N159UP

Service difficulty reports · 202

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 = 'N159UP' 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 IPXA2026082163543Bulb · burned outLAV AUX LIGHT INOPERATIVE. REPLACED LAV AUX LIGHT BULB IAW AMM 33-51-21, OPS CHECKED GOOD.Aug 21, 2026 · N159UP · Airbus A300F4622R · Passenger Compartment LightingSDR IPXA2026071688814Lock · stuckMAIN CABIN DOOR LOCK RELEASE PUSH BUTTON STUCK IN DOWN POSITION. DOOR WILL NOT STAY OPEN LOCKED POSITION. PUSHED STUCK DOOR LOCK RELEASE BUTTON. BUTTON RELEASED PROPERLY AS ADVERTISED. PERFORMED PROPER DOOR OPERATION PER AMM 52-00-00/001. DOOR STAYS OPEN AND LJul 16, 2026 · N159UP · Airbus A300F4622R · Passenger/Crew DoorsSDR IPXA2026042766665Light · inoperativeLAVATORY EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED LAVATORY AUX EMERGENCY LIGHT ASSY IAW AMM 33-51-21/401. OPS CHECK GOOD.Apr 24, 2026 · N159UP · Airbus A300F4622R · Emergency LightingSDR IPXA2026031113413Windshield Wiper · malfunctionedAIR TURN BACK, UNCOMMANDED WINDSHIELD WIPE OPERATION WITH SWITCH OFF ON CLIMB OUT EXCEEDED 230KT LIMITATION. MAX SPEED REACHED. 250 KTS. WIPER OPERATED ON DRY WINDSHIELD FOR APPROX 15 MINUTES. THIS RESULTED IN R/R 25DB PER TSM 30-45-00/101 AND ESPM 20-46-50. OMar 10, 2026 · N159UP · Airbus A300F4622R · Windshield/Door Rain/Ice RemovalSDR IPXA2025120229938Slide · obstructedON GROUND WHILE SECURING FOR FLIGHT, MAIN ENTRY DOOR SLIDE WOULD NOT ARM - LEVER WOULD NOT MOVE TO THE ARMED POSITION. UPON TROUBLESHOOTING INSPECTED L1 & MCD SEALS. NO FAULTS FOUND AT THIS TIME. FOUND L1 DOOR SLIDE EJECTOR BAG RELEASE CABLE/ QUICK DISCONNECTDec 2, 2025 · N159UP · Airbus A300F4622R · Escape SlideSDR IPXA2025072139249Bottle · dischargedL-1 DOOR EMERGENCY OPERATING CYLINDER INADVERTENTLY DISCHARGED REPLACED DIAPHRAGM, SEALS, SHEAR PIN, AND SERVICED DOOR DAMPER CYLINDER - OPS CHECKS GOOD AT THIS TIME. SAFETY PIN REMOVED IAW MM 52-10-14/301Jul 21, 2025 · N159UP · Airbus A300F4622R · Passenger/Crew DoorsSDR IPXA2025052809506Slide · malfunctionedDOOR SLIDE ONLY DISARMS WITH EXTREME FORCE LUBRICATED GIRT BAR AND SEVERAL OTHER MECHANISMS IN THE SYSTEM REF AMM 52-10-30/601 OPS CHECKS GOODMay 28, 2025 · N159UP · Airbus A300F4622R · Escape SlideSDR IPXA2025031447289Unknown · noiseVERY HIGH PITCH NOISE FROM MAIN CABIN DECK CARGO DOOR OR CREW ENTRY DOOR AREA. CABIN PRESSURE AND CABIN ALTITUDE WERE ALL NORMAL (DIFF 8.0 V/S 0, CABIN ALTITUDE 5 AT FL 320). ALL ECAM DOOR INDICATIONS PRESSURIZED A/C PER AMM 05-51-00/001. NO NOISE FROM CREW ENMar 14, 2025 · N159UP · Airbus A300F4622R · Cargo/Baggage DoorsSDR IPXA2025020608461Switch · wornIMMEDIATELY AFTER TAKEOFF "FORWARD CARGO DOOR NOT CLOSED" AND "CHECK 0001 TIMES" WHICH LED US TO COMPLETE AN AIR TURN BACK AS AIRCRAFT DIDNT SEEM TO BE PRESSURIZING. REMOVED & REPLACED DOOR WARNING SWITCH 14WS PER AMM 52-71-00/401. OPS CHECK GOOD. ADJUSTMENTFeb 6, 2025 · N159UP · Airbus A300F4622R · Door Warning SystemSDR IPXA2024090969718Handle · bindingAFTER BLOCK IN, CREW WAS UNABLE TO DISARM THE ESCAPE SLIDE. DISARM HANDLE MOVES 3/4 WAY, BUT WILL BOT FULLY DISARM. INSPECTED PASSENGER CREW ENTRY DOOR JAWS SLIDERS AND GIRT BAR TOLERANCES IAW AMM 52-10-30/601. ALL ARE WITHIN TOLERENCES. CLEANED ALL MECHANICALSep 7, 2024 · N159UP · Airbus A300F4622R · Passenger/Crew DoorsSDR IPXA2024072956769Girt Bar · fodDIFFICULTY DISARMING SLIDE. LEVER WAS CATCHING ON SOMETHING. REMOVED DEBRIS FROM GIRT BAR FITTINGS AND CLEANED AS REQUIRED. SLIDE ARMING LEVER OPS CHECKS GOOD. REF AMM 52-10-11Jul 29, 2024 · N159UP · Airbus A300F4622R · Emergency EquipmentSDR IPXA202407096961Latch · out of adjustCREW ENTRY DOOR AFT LATCH INDICATION HALF RED HALF GREEN. MADE ADUSTMENT AND PERFORMED FUNCTIONAL TEST OF FWD PASSENGER/CREW DOOR IAW AMM 52-10-11. OPS CHECK GOODJun 28, 2024 · N159UP · Airbus A300F4622R · Passenger/Crew DoorsSDR IPXA2024070106961Latch · out of positionCREW ENTRY DOOR AFT LATCH INDICATION HALF RED HALF GREEN. OPENJun 28, 2024 · N159UP · Airbus A300F4622R · Passenger/Crew DoorsSDR IPXA2024062384287Skin · crackedRT WING, UPPER SURFACE, APPROX RIB 18, HAVE A CRACK ON SKIN. DOT 103-199 INSTALLED REPAIR AS REQUIRED IAW SRM 57-51-12 PARA G FIG 207 RIVETS INSTALLED.May 28, 2024 · N159UP · Airbus A300F4622R · Wing, Plate/SkinSDR IPXA2024062623455Frame · damagedLEFT FR47 HOLE IS REAMED TO A SIZE OF .610" WITH NO DAMAGE INDICATIONS. ACCOMPLISH THE REPAIR PER EO-90513-REQ1 AND EA 300-5710-27-A3600 REV. -.May 11, 2024 · N159UP · Airbus A300F4622R · Fuselage Main, FrameSDR IPXA2024062601474Panel · damagedPANEL 131GE HAS DAMAGED EDGE SEAL . REPAIRED DAMAGE EDGE SEAL IN PANEL 131GE, I.A.W. EO NO.: A300-5320-42722-F. PANEL #131GE, WAS REPAIRED IAW EO A300-5320-42722-F. NO FURTHER ACTON REQUIRED.May 3, 2024 · N159UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2024062404353Panel · tornPANEL 132SG HAS TORN FIBERGLASS AND EDGE DAMAGE. REPAIRED FIBERGLASS BREAKS AND EDGE DAMAGE IAW EO NO: A300-5320-42722-F.May 3, 2024 · N159UP · Airbus A300F4622R · Fuselage Structure (General)SDR IPXA2024062404288Panel · tornPANEL 152QF HAS TORN FIBERGLASS AND DELAMINATED. REPAIRED TORN FIBERGLASS AND DELAMINATION OF PANEL 152QF, I.A.W. EO. A300-5320-42722-F.May 3, 2024 · N159UP · Airbus A300F4622R · Fuselage Structure (General)SDR IPXA2024062404413Floor Panel · damaged**SUPPLEMENTAL SDR** FAULT: PANEL 132G HAS FIBERGLASS DAMAGE AND EDGE DAMAGE. DOT 109/080. REPAIRED FIBERGLASS TORN AND EDGE DAMAGE IN PANEL 132 QG, IAW (SREO) EO NO: A300-5320-42722-F. REVIEWEDMay 3, 2024 · N159UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2024062104353Panel · damagedPANEL 132SG HAS TORN FIBERGLASS AND EDGE DAMAGE. DOT 109/078. REPAIRED FIBERGLASS BREAKS AND EDGE DAMAGE IAW EO NO: A300-5320-42722-F. MAJOR REPAIRMay 3, 2024 · N159UP · Airbus A300F4622R · Fuselage Structure (General)SDR IPXA2024062104288Panel · damagedPANEL 152QF HAS TORN FIBERGLASS AND DELAMINATED. DOT 109/075. REPAIRED TORN FIBERGLASS AND DELAMINATION OF PANEL 152QF, I.A.W. EO. A300-5320-42722-F. MAJOR REPAIRMay 3, 2024 · N159UP · Airbus A300F4622R · Fuselage Structure (General)SDR IPXA2024062104413Panel · damagedPANEL 132G HAS FIBERGLASS DAMAGE AND EDGE DAMAGE. DOT 109/080. REPAIRED FIBERGLASS TORN AND EDGE DAMAGE IN PANEL 132 QG, IAW (SREO) EO NO: A300-5320-42722-F. MAJOR REPAIRMay 3, 2024 · N159UP · Airbus A300F4622R · Fuselage Structure (General)SDR IPXA2024061489771Floor Panel · delaminatedFLOOR PANEL 143DF SOAKED AND DELAMINATE. FABRICATED FWD CARGO FLOOR PANEL 143DF IAW A300-5320-40552. JOB COMPLETE. REVIEWEDMay 2, 2024 · N159UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2024052092058Skin · crackedTHE L/H CENTER FLAP ASSY HAS A CRACK (1EA) AT RIB LOCATION 26, AFT SIDE. AREA MARKED IN RED. ACCOMPLISH CATEGORY A PERMANENT REPAIR PER EO-90269-REQ1 AND EA 300-5750-27-A3581 REV.Apr 26, 2024 · N159UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2024052092103Skin · crackedTHE L/H CENTER FLAP ASSY HAS A CRACK (1EA) AT RIB LOCATION 27, AFT SIDE. AREA MARKED IN RED. ACCOMPLISH CATEGORY A PERMANENT REPAIR PER EO-90269-REQ1 AND EA 300-5750-27-A3581 REV.Apr 26, 2024 · N159UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2024052075373Skin · crackedTHE R/H CENTER FLAP ASSY HAS A CRACK (1EA) AT RIB LOCATION 18 AFT SIDE. AREA MARKED IN RED. ACCOMPLISH CATEGORY A PERMANENT REPAIR PER EO-90290-REQ1 AND EA 300-5750-27-A3580 REV -.Apr 25, 2024 · N159UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2024052075328Skin · crackedTHE R/H CENTER FLAP ASSY HAS A CRACK (1EA) AT RIB LOCATION 13 AFT SIDE. AREA MARKED IN RED. ACCOMPLISH CATEGORY A PERMANENT REPAIR PER EO-90290-REQ1 AND EA 300-5750-27-A3580 REV -. MAJOR REPAIR.Apr 25, 2024 · N159UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2024052075065Skin · crackedTHE R/H CENTER FLAP ASSY HAS A CRACK (1EA) AT RIB LOCATION 12 AFT SIDE. AREA MARKED IN RED. ACCOMPLISH CATEGORY A PERMANENT REPAIR PER EO-90290-REQ1 AND EA 300-5750-27-A3580 REV.Apr 25, 2024 · N159UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2024052075380Skin · crackedTHE R/H CENTER FLAP ASSY HAS A CRACK (1EA) AT RIB LOCATION 19 AFT SIDE. AREA MARKED IN RED. ACCOMPLISH CATEGORY A PERMANENT REPAIR PER EO-90290-REQ1 AND EA 300-5750-27-A3580 REV.Apr 25, 2024 · N159UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2024052075365Skin · crackedTHE R/H CENTER FLAP ASSY HAS A CRACK (1EA) AT RIB LOCATION 17 AFT SIDE. AREA MARKED IN RED. ACCOMPLISH CATEGORY A PERMANENT REPAIR PER EO-90290-REQ1 AND EA 300-5750-27-A3580 REV.Apr 25, 2024 · N159UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2024052075478Doubler · crackedMAJOR REPAIR, THE R/H CENTER FLAP ASSY HAS A CRACK (1EA) AT RIB LOCATION 11 AFT SIDE. AREA MARKED IN RED. INSTALLED NEW REPAIR FLANGE AND REINFORCEMENT REPAIR ANGLE I.A.W. A300-600 S.R.M. 51-40-21.Apr 25, 2024 · N159UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2024052075469Skin · crackedTHE R/H CENTER FLAP ASSY HAS MULTIPLE CRACKS (2EA) AT RIB LOCATION 26 AFT & FWD SIDES. AREA MARKED IN RED. ACCOMPLISH CATEGORY A PERMANENT REPAIR PER EO-90290-REQ1 AND EA 300-5750-27-A3580 REV-.Apr 25, 2024 · N159UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2024052075428Skin · crackedTHE RT CENTER FLAP ASSY HAS A CRACK (1EA) AT RIB LOCATION 25 AFT SIDE. ACCOMPLISH CATEGORY A PERMANENT REPAIR PER EO-90290-REQ1 AND EA 300-5750-27-A3580 REV -.Apr 25, 2024 · N159UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2024062546410Inlet · crackedNR 2 ENGINE INLET COWL ANTI-ICE DUCT FLANGE IS CRACKED AT INLET COWL AFT BULKHEAD. INSTALLED INLET COWL ANTI-ICE DUCT IAW AMM 30-21-00-401.- PERFORMED LEAK TEST IAW AMM 71-00-00/501 NO LEAKS FOUND. DYE PENETRANT INSPECTION FOR THE NR 2 ENGINE INLET COWL WAS PApr 24, 2024 · N159UP · Airbus A300F4622R · Engine Air Intake SystemSDR IPXA2024061846640Bulkhead Web · damagedFAULT: #2 ENGINE INLET COWL AFT BULKHEAD IS DAMAGED AROUND I/B P-2 LINE. DOT 142-53. INSTALLED NEW WEB AND SPLICE. IAW A300-600 SRM 51-40-21. REVIEWEDApr 24, 2024 · N159UP · Airbus A300F4622R · Turbine Engine Accessory DriveSDR IPXA2024051859424Floor Panel · brokenMAIN DECK CARGO FLOOR PANEL 232WG IS BROKEN FABRICATE PNL FROM 5024N400001SS-G BACH #4055277 IAW SREO-40552-REQ001 C/WApr 24, 2024 · N159UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2024051859256Floor Panel · brokenMAIN DECK CARGO FLOOR PANEL 221CG IS BROKEN FABRICATED PNL 221CG FROM 5024N400001SS-G BACH # 4055277 IAW SREO-40552-REQ001 (APPX B) C/W.Apr 24, 2024 · N159UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2024051759338Floor Panel · brokenMAIN DECK CARGO FLOOR PANEL 232LF IS BROKEN FABRICATED PANEL FROM 5024N400001SS-G, BATCH #4055277 IAW S.R.E.O A300-5320-40552-B C/W.Apr 24, 2024 · N159UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2024053028466Cover · damagedCREW DOOR, EXTERNAL SKIN HEX COVERS DAMAGED; DOT 117-020. REMOVED AND REPLACED CREW DOOR HIST POINT COVERS IAW AMM 11-00-11/001.Apr 23, 2024 · N159UP · Airbus A300F4622R · Passenger/Crew DoorsSDR IPXA2024051738316Floor Panel · brokenRH FLOOR PANEL 252 KM BROKEN DOT 44-007 FABRICATED PANEL 252KM FROM 5024N400001SS-G, BATCH# 4055277 PER SREO A300-5320-40552--B C/W.Apr 23, 2024 · N159UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2024042328466Skin · damagedCREW DOOR, EXTERNAL SKIN HEX COVERS DAMAGED;Apr 23, 2024 · N159UP · Airbus A300F4622R · Passenger/Crew DoorsSDR IPXA2024062015716Hinge · damagedDAMAGE FOUND IN AFT HINGE OF PIANO HINGE FITTINGS (ALUMINIUM LAYER 19F, 20F, 21F, 22F, 24F, 25F, 26F) (STEEL LAYER 20D). INSTALLED NEW HINGE AT MDC DOOR AFT SECTION, IAW A300-600 SRM 51-40-21, AND SRM 51-49-00. (T89019). VERIFIED HINGE WAS INSTALLED USING EXApr 22, 2024 · N159UP · Airbus A300F4622R · Fuselage, Door HingeSDR IPXA2024061815861Support Bracket · crackedE.E COMARTMENT, FR 10 UNDER RH FLOOR OF COCKPIT (BL 7097) BRACKET SUPPORT IS CRACKED. DOT 103-33 INSTALLED WEB AND ANGLE IAW-A300-600 SRM-51-40-21.Apr 22, 2024 · N159UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2024061116226Crossbeam · mechanic errorE/E COMPARTMENT, FR16A, UNDER PANEL 121RF, DOUBLE DRILLED SCREW HOLE, BRACKET SUPPORT IS DAMAGE. INSTALLED NEW CROSSBEAM IAW SRM 51-40-21.Apr 22, 2024 · N159UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2024062596080Seat Track · corrodedSEAT TRACK BETWEEN FR79 AND FR80 HAS CORROSION AT Y0. INSTALLED NEW SEAT TRACK, U-SECCTION SPLICE (02 E/A) AND REPAIR ANGLE (01 E/A) IAW SRM 53-10-16 AND S.R.M. 51-40-21. ACCOMPLISH CATEGORY A REPAIR PER SRM REV 40 CHAPTER 53-10-16-201 PARAGRAPH 4 FIGURE 201Apr 20, 2024 · N159UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2024061296583Bracket · crackedCRACKED BRACKETS AT FWD CARGO BULKHEAD FR38.2 INNER SIDE OF AFR CARGO WALL. VERIFIED INSTALLATION OF 5 EA BRACKETS ON FWD CARGO BULKHEAD FR38.2 IAW-A300-600 SRM-51-40-21.Apr 20, 2024 · N159UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2024061296571Bracket · brokenBROKEN BRACKETS SUPPORT AT FWD CARGO BULKHEAD FR 38.2 L/H WALL (2 EA). APPLIED PROTECTIVE SURFACE TREATMENT IAW SRM 51-21-10 AND EO M-5100-2780-L REQUEST TO INSTALL. INSTALLED BRACKETS (2EA) IAW SRM A300-600 51-40-21.Apr 20, 2024 · N159UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2024061285949Skirt · crackedNR 1 ENGINE OBD T/R CENTER UPPER EDGE PYLON SIDE FWD FINGER ( SKIRT ) CRACKED. INSTALLED NEW PART EXTRUSION EDGING ON NR 1 ENGINE OBD T/R CENTER UPPER EDGE PYLON SIDE FWD. FINGER IAW SRM 51-40-21.Apr 19, 2024 · N159UP · Airbus A300F4622R · Engine Thrust ReverserSDR IPXA2024010285037Unknown · unknownATB. GEAR DID NOT RETRACT, PUT HANDLE DOWN GOT 3 GREEN T/S PER TSM 32-61-00/101, REPLACED PROXIMITY DETECTOR PROCESSING UNIT, 54GB, PER AMM 32-31-71/401; OPS CHKS GOOD, OK FOR SVCDec 28, 2023 · N159UP · Airbus A300F4622R · Landing Gear Retraction/Extension SystemSDR IPXA2023072493714Control Lever · inoperativeAFTER TO IN IAH PLACED THE GEAR LEVER IN THE "UP" POSITION. GEAR REMAINED DOWN, "L/G RETRACTION INOP" ON ECAM. MOVED GEAR LEVER TO "DOWN" POSITION CYCLED BACK TO "UP" AND GEAR EXTENDED NORMALLY IN AUS. LANDING GEAR RETRACT SYS DEFERRED PER MEL 32-30-01. DMP 32Jul 20, 2023 · N159UP · Airbus A300F4622R · Landing Gear Selector
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