N150UP

Service difficulty reports · 241

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR IPXA2026090472160Drain Line · leakingDESCENDING OUT OF FL 30500, APU AUTO SHUTDOWN. STATUS PAGE STATES APU INOP. REPLACED APU PER AMM 49-10-00/401.Sep 3, 2026 · N150UP · Airbus A300F4622R · APU Oil SystemSDR IPXA2026080511366Brake · indicationEMERGENCY 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 VALVJul 11, 2026 · N150UP · Airbus A300F4622R · Landing Gear Brake SystemSDR IPXA2026071311366Brake · indicationEMERGENCY 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/Jul 11, 2026 · N150UP · Airbus A300F4622R · Landing Gear Brake SystemSDR IPXA2026020289871Bottle · low pressureFOUND 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.Feb 2, 2026 · N150UP · Airbus A300F4622R · Passenger/Crew DoorsSDR IPXA2026011389555Skin · crackedLEFT 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 PREJan 7, 2026 · N150UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2026011389650Skin · crackedLEFT 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. -.Jan 7, 2026 · N150UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2026020976672Panel · fomREMOVE 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) DJan 6, 2026 · N150UP · Airbus A300F4622R · Wing, Plate/SkinSDR IPXA2026020976698Flap · fomREMOVE 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) DJan 6, 2026 · N150UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2025110696806Flap · damagedRIGHT 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.Oct 22, 2025 · N150UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2025102008002Flap System · faultedON 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 ROct 16, 2025 · N150UP · Airbus A300F4622R · Trailing Edge Flap Control SystemSDR IPXA2025100308219Aileron · damagedWHILE RETRACTING FLAPS- INBOARD FLAP SKEWED CAUSING DAMAGE TO RIGHT WING ALL SPEED AILERON. PERFORMED PERMANENT REPAIR IAW EO-95289.Sep 30, 2025 · N150UP · Airbus A300F4622R · AileronsSDR IPXA2025021380676Fitting · gougedLOWER FUSELAGE, TAIL JACK FITTING HAS GOUGES. DOT 103-133C. INSTALLED JACK POINT BALL IAW A-300 AMM 20-21-12/001.Feb 11, 2025 · N150UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2025021446485Fairing · damagedFAIRING # 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.Feb 8, 2025 · N150UP · Airbus A300F4622R · Nacelle/Pylon StructureSDR IPXA20250219327Door Seal · torn**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 PRFeb 7, 2025 · N150UP · Airbus A300F4622R · Passenger/Crew DoorsSDR IPXA2025021825288Skin · gougedFAULT-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). REVIEWEDFeb 7, 2025 · N150UP · Airbus A300F4622R · Fuselage Main, Plate/SkinSDR IPXA2025021725369Skin · gougedL1 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. NOFeb 7, 2025 · N150UP · Airbus A300F4622R · Passenger/Crew DoorsSDR IPXA2025021025369Skin · gougedL1 CREW DOOR EXTERNAL LOWER SKIN HAS GOUGES .89-25 PERFORMED HFEC ON BLENDED AREA. NO DEFECTS FOUND. IAW NTM 51-10-08 PART 6. T96524Feb 7, 2025 · N150UP · Airbus A300F4622R · Passenger/Crew DoorsSDR IPXA2025021025327Door Seal · torn**SDR FILED OPEN** FAULT , 52-10, APG = L1 CREW DOOR SEAL HAS TORN AT PLACES . 89-24 APPROVED.Feb 7, 2025 · N150UP · Airbus A300F4622R · Passenger/Crew DoorsSDR IPXA2025021411890Landing · damagedFAULT: 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 PFeb 6, 2025 · N150UP · Airbus A300F4622R · Wing Main, Frame StructureSDR IPXA2025021570871Support · corrodedAFT 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 Feb 4, 2025 · N150UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2025021170871Support · corrodedOPEN. 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: 0004233085Feb 4, 2025 · N150UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2024082743509Vane · gougedR/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.Aug 25, 2024 · N150UP · Airbus A300F4622R · Leading Edge DevicesSDR IPXA2024082643652Skin · gougedGOUGED 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 51-75-10Aug 25, 2024 · N150UP · Airbus A300F4622R · Leading Edge DevicesSDR IPXA2024082643509Vane · gougedR/H KRUEGER FLAP MOVABLE VANE SKIN GOUGEDAug 25, 2024 · N150UP · Airbus A300F4622R · Leading Edge DevicesSDR IPXA2024082643615Intercostal · crackedFOUND CRACKED INTERCOSTAL , NEAR R/H KRUEGER FLAP, RETRACT STOP R/R INTERCOSTAL IAW SRM 51-40-21.Aug 25, 2024 · N150UP · Airbus A300F4622R · Leading Edge DevicesSDR IPXA2024082734194Panel · damagedRT. KRUEGER FLAP PANEL P/N A 5351020701101 DAMAGED. RETRACTS BEYOND FLUSH. VERIFIED AND WITNESSED INSTALLATION OF R/H WING KRUEGER FLAP PER A300 AMM 27-87-11-0401Aug 24, 2024 · N150UP · Airbus A300F4622R · Leading Edge DevicesSDR IPXA2024082634194Panel · damaged*SDR FILED OPEN* RT. KRUEGER FLAP PANEL P/N A 5351020701101 DAMAGED. RETRACTS BEYOND FLUSH.Aug 24, 2024 · N150UP · Airbus A300F4622R · Leading Edge DevicesSDR IPXA2024071735650Windshield · crackedL/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.Jul 16, 2024 · N150UP · Airbus A300F4622R · Flight Compartment WindowsSDR IPXA2024030565124Power Supply · no test*SUPPLEMENTAL SDR* ASPSU FAILED OPS TEST R&R ASPSU 70WN PER A300 AMM 52-73-18, OPS CK GOOD.Mar 2, 2024 · N150UP · Airbus A300F4622R · DoorsSDR IPXA2024030465124Power Supply · no test*SDR FILED OPEN* ASPSU FAILED OPS TESTMar 2, 2024 · N150UP · Airbus A300F4622R · DoorsSDR IPXA2024012413312Fairing · puncturedL/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 COMPJan 24, 2024 · N150UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2024011648167Bottle · emptyDOOR 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, PLAJan 16, 2024 · N150UP · Airbus A300F4622R · Emergency EquipmentSDR IPXA2023110644897Skin · damagedGOUGE 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 .Nov 6, 2023 · N150UP · Airbus A300F4622R · Cargo/Baggage DoorsSDR IPXA2023081893955Light · unsecureLAVATORY MIRROR LIGHT NOT SECURED. LENS COVER ALSO DETACHED.REINSTALLED LAVATORY LIGHT IAW AMM 33-51-21. OPS CHECK GOOD.Aug 17, 2023 · N150UP · Airbus A300F4622R · Passenger Compartment LightingSDR IPXA2022121989142None · noneDOOR 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 M798263Dec 19, 2022 · N150UP · Airbus A300F4622R · Emergency EquipmentSDR IPXA2022080684966Support Bracket · brokenINSPECTION TYPE:SEGENG 1 O/B COWL CIRCUNFERENTIAL LATCH UPPER BRACKET IS BROKEN.REMOVED AND REPLACED IAW SRM 51-40-21.Aug 6, 2022 · N150UP · Airbus A300F4622R · Crew Oxygen SystemSDR IPXA2022080684971Annular Shell · crackedINSPECTION TYPE:SEG#1 ENGINE TR I/B LOCK INDICATOR ANGLE IS CRACKREMOVED AND REPLACED PER SRM 51-40-21Aug 6, 2022 · N150UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2022080584950Flap · crackedINSPECTION TYPE:SEGPANEL 143CL LEADING EDGE IS CRACK.REMOVED AND REPLACED IAW SRM 51-40-21.Aug 5, 2022 · N150UP · Airbus A300F4622R · Aerodynamic FairingsSDR IPXA2022080484918Shear Web · crackedINSPECTION TYPE:SEGMAIN DECK RH SIDE PLATE BETWEEN FR 77 AND FR78 CRACKED.REMOVED AND REPLACED PER SRM 51-40-21.Aug 4, 2022 · N150UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2022080484917Shear Web · crackedINSPECTION TYPE:SEGMAIN DECK RH SIDE PLATE BETWEEN FR 77 AND FR78 IS CRACKED.REMOVED AND REPLACED PER SRM 51-40-21.Aug 4, 2022 · N150UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2022080384861Floor Panel · damagedINSPECTION TYPE:SEGPNL 232ZG DAMAGEFABBED IAW SRTEO A300-5320-40552-BJul 28, 2022 · N150UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2022072884652Crossbeam · bentINSPECTION 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.Jul 28, 2022 · N150UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2022072884651Crossbeam · bentINSPECTION 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.Jul 28, 2022 · N150UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2022072884650Panel · crackedINSPECTION TYPE:SEGPRECOOLER PANEL 413BL HAS 1EA CRACK ON LOWER CORNER.ACCOMPLISHED DOUBLER REPAIR PER SRM 54-52-51 FIG 205.Jul 28, 2022 · N150UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2022072884653Crossbeam · bentINSPECTION 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.Jul 28, 2022 · N150UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2022072784616Door Track · crackedINSPECTION TYPE:SEGRH PYLON O/B SIDE ACCESS PANEL 424ER CRACKED.WELD REPAIR PER SRM 54-50-00Jul 27, 2022 · N150UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2022072784615Panel · crackedINSPECTION TYPE:SEGPRECOOLER PANEL 413BL HAS 1EA CRACK ON VENT GRILLS.ACCOMPLISHED WELD REPAIR PER SRM 54-52-51Jul 27, 2022 · N150UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2022072784614Panel · crackedINSPECTION TYPE:SEGPRECOOLER PANEL 423BL HAS 2EA CRACKS ON VENT GRILLS.ACCOMPLISHED WELD REPAIR PER SRM 54-52-51Jul 27, 2022 · N150UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2022080484912Floor Panel · brokenINSPECTION TYPE:SEG**SUPPLEMENTAL SDR**COCKPIT FLOOR PANEL 211HP IS BROKEN (REAR CORNER)REPAIRED FLOOR PANEL 211HP IAW EO A300-5320-42722-FJul 25, 2022 · N150UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2022080484911Floor Panel · crackedINSPECTION TYPE:SEG**SUPPLEMENTAL SDR**MAIN CARGO COMPARTMENT FLOOR PANEL 252KM CRACKEDREPAIRED FLOOR PANEL 252KM IAW EO A300-5320-42722-FJul 25, 2022 · N150UP · Airbus A300F4622R · Fuselage Floor Panel
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