N158UP

Service difficulty reports · 166

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 = 'N158UP' 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 IPXA2026102027627Fitting · crackedNLG UPLOCK ACTUATOR FIXTURE CRACKED. INSTALLED UPLOCK FIXTURE IAW AMM 32-31-14/401 AND 20-21-12/001.Oct 19, 2026 · N158UP · Airbus A300F4622R · Fuselage Main, Attach FittingsSDR IPXA202610051117Rib · crackedCREATED TO CAPTURE ENG STATUS AND COMPLETION FOR TASK CARD T3F18E009MQ3S. ACCOMPLISH REPAIR IN ACCORDANCE WITH EO-98679-REQ1 AND STE PNA EA 300-5753-27-A4632, REV. _.Oct 2, 2026 · N158UP · Airbus A300F4622R · Wing, Rib/BulkheadSDR IPXA2026101239996Warning Buzzer · brokenAVI CREW ENTRY DOOR, DOOR WARNING BUZZER (FINN: 11WN) IS BROKEN. REPLACED WARNING HORN (BUZZER) AND CARRIED OUT OPS CHECK GOOD IAW AMM 52-73-12/401.Oct 1, 2026 · N158UP · Airbus A300F4622R · Passenger/Crew DoorsSDR IPXA2026100639564Panel · crackedAFTER REMOVAL OF SEAL, FOUND PANEL 423BL CRACKED. INSTALLED DOUBLER ON PANEL 423BL IAW SRM 54-52-51-201-C1, PARAGRAPH D.2. STEP U, FIGURE 204.Oct 1, 2026 · N158UP · Airbus A300F4622R · Nacelle/Pylon, Main FrameSDR IPXA2026100239996Warning Buzzer · brokenAVI CREW ENTRY DOOR, DOOR WARNING BUZZER (FINN: 11WN) IS BROKEN.Oct 1, 2026 · N158UP · Airbus A300F4622R · Door Warning SystemSDR IPXA2026100181758Access Panel · crackedLEFT WING BELOW KRUGER FLAP ACCESS PANEL 513AB STRUCTURE (RING) CRACKED. INTERNAL DOUBLER WAS REMOVED AT LH WING BELOW KRUGER FLAP ACCESS PANEL 513AB IAW A300-600 SRM 51-40-21-001. INSTALLED INTERNAL DOUBLER ON LH WING BELOW KRUGER FLAP ACCESS PANEL 513AB IAW Sep 29, 2026 · N158UP · Airbus A300F4622R · Wing, Plate/SkinSDR IPXA2026092628088Angle · crackedFR 79 R/H DURING REMOVAL "Z" PROFILE FOUND ANGLE CRACKED. INSTALLED ANGLE PER SRM TASK:51-40-21-001 PAR. 6.Sep 25, 2026 · N158UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026100508332Crossbeam · brokenMDC FR 79 R/H Y2127.6 FOUND CROSS BEAM WITH CRACK. ACCOMPLISH REPAIR IN ACCORDANCE WITH EO-98797 AND STE PNA EA 300-5318-27-A4649, REV. _.Sep 24, 2026 · N158UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2026100608317Crossbeam · crackedMDC FR 79 -Y2127.6 FOUND CROSS BEAM WITH CRACK.ACCOMPLISH REPAIR IN ACCORDANCE WITH EO-98797 AND STE PNA EA 300-5318-27-A4649, REV. _.Sep 24, 2026 · N158UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2026100816052Lug · brokenRIGHT ELEVATOR ATTACH FITTING NR 2 SAFETY LUG IS BROKEN. INSTALLED NEW LOCKING PLATE PER SRM 51-40-21-001, & 55-26-11-201.Sep 24, 2026 · N158UP · Airbus A300F4622R · Elevator Miscellaneous StructureSDR IPXA2026100650463Strap · corrodedRIGHT WING FIXED TRAILING EDGE LOWER SURFACE INBD SIDE JUST OUTBD OF RT FLAP HAS SKIN BULDGING WITH INTERNAL CORROSION. REMOVED LOWER SKIN PANEL (1EA) AT R/W FIXED TRAILING EDGE FOR ACCESS IAW SRM 51-40-21. INSTALLED NEW STRAP AND RE-INSTALLED LOWER SKIN PANESep 21, 2026 · N158UP · Airbus A300F4622R · Wing Miscellaneous StructureSDR IPXA2026101639999Skin · corrodedLEFT WING UPPER SURFACE OUTBD FIXED TRAILING EDGE INBD AFT SIDE IS BULGING AROUND A FASTNER, POSSIBLE INTERNAL CORROSION. INSTALLED LANDING P/N UPA57246385200 AT LH WING IAW A300-600 SRM 51-40-21-001.Sep 20, 2026 · N158UP · Airbus A300F4622R · Wing, Plate/SkinSDR IPXA2026100101667Frame · crackedMAJOR REPAIR. CENTER FUSELAGE BASE FRAME FITTING FR44 LT HAS SIGNS OF CRACK. CRACK EXTENDS ENTIRE TOP SURFACE AND STOPS JUST PAST EDGE ON FWD SURFACE OF FRAME. ACCOMPLISHED REPAIR IAW EO 46789-JIC 7 AND EO-46789-REQ 6 (APPX J).Sep 17, 2026 · N158UP · Airbus A300F4622R · Fuselage Main, FrameSDR IPXA2026100101697Frame · crackedMAJOR REPAIR. CENTER FUSELAGE BASE FRAME FITTING FR45 LH SIDE HAS SIGNS OF CRACK. AFTER FURTHER EVALUATION FOUND CRACK LENGTH IS 0.100". ACCOMPLISHED REPAIR IAW EO 46789-JIC 7 AND EO-46789-REQ 6 (APPX J).Sep 17, 2026 · N158UP · Airbus A300F4622R · Fuselage Main, FrameSDR IPXA2026100102772Panel · crackedPANEL 423BL LOWER AREA WITH 2 CRACKS. REMOVED (IEA) SEAL AND SEAL RETAINER AT PANEL 423BL IAW SRM 51-40-21. REINSTALLED SEAL AND SEAL RETAINER AT PANEL 423BL IAW SRM 51-40-21.Sep 17, 2026 · N158UP · Airbus A300F4622R · Nacelle/Pylon, Main FrameSDR IPXA2026100101699Shear Tie · crackedMAJOR REPAIR. CENTER FUSELAGE BASE FRAME FITTING FR46 LH SIDE HAS SIGNS OF CRACK. ACCOMPLISHED EO-46789-JIC007.Sep 17, 2026 · N158UP · Airbus A300F4622R · Fuselage Internal Mounting StructureSDR IPXA2026100102793Panel · crackedPANEL 423BL EXTERNAL SURFACE WITH A CRACK. VERIFIED RECEIVED THE REPAIRED PANEL 423BL BY WELDING ON TRAVELER # T26/1879228, NOTE: THE INSTALLATION WILL BE ACCOMPLISED ON TASKCARD: T3F18E007EGD6.Sep 17, 2026 · N158UP · Airbus A300F4622R · Nacelle/Pylon, Plate/SkinSDR IPXA2026100102892Access Panel · crackedPANEL 413BL, EXTERNAL SURFACE WITH A CRACK DOT 53-024. RECEIVED THE REPAIRED PANEL 413BL BY WELDING ON TRAVELER # T26/1879227, NOTE: THE INSTALLASION WILL BE ACCOMPLISED ON TASK CARD T3F18E007EGD6.Sep 17, 2026 · N158UP · Airbus A300F4622R · Nacelle/Pylon, Plate/SkinSDR IPXA2026092801699Shear Tie · crackedMAJOR REPAIR. CENTER FUSELAGE BASE FRAME FITTING FR46 LT SIDE HAS SIGNS OF CRACK. ACCOMPLISHED THE FOLLOWING STEPS: 58 TO 63 IAW EO-46789-JIC007.Sep 17, 2026 · N158UP · Airbus A300F4622R · Fuselage Internal Mounting StructureSDR IPXA2026092801667Shear Tie · crackedMAJOR REPAIR. CENTER FUSELAGE BASE FRAME FITTING FR44 LH SIDE HAS SIGNS OF CRACK. VERIFIED C/W STEPS: 41 AND 42 OF EO-46789-JIC007 (T3F18E009P8WZ)Sep 17, 2026 · N158UP · Airbus A300F4622R · Fuselage Internal Mounting StructureSDR IPXA2026092801697Shear Tie · crackedMAJOR REPAIR. CENTER FUSELAGE BASE FRAME FITTING FR45 LH SIDE HAS SIGNS OF CRACK. ACCOMPLISHED ROTPROBPROBE INSPECTION IAW NTM 51-10-01 PART 6. CRACK TERMINATES AT STOP DRILL.Sep 17, 2026 · N158UP · Airbus A300F4622R · Fuselage Internal Mounting StructureSDR IPXA2026093076928Skin · corrodedRIGHT WING OUTBOARD FIXED TRAILING EDGE WEDGE HAS 4 SPOTS OF CORROSION. REMOVED RT WING OUTBOARD FIXED TRAILING EDGE WEDGE I.A.W. A300-600 SRM 51-40-21. INSTALLED NEW SECTION PANEL TRAILING EDGE PER SRM A300-600 TASK: 51-40-21.Sep 16, 2026 · N158UP · Airbus A300F4622R · Wing, Plate/SkinSDR IPXA2026092177194Bracket · crackedFR FROM E&E COCKPIT FLOOR STRUCTURE AT RH FR 10 HAS A CRACKED ANGLE. INSTALLED NEW ANGLE BRACKET AT E&E COCKPIT FLOOR STRUCTURE AT RH FR 10 IAW A300-600 SRM 51-40-21.Sep 16, 2026 · N158UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026092443712Bracket · crackedMAIN DECK, FLOOR BRACKET UNDER FR 79 AND Y1580 IS CRACKED. REMOVED FLOOR BRACKET WITH CRACK, IAW SRM 51-40-21. INSTALLED FLOOR BRACKET FOR MAIN DECK AT FR 79 Y1580 IAW SRM 51-40-21.Sep 14, 2026 · N158UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026092444327Web · crackedMAIN DECK, FLOOR WEB AT FR 74 AND Y2127 IS CRACKED. INSTALLED PLATE SUPPORT AT FR 74, Y2127 PER SRM 51-40-21-00A.Sep 14, 2026 · N158UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026092443777Floor Support · crackedMAIN DECK, FLOOR STRUCTURE AT FR 75 AND Y2127 IS CRACKED. INSTALLED NEW PART AT MAIN DECK, FLOOR STRUCTURE AT FR 75 AND Y2127 IAW SRM 51-40-21.Sep 14, 2026 · N158UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026101915093Fitting · crackedLEFT KEEL BEAM AT THE LEVEL OF CONNECTING FITTING BETWEEN FR13A AND 14 IN NOSE LANDING GEAR FIGURE 3, VIEW B AND C. FOUND CRACK ON FORWARD LOWER HOLE 4 O`CLOCK POSITION FACING OUTBOARD. ACCOMPLISH THE REPAIR PER EO-98843 AND STE PNA EA 300-5312-27-A4650, REV-.Sep 12, 2026 · N158UP · Airbus A300F4622R · Fuselage Main, KeelSDR IPXA2026101215031Keelbeam · crackedRIGHT KEEL BEAM AT THE LEVEL OF CONNECTING FITTING BETWEEN FR13A AND 14 IN NOSE LANDING GEAR FIGURE 3, VIEW B AND C. FOUND CRACK ON FORWARD LOWER HOLE 4&9 O`CLOCK POSITION FACING OUTBOARD. REMOVED WEB BETWEEN FR 13A AND 14 R/H SIDE OF NOSE LANDING GEAR BOX IN Sep 12, 2026 · N158UP · Airbus A300F4622R · Fuselage Main, KeelSDR IPXA2026092815031Keelbeam · crackedMAJOR REPAIR, RIGHT KEEL BEAM AT THE LEVEL OF CONNECTING FITTING BETWEEN FR13A AND 14 IN NOSE LANDING GEAR FIGURE 3, VIEW B AND C. FOUND CRACK ON FORWARD LOWER HOLE 4&9 O`CLOCK POSITION FACING OUTBOARD. AS PER REQUEST, PERFORMED EXTERNAL HFEC SURFACE INSPECTSep 12, 2026 · N158UP · Airbus A300F4622R · Fuselage Main, KeelSDR IPXA2026092815093Keelbeam · crackedMAJOR REPAIR, LEFT KEEL BEAM AT THE LEVEL OF CONNECTING FITTING BETWEEN FR13A AND 14 IN NOSE LANDING GEAR FIGURE 3, VIEW B AND C. FOUND CRACK ON FORWARD LOWER HOLE 4 O`CLOCK POSITION FACING OUTBOARD. VERIFIED REMOVAL OF L/H NLG DOOR TORQUE TUBE I.A.W. A300-6Sep 12, 2026 · N158UP · Airbus A300F4622R · Fuselage Main, KeelSDR IPXA2026101803114Skin · crackedRT WING, CENTER FLAP, TOP SKIN RIB FLANGE. 1 EA CRACK NOTED AT RIB 25. ACCOMPLISH REPAIR IN ACCORDANCE WITH EO-98679 AND EA 300-5753-27-A4632, REV-.Sep 11, 2026 · N158UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2026092605733Floor Panel · crackedMAIN DECK FLOOR STRUCTURE Z-PROFILE ON R/H SIDE AT FR 75 UNDER FLOOR PANEL 262PF IS CRACKED. INSTALLED Z PROFILE AT R/H SIDE AT FR 75 UNDER FLOOR PANEL 262PF PER SRM 51-40-21-001.Sep 11, 2026 · N158UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2026092405633Tee Angle · crackedMAIN DECK FLOOR STRUCTURE T-PROFILE ON LT SIDE AT FR 80 IS CRACKED, INSTALLED NEW PROFILE-T I.A.W. A300-600 SRM 51-40-21.Sep 11, 2026 · N158UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026092105610Profile · crackedMAIN DECK FLOOR STRUCTURE T-PROFILE ON RT SIDE AT FR 80 IS CRACKED. INSTALLED NEW T-PROFILE SRM 51-40-21-001.Sep 11, 2026 · N158UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026092823749Fairing · crackedCRACK ON #1 ENG AFT LWR PYLON FAIRING, LOWER SKIN. LOWER AFT FAIRING REMOVED AND INSTALLED ON MPC 400 T3F18E007EGD6.Sep 1, 2026 · N158UP · Airbus A300F4622R · Nacelle/Pylon, Main FrameSDR IPXA2026050302068Slide · no testESCAPE SLIDE FAILED LIGHT TEST. CLEANED AND TIGHTENED LOOSE PTT SWITCH. OPS CHECKS GOOD PER AMM 52-73-11.May 3, 2026 · N158UP · Airbus A300F4622R · Escape SlideSDR IPXA2026042352149Slide · faultedRED FLASHING DOOR SLIDE ARMED LIGHT IS FLASHING WITH SLIDE DISARMED PERFORMED OPERATIONAL CHECK OF EMERGENCY ESCAPE SLIDE WARNING LIGHT IN REFERENCE TO AMM 52-73-11. OPS CHECK GOOD. NO DMP. PLACARD REMOVED.Apr 23, 2026 · N158UP · Airbus A300F4622R · Escape SlideSDR IPXA2025081144210Power Supply · inoperativeEMERGENCY LIGHTS POWER SUPPLY UNITS FAILED BITE CHECK -ER AMM 33-51-00-0501 REF PS1 STEP 23. C/W BITE CHECK IAW AMM 33-51-00-0501, NO FAULTS FOUND, CHECK OK AT THIS TIMEAug 1, 2025 · N158UP · Airbus A300F4622R · Emergency LightingSDR IPXA202508044210Power Supply · no testEMERGENCY LIGHTS POWER SUPPLY UNITS FAILED BITE CHECK -ER AMM 33-51-00-0501 REF PS1 STEP 23 C/W BITE CHECK IAW AMM 33-51-00-0501, NO FAULTS FOUND, CHECK OK AT THIS TIMEAug 1, 2025 · N158UP · Airbus A300F4622R · Emergency LightingSDR IPXA2025031483584Coupling · leakingFUEL APPEARS TO BE MIGRATING FROM L INNER TO CENTER TANK AT 2-300LBS/HR.(1300LBS OVER 4 HR FLT.) AIRCRAFT OPERATED IN PAYLOAD, (CTR AND TRIM DEACTIVATED.) PERFORMED GVI ON LH CENTER TANK ENGINE FEED LINES IN CENTER TANK THAT GOES TO THE PUMP FOUND 2 COUPLING LMar 11, 2025 · N158UP · Airbus A300F4622R · Aircraft Fuel Distribution SystemSDR IPXA2025031283584Fuel Tank · leaking*SDR FILED OPEN* FUEL APPEARS TO BE MIGRATING FROM L INNER TO CENTER TANK AT 2-300LBS/HR.(1300LBS OVER 4 HR FLT.) AIRCRAFT OPERATED IN PAYLOAD, (CTR AND TRIM DEACTIVATED.) VERIFIED FUEL IS TRANSFERRING SLOWLY BETWEEN LEFT INNER TANK AND CENTER TANK USING LEFT Mar 11, 2025 · N158UP · Airbus A300F4622R · Fuel StorageSDR IPXA2025021309682Indicator · malfunctionedCREW DOOR, WITH DOOR OPEN AND DISARMED, FOUND WARNING LIGHT (7WN) BLINKING, NO WARNING HORN. CLEANED SWITCH 13WN AND PERF ADJ TEST IAW MM 52-10-11/501 TEST NORMAL DEFERRAL CLEARED PLAC RMVDFeb 12, 2025 · N158UP · Airbus A300F4622R · Door Warning SystemSDR IPXA2025020323495Transfer Sys · inoperativeA/C IN PAYLOAD MODE. CTR TANK FUEL 100# AT ENG START. STEADILY INCREASE DURING FLT + 1 HR AFTER T/O 700LBS +2 HRS=1000LBS +3HR+1250LBS CTR TANK. AT ENG. SHUTDOWN 1260 REVERSED MEL 28-28-26-1-1 AFTER REMOVAL AND REPLACEMENT OF CGCC IAW AMM 31-46-11 AND REMOVAL Feb 1, 2025 · N158UP · Airbus A300F4622R · Aircraft Fuel Distribution SystemSDR IPXA2025010295911Slide · warning lightMAIN ENTRY DOOR L-1 SLIDE PRESSURE INDICATION IN RED BAN L-1 DOOR ESCAPE SLIDE PRESSURE INDICATIONS CHECKS GOOD IAW AMM 25-61-20.Jan 2, 2025 · N158UP · Airbus A300F4622R · Emergency EquipmentSDR IPXA2024070218398Warning Buzzer · inoperativeEMERGENCY DOOR SLIDE BUZZER INOP REMOVED AND REPLACED ENTRY DOOR SLIDE WARNING BUZZER IAW AMM 52-73-12/401. OPS CHECK GOODJul 2, 2024 · N158UP · Airbus A300F4622R · Emergency ExitsSDR IPXA2024051574929Unknown · vibration**ATB** **SDR FILED OPEN** CLIMBING THROUGH 3500 FT EXPERIENCED HIGH VIBRATION THAT SHOOK THE A/C.WE LEVELED OFF AT 6000 AND REDUCED TO GREEN DOT. VIBRATION WENT AWAY. NO ECAM OR ABNORMAL INDICATIONS. FIBER GLASS DUST CAME OUTMay 15, 2024 · N158UP · Airbus A300F4622R · Fuselage Structure (General)SDR IPXA2024040269813Adapter · corrodedMAIN CARGO RH, FR 20, CLS ADAPTER (NEXT TO 232EF PANEL AND NEXT TO SEAT TRACK -Y1959) WITH CORROSION AND IS BROKEN. D0T 103-024 REVIEWED. REMOVED MAIN CARGO RH FR 20 CLS ADAPTER IAW A300-600 SRM 51-40-21.Mar 8, 2024 · N158UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2024040339914Seat Track · corrodedMAIN CABIN LEFT SIDE SEAT TRACK Y794 HAS CORROSION AT FR 82 15-07 REVIEWED . REMOVED SEAT TRACK Y852 FROM FR 78.5 TO FR82 IAW A300-600 SRM 53-10-16. LOCATED AND DRILLED SEAT TRACK IAW SRM 53-10-16 AND SRM 51-40-44.Mar 7, 2024 · N158UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2024040339682Seat Track · corrodedMAIN CABIN LEFT SIDE SEAT TRACK Y450 HAS CORROSION AT FR 82 15-06 REVIEWED. REMOVED SEAT TRACK Y450 FROM FR79.5 TO FR82 IAW A300-600 SRM 53-10-16. ACCOMPLISH MAJOR PERMANENT REPAIR PER SRM 53-10-16-201 PARAGRAPH 4 FIGURE 201B (REV 40).Mar 7, 2024 · N158UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2024040339480Seat Track · corrodedMAIN CABIN RIGHT SIDE SEAT TRACK -Y450 HAS CORROSION AT FR 82 15-03 REVIEWED. REMOVED SEAT TRACK -Y450 FROM FR78.5 TO FR82. IAW A300-600 SRM 53-10-16-201. TREATED AND PRIMED SEAT TRACK AND SPLICES. IAW A300-600 SRM 51-21-10.Mar 7, 2024 · N158UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings
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