# Service difficulty reports: N129UP A list on [N129UP](https://openairdocs.org/aircraft/N129UP.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 6 · 253 reports - [SDR IPXA2026091912039](https://openairdocs.org/sdr/IPXA2026091912039.md): Cover · detached · Sep 18, 2026 · N129UP · Airbus A300F4622R · Passenger/Crew Doors > CREW DOOR UPPER HANDLE COVER FELL OFF. INSTALLED CREW DOOR UPPER HANDLE COVER IAW AMM 52-11-11-27 THIS CLEARS DEFERRAL AND PLACARD REMOVED - [SDR IPXA2026042808251](https://openairdocs.org/sdr/IPXA2026042808251.md): Door · leaking · Apr 21, 2026 · N129UP · Airbus A300F4622R · Passenger/Crew Doors > SQUEALING NOISE FROM MAIN ENTRY DOOR WHEN PRESSURIZED. INSTALLED INNER DOOR HANDLE AND LINING PER MM 52-11-21. - [SDR IPXA2026042208251](https://openairdocs.org/sdr/IPXA2026042208251.md): Shaft · loose · Apr 21, 2026 · N129UP · Airbus A300F4622R · Passenger/Crew Doors > SQUEALING NOISE FROM MAIN ENTRY DOOR WHEN PRESSURIZED. TIGHTENED MOUNTING HARDWARE FOR LOCKING SHAFT BLOCK, NOTED SLIGHT CHANGE IN SQUEALING SOUND IAW AMM 52-11-21. - [SDR IPXA2025111955197](https://openairdocs.org/sdr/IPXA2025111955197.md): Door · corroded · Nov 13, 2025 · N129UP · Airbus A300F4622R · Fluid Service Doors > LAVATORY SERVICING PANEL ACCESS DOOR OPEN / CLOSE LATCH FROM CTR EXTERNAL FOUND DAMAGED ( UN SERVICEABLE) LAVATORY SERVICE DOOR REMOVED IAW A300-600 SRM 51-40-21.FABRICATED, LOCATED AND DRILLED NEW REPAIR PARTS (DOUBLER AND SHIM) IAW A300-600 SRM 52-42-11/FI - [SDR IPXA2025111053801](https://openairdocs.org/sdr/IPXA2025111053801.md): Floorbeam · corroded · Nov 7, 2025 · N129UP · Airbus A300F4622R · Fuselage Main, Floor Beam > BULK CARGO PIT FR.#66 STRUCTURAL BEAM UNDER LH FLOOR PANEL #161GF HEAVY CORROSION. INSTALLED NUTPLATES AND CROSSBEAM IAW SRM 51-40-21. - [SDR IPXA2025110746890](https://openairdocs.org/sdr/IPXA2025110746890.md): Doubler · corroded · Nov 6, 2025 · N129UP · Airbus A300F4622R · Fuselage Main, Structure > LAVATORY SERVICE PANEL 121DL BLANKING PLUG REINFORCEMENT DOUBLER IS CORRODED. REMOVED AND REPLACED BLANKING PLUG AT LAV SERVICE PANEL 121DL IAW SRM 51-40-21. - [SDR IPXA2025103113680](https://openairdocs.org/sdr/IPXA2025103113680.md): Floor Panel · damaged · Oct 29, 2025 · N129UP · Airbus A300F4622R · Fuselage Floor Panel > FLOOR PANEL 132AH IS BROKEN IN HALF. FLOOR PANEL 132AH FAB COMPLETED IAW SREO-16407-REQ002 ((APPX C) A300 FWD/AFT LOWER CARGO COMPARTMENT FLOOR PANEL FABRICATION (SREO)). REVIEWED - [SDR IPXA2025103171956](https://openairdocs.org/sdr/IPXA2025103171956.md): Floor Panel · damaged · Oct 27, 2025 · N129UP · Airbus A300F4622R · Fuselage Floor Panel > MCD FLOOR PANEL 221EG IS BROKEN. FLOOR PANEL 221EG FAB COMPLETED IAW SREO-16407-REQ002 ((APPX C) A300 FWD/AFT MAIN CARGO COMPARTMENT FLOOR PANEL FABRICATION (SREO)). - [SDR IPXA2025110149647](https://openairdocs.org/sdr/IPXA2025110149647.md): Plate · cracked · Oct 19, 2025 · N129UP · Airbus A300F4622R · Wing Main, Frame Structure > LEFT WING CENTER FLAP, METALIC PLATE ON TOP SURFACE LE SIDE HAS GOUGING AND SHOWS EVIDENCE OF A CRACK. REMOVED AND REMPLACED METALIC PLATE ON TOP SURFACE LE SIDE IAW SRM 51-40-21. - [SDR IPXA2025111813903](https://openairdocs.org/sdr/IPXA2025111813903.md): Frame · cracked · Oct 17, 2025 · N129UP · Airbus A300F4622R · Fuselage Main, Frame > AIR CONDITION BAY, FR 46RH, BASE FRAME FITTINGS HAS A CRACK. VERIFIED ACCOMPLISHED REPAIR IAW EO-46789-JIC008 REV1. BASE FRAME FITTING FR 46 R/H STRG 35. - [SDR IPXA2025111412206](https://openairdocs.org/sdr/IPXA2025111412206.md): Support Fitting · cracked · Oct 17, 2025 · N129UP · Airbus A300F4622R · Horizontal Stabilizer Miscellaneous Structure > HORIZONTAL STAB, 2EA CRACKED BRACKETS ATTACHMENT FOR RH UPPER THS TO FUSELAGE FAIRING. DOT NO. 17-55. INSTALLED 2 EA BRACKETS AT RH UPPER THS TO FUSELAGE FAIRING IAW SRM 51-40-21. - [SDR IPXA2025111112361](https://openairdocs.org/sdr/IPXA2025111112361.md): Bracket · cracked · Oct 17, 2025 · N129UP · Airbus A300F4622R · Horizontal Stabilizer Miscellaneous Structure > CRACKED BRACKET ATTACHMENT FOR LH UPPER THS TO FUSELAGE FAIRING FWD AREA. DOT NO. 17-57. INSTALLED BRAKET SUPPORT P/N: A5517155320451 AT L/H UPPER THS TO FUSELAGE FAIRING IAW A300-600 SRM 51-40-40 IAW A300-600 SRM 51-40-21. - [SDR IPXA2025110405938](https://openairdocs.org/sdr/IPXA2025110405938.md): Profile · broken · Oct 16, 2025 · N129UP · Airbus A300F4622R · Fuselage Miscellaneous Structure > LEFT FRAME 82 THE CORNER ANGLE IS BROKEN. REMOVED PROFILE -T P/N: A53981401200 AT ZONE 200 L/H FR 82 I.A.W. A300-600 SRM 51-40-21. INSTALLED NEW PROFILE Z AT LH FR 82 IAW A300 SRM 51-40 21. - [SDR IPXA2025103198494](https://openairdocs.org/sdr/IPXA2025103198494.md): Floor Panel · damaged · Oct 16, 2025 · N129UP · Airbus A300F4622R · Fuselage Floor Panel > UPPER MAIN CARGO FLOOR PANEL 232KH DELAMINATED AND BROKEN. FLOOR PANEL 232KH FAB COMPLETED IAW SREO-16407-REQ002 ((APPX C). - [SDR IPXA2025103195901](https://openairdocs.org/sdr/IPXA2025103195901.md): Floor Panel · damaged · Oct 16, 2025 · N129UP · Airbus A300F4622R · Fuselage Floor Panel > UPPER MAIN CARGO FLOOR PANEL 222EG DAMAGED AND DELAMINATED. FLOOR PANEL 222EG FAB COMPLETED IAW SREO-16407-REQ002 ((APPX C). - [SDR IPXA2025103198283](https://openairdocs.org/sdr/IPXA2025103198283.md): Floor Panel · damaged · Oct 16, 2025 · N129UP · Airbus A300F4622R · Fuselage Floor Panel > UPPER MAIN CARGO FLOOR PANEL 231KH DAMAGED AND BROKEN. FLOOR PANEL 231KH FAB COMPLETED IAW SREO-16407-REQ002 ((APPX C) CARGO COMPARTMENT FLOOR PANEL FABRICATION (SREO)). - [SDR IPXA2025103195609](https://openairdocs.org/sdr/IPXA2025103195609.md): Floor Panel · broken · Oct 16, 2025 · N129UP · Airbus A300F4622R · Fuselage Floor Panel > UPPER MAIN CARGO FLOOR PANEL # 222DG BROKEN. 89-1589. LOORBOARD PANEL 222DG FAB COMPLETED IAW SREO-16407-REQ002,APPX C A300 FWD/AFT LOWER CARGO COMPARTMENT FLOOR PANEL FABRICATION. - [SDR IPXA2025102805909](https://openairdocs.org/sdr/IPXA2025102805909.md): Profile · broken · Oct 16, 2025 · N129UP · Airbus A300F4622R · Fuselage Miscellaneous Structure > FAULT/STR/ZONE 200 R/H FR 82 THE CORNER ANGLE IS BROKEN. REMOVED PROFILE -T R/H FR 82 I.A.W. SRM 51-40-21. INSTALLED NEW PROFILE-T AT ZONE 200 R/H FR 82 I.A.W. A300-600 SRM 51-40-21. - [SDR IPXA2025111380204](https://openairdocs.org/sdr/IPXA2025111380204.md): Seat Track · corroded · Oct 15, 2025 · N129UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings > MAIN DECK SEAT TRACK AT FR79/FR80, Y0 HAS CORROSION. INSTALLED SEAT TRACK AT Y '0' FR 79 TO FR 80 USING FASTNERS PN HL10VF8-6 B# 0004989789, NSA5075-8 38 EACH B# 0004145036, HL12-6-6 B# 0004304262 16 EACH, HL10VF6-5 B# 0004426225 6 EACH, NSA5075-6 B# 00042919 - [SDR IPXA2025110470051](https://openairdocs.org/sdr/IPXA2025110470051.md): Skin · cracked · Oct 15, 2025 · N129UP · Airbus A300F4622R · Wing, Plate/Skin > RH WING, UPPER SURFACE, CLOSE TO RIB 18, REAR SPAR, SKIN HAS A CRACK DOT 103-51. REMOVED RIVETS AND BOLTS AFFECTED BY THE REPAIR ON RH WING UPPER SURFACE CLOSE TO RIB 18 REAR SPAR IAW A300-600F SRM 57-51-12. INSTALLED BUTTSTRAP, PACKING STRIP, REINFORCEMENT PL - [SDR IPXA2025110570051](https://openairdocs.org/sdr/IPXA2025110570051.md): Skin · cracked · Oct 15, 2025 · N129UP · Airbus A300F4622R · Wing, Plate/Skin > RIGHT WING, UPPER SURFACE, CLOSE TO RIB 18, REAR SPAR, SKIN HAS A CRACK. - [SDR IPXA2025110382369](https://openairdocs.org/sdr/IPXA2025110382369.md): Floorbeam · bent · Oct 15, 2025 · N129UP · Airbus A300F4622R · Fuselage Main, Floor Beam > MAIN DECK FLOOR STRUCTURE- CROSSBEAM BENT AT FR48 BETWEEN -Y450 AND -Y953, VERIFIED CROSSBEAM REPLACED ON SREO. COMPLIED WITH SREO-75878-REQ001. - [SDR IPXA2025102882408](https://openairdocs.org/sdr/IPXA2025102882408.md): Floorbeam · cracked · Oct 15, 2025 · N129UP · Airbus A300F4622R · Fuselage Main, Floor Beam > FAULT - STR - Z241 -MAIN DECK FLOOR STRUCTURE- CROSSBEAM CRACKED (BUCKLING) AT FR51 BETWEEN -Y450 AND -Y953, DOT 78-20. ACCOMPLISHED WITH SREO-75878-REQ001. REVIEWED - [SDR IPXA2025103054985](https://openairdocs.org/sdr/IPXA2025103054985.md): Support · cracked · Oct 14, 2025 · N129UP · Airbus A300F4622R · Wing Miscellaneous Structure > LH WING FIXED LEADING EDGE SUPPORT CRACKED AT LWR CORNER INSIDE ACCESS PANEL 524GB, INSTALLED PLATE P\N: R5724018520000 BATCH: 0004437520, LH WING FIXED LEADING EDGE SUPPORT IAW A300-600 SRM 57-41-11 PAGE 211 FIGURE 202 (SHEET 2) AND SRM 51-40-21. - [SDR IPXA2025110362365](https://openairdocs.org/sdr/IPXA2025110362365.md): Web · gouged · Oct 14, 2025 · N129UP · Airbus A300F4622R · Wing Miscellaneous Structure > LEFT WING T/E REAR SPAR UNDER #5 SPOILER O/B SUPPORT WEB GOUGED, REMOVED CRACKED SUPPORT WEB IAW A300-600 SRM 51-40-21. INSTALLED NEW SUPPORT WEB IAW A300-600 SRM 51-40-21. - [SDR IPXA2025103146907](https://openairdocs.org/sdr/IPXA2025103146907.md): Rib · cracked · Oct 14, 2025 · N129UP · Airbus A300F4622R · Wing, Rib/Bulkhead > RH WING T/E UPPER SKIN CHANNEL BELOW THE NO.3 SPOILER I/B HINGE IS CRACKED. DOT NO. 17-22. INSTALLED WEB IAW A300-600 SRM 51-40-21. - [SDR IPXA2025111826351](https://openairdocs.org/sdr/IPXA2025111826351.md): Floor Support · corroded · Oct 12, 2025 · N129UP · Airbus A300F4622R · Fuselage Miscellaneous Structure > BULK CARGO RH FLOOR BRACKET HAS CORROSION. DOT 28-1180. INSTALLED NEW FLOOR BRACKET IAW SRM 51-40-21. - [SDR IPXA2025102913554](https://openairdocs.org/sdr/IPXA2025102913554.md): Bracket · cracked · Oct 11, 2025 · N129UP · Airbus A300F4622R · Fuselage Main, Structure > NLG WW LH WHEEL GUIDE STRUT UPPER ATTACHED SUPPORT MOUNT IS CRACKED, DOT 55-033. INSTALLED NEW BRACKET-GUIDE STRUT NLG IAW A300-600 SRM 51-40-21. REVIEWED - [SDR IPXA2025102812902](https://openairdocs.org/sdr/IPXA2025102812902.md): Floor Support · cracked · Oct 11, 2025 · N129UP · Airbus A300F4622R · Fuselage Miscellaneous Structure > FAULT-Z120-STR-FLOOR STRUCTURE SUPPORT ANGLES CRACKED L/H, @ FR.38 FWD CARGO JUST BELOW MAIN DECK FLOOR. DOT 85/1095. REMOVED CRACKED SUPPORT ANGLE L/H AT FR.38 I.A.W. A300-600 SRM 51-40-21. ++INSTALLED NEW SUPPORT IAW A300-600 SRM 51-40-21. - [SDR IPXA2025102812925](https://openairdocs.org/sdr/IPXA2025102812925.md): Floor Support · cracked · Oct 11, 2025 · N129UP · Airbus A300F4622R · Fuselage Miscellaneous Structure > FAULT-Z120-STR-FLOOR STRUCTURE SUPPORT ANGLES CRACKED R/H, @ FR.38 FWD CARGO JUST BELOW MAIN DECK FLOOR. DOT 85/1096. REMOVED SUPPORT ANGLE R/H AT FR.38 I.A.W. A300-600 SRM 51-40-21. ++INSTALLED NEW SUPPORT IAW A300-600 SRM 51-40-21. - [SDR IPXA2025111295291](https://openairdocs.org/sdr/IPXA2025111295291.md): Adapter · corroded · Oct 10, 2025 · N129UP · Airbus A300F4622R · Fuselage Main, Structure > MDC CLS ADAPTER AT FR26 Y0 RT IS CORRODED. INSTALLED CLS ADAPTER AND FLOOR STRUCTURE AT FR26 Y0 RH IAW A300-600 SRM 51-40-21-001, SRM 51-75-10-201 SRM 51-76-00-001. - [SDR IPXA2025110895377](https://openairdocs.org/sdr/IPXA2025110895377.md): Adapter · corroded · Oct 10, 2025 · N129UP · Airbus A300F4622R · Fuselage Main, Structure > MAJOR REPAIR - MDC CLS ADAPTER AT FR65 Y0 LH IS CORRODED. ACCOMPLISHED STEP # 9 E.A#: 300-5317-27-A4193 PRELIMINARY 1: "RESTORE SURFACE PROTECTION AND PAINT SCHEME ACCORDING TO SRM 51-23-10 AND 51-75-10. - [SDR IPXA2025111394837](https://openairdocs.org/sdr/IPXA2025111394837.md): Rib · cracked · Oct 10, 2025 · N129UP · Airbus A300F4622R · Trailing Edge Flaps > MAJOR REPAIR, LEFT WING, CENTER FLAP, TOP SKIN RIB FLANGE, ONE CRACK INDICATION NOTED AT RIB 15. ACCOMPLISH REPAIR IN ACCORDANCE WITH EO-95517-REQ1 AND VT-MAE EA 300-5750-27-A4185, REV -. - [SDR IPXA2025111295293](https://openairdocs.org/sdr/IPXA2025111295293.md): Adapter · corroded · Oct 10, 2025 · N129UP · Airbus A300F4622R · Fuselage Main, Structure > MDC CLS ADAPTER AT FR27 Y0 LH IS CORRODED. INSTALLED CLS ADAPTER AND FLOOR STRUCTURE AT FR27 Y0 LH IAW SRM 51-40-21-001, SRM 51-75-10-201 SRM 51-76-00-001. - [SDR IPXA2025111295254](https://openairdocs.org/sdr/IPXA2025111295254.md): Adapter · corroded · Oct 10, 2025 · N129UP · Airbus A300F4622R · Fuselage Main, Structure > MDC CLS ADAPTER AT FR26 Y0 LH IS CORRODED. INSTALLED CLS ADAPTER AND FLOOR STRUCTURE AT FR26 Y0 LH IAW SRM 51-40-21-001, SRM 51-75-10-201 SRM 51-76-00-001. - [SDR IPXA2025111295296](https://openairdocs.org/sdr/IPXA2025111295296.md): Adapter · corroded · Oct 10, 2025 · N129UP · Airbus A300F4622R · Fuselage Main, Structure > MDC CLS ADAPTER AT FR27 Y0 RH IS CORRODED. INSTALLED CLS ADAPTER AND FLOOR STRUCTURE AT FR27 Y0 RH IAW A300-600 SRM 51-40-21-001, SRM 51-75-10-201 SRM 51-76-00-001. - [SDR IPXA2025110895397](https://openairdocs.org/sdr/IPXA2025110895397.md): Adapter · corroded · Oct 10, 2025 · N129UP · Airbus A300F4622R · Fuselage Main, Structure > MAJOR REPAIR - MDC CLS ADAPTER AT FR38.2 Y0 LH IS CORRODED. COMPLIED WITH EO-95476-REQ1 AND EA300-5314-27-A418. - [SDR IPXA2025110995367](https://openairdocs.org/sdr/IPXA2025110995367.md): Adapter · corroded · Oct 10, 2025 · N129UP · Airbus A300F4622R · Fuselage Main, Structure > MAJOR REPAIR - MDC CLS ADAPTER AT FR38.2 Y0 RH IS CORRODED. - [SDR IPXA2025110895344](https://openairdocs.org/sdr/IPXA2025110895344.md): Adapter · corroded · Oct 10, 2025 · N129UP · Airbus A300F4622R · Fuselage Main, Structure > MAJOR REPAIR - MDC CLS ADAPTER AT FR30 Y0 LT IS CORRODED. ACCOMPLISH PERMANENT REPAIR IN ACCORDANCE WITH EO-95477-REQ1 AND VT-MAE EA 300-5314-27-A4191 REV -. - [SDR IPXA2025110895440](https://openairdocs.org/sdr/IPXA2025110895440.md): Adapter · corroded · Oct 10, 2025 · N129UP · Airbus A300F4622R · Fuselage Main, Structure > MAJOR REPAIR - MDC CLS ADAPTER AT FR61 Y0 RT IS CORRODED. ACCOMPLISH PERMANENT REPAIR IN ACCORDANCE WITH EO-95478-REQ1 AND VT-MAE EA 300-5317-27-A4192 REV -.. - [SDR IPXA2025103193086](https://openairdocs.org/sdr/IPXA2025103193086.md): Skin · dented · Oct 10, 2025 · N129UP · Airbus A300F4622R · Trailing Edge Flaps > RIGHT WING INBD FLAP HAS A DENT ON OTBD TOP SKIN. ACCOMPLISHED IAW EO-95578-REQ1 REV. 2 AND VT-MAE EA 300-5751-27-A4197, REV -. - [SDR IPXA2025111094874](https://openairdocs.org/sdr/IPXA2025111094874.md): Angle · cracked · Oct 10, 2025 · N129UP · Airbus A300F4622R · Nacelle/Pylon, Main Frame > NR 2 ENG PYLON UPPER, ANGLE UNDER 423AL IS CRACKED IN TWO LOCATIONS, ACROSS BOLT HOLE AND FWD OF BOLTS. DOT #85/1018 CERTIFIED. REMOVED STRUCTURAL BEAM I.A.W. SRM 51-40-21.FABRICATED, LOCATED AND DRILLED NEW CROSSBEAM IAW A300-600 SRM 51-31-00 AND DWR# A53974 - [SDR IPXA2025110895368](https://openairdocs.org/sdr/IPXA2025110895368.md): Adapter · corroded · Oct 10, 2025 · N129UP · Airbus A300F4622R · Fuselage Main, Structure > MDC CLS ADAPTER AT FR38.1 Y0 LH IS CORRODED. COMPLIED WITH UPS EO-95474-REQ1 AND VTMAE EA300-5314-27-A4189. - [SDR IPXA2025110895352](https://openairdocs.org/sdr/IPXA2025110895352.md): Adapter · corroded · Oct 10, 2025 · N129UP · Airbus A300F4622R · Fuselage Main, Structure > CLS ADAPTER AT FR33 Y0 LH IS CORRODED. COMPLIED WITH EO-95473-REQ1 AND VTMAE EA300-5314-27-A4190. - [SDR IPXA2025110373140](https://openairdocs.org/sdr/IPXA2025110373140.md): Roller · excess play · Oct 9, 2025 · N129UP · Airbus A300F4622R · Passenger/Crew Doors > ROLLER UPPER REW DOOR FWD HAS AXIAL PLAY. REPLACED BEARING AND SPACE, ROLLER UPPER DOOR FWD IAW A300 SRM 51-40-21. - [SDR IPXA2025110373123](https://openairdocs.org/sdr/IPXA2025110373123.md): Roller · excess play · Oct 9, 2025 · N129UP · Airbus A300F4622R · Passenger/Crew Doors > CREW DOOR ROLLER AFT SIDE HAS AXIAL PLAY DOR ALEX-04. REPLACED ROLLER,CREW DOOR AFT SIDE IAW A300 SRM 51-40-21. - [SDR IPXA2025101881185](https://openairdocs.org/sdr/IPXA2025101881185.md): Floor Panel · damaged · Oct 9, 2025 · N129UP · Airbus A300F4622R · Fuselage Floor Panel > FAULT-MXP-531625-01-1-153-JIC-INT-152KG FLOOR PANEL IS DAMAGED. FLOOR PANEL 152KG FABRICATION IS COMPLETE IAW SREO-16407-REQ002 ((APPX C). - [SDR IPXA2025101881141](https://openairdocs.org/sdr/IPXA2025101881141.md): Floor Panel · damaged · Oct 9, 2025 · N129UP · Airbus A300F4622R · Fuselage Floor Panel > FAULT- MXP-531625-01-1-153-JIC-INT- 151UF FLOOR PANEL IS DAMAGED. FLOOR PANEL 151UF FABRICATION IS COMPLETE IAW SREO-16407-REQ002 ((APPX C). - [SDR IPXA2025101881096](https://openairdocs.org/sdr/IPXA2025101881096.md): Floor Panel · damaged · Oct 9, 2025 · N129UP · Airbus A300F4622R · Fuselage Floor Panel > FAULT-MXP-531625-01-1-153-JIC-INT-151KG FLOOR PLANEL IS DAMAGED. FLOOR PANEL 151KG FABRICATION IS COMPLETE IAW SREO-16407-REQ002 ((APPX C). - [SDR IPXA72672](https://openairdocs.org/sdr/IPXA72672.md): Panel · broken · Oct 9, 2025 · N129UP · Airbus A300F4622R · Passenger/Crew Doors > FWD CREW DOOR PANEL 831GZ BROKEN IN CORNER. REPAIRED CREW DOOR PANEL 831GZ IAW A300 AMM 25-00-00/801 USED 1/4 OF TUBE ADHESIVE P/N: 04-001-0176 BTCH: 4433029. REVIEWED Next page: https://openairdocs.org/aircraft/N129UP/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 = 'N129UP' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N129UP/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.