# Service difficulty reports: N138UP A list on [N138UP](https://openairdocs.org/aircraft/N138UP.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 5 · 250 reports - [SDR IPXA2026081700279](https://openairdocs.org/sdr/IPXA2026081700279.md): Seal · leaking · Aug 14, 2026 · N138UP · Airbus A300F4622R · Passenger/Crew Doors > HOWLING SOUND COMING FROM MAIN CABIN DOOR DURING ENTIRE FLIGHT. CRUISE, CLIMB, DESCENT. R & R L1 DOOR SEAL IAW AMM 52-10-18 UP TO & INCL 2.D.(6). REQUIRES TEST AND LEAK CHECK. C/W REMAINING STEPS OF AMM 52-10-18, TEST GOOD. REF T3F18E009AJ1A FOR LEAK CHECK REQ - [SDR IPXA2026041338309](https://openairdocs.org/sdr/IPXA2026041338309.md): Lamp · inoperative · Apr 10, 2026 · N138UP · Airbus A300F4622R · Emergency Lighting > LAV EMERGENCY LIGHT INOP. RELAMPED W/REF TO MM 33-51-21 PB 0401 - [SDR IPXA2026041037458](https://openairdocs.org/sdr/IPXA2026041037458.md): Lamp · inoperative · Apr 10, 2026 · N138UP · Airbus A300F4622R · Emergency Lighting > LAV EMERGENCY LIGHT INOP. RELAMPED LAVATORY AUXILILART/MIRROR LIGHT IAW AMM 33-51-21/401, OPS CHECK GOOD. - [SDR IPXA2026012197113](https://openairdocs.org/sdr/IPXA2026012197113.md): Lamp · inoperative · Jan 21, 2026 · N138UP · Airbus A300F4622R · Emergency Lighting > SMALL SQUARE EMERGENCY EXIT LIGHT IN LAV INOP ON LOW SETTING. REPLACED THE LAMPS IAW AMM 33-51-17/401. OPS CHECKED GOOD. - [SDR IPXA2025121067021](https://openairdocs.org/sdr/IPXA2025121067021.md): Door · binding · Dec 10, 2025 · N138UP · Airbus A300F4622R · Passenger/Crew Doors > CREW ENTRY DOOR DIFFICULT TO OPEN AND APPEARS TO BIND IN FANNIE HANDLE DOES NOT STAY UP IN ELEVATED POSITION. UNSURE OF WHERE IT IS CATCHING. INSTALLED L1 DOOR REF AMM 52-11-11/401 UP TO AND 2 F (8). - [SDR IPXA2025111882952](https://openairdocs.org/sdr/IPXA2025111882952.md): Actuator · inoperative · Nov 15, 2025 · N138UP · Airbus A300F4622R · Auto Flight System > YAW DAMPER KICKED OFF WOULD NOT RESET. REPLACED YAW DAMPER ACTUATOR IAW AMM 22-23-22/401 OPS AND LEAKS CHECKS GOOD OK FOR SERVICE. ALL WORK ACCOMPLISHED BY ALL CAT 3 QUALIFIED TECH. - [SDR IPXA2025111782952](https://openairdocs.org/sdr/IPXA2025111782952.md): Actuator · faulted · Nov 15, 2025 · N138UP · Airbus A300F4622R · Auto Flight System > EMERGENCY DECLARED, YAW DAMPER KICKED OFF WOULD NOT RESET. REPLACED YAW DAMPER ACTUATOR IAW AMM 22-23-22/401 OPS AND LEAKS CHECKS GOOD OK FOR SERVICE. ALL WORK ACCOMPLISHED BY ALL CAT 3 QUALIFIED TECH. - [SDR IPXA2025120741156](https://openairdocs.org/sdr/IPXA2025120741156.md): Skin · punctured · Oct 18, 2025 · N138UP · Airbus A300F4622R · Trailing Edge Flaps > MAJOR REPAIR, DURING CLEAN UP, PUNCTURED INNER FLAP LOWER SKIN INFO SENT TO ENGINEERING ALL STEPS OF EO-95467-REQ4 COMPLETED. THIS IS A PERMANENT REPAIR. THIS DEFERRAL IS NOW CLOSED. - [SDR IPXA2025080215434](https://openairdocs.org/sdr/IPXA2025080215434.md): Fitting · cracked · Jul 14, 2025 · N138UP · Airbus A300F4622R · Fuselage Miscellaneous Structure > CRACK FOUND AT BASE FITTING FR45, RH SIDE.THIS JOB WAS PERFORMED IAW EO-46789-JIC008. (REPAIR - BASE FRAME FITTING, FR 41 TO FR 46, RH SIDE (SB A300-57-6177)) [T3F18E00711GE] STEPS 43 THROUGH 53 - [SDR IPXA2025080115449](https://openairdocs.org/sdr/IPXA2025080115449.md): Fitting · cracked · Jul 14, 2025 · N138UP · Airbus A300F4622R · Fuselage Miscellaneous Structure > CRACK FOUND AT BASE FITTING FR46, RIGHT SIDE.ACCOMPLISHED EO-46789-JIC008 REPAIR OF FR46 RH SIDE BASE FITTING COMPLETE. - [SDR IPXA2025080115146](https://openairdocs.org/sdr/IPXA2025080115146.md): Fitting · cracked · Jul 14, 2025 · N138UP · Airbus A300F4622R · Fuselage Miscellaneous Structure > CRACK FOUND AT BASE FITTING FR44, RH SIDE. THIS JOB WAS PERFORMED IAW EO-46789-JIC008, REPAIR - BASE FRAME FITTING, FR 41 TO FR 46, RH SIDE (SB A300-57-6177). - [SDR IPXA2025081943612](https://openairdocs.org/sdr/IPXA2025081943612.md): Skin · damaged · Jul 9, 2025 · N138UP · Airbus A300F4622R · Passenger/Crew Doors > CREW DOOR UPPER INNER SKIN HAS BARE METAL EXPOSED. CLEANED AREA AND RESTORED SURFACE PROTECTION IAW A300-600 SRM 51-21-10, SRM 51-75-10 AND AMM 12-21-11. - [SDR IPXA2025081941352](https://openairdocs.org/sdr/IPXA2025081941352.md): Door · corroded · Jul 9, 2025 · N138UP · Airbus A300F4622R · Passenger/Crew Doors > *** SUPPLEMENTAL SDR *** FAULT: STR-ZONE 831- ALL FASTENERS AROUND CREW DOOR EXTERNAL SURFACE CORRODED. JP-110 REVIEWED - [SDR IPXA2025080637021](https://openairdocs.org/sdr/IPXA2025080637021.md): Support · corroded · Jul 9, 2025 · N138UP · Airbus A300F4622R · Fuselage Miscellaneous Structure > FAULT- STR- ZONE 100- AFT CARGO FR 58 RH SLOPE STRUCTURE (P/N F539-71534-006-00) IS CORRODED IN 2EA PLACES. 91148554.REMOVED AFT CARGO FR 58 PROFILE BRACKET P/N F539-71534-006-00 IAW A300-600 SRM 51-40-21.RECEIVED NEW SECTION SUPPORT (01EA)P/N F5397153400600 B - [SDR IPXA2025080637267](https://openairdocs.org/sdr/IPXA2025080637267.md): Support · corroded · Jul 9, 2025 · N138UP · Airbus A300F4622R · Fuselage Miscellaneous Structure > FAULT- STR- ZONE 100- FR 57 LH SLOPE STRUCTURE HAS CORROSION IN 1 PLACED MARKED IN RED. 91148554. REMOVED AFT CARGO FR 57 LH PROFILE BRACKET P/N F539-71534-006-00 IAW A300-600 SRM 51-40-21.RECEIVED NEW SECTION SUPPORT (01EA) P/N F5397153400600 BCH# 0004416282. - [SDR IPXA2025080537837](https://openairdocs.org/sdr/IPXA2025080537837.md): Angle · cracked · Jul 9, 2025 · N138UP · Airbus A300F4622R · Nacelle/Pylon Miscellaneous Structure > FAULT: STR-ZONE 400-#1 PYLON-INSIDE 475AL O/B SIDE 7TH FRAME FROM FWD SIDE-LOWER PART OF FRAME BROKEN ANGLE-109-VWV-91195430.FAB BROKEN ANGLE LOCATED AND DRILLED IAW A300-600 SRM.APPLIED TREATED AND PRIMER TO NEW ANGLE WITH P/N#ALODINE1132 BTCH#4381945 QTY: 1E - [SDR IPXA2025080138044](https://openairdocs.org/sdr/IPXA2025080138044.md): Attach Angle · cracked · Jul 9, 2025 · N138UP · Airbus A300F4622R · Nacelle/Pylon, Attach Fittings > NR 1 PYLON-INSIDE 475AL 4TH STIFFENER FROM AFT END ON I/B SIDE HAS UPPER ATTACH ANGLE BROKEN-109-VWV-91195430 VERIFIED INSTALLATION OF NEW ANGLE. - [SDR IPXA2025071043612](https://openairdocs.org/sdr/IPXA2025071043612.md): Skin · damaged · Jul 9, 2025 · N138UP · Airbus A300F4622R · Passenger/Crew Doors > CREW DOOR UPPER INNER SKIN HAS BARE METAL EXPOSED. - [SDR IPXA2025071041352](https://openairdocs.org/sdr/IPXA2025071041352.md): Fastener · corroded · Jul 9, 2025 · N138UP · Airbus A300F4622R · Passenger/Crew Doors > ALL FASTENERS AROUND CREW DOOR EXTERNAL SURFACE CORRODED. - [SDR IPXA2025081918111](https://openairdocs.org/sdr/IPXA2025081918111.md): Panel · cracked · Jul 8, 2025 · N138UP · Airbus A300F4622R · Passenger/Crew Doors > PANEL 831BZ HAS CRACK (.500 IN). 91148554 APPLIED ADHESIVE TO DAMAGE AREA OF PANEL 831BZ. P/N EC3532, B/N 0004408668. CURED AND SANDED. IAW AMM 25-00-00/801 PARA 4 REPAIR A STEP (B). RESTORED PROTECTIVE COATING AT REPAIRED AREA. P/N WS-3-BR227K1Q, B/N 00043190 - [SDR IPXA2025081918116](https://openairdocs.org/sdr/IPXA2025081918116.md): Panel · cracked · Jul 8, 2025 · N138UP · Airbus A300F4622R · Passenger/Crew Doors > PANEL 831AZ HAS CRACK (.600 IN). 91148554 REPAIRED CRACK WITH 08-116, BATCH 4394542. IAW AMM A300-600 52-34-13/801 PARA 4.3.B.4-6. PAINTED REPAIRED AREA WITH.05 OZ OF 16-407, BATCH 4352735. CUP 02-012-176. IAW AMM A300-600 52-34-13/801 PARA 4.3.C.1. - [SDR IPXA2025081922065](https://openairdocs.org/sdr/IPXA2025081922065.md): Sight Glass · scratched · Jul 8, 2025 · N138UP · Airbus A300F4622R · Emergency Equipment > L-1 CREW DOOR EMERGENCY SLIDE COVER LOOKING GLASS IS SCRATCHED AND UNABLE TO SEE THROUGH INSTALLED CREW DOOR EMERGENCY SLIDE COVER IAW A300 AMM 52-10-13/401. - [SDR IPXA2025080620169](https://openairdocs.org/sdr/IPXA2025080620169.md): Skin · gouged · Jul 8, 2025 · N138UP · Airbus A300F4622R · Fuselage Main, Plate/Skin > FUSELAGE TAIL LOWER JACK SECTION, REINFORCE DOUBLER HAS MULTIPLE GOUGES (5EA) AND (1EA) DENT. INSTALLED FILLER, DOUBLER AND BALL AT FUSELAGE TAIL LOWER JACK SECTION IAW 53-10-12-201 PARA 13 FIGURE 210 REV 42 AND SRM 51-40-21. - [SDR IPXA2025072822969](https://openairdocs.org/sdr/IPXA2025072822969.md): Frame · broken · Jul 8, 2025 · N138UP · Airbus A300F4622R · Nacelle/Pylon, Frame/Spar/Rib > NUMBER 2 PYLON, INSIDE 485AL OTBD SIDE 5TH FRAME FWD FROM AFT END HAS BROKEN STIFFENER ON LOWER END. CLIP AND FRAME WAS INSTALLED IAW A300/600 SRM 51-40-21. - [SDR IPXA2025070918111](https://openairdocs.org/sdr/IPXA2025070918111.md): Panel · cracked · Jul 8, 2025 · N138UP · Airbus A300F4622R · Passenger/Crew Doors > PANEL 831BZ HAS CRACK (.500 IN). - [SDR IPXA2025070918116](https://openairdocs.org/sdr/IPXA2025070918116.md): Panel · cracked · Jul 8, 2025 · N138UP · Airbus A300F4622R · Passenger/Crew Doors > PANEL 831AZ HAS CRACK (.600 IN). - [SDR IPXA2025070922065](https://openairdocs.org/sdr/IPXA2025070922065.md): Sight Glass · scratched · Jul 8, 2025 · N138UP · Airbus A300F4622R · Emergency Equipment > L-1 CREW DOOR EMERGENCY SLIDE COVER LOOKING GLASS IS SCRATCHED AND UNABLE TO SEE THROUGH - [SDR IPXA2025080607418](https://openairdocs.org/sdr/IPXA2025080607418.md): Floor Support · broken · Jul 7, 2025 · N138UP · Airbus A300F4622R · Fuselage Miscellaneous Structure > MDC FLOOR STRUCTURE REINFORCEMENT SUPPORT CRACKED BTWN FR 38 AND FR 38.1 AT -Y2127.5. INSTALLED NEW FLOOR SUPPORT IAW SRM 51-40-21 WITH FASTENERS AND SEALANT. - [SDR IPXA2025080106493](https://openairdocs.org/sdr/IPXA2025080106493.md): Roller · gouged · Jul 7, 2025 · N138UP · Airbus A300F4622R · Fuselage Floor Panel > AFT CARGO COMPT ROLLER @ FRAME 57 LBL 30 DAMAGED. REMOVED AND REPLACED ROLLER BRAKING IAW AMM 25-58-34/0401.VERIFIED 1 EACH ROLLER REMOVED AND REPLACED. JOB COMPLETE. - [SDR IPXA2025071607273](https://openairdocs.org/sdr/IPXA2025071607273.md): Floor Panel · broken · Jul 7, 2025 · N138UP · Airbus A300F4622R · Fuselage Floor Panel > MAJOR REPAIR, MDC FLOOR PANEL 231QH WITH CORNER BROKEN FABRICATED FLOOR PANEL 231QH IAW A300 SREO-16407-REQ001. PAINTED IAW AMM 25-00-00/801. - [SDR IPXA2025073189108](https://openairdocs.org/sdr/IPXA2025073189108.md): Fire Seal · cracked · Jul 6, 2025 · N138UP · Airbus A300F4622R · Nacelle/Pylon, Main Frame > RIGHT PYLON, LOWER MIDDLE FIRE SEAL HAS A CRACK. REMOVED AND REPLACED LOWER FIRE SEAL, IAW SRM 51-40-21. - [SDR IPXA2025072388961](https://openairdocs.org/sdr/IPXA2025072388961.md): Fitting · cracked · Jul 6, 2025 · N138UP · Airbus A300F4622R · Fuselage Miscellaneous Structure > LEFT HAND HORIZONTAL JUCTION AREA AT FRAME 47 HOLE #A HAS CRACK AND DAMAGE INDICATIONS IN THE ALL LAYERS IN THE 9 O`CLOCK POSTION FACEING FORWARD. VERIFIED REPAIR HAS BEEN ACCOMPLISHED IAW EO-94545-REQ1 AND EA 300-5710-27-A4027 REV. -. - [SDR IPXA2025071588161](https://openairdocs.org/sdr/IPXA2025071588161.md): Floor Panel · damaged · Jul 6, 2025 · N138UP · Airbus A300F4622R · Fuselage Floor Panel > MAIN DECK FLOOR PANEL 231NG IS DAMAGED. FABRICATED FLOOR PANEL 231NG IAW A300 SREO-16407-REQ001, VERIFIED FABRICATION AND PAINT. - [SDR IPXA2025081278063](https://openairdocs.org/sdr/IPXA2025081278063.md): Floor Panel · damaged · Jul 5, 2025 · N138UP · Airbus A300F4622R · Fuselage Floor Panel > FWD CARGO CMPT, FLOOR PANEL 132MG; FR 27-32 RH IS DAMAGED. FABRICATED FLOOR PANEL 132MG IAW SREO-16407-REQ003 STEPS 1 - 19. - [SDR IPXA2025081278133](https://openairdocs.org/sdr/IPXA2025081278133.md): Floor Panel · damaged · Jul 5, 2025 · N138UP · Airbus A300F4622R · Fuselage Floor Panel > FWD CARGO CMPT, FLOOR PANEL 131MG; FR 27-32 LH IS DAMAGED. INSTALLED FABRICATED REPLACEMENT FLOOR PANEL FOR FWD PIT IAW SREO-16407-REQ002 ((APPX C)) JOB COMPLETE. REVIEWED - [SDR IPXA2025072480095](https://openairdocs.org/sdr/IPXA2025072480095.md): Support Bracket · cracked · Jul 5, 2025 · N138UP · Airbus A300F4622R · Fuselage Miscellaneous Structure > FWD CARGO CMPT FR 38.2; UPPER FLOORBEAM, LOWER CHANNEL SUPPORT BRACKETS (3EA) ARE CRACKED.REMOVED SUPPORT BRACKETS (3EA) AT FRAME 38.2 UPPER FLOOR BEAM IAW A300/600 SRM 51-40-21.FABRICATED NEW BRACKETS (3EA) ON FWD CARGO CMPT FROM MAT. 2024-T3.032C BTCH#:00043 - [SDR IPXA2025072970736](https://openairdocs.org/sdr/IPXA2025072970736.md): Seat Track · corroded · Jul 4, 2025 · N138UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings > MAJOR REPAIR, FLOOR C73 TO C74 AND Y 852 SEAT TRACK WITH EVIDENCE OF CORROSION INSTALLED NEW SEAT TRACK SECCTION ON MDC FLOOR STRUCTURE C71 TO C74 AND Y 852 IAW SRM 53-10-16. RESTORED PROTECTIVE SURFACE ON SEAT TRACK REPAIRED IAW SRM 51 75 10.51 10 16. - [SDR IPXA2025072870669](https://openairdocs.org/sdr/IPXA2025072870669.md): Web · cracked · Jul 4, 2025 · N138UP · Airbus A300F4622R · Fuselage Miscellaneous Structure > MDC FLOOR BETWEEN C73 TO 74 Y2127.5 WEB WITH EVIDENCE OF CRACK IN THE LOWER SURFACE INSTALLED NEW WEB BTW FR73 AND FR74 AT 2127.5 IAW A300-600 SRM 51-40-21. - [SDR IPXA2025080750211](https://openairdocs.org/sdr/IPXA2025080750211.md): Adapter · corroded · Jul 3, 2025 · N138UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings > CORROSION FOUND ON SEAT TRACK (5 LOCATIONS, EACH ONE ON A FRAME) BTW FR21&FR27 -Y65.5 INSTALLED NEW SEAT TRACK ADAPTER, CLS (4E/A) AND NUTPLATES (10E/A) IAW A300-600 SRM 51-40-21. - [SDR IPXA2025072053158](https://openairdocs.org/sdr/IPXA2025072053158.md): Fitting · cracked · Jul 3, 2025 · N138UP · Airbus A300F4622R · Fuselage Miscellaneous Structure > CRACK FOUND AT ANGLE-FITTING FR10 Y953 (PN A53612356200) INSTALLED 01 ANGLE FITTING P/N A5361235620000, BCH #0004410795, USING 11 SOLID RIVET IAW SRM 51-40-21 AND SRM 51-21-10 - [SDR IPXA2025071555684](https://openairdocs.org/sdr/IPXA2025071555684.md): Floor Panel · cracked · Jul 3, 2025 · N138UP · Airbus A300F4622R · Fuselage Floor Panel > MAIN DECK FLOOR PANEL 232EF IS CRACKED. FABRICATED FLOOR PANEL 232EF IAW SREO-16407-REQ001. PAINTED IAW AMM 25-00-00/801. - [SDR IPXA2025071655568](https://openairdocs.org/sdr/IPXA2025071655568.md): Floor Panel · broken · Jul 3, 2025 · N138UP · Airbus A300F4622R · Fuselage Floor Panel > MAJOR REPAIR, MAIN DECK CARGO FLOOR PANEL 232WG INSERT IS BROKEN (1 EA) FABRICATED FLOOR PANEL 232WG IAW A300 SREO-16407-REQ001. PAINTED IAW A300 AMM 25-00-00/801. - [SDR IPXA2025071655508](https://openairdocs.org/sdr/IPXA2025071655508.md): Floor Panel · broken · Jul 3, 2025 · N138UP · Airbus A300F4622R · Fuselage Floor Panel > MAJOR REPAIR. MAIN DECK CARGO FLOOR PANEL 241LM BROKEN FABRICATED FLOOR PANEL 241LM IAW A300 SREO-16407-REQ001. - [SDR IPXA2025071555422](https://openairdocs.org/sdr/IPXA2025071555422.md): Floor Panel · broken · Jul 3, 2025 · N138UP · Airbus A300F4622R · Fuselage Floor Panel > MAIN DECK FLOOR PANEL 242LJ IS BROKEN. FABRICATED FLOOR PANEL 242LJ IAW A300 SREO-16407-REQ001. - [SDR IPXA2025071555902](https://openairdocs.org/sdr/IPXA2025071555902.md): Floor Panel · broken · Jul 3, 2025 · N138UP · Airbus A300F4622R · Fuselage Floor Panel > MAIN DECK FLOOR PANEL 231PJ IS DAMAGED AUDIT COMPLETE - [SDR IPXA2025071855684](https://openairdocs.org/sdr/IPXA2025071855684.md): Floor Panel · cracked · Jul 3, 2025 · N138UP · Airbus A300F4622R · Fuselage Floor Panel > MAIN DECK FLOOR PANEL 232EF IS CRACKED AUDIT COMPLETE - [SDR IPXA2025072138048](https://openairdocs.org/sdr/IPXA2025072138048.md): Rib · cracked · Jul 2, 2025 · N138UP · Airbus A300F4622R · Wing, Rib/Bulkhead > MAJOR REPAIR, RH WING, CENTER FLAP, TOP SKIN RIB FLANGE, 2 CRACK INDICATION NOTED AT RIB 25. CIRCLED IN RED. VERIFIED PERMANENT REPAIR ACCOMPLISHED IAW EO-94347-REQ1 AND VT-MAE EA 300-5750-27-A4024, REV. -. - [SDR IPXA2025072138064](https://openairdocs.org/sdr/IPXA2025072138064.md): Rib · cracked · Jul 2, 2025 · N138UP · Airbus A300F4622R · Wing, Rib/Bulkhead > RH WING, CENTER FLAP, TOP SKIN RIB FLANGE, 1 CRACK INDICATION NOTED AT RIB 19. CIRCLED IN RED. VERIFIED REPAIR WAS ACCOMPLISHED IAW E0-94347-REQ1 AND EA 300-5750-27-A4024. - [SDR IPXA2025072137992](https://openairdocs.org/sdr/IPXA2025072137992.md): Rib · cracked · Jul 2, 2025 · N138UP · Airbus A300F4622R · Wing, Rib/Bulkhead > RH WING, CENTER FLAP, TOP SKIN RIB FLANGE, 2 CRACK INDICATION NOTED AT RIB 26. CIRCLED IN RED. VERIFIED REPAIR HAS BEEN ACCOMPLISHED IAW VT-MAE EA 300-5720-27-A4024 REV- AND EO-94347-REQ1. - [SDR IPXA2025071230622](https://openairdocs.org/sdr/IPXA2025071230622.md): Adapter · corroded · Jul 2, 2025 · N138UP · Airbus A300F4622R · Fuselage Miscellaneous Structure > FOUND CORROSION AT CLS ADAPTER FR77 -Y1580.5 REMOVE AND REPLACE THE FR 78 CLS ADAPTER (P/N: A53275455204) LOCATED BETWEEN -Y1221.2 AND -Y1580.5 PER AIRBUS DRAWING A53278756 REQUIREMENTS AND A300-600F SRM CHAPTER 51 REQUIREMENTS. UPS CONSIDERS THIS A MINOR REPA Next page: https://openairdocs.org/aircraft/N138UP/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 = 'N138UP' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N138UP/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.