# Service difficulty reports: N150UP A list on [N150UP](https://openairdocs.org/aircraft/N150UP.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 · 241 reports - [SDR IPXA2026090472160](https://openairdocs.org/sdr/IPXA2026090472160.md): Drain Line · leaking · Sep 3, 2026 · N150UP · Airbus A300F4622R · APU Oil System > DESCENDING OUT OF FL 30500, APU AUTO SHUTDOWN. STATUS PAGE STATES APU INOP. REPLACED APU PER AMM 49-10-00/401. - [SDR IPXA2026080511366](https://openairdocs.org/sdr/IPXA2026080511366.md): Brake · indication · Jul 11, 2026 · N150UP · Airbus A300F4622R · Landing Gear Brake System > EMERGENCY DECLARED, UPON LOWERING THE GEAR FOR LANDING, BRAKE RELEASE SIGNAL FOR WHEELS 5 & 8 WAS MISSING. CYCLED THE ANTI-SKID SWITCH & ELECTED TO FOLLOW ANTI-SKID FAULT CHKLIST. RELEASE SIGNAL FOR WHEEL 6 ALSO DISAPP, CHECKED RESISTANCE FOR BRAKE SERVO VALV - [SDR IPXA2026071311366](https://openairdocs.org/sdr/IPXA2026071311366.md): Brake · indication · Jul 11, 2026 · N150UP · Airbus A300F4622R · Landing Gear Brake System > EMERGENCY DECLARED, UPON LOWERING THE GEAR FOR LANDING, BRAKE RELEASE SIGNAL FOR WHEELS 5 & 8 WAS MISSING. CYCLED THE ANTI-SKID SWITCH AND ELECTED TO FOLLOW ANTISKID FAULT CHECKLIST. REPLACED BSCU (29GG) IAW AMM 32-42-72/401 OPS CHECKS NORMAL PER AMM 32-42-00/ - [SDR IPXA2026020289871](https://openairdocs.org/sdr/IPXA2026020289871.md): Bottle · low pressure · Feb 2, 2026 · N150UP · Airbus A300F4622R · Passenger/Crew Doors > FOUND L1 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER NO AIR PRESSURE. REPLACED LEAKING DIAPHRAGM AND SEALS REF MM 52-10-14. SERVICED WITH NITROGEN. LEAK CKD GOOD. THIS CLEARS DEFERRAL. - [SDR IPXA2026011389555](https://openairdocs.org/sdr/IPXA2026011389555.md): Skin · cracked · Jan 7, 2026 · N150UP · Airbus A300F4622R · Trailing Edge Flaps > LEFT WING, CENTER FLAP, TOP SKIN RIB FLANGE; 3 CRACKS NOTED AT RIB27. CIRCLED IN RED. REAMED DAMAGED SHEARED FASTENER HOLE FROM 0.156" TO 0.187" IAW A300 SRM 51-40-44. OK TO INSTALL REPAIR PARTS GIVEN. COMPLIED WITH STEP 4 E OF E.A.#: 300-5753-27-A4260 PRE - [SDR IPXA2026011389650](https://openairdocs.org/sdr/IPXA2026011389650.md): Skin · cracked · Jan 7, 2026 · N150UP · Airbus A300F4622R · Trailing Edge Flaps > LEFT WING, CENTER FLAP, TOP SKIN RIB FLANGE; 3 CRACKS NOTED AT RIB26. ACCOMPLISHED REPAIR IN ACCORDANCE WITH EO-96213-REQ1 AND VT-MAE EA 300-5753-27-A4260, REV. -. - [SDR IPXA2026020976672](https://openairdocs.org/sdr/IPXA2026020976672.md): Panel · fom · Jan 6, 2026 · N150UP · Airbus A300F4622R · Wing, Plate/Skin > REMOVE 633BB, 634BB, 633AT, AND 634AT TO FOM. REMOVED RT WING FAIRINGS 633BB, 634BB, 633AT, AND 634AT IAW AMM 27-50-21-401, INSTALLED PANELS 633AT AND 634AT IAW AMM 27-50-21/401, STEP 3B, (6) D - [SDR IPXA2026020976698](https://openairdocs.org/sdr/IPXA2026020976698.md): Flap · fom · Jan 6, 2026 · N150UP · Airbus A300F4622R · Trailing Edge Flaps > REMOVE RIGHT WING CENTER FLAP TO FOM. REMOVED RT WING MOVABLE FAIRING 633BB,634BB IAW AMM 27-50-21/401 INTALLED PANELS 533AT AND 534AT IAW AMM 27-50-21/401 STEP 3B (6) D - [SDR IPXA2025110696806](https://openairdocs.org/sdr/IPXA2025110696806.md): Flap · damaged · Oct 22, 2025 · N150UP · Airbus A300F4622R · Trailing Edge Flaps > RIGHT NR 1 FLAP DAMAGED, APPROX 74 INCHES FROM INBOARD EDGE AND 16 INCHES FROM TRAILING EDGE. INSTALLED REPAIR DOUBLERSEALED WITH P/N 1440B1-2AM654SK (PO/RO # SP2843294) PER EO-95513-REQ3. - [SDR IPXA2025102008002](https://openairdocs.org/sdr/IPXA2025102008002.md): Flap System · faulted · Oct 16, 2025 · N150UP · Airbus A300F4622R · Trailing Edge Flap Control System > ON APPROACH RECEIVED FLAPS SYS 1&2 FAULT. FLAPS WOULD GO TO 20 THEN COMEBACK UP A FEW DEGREES AND THEN GIVE A JAM INDICATION OF FLAP SYS 1&2 FAULT. ++REPLACED #4 JACKSCREW PER AMM 27-54-24-401. OPS CHECK GOOD. VERIFIED AND WITNESSED #4 JACKSCREW INSTALLATION R - [SDR IPXA2025100308219](https://openairdocs.org/sdr/IPXA2025100308219.md): Aileron · damaged · Sep 30, 2025 · N150UP · Airbus A300F4622R · Ailerons > WHILE RETRACTING FLAPS- INBOARD FLAP SKEWED CAUSING DAMAGE TO RIGHT WING ALL SPEED AILERON. PERFORMED PERMANENT REPAIR IAW EO-95289. - [SDR IPXA2025021380676](https://openairdocs.org/sdr/IPXA2025021380676.md): Fitting · gouged · Feb 11, 2025 · N150UP · Airbus A300F4622R · Fuselage Main, Structure > LOWER FUSELAGE, TAIL JACK FITTING HAS GOUGES. DOT 103-133C. INSTALLED JACK POINT BALL IAW A-300 AMM 20-21-12/001. - [SDR IPXA2025021446485](https://openairdocs.org/sdr/IPXA2025021446485.md): Fairing · damaged · Feb 8, 2025 · N150UP · Airbus A300F4622R · Nacelle/Pylon Structure > FAIRING # 485 AL HAS CRACK AT LH SIDE AFT SECTION. 89-29. INSTALLED MISSING BLIND RIVET ON AFT LOWER EXTERNAL SKIN AT RIGHT SIDE AND LEFT SIDE OF THE #2 ENGINE PYLON PANEL #485AL IAW SRM 51-40-21. - [SDR IPXA20250219327](https://openairdocs.org/sdr/IPXA20250219327.md): Door Seal · torn · Feb 7, 2025 · N150UP · Airbus A300F4622R · Passenger/Crew Doors > **SUPPLEMENTAL SDR** FAULT, 52-10, APG = L1 CREW DOOR SEAL HAS TORN AT PLACES. 89-24. REMOVED AND REPLACED CREW DOOR SEAL, P/N: F5218135620000, BTCH:0004352794,I.A.W A300-AMM 52-11-11/401, SRM 51-40-21 PARAGRAPH 5. PRESSURIZATION CHECK REQUIRED. PERFORMED PR - [SDR IPXA2025021825288](https://openairdocs.org/sdr/IPXA2025021825288.md): Skin · gouged · Feb 7, 2025 · N150UP · Airbus A300F4622R · Fuselage Main, Plate/Skin > FAULT-MXP-ZL-300-01-1-300JIC - STRS ZONE 180. TAIL JACK POINT HAS DAMAGE ON THE DOUBLER AND SKIN AFT OF THE DOUBLER. ACCOMPLISH THE PERMANENT REPAIR PER SRM 53-10-12-201 PARAGRAPH 13 FIGURE 210 (REV. 41). REVIEWED - [SDR IPXA2025021725369](https://openairdocs.org/sdr/IPXA2025021725369.md): Skin · gouged · Feb 7, 2025 · N150UP · Airbus A300F4622R · Passenger/Crew Doors > L1 CREW DOOR EXTERNAL LOWER SKIN HAS GOUGES.89-25. BLENDED AREA IAW-A300-SRM-51-73-10. MAX DEPTH WAS.003 (T04010) FOUND TO BE WITHIN LIMITS IAW-A300SRM-52-11-00. FIGURE 102. ORIGINAL THICKNES.09 REMAINING MATERIAL.0897. PERFORMED HFEC ON BLENDED AREA. NO - [SDR IPXA2025021025369](https://openairdocs.org/sdr/IPXA2025021025369.md): Skin · gouged · Feb 7, 2025 · N150UP · Airbus A300F4622R · Passenger/Crew Doors > L1 CREW DOOR EXTERNAL LOWER SKIN HAS GOUGES.89-25 PERFORMED HFEC ON BLENDED AREA. NO DEFECTS FOUND. IAW NTM 51-10-08 PART 6. T96524 - [SDR IPXA2025021025327](https://openairdocs.org/sdr/IPXA2025021025327.md): Door Seal · torn · Feb 7, 2025 · N150UP · Airbus A300F4622R · Passenger/Crew Doors > **SDR FILED OPEN** FAULT, 52-10, APG = L1 CREW DOOR SEAL HAS TORN AT PLACES. 89-24 APPROVED. - [SDR IPXA2025021411890](https://openairdocs.org/sdr/IPXA2025021411890.md): Landing · damaged · Feb 6, 2025 · N150UP · Airbus A300F4622R · Wing Main, Frame Structure > FAULT: Z500-STR-L/WING UNDER KRUEGER L/E PANEL AFT AREA HAS SEVERAL NICKS (9EA MARKED IN RED). DOT 34-022. REMOVED FLANGE (LANDING) FROM LH WING KRUEGER WITH SEVERAL NICKS 9(EA) AND REPLACED WITH A NEW ONE P/N A5724200920000, BATCH 0004365682 USING FASTENERS P - [SDR IPXA2025021570871](https://openairdocs.org/sdr/IPXA2025021570871.md): Support · corroded · Feb 4, 2025 · N150UP · Airbus A300F4622R · Fuselage Miscellaneous Structure > AFT CARGO CEILING SUPPORT AT FR 54 HAS 1(EA) FASTENER HOLE WITH CORROSION DOT 07586-01. REMOVE AND REPLACE 1 EACH SUPPORT (P/N: A53410767204) PER PRODUCTION DRAWING REQUIREMENTS AND SRM CHAPTER 51 REQUIREMENTS. USE ORIGINAL PART AS SAMPLE IN ACCORDANCE WITH - [SDR IPXA2025021170871](https://openairdocs.org/sdr/IPXA2025021170871.md): Support · corroded · Feb 4, 2025 · N150UP · Airbus A300F4622R · Fuselage Miscellaneous Structure > OPEN. AFT CARGO CEILING SUPPORT AT FR 54 HAS 1(EA) FASTENER HOLE WITH CORROSION DOT 07586-01 INSTALLED SUPPORT IAW A300 SRM 51-40-21. PN: CCR264SS3-04, BN: 0004364298 MS20426AD5-9, BN: 0004233085 - [SDR IPXA2024082743509](https://openairdocs.org/sdr/IPXA2024082743509.md): Vane · gouged · Aug 25, 2024 · N150UP · Airbus A300F4622R · Leading Edge Devices > R/H KRUEGER FLAP MOVABLE VANE SKIN GOUGED CLEANED AREA ON KRUEGER FLAP SKIN AND APPLIED TOPCOAT I/A/W AIRBUS A300-600 SRM 51-73-10-201, 51-75-10. - [SDR IPXA2024082643652](https://openairdocs.org/sdr/IPXA2024082643652.md): Skin · gouged · Aug 25, 2024 · N150UP · Airbus A300F4622R · Leading Edge Devices > GOUGED SKIN ON R/H WING LWR SKIN,AFT SIDE OF R/H KRUEGER FLAP CUTOUT FOUND SKIN DAMAGE ON RT WING LWR SKIN AFT SIDE OF KRUEGER FLAP CUT OUT WAS FOUND TO BE IN TOP COAT ONLY. RESTORED FINISH IAW SRM 51-75-10 - [SDR IPXA2024082643509](https://openairdocs.org/sdr/IPXA2024082643509.md): Vane · gouged · Aug 25, 2024 · N150UP · Airbus A300F4622R · Leading Edge Devices > R/H KRUEGER FLAP MOVABLE VANE SKIN GOUGED - [SDR IPXA2024082643615](https://openairdocs.org/sdr/IPXA2024082643615.md): Intercostal · cracked · Aug 25, 2024 · N150UP · Airbus A300F4622R · Leading Edge Devices > FOUND CRACKED INTERCOSTAL, NEAR R/H KRUEGER FLAP, RETRACT STOP R/R INTERCOSTAL IAW SRM 51-40-21. - [SDR IPXA2024082734194](https://openairdocs.org/sdr/IPXA2024082734194.md): Panel · damaged · Aug 24, 2024 · N150UP · Airbus A300F4622R · Leading Edge Devices > RT. KRUEGER FLAP PANEL P/N A 5351020701101 DAMAGED. RETRACTS BEYOND FLUSH. VERIFIED AND WITNESSED INSTALLATION OF R/H WING KRUEGER FLAP PER A300 AMM 27-87-11-0401 - [SDR IPXA2024082634194](https://openairdocs.org/sdr/IPXA2024082634194.md): Panel · damaged · Aug 24, 2024 · N150UP · Airbus A300F4622R · Leading Edge Devices > *SDR FILED OPEN* RT. KRUEGER FLAP PANEL P/N A 5351020701101 DAMAGED. RETRACTS BEYOND FLUSH. - [SDR IPXA2024071735650](https://openairdocs.org/sdr/IPXA2024071735650.md): Windshield · cracked · Jul 16, 2024 · N150UP · Airbus A300F4622R · Flight Compartment Windows > L/1 WINDSHIELD CRACKED R&R LH WINDSHIELD IAW A300 AMM 56-11-11. R&R #1 WINDOW TEMP REGULATOR AS PRECAUTION TO DUE WINDSHIELD CRACKING DUE TO HEAT STRESS IAW A300 30-42-11. OPS CHECK NORMAL. - [SDR IPXA2024030565124](https://openairdocs.org/sdr/IPXA2024030565124.md): Power Supply · no test · Mar 2, 2024 · N150UP · Airbus A300F4622R · Doors > *SUPPLEMENTAL SDR* ASPSU FAILED OPS TEST R&R ASPSU 70WN PER A300 AMM 52-73-18, OPS CK GOOD. - [SDR IPXA2024030465124](https://openairdocs.org/sdr/IPXA2024030465124.md): Power Supply · no test · Mar 2, 2024 · N150UP · Airbus A300F4622R · Doors > *SDR FILED OPEN* ASPSU FAILED OPS TEST - [SDR IPXA2024012413312](https://openairdocs.org/sdr/IPXA2024012413312.md): Fairing · punctured · Jan 24, 2024 · N150UP · Airbus A300F4622R · Trailing Edge Flaps > L/H WING I/B FLAP, I/B AFT FLAP TRACK FAIRING O/B SIDE 30" FROM AFT END HAS 2"X2" DENT WITH 1/2" PUNCTURE. REMOVED DAMAGE AS NEEDED. FABRICATED NEW CORE PLUG AND INSTALLED WITH ADHESIVE PER SRM 57-20-35, CURED AS REQUIRED. REPAIRED PER SRM 57-20-35. CURE COMP - [SDR IPXA2024011648167](https://openairdocs.org/sdr/IPXA2024011648167.md): Bottle · empty · Jan 16, 2024 · N150UP · Airbus A300F4622R · Emergency Equipment > DOOR BOTTLE PRESSSURE IS AT 0 PSI REVERSED DMP IAW MEL 52-11-01-2-4, SERVICED FWD DOOR (L1) DAMPER AND EMERGENCY OPERATION CYLINDER IAW AMM 52-10-14/301 PARA 3 D (F) TO OPERATION PRESSURE INDICATED ON PLACARD ON SUPPORT ARM LINNING, THIS ACTION CLEARS DMI, PLA - [SDR IPXA2023110644897](https://openairdocs.org/sdr/IPXA2023110644897.md): Skin · damaged · Nov 6, 2023 · N150UP · Airbus A300F4622R · Cargo/Baggage Doors > GOUGE AFT SIDE OF AFT CARGO DOOR CUTOUT APROX. 20" FROM LOWER CORNER. AFTER FURTHER INVESTIGATION DAMAGED AREA FOUND TO BE WITHIN LIMITS IAW SRM 53-17-12. NO FURTHER DAMAGE NOTED AT THIS TIME. DAMAGE LENGTH 2.5 INCHES BLEND DEPTH REMAINING THICKNESS.152. - [SDR IPXA2023081893955](https://openairdocs.org/sdr/IPXA2023081893955.md): Light · unsecure · Aug 17, 2023 · N150UP · Airbus A300F4622R · Passenger Compartment Lighting > LAVATORY MIRROR LIGHT NOT SECURED. LENS COVER ALSO DETACHED.REINSTALLED LAVATORY LIGHT IAW AMM 33-51-21. OPS CHECK GOOD. - [SDR IPXA2022121989142](https://openairdocs.org/sdr/IPXA2022121989142.md): None · none · Dec 19, 2022 · N150UP · Airbus A300F4622R · Emergency Equipment > DOOR SLIDE ACCUMULATOR PRESSURE IN RED BAND.C/W INSPECTION /CHECK OF DUAL ESCAPE SLIDE OF L1 DOOR INFLATION RESERVOIR PRESSURE IAW AMM 25-61-20-06-01. FOUND TO BE NORMAL AND SERVICEABLE. THIS CLEARS M798263 - [SDR IPXA2022080684966](https://openairdocs.org/sdr/IPXA2022080684966.md): Support Bracket · broken · Aug 6, 2022 · N150UP · Airbus A300F4622R · Crew Oxygen System > INSPECTION TYPE:SEGENG 1 O/B COWL CIRCUNFERENTIAL LATCH UPPER BRACKET IS BROKEN.REMOVED AND REPLACED IAW SRM 51-40-21. - [SDR IPXA2022080684971](https://openairdocs.org/sdr/IPXA2022080684971.md): Annular Shell · cracked · Aug 6, 2022 · N150UP · Airbus A300F4622R · Fuselage Main, Structure > INSPECTION TYPE:SEG#1 ENGINE TR I/B LOCK INDICATOR ANGLE IS CRACKREMOVED AND REPLACED PER SRM 51-40-21 - [SDR IPXA2022080584950](https://openairdocs.org/sdr/IPXA2022080584950.md): Flap · cracked · Aug 5, 2022 · N150UP · Airbus A300F4622R · Aerodynamic Fairings > INSPECTION TYPE:SEGPANEL 143CL LEADING EDGE IS CRACK.REMOVED AND REPLACED IAW SRM 51-40-21. - [SDR IPXA2022080484918](https://openairdocs.org/sdr/IPXA2022080484918.md): Shear Web · cracked · Aug 4, 2022 · N150UP · Airbus A300F4622R · Fuselage Main, Structure > INSPECTION TYPE:SEGMAIN DECK RH SIDE PLATE BETWEEN FR 77 AND FR78 CRACKED.REMOVED AND REPLACED PER SRM 51-40-21. - [SDR IPXA2022080484917](https://openairdocs.org/sdr/IPXA2022080484917.md): Shear Web · cracked · Aug 4, 2022 · N150UP · Airbus A300F4622R · Fuselage Main, Structure > INSPECTION TYPE:SEGMAIN DECK RH SIDE PLATE BETWEEN FR 77 AND FR78 IS CRACKED.REMOVED AND REPLACED PER SRM 51-40-21. - [SDR IPXA2022080384861](https://openairdocs.org/sdr/IPXA2022080384861.md): Floor Panel · damaged · Jul 28, 2022 · N150UP · Airbus A300F4622R · Fuselage Miscellaneous Structure > INSPECTION TYPE:SEGPNL 232ZG DAMAGEFABBED IAW SRTEO A300-5320-40552-B - [SDR IPXA2022072884652](https://openairdocs.org/sdr/IPXA2022072884652.md): Crossbeam · bent · Jul 28, 2022 · N150UP · Airbus A300F4622R · Fuselage Main, Structure > INSPECTION TYPE:SEGMAIN DECK CARGO FLOOR CROSSBEAM AT FR50 BETWEEN Y450 AND Y953 IS BENT.REMOVED AND REPLACED CROSSBEAM PER UPS EO A300-5310-75878-B. - [SDR IPXA2022072884651](https://openairdocs.org/sdr/IPXA2022072884651.md): Crossbeam · bent · Jul 28, 2022 · N150UP · Airbus A300F4622R · Fuselage Main, Structure > INSPECTION TYPE:SEGMAIN DECK CARGO FLOOR CROSSBEAM AT FR48 BETWEEN Y450 AND Y953 IS BENT.REMOVED AND REPLACED CROSSBEAM PER UPS EO A300-5310-75878-B. - [SDR IPXA2022072884650](https://openairdocs.org/sdr/IPXA2022072884650.md): Panel · cracked · Jul 28, 2022 · N150UP · Airbus A300F4622R · Fuselage Main, Structure > INSPECTION TYPE:SEGPRECOOLER PANEL 413BL HAS 1EA CRACK ON LOWER CORNER.ACCOMPLISHED DOUBLER REPAIR PER SRM 54-52-51 FIG 205. - [SDR IPXA2022072884653](https://openairdocs.org/sdr/IPXA2022072884653.md): Crossbeam · bent · Jul 28, 2022 · N150UP · Airbus A300F4622R · Fuselage Main, Structure > INSPECTION TYPE:SEGMAIN DECK CARGO FLOOR CROSSBEAM AT FR49 BETWEEN Y450 AND Y953 IS BENT.REMOVED AND REPLACED CROSSBEAM PER UPS EO A300-5310-75878-B. - [SDR IPXA2022072784616](https://openairdocs.org/sdr/IPXA2022072784616.md): Door Track · cracked · Jul 27, 2022 · N150UP · Airbus A300F4622R · Fuselage Main, Structure > INSPECTION TYPE:SEGRH PYLON O/B SIDE ACCESS PANEL 424ER CRACKED.WELD REPAIR PER SRM 54-50-00 - [SDR IPXA2022072784615](https://openairdocs.org/sdr/IPXA2022072784615.md): Panel · cracked · Jul 27, 2022 · N150UP · Airbus A300F4622R · Fuselage Main, Structure > INSPECTION TYPE:SEGPRECOOLER PANEL 413BL HAS 1EA CRACK ON VENT GRILLS.ACCOMPLISHED WELD REPAIR PER SRM 54-52-51 - [SDR IPXA2022072784614](https://openairdocs.org/sdr/IPXA2022072784614.md): Panel · cracked · Jul 27, 2022 · N150UP · Airbus A300F4622R · Fuselage Main, Structure > INSPECTION TYPE:SEGPRECOOLER PANEL 423BL HAS 2EA CRACKS ON VENT GRILLS.ACCOMPLISHED WELD REPAIR PER SRM 54-52-51 - [SDR IPXA2022080484912](https://openairdocs.org/sdr/IPXA2022080484912.md): Floor Panel · broken · Jul 25, 2022 · N150UP · Airbus A300F4622R · Fuselage Floor Panel > INSPECTION TYPE:SEG**SUPPLEMENTAL SDR**COCKPIT FLOOR PANEL 211HP IS BROKEN (REAR CORNER)REPAIRED FLOOR PANEL 211HP IAW EO A300-5320-42722-F - [SDR IPXA2022080484911](https://openairdocs.org/sdr/IPXA2022080484911.md): Floor Panel · cracked · Jul 25, 2022 · N150UP · Airbus A300F4622R · Fuselage Floor Panel > INSPECTION TYPE:SEG**SUPPLEMENTAL SDR**MAIN CARGO COMPARTMENT FLOOR PANEL 252KM CRACKEDREPAIRED FLOOR PANEL 252KM IAW EO A300-5320-42722-F Next page: https://openairdocs.org/aircraft/N150UP/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 = 'N150UP' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N150UP/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.