REMOVED AND REPLACED IAW SRM 53-03, FIGURE 2A, SHEET 1, PAGE 4A. - [SDR CALA0000927](https://openairdocs.org/sdr/CALA0000927.md): Structure · cracked · Jun 20, 2000 · N10834 · Doug DC982 · Landing Gear Doors > INSPECTION FOUND A.5 INCH CRACK IN RT MLG I/B DOOR AFT LOWER CORNER AT REPAIR DOUBLER. REMOVED AND REPLACED DOUBLER IAW SRM 51-30-1. - [SDR CALA0000920](https://openairdocs.org/sdr/CALA0000920.md): Structure · bent · Jun 19, 2000 · N10834 · Doug DC982 · Cargo/Baggage Doors > INSPECTION FOUND THE AFT LOWER CORNER OF AFT CARGO DOOR BENT. REPAIRED AREA IAW ECRA 5230-01557. - [SDR CALA0000919](https://openairdocs.org/sdr/CALA0000919.md): Stop · gouged · Jun 19, 2000 · N10834 · Doug DC982 · Cargo/Baggage Doors > INSPECTION FOUND FORWARD CARGO DOOR FORWARD SEAL FLANGE DOOR STOPS A-E GOUGED. REPAIRED AREAS IAW ECRA 5330-02819. - [SDR CALA0000918](https://openairdocs.org/sdr/CALA0000918.md): Cargo Track · corroded · Jun 19, 2000 · N10834 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings > INSPECTION FOUND LT CARGO TIE DOWN TRACK IN AFT PIT CORRODED AROUND CLIP NUT HOLES AT FS 1155 - 1320, LONGERON 27L. THE TIE DOWN TRACK WAS REMOVED AND REPLACED IAW SRM 51-10-4. - [SDR CALA0000917](https://openairdocs.org/sdr/CALA0000917.md): Pan · gouged · Jun 19, 2000 · N10834 · Doug DC982 · Cargo/Baggage Doors > INSPECTION FOUND AFT CARGO DOOR PAN GOUGED AT STOP NR 5 ON FORWARD EDGE AND AT STOP NR 4 ON AFT EDGE. BOTH AREAS WERE REPAIRED IAW ECRA 5330-02819. - [SDR CALA0000916](https://openairdocs.org/sdr/CALA0000916.md): Support Bracket · cracked · Jun 19, 2000 · N10834 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND A.5 INCH CRACK IN SUPPORT AT TAIL COMPARTMENT RT SIDE IN CEILING JUST AFT OF FRAME STA 1380. THE CRACK WAS STOP DRILLED AND A STACKED ANGLE REPAIR WAS INSTALLED IAW SRM 51-30-2 AND 53-01. - [SDR CALA0000911](https://openairdocs.org/sdr/CALA0000911.md): Skin · dented · Jun 16, 2000 · N10834 · Doug DC982 · Cargo/Baggage Doors > INSPECTION FOUND AFT CARGO DOOR OUTER SKIN DENTED JUST ABOVE AFT ACCESS PANEL. THE DENTED AREA WAS CUT OUT IAW SRM 52-05, FIGURE 1 AND A REPAIR DOUBLER WAS INSTALLED IAW SRM 52-05, FIGURE 1 AND 51-30-2. - [SDR CALA0000906](https://openairdocs.org/sdr/CALA0000906.md): Channel · cracked · Jun 15, 2000 · N10834 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND SUPPORT CHANNELS CRACKED AT CENTER FLOOR PANEL BETWEEN FS 886 AND 946. THE CRACKS WERE 2 INCHES LONG. THE FLOOR PANEL WAS REMOVED IAW SRM 51-30-1. THE SUPPORT CHANNELS WERE REMOVED AND NEW CHANNELS WERE INSTALLED IAW 51-10-4 AND 51-30-0. T - [SDR CALA0000905](https://openairdocs.org/sdr/CALA0000905.md): Cargo Track · corroded · Jun 15, 2000 · N10834 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings > INSPECTION FOUND MID CARGO RT TRACK AFT OF DOOR CORRODED UNDER NUT CLIPS AT FS 683 - 786, LONGERON 27R. THE TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 51-10-4, 51-30-1, AND 51-30-2. - [SDR CALA0000904](https://openairdocs.org/sdr/CALA0000904.md): Rib · cracked · Jun 15, 2000 · N10834 · Doug DC982 · Wing, Rib/Bulkhead > INSPECTION FOUND A 6 INCH CRACK IN RT WING L/E RIB AT TRACK NR 8, XRS 248. THE CRACK WAS STOP DRILLED IAW SRM 57-01, FIGURE 3. A REPAIR ANGLE WAS INSTALLED IAW SRM 57-10, FIGURE 3 AND 51-30-2. - [SDR CALA0000902](https://openairdocs.org/sdr/CALA0000902.md): Skin · dented · Jun 15, 2000 · N10834 · Doug DC982 · Fuselage Main, Plate/Skin > INSPECTION FOUND EXTERNAL FUSELAGE SKIN DENTED AT STA 389, LONGERON 24L. THE SKIN WAS REPAIRED IAW SRM 53-04, SHEETS 12 & 20. - [SDR CALA0000901](https://openairdocs.org/sdr/CALA0000901.md): Skin · canning · Jun 14, 2000 · N10834 · Doug DC982 · Fuselage Main, Plate/Skin > INSPECTION FOUND RIGHT FUSELAGE SKIN OIL CANNING AT STA 484, LONGERON 23R-24R. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 38. - [SDR CALA0000900](https://openairdocs.org/sdr/CALA0000900.md): Support Bracket · cracked · Jun 14, 2000 · N10834 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND A.5 INCH CRACK IN EXTERNAL FUSELAGE LOWER SURFACE WING TO BODY FAIRING SUPPORT TEE AT FS 916. THE SUPPORT WAS REMOVED AND A REPLACEMENT SUPPORT ANGLE WAS INSTALLED IAW SRM 51-30-5. - [SDR CALA0000897](https://openairdocs.org/sdr/CALA0000897.md): Vane · cracked · Jun 13, 2000 · N10834 · Doug DC982 · Wing, Plate/Skin > INSPECTION FOUND A.25 INCH CRACK IN NR 2 RT FIXED VANE I/B LOWER SURFACE. REPAIRED AND BONDED DOUBLER WITH RIVETS IAW SRM 57-04 AND 51-71-00. - [SDR CALA0000896](https://openairdocs.org/sdr/CALA0000896.md): Pan · gouged · Jun 13, 2000 · N10834 · Doug DC982 · Cargo/Baggage Doors > INSPECTION FOUND FORWARD CARGO DOOR FORWARD PAN FLANGE STOPS H-L GOUGED. THE GOUGED AREAS WERE TRIMMED OUT AND REPAIR DOUBLERS WERE INSTALLED IAW ECRA 5330-02819, SRM 51-10-3, 51-10-4, AND 51-30-2. - [SDR CALA0000873](https://openairdocs.org/sdr/CALA0000873.md): Skin · dented · Jun 13, 2000 · N10834 · Doug DC982 · Fuselage Main, Plate/Skin > INSPECTION FOUND EXTERNAL FUSELAGE SKIN DENTED WITH A.5 INCH CRACK AT FS 315 BETWEEN LONGERON 22L AND 23L. THE DENT WAS BLENDED OUT IAW SRM 53-04, FIGURE 38. THE CRACK WAS CUT OUT AND A FINGER DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 38, 51-10-3, AND 51- - [SDR CALA0000865](https://openairdocs.org/sdr/CALA0000865.md): Skin · corroded · Jun 10, 2000 · N10834 · Doug DC982 · Fuselage Main, Plate/Skin > INSPECTION FOUND LT AFT UPPER FUSELAGE SKIN CORRODED AROUND FASTENERS JUST BELOW DORSAL FIN AT STA 1429 - 1435. A REPAIR STRAP WAS INSTALLED IAW SRM 53-05, 51-10-3, AND 51-30-5. - [SDR CALA0000864](https://openairdocs.org/sdr/CALA0000864.md): Cargo Track · corroded · Jun 10, 2000 · N10834 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings > INSPECTION FOUND MID CARGO TIE DOWN TRACK CORRODED AT FS 595 - 785, LONGERON 27L. THE TIE DOWN TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 51-30-1, 51-10-4, AND 51-10-3. - [SDR CALA0000863](https://openairdocs.org/sdr/CALA0000863.md): Seat Track · corroded · Jun 10, 2000 · N10834 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings > INSPECTION FOUND SEAT TRACK CORRODED AT FS 1032 - 1309, RBL 24. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED IAW SRM 51-30-2, 53-05, AND 51-10-3. - [SDR CALA0000850](https://openairdocs.org/sdr/CALA0000850.md): Seat Track · corroded · Jun 8, 2000 · N10834 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings > INSPECTION FOUND SEAT TRACK CORRODED AT FS 670, RBL 22.5. THE SEAT TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 51-30-2, 53-05, FIGURE 4F, AND 51-10-3. - [SDR CALA0000849](https://openairdocs.org/sdr/CALA0000849.md): Pan · cracked · Jun 8, 2000 · N10834 · Doug DC982 · Cargo/Baggage Doors > INSPECTION FOUND A 2 INCH CRACK IN AFT CARGO DOOR PAN AT FORWARD DOOR CAM AREA. THE OLD DOUBLER WAS REMOVED AND A NEW DOOR PAN DOUBLER WAS INSTALLED IAW SRM 51-30-2, 52-05, FIGURE 26A, 51-10-4, 51-10-3. - [SDR CALA0000848](https://openairdocs.org/sdr/CALA0000848.md): Seat Track · corroded · Jun 8, 2000 · N10834 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings > INSPECTION FOUND RIGHT O/B SEAT TRACK CORRODED AT FS 218 - 238. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED IAW SRM 53-05, FIGURE 4, 51-10-3, 51-10-4, 51-30-1, 51-30-5, AND 51-30-6. - [SDR CALA0000847](https://openairdocs.org/sdr/CALA0000847.md): Seat Track · corroded · Jun 8, 2000 · N10834 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings > INSPECTION FOUND LT CENTER SEAT TRACK CORRODED AT FS 1088 - 1231. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED IAW SRM 51-30-1, 51-30-2, 51-30-5, AND 53-05, FIGURE 4. - [SDR CALA0000842](https://openairdocs.org/sdr/CALA0000842.md): Web · punctured · Jun 7, 2000 · N10834 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND HOLE PUNCTURED IN RT CUSP WEB UNDER FLOOR SUPPORT AT FS 200, RBL 44. THE FLOOR SUPPORT WAS REMOVED IAW SRM 51-30-2. A DOUBLER AND FILLER WERE INSTALLED IAW SRM 53-01, FIGURE 2 AND 51-30-2. THE FLOOR SUPPORT WAS REINSTALLED IAW SRM 51-30-1. - [SDR CALA0000841](https://openairdocs.org/sdr/CALA0000841.md): Seat Track · corroded · Jun 7, 2000 · N10834 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings > INSPECTION FOUND LEFT O/B SEAT TRACK CORRODED AT FS 1174 - 1207, LBL 54. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED IAW SRM 51-30-1, 53-05, FIGURE 4, AND 51-10-4. - [SDR CALA0000840](https://openairdocs.org/sdr/CALA0000840.md): Seat Track · corroded · Jun 7, 2000 · N10834 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings > INSPECTION FOUND SEAT TRACK LUGS CORRODED AT FS 378, RBL 22.5. THE SEAT TRACK WAS REMOVED AND NEW SEAT TRACK WAS INSTALLED IAW SRM 51-30-1, 51-30-2, 51-10-4, AND 53-05-4. - [SDR CALA0000839](https://openairdocs.org/sdr/CALA0000839.md): Floor Support · corroded · Jun 7, 2000 · N10834 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND FLOOR SUPPORTS CORRODED AT STA 160 - 200, LBL 44.5 AND STA 180, LBL 16 - 36. THE FLOOR SUPPORTS WERE REMOVED AND NEW FLOOR SUPPORTS WERE INSTALLED IAW SRM 51-30-2, 51-10-4, AND 51-30-5. - [SDR CALA0000838](https://openairdocs.org/sdr/CALA0000838.md): Mount · corroded · Jun 7, 2000 · N10834 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND G-2 GALLEY I/B FORWARD MOUNT FITTING CORRODED. THE FITTING WAS REMOVED AND AND NEW FITTING WAS INSTALLED IAW SRM 51-30-5. - [SDR CALA0000817](https://openairdocs.org/sdr/CALA0000817.md): Attach Angle · cracked · Jun 2, 2000 · N10834 · Doug DC982 · Fuselage Main, Attach Fittings > INSPECTION FOUND R-1 DOOR THRESHOLD AFT ATTACH ANGLE CRACKED AND CORRODED. THE ANGLE AND DOUBLER WERE REMOVED AND A NEW ANGLE AND DOUBLER WERE INSTALLED IAW SRM 51-30-1, 51-30-2, 51-10-2, 51-10-4, AND 51-10-3. - [SDR CALA0000816](https://openairdocs.org/sdr/CALA0000816.md): Floor Support · corroded · Jun 2, 2000 · N10834 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND FLOOR SUPPORT CORRODED BETWEEN STA 200 AND 250, LBL 18. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-30-2, 51-10-3, AND 51-30-5. - [SDR CALA0000815](https://openairdocs.org/sdr/CALA0000815.md): Floor Support · corroded · Jun 2, 2000 · N10834 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND FLOOR SUPPORT AT L-2 DOOR, STA 1155. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-30-1, 51-10-4, AND 51-10-3. - [SDR CALA0000788](https://openairdocs.org/sdr/CALA0000788.md): Rib · cracked · Jun 1, 2000 · N10834 · Doug DC982 · Trailing Edge Flaps > INSPECTION FOUND A 3 INCH CRACK IN I/B RIB OF RIGHT FLAP WEDGE ASSEMBLY NR 6. THE CRACK WAS DRILLED OUT AND A NEW RIB WAS INSTALLED IAW SRM 51-10-3, 51-30-2, AND 51-30-5. - [SDR CALA9801347](https://openairdocs.org/sdr/CALA9801347.md): Tail Cone · warped · Jul 24, 1998 · N10834 · Doug DC982 · Aerodynamic Fairings > THE FORCE REQUIRED TO RELEASE TAIL CONE DURING FUNCTIONAL CHECK WAS EXCESSIVE. THE TAIL CONE HUNG UP ON RIGHT SIDE LATCH PINS. A SERVICEABLE TAIL CONE WAS INSTALLED AND ADJUSTED IAW MM 53-53-00. - [SDR CALA9801323](https://openairdocs.org/sdr/CALA9801323.md): Skin · dented · Jul 23, 1998 · N10834 · Doug DC982 · Fuselage Main, Plate/Skin > INSPECTION FOUND LT FUSELAGE SKIN DENTED AT STA 229-237 ABOVE CUSP LINE. A REPAIR WAS INSTALLED IAW ECRA 5330-02687. - [SDR CALA9801322](https://openairdocs.org/sdr/CALA9801322.md): Beam · corroded · Jul 22, 1998 · N10834 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND CORROSION ON MID BAG BIN Z BEAM AT THRESHOLD, STA 636-693. CORROSION WAS ALSO FOUND ON AFT BAG BIN Z BEAM AT THRESHOLD STA 1155-1212. REPAIRS WERE INSTALLED IAW SRM 53-05, FIGURE 63. Next page: https://openairdocs.org/deregistered/N10834-2007-06-01/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 = 'N10834' AND deregistration_id = 'N10834-2007-06-01' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N10834-2007-06-01/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.