N125UP

Service difficulty reports · 297

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 = 'N125UP' 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 IPXA2026082508532Slide · unwanted deploySLIDE DEPLOYED L1 DOOR SLIDE PLACED ON MEL 52-11-01-2-3, PLACARD INSTALLED, DI LOG UPDATED. DMP COMPLIED WIITH. (SLIDE REMOVED). VERIFIED SAFETY PIN REMOVED AND PRESSURE ON SLIDE IAW GMM 04-02.Aug 25, 2026 · N125UP · Airbus A300F4622R · Escape SlideSDR IPXA2026072435588Bulb · inoperativeLAV AUX LIGHT INOP REMOVED AND REPLACED LAV AUX LIGHT BULB REF AMM 33-51-21, OPS CHECK GOOD.Jul 24, 2026 · N125UP · Airbus A300F4622R · Passenger Compartment LightingSDR IPXA2026050399528Stop · brokenWHILE ATTEMPTING TO ROB THE MAIN ENTRY DOOR EXTERIOR DOOR HANDLE LEVER STOP, IT BROKE. INSTALLED L1 DOOR HANDLE STOP PER AMM 52-11-11. MATCH DRILLED NEW STOP REF SRM 51-40-20May 3, 2026 · N125UP · Airbus A300F4622R · Passenger/Crew DoorsSDR IPXA2026021024123Switch · out of toleranceATB, FWD CARGO DOOR NOT CLOSED ON ECAM AFTER TAKEOFF . COULD NOT PRESSURIZE THE AIRCRAFT. FWD CARGO DOOR VERIFIED TO BE CLOSED AND LATCHED. DEFERRED FWD CARGO DOOR INDICATION REF: MEL 52-71-01-2. PLACARD INSTALLED, DMP C/W. PRESSURIZATION CHECKS NORMAL. ACCOFeb 10, 2026 · N125UP · Airbus A300F4622R · Door Warning SystemSDR IPXA2025121540049Spcc · faultedDURING APPROACH, RECEIVED SLAT SYS 1+2 FAULT. RAN QRH AND ECAM. INITIALLY PLANNED <15 SLAT WITH 40 FLAP LANDING. WHEN WE SELECTED FLAPS 30/40, SYS 1 SELF CORRECTED, SLATS DEPLOYED TO APPROX 30 THEN. REF T3F18E007Y8MD REMOVED AND REPLACED #2 SFCC PER AMM 27-51Dec 15, 2025 · N125UP · Airbus A300F4622R · Leading Edge Slat Control SystemSDR IPXA2025063082924Light · detachedPASSENGER/CREW DOOR WARNING LIGHT ASSY HANGING OUT OF DOOR LINER. SECURED PASSENGER/CREW DOOR WARNING LIGHT HOUSING IAW AMM 52-73-11. OPS CHECK GOOD.Jun 30, 2025 · N125UP · Airbus A300F4622R · Door Warning SystemSDR IPXA2025060912703Support Angle · deformedNR 2 PYLON FWD FAIRING LH AND RH SIDE SUPPORT ANGLES DEFORMED FWD OF RIB 4A. DOT# 110-99 JP-110. ACCOMPLISHED E.A.#: 300-5452-27-A3926, PRELIMINARY 6, STEP #38: INSTALLED IAW DRAWING A54612175 AND SRM 51-40-21.May 5, 2025 · N125UP · Airbus A300F4622R · Nacelle/Pylon Miscellaneous StructureSDR IPXA2025050512703Skin · deformedNR 2 PYLON FWD FAIRING LH AND RH SIDE SUPPORT ANGLES (P/N A54612200200/201)DEFORMED FWD OF RIB J4. DOT# 110-99 JP-110May 5, 2025 · N125UP · Airbus A300F4622R · Nacelle/Pylon, Plate/SkinSDR IPXA2025061833324Support Angle · deformedNUMBER 2 PYLON FWD FAIRING LH AND RH SIDE SUPPORT ANGLES (P/N A54612232200/201)DEFORMED FWD OF RIB 4A. DOT# 110-99 JP-110 REFORMED AREA AT #2 PYLON FWD FAIRING L/H AND R/H SIDE SUPPORT ANGLES P/N A54612232200/201 FWD OF RIB 4A IAW SREO-41097-C. AND EA 3005452-Apr 30, 2025 · N125UP · Airbus A300F4622R · Nacelle/Pylon Miscellaneous StructureSDR IPXA2025050533324Skin · deformed#2 PYLON FWD FAIRING LH AND RH SIDE SUPPORT ANGLES (P/N A54612232200/201)DEFORMED FWD OF RIB J4. DOT# 110-99 JP-110 VERIFIED REMOVAL OF 2 EA SUPPORT ANGLES IAW-A300-SRM-51-40-21Apr 30, 2025 · N125UP · Airbus A300F4622R · Nacelle/Pylon StructureSDR IPXA2025061910294Skin · wrinkledNR 1 ENGINE NACELLE FORWARD SKIN PANEL WRINKLED AT RIB J1 ACCOMPLISH PERMANENT REPAIR IN ACCORDANCE WITH EO-93897-REQ1 AND VT-MAE EA 300-5452-27-A3925 REV. - . CAUTION: THE WORK INSTRUCTIONS CONTAINED WITHIN (OR APPROVED BY) THIS EO CONTAIN RII INSPECTION REQUApr 29, 2025 · N125UP · Airbus A300F4622R · Nacelle/Pylon, Plate/SkinSDR IPXA2025061810362Skin · wrinkledNUMBER 2 ENGINE NACELLE FORWARD SKIN PANEL WRINKLED THE CURRENT CONFIGURATION OF AIRCRAFT AND PYLON: ENGINE REMOVED, DAMAGED SKIN REMOVED,DAMAGED LH AND RH SIDE SUPPORT ANGLES REMOVED (ITEM 170 ON SRM 54-52-11 FIG 1)ACCOMPLISHED STEP 5 OF EA: 300-5452-27-A3926Apr 29, 2025 · N125UP · Airbus A300F4622R · Nacelle/Pylon, Plate/SkinSDR IPXA2025050510362Skin · wrinkled#2 ENGINE NACELLE FORWARD SKIN PANEL WRINKLED VERIFIED ACCOMPLISHMENT OF STEP 17 PER EA: 300-5452-27-A3926 PRELIMINARY 3.<BR>VALIDATED DVI INSPECTION ON PYLON PRIMARY STRUCTURE, NO DAMAGE FOUND.Apr 29, 2025 · N125UP · Airbus A300F4622R · Nacelle/Pylon, Plate/SkinSDR IPXA2025050510294Skin · wrinkled#1 ENGINE NACELLE FORWARD SKIN PANEL WRINKLED AT RIB J1 VERIFIED ACCOMPLISHMENT OF EA #300-5452-27-A3925 PRELIMINARY 3 STEPS 20, 21 AND 22<BR>NO DISCREPANCIES NOTED AT THIS TIME.Apr 29, 2025 · N125UP · Airbus A300F4622R · Nacelle/Pylon, Plate/SkinSDR IPXA2025052564732Skin · crackedTWO CRACKS FOUND INSIDE HOLE T ON FR47 RH HORIZONTAL JUNCTION. ACCOMPLISH THE REPAIR PER EO-93655-REQ1 REV. 2 AND EA 300-5710-27-A3905 REV. A. CAUTION: THE WORK INSTRUCTIONS CONTAINED WITHIN (OR APPROVED BY) THIS EO CONTAIN RII INSPECTION REQUIREMENTS AND RII Apr 21, 2025 · N125UP · Airbus A300F4622R · Fuselage Main, Plate/SkinSDR IPXA2025052534907Skin · crackedCRACK FOUND IN FASTENER HOLE ON BULK CARGO DOOR SCUFF PLATE. AREA MARKED IN RED. ACCOMPLISHED E.A.#: 300-5317-27-A3915, PRELIMINARY 1, STEP# 2: "INCREMENTALLY REAM THE 1 EACH CRACKED HOLE IN STEPS OF 0.4 MM UNTIL DAMAGE FREE AND ROUND CONDITION ACHIEVED OR MAXApr 18, 2025 · N125UP · Airbus A300F4622R · Fuselage Main, Plate/SkinSDR IPXA2025052562688Skin · crackedCRACK FOUND IN HOLE T ON FR47 LH HORIZONTAL JUNCTION. ACCOMPLISH THE REPAIR PER EO-93642-REQ1 AND EA 300-5710-27-A3893 REV. -. CAUTION: THE WORK INSTRUCTIONS CONTAINED WITHIN (OR APPROVED BY) THIS EO CONTAIN RII INSPECTION REQUIREMENTS AND RII BUY - OFF WHICH Apr 17, 2025 · N125UP · Airbus A300F4622R · Fuselage Main, FrameSDR IPXA2025061837191Door Frame · gougedCREW DOOR, AFT FRAME (FR16.1) MECHANISM LOCK FITTING HAS GOUGE. DOT 103-62 (ATTACHED PHOTO) REMOVED MINOR GOUGE AT LOCK FITTING IAW SRM A300-600 51-73-11 MATERIAL THIKNESS IS 1.100" AND MATERIAL LOSS 0.003 AND REMAINING THIKNESS IS 1.197" THERE IS WHTIN INApr 16, 2025 · N125UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2025061837628Lock · damagedCREW DOOR, INNER SURFACE, UPPER SIDE, BRACKET SUPPORT AT AFT LOCK HOLE HAS GOUGE. DOT 103-64 (ATTACHED PHOTO) REMOVED MINOR GAUGE IAW SRM A300-600 51-73-11 MATERIAL LOSS 0.002 WITHIN LIMITS IAW SRM 51-73-11. T988826 C18-C02 OK TO RESTORE SURFACE PROTECTION. APApr 16, 2025 · N125UP · Airbus A300F4622R · Passenger/Crew DoorsSDR IPXA2025052546455Skin · crackedTWO CRACKS FOUND IN HOLE A ON RH FR47 HORIZONTAL JUNCTION. ACCOMPLISH THE REPAIR PER EO-93655-REQ1 REV. 2 AND EA 300-5710-27-A3905 REV. A. CAUTION: THE WORK INSTRUCTIONS CONTAINED WITHIN (OR APPROVED BY) THIS EO CONTAIN RII INSPECTION REQUIREMENTS AND RII BUY Apr 16, 2025 · N125UP · Airbus A300F4622R · Fuselage Main, Plate/SkinSDR IPXA2025052546480Skin · crackedCRACK FOUND IN HOLE C ON RH FR47 HORIZONTAL JUNCTION. ACCOMPLISH THE REPAIR PER EO-93655-REQ1 REV. 2 AND EA 300-5710-27-A3905 REV. A. CAUTION: THE WORK INSTRUCTIONS CONTAINED WITHIN (OR APPROVED BY) THIS EO CONTAIN RII INSPECTION REQUIREMENTS AND RII BUY - OFFApr 16, 2025 · N125UP · Airbus A300F4622R · Fuselage Main, Plate/SkinSDR IPXA2025052546594Skin · crackedCRACK FOUND IN HOLE S ON RH FR47 HORIZONTAL JUNCTION. ACCOMPLISH THE REPAIR PER EO-93655-REQ1 REV. 2 AND EA 300-5710-27-A3905 REV. A. CAUTION: THE WORK INSTRUCTIONS CONTAINED WITHIN (OR APPROVED BY) THIS EO CONTAIN RII INSPECTION REQUIREMENTS AND RII BUY - OFFApr 16, 2025 · N125UP · Airbus A300F4622R · Fuselage Main, FrameSDR IPXA2025052546546Skin · crackedCRACK FOUND IN HOLE E ON RH FR47 HORIZONTAL JUNCTION. ACCOMPLISH THE REPAIR PER EO-93655-REQ1 REV. 2 AND EA 300-5710-27-A3905 REV. A. CAUTION: THE WORK INSTRUCTIONS CONTAINED WITHIN (OR APPROVED BY) THIS EO CONTAIN RII INSPECTION REQUIREMENTS AND RII BUY - OFFApr 16, 2025 · N125UP · Airbus A300F4622R · Fuselage Main, FrameSDR IPXA2025052546559Skin · crackedCRACK FOUND IN HOLE G ON RH FR47 HORIZONTAL JUNCTION. ACCOMPLISH THE REPAIR PER EO-93655-REQ1 REV. 2 AND EA 300-5710-27-A3905 REV. A. CAUTION: THE WORK INSTRUCTIONS CONTAINED WITHIN (OR APPROVED BY) THIS EO CONTAIN RII INSPECTION REQUIREMENTS AND RII BUY - OFFApr 16, 2025 · N125UP · Airbus A300F4622R · Fuselage Main, FrameSDR IPXA2025052344612Bracket · crackedLH HORIZONTAL STAB LEADING EDGE APRON SUPPORT BRACKET P/N: A5517155120451 BROKEN. INSTALLATION OF NEW BRACKET P/N: A5517155120451, B/N:0004388210 IAW A300-600F SRM 51-40-21. FASTENERS USED: FOUR HI-LOKS P/N HL10VF6-6, BATCH #0004358134 AND FOUR COLLARS P/N NApr 16, 2025 · N125UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2025041637628Support Bracket · gougedCREW DOOR, INNER SURFACE, UPPER SIDE, BRACKET SUPPORT AT AFT LOCK HOLE HAS GOUGE.Apr 16, 2025 · N125UP · Airbus A300F4622R · Passenger/Crew DoorsSDR IPXA2025041637191Door Frame · gougedCREW DOOR, AFT FRAME (FR16.1) MECHANISM LOCK FITTING HAS GOUGE.Apr 16, 2025 · N125UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2025052507731Frame · crackedCRACK FOUND IN HOLE G ON FR47 LH HORIZONTAL JUNCTION. COMPLIED WITH STEP 15 OF PRELIM 1 EA-300-5710-27-A3893.Apr 14, 2025 · N125UP · Airbus A300F4622R · Fuselage Main, FrameSDR IPXA2025052508352Floor Support · crackedMDC FLOOR STRUCTURE RH SIDE FR38.1 SUPPORT (DOG BONE) CRACKED. DOT 11-056 THE SPARE PART IS CONSUMABLE AND DOES NOT HAVE A UPS PARTS TAG. (SEE ATTACHMENT).Apr 14, 2025 · N125UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2025060308262Floor Support · crackedMDC FLOOR STRUCTURE RH SIDE FR38.2 SUPPORT (DOG BONE) CRACKED.Apr 14, 2025 · N125UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2025052307518Crossbeam · bentMAIN DECK CROSSBEAM AT FR 48 BETWEEN -Y450 AND -Y953 BENT.DOT# 110-61 JP-110. INSTALLED NEW CROSSBEM I.A.W A300-600 SREO 75878-REQ001.Apr 14, 2025 · N125UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2025052395256Bracket · gougedLH WING, UPPER SURFACE, ATTACHMENT WTB FAIRIG AREA, BRACKET SUPPORT HAS GOUGE (2EA). DOT 103-34 (ATTACHED PHOTO). NSTALLED NEW BRACKET IAW A300-600 SRM 51-40-21. RIVET P/N: CR3213-6-03 BATCH: 0004194656, HI-LOCK P/N: DAN5-6-6 BATCH: 0004178101, COLLAR P/N: NSApr 14, 2025 · N125UP · Airbus A300F4622R · Wing StructureSDR IPXA2025052307579Crossbeam · bentMAIN DECK CROSSBEAM AT FR 49 BETWEEN -Y450 AND -Y953 BENT. DOT# 110-62 JP-110. INSTALLED NEW CROSSBEM I.A.W A300-600 SREO 75878-REQ001. REVIEWEDApr 14, 2025 · N125UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2025042908379Floor Panel · damagedMDC FLOOR PANEL 231KJ IS DAMAGED AND BROKEN. FABRICATED MAIN DECK FLOOR PANEL 231KJ IAW SREO-16407-REQ001.Apr 14, 2025 · N125UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2025042788628Seat Track · damagedMDC FLOOR STRUCTURE FR79/Y0 UNDER FLOOR PANEL 261EM SEAT TRACK CORRODED.Apr 13, 2025 · N125UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2025050794051Adapter · corrodedMDC FLOOR PANEL 251WG FWD ADAPTER CLS WITH CORROSION .Apr 13, 2025 · N125UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2025050793709Adapter · corrodedMDC FR57.1/Y-0 UNDER FLOOR PANEL 252LG CLS ADAPTER CORRODED.Apr 13, 2025 · N125UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2025050793730Adapter · corrodedMDC ON PANEL 251 WG ADAPTER CLS WITH CORROSION.Apr 13, 2025 · N125UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2025050793732Adapter · corrodedMDC FLOOR STRUCTURE FR58/Y-0 UNDER FLOOR PANEL 251FM CLS ADAPTER CORRODED. ACCOMPLISH PERMANENT REPAIR IN ACCORDANCE WITH EO-93740-REQ1 AND VT-MAE EA 300-5316-27-A3909 REV. - .Apr 13, 2025 · N125UP · Airbus A300F4622R · Fuselage Main, Attach FittingsSDR IPXA2025052389112Floorbeam · crackedMDC FLOOR STRUCTURE FR79 RH SIDE FLOOR PANEL 262AH PROFILE CRACKED. DOT 11-026. ACCOMPLISH PERMANENT REPAIR IN ACCORDANCE WITH EO-93576-REQ1 AND VT-MAE EA 300-5318-27-A3917, REV. -.Apr 13, 2025 · N125UP · Airbus A300F4622R · Fuselage Main, Floor BeamSDR IPXA2025043093692Floor Panel · brokenMDC FLOOR PANEL 251FM BROKEN. DOT 11-040 REVIEWEDApr 13, 2025 · N125UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2025050689112Profile · cracked**SDR FILED OPEN**FAULT: STR-Z200 MDC FLOOR STRUCTURE FR79 RH SIDE FLOOR PANEL 262AH PROFILE CRACKED. DOT 11-026 VERIFIED INSTALLATION OF MDC FLOOR IN FR79 RH Z PROFILE IAW A300-600F SRM 51-40-21. MATERIALS USED: SEALANT P/N 04-001-0109, BATCH #0004371367, SOApr 13, 2025 · N125UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2025050694089Profile · cracked**SDR FILED OPEN**FAULT-STR-Z200-MDC FLOOR IN C65 LH Z PROFILE HAVE A CRACK DOT 07-119 VERIFIED INSTALLATION OF MDC FLOOR IN C65 LH Z PROFILE IAW A300-600F SRM 51-40-21. MATERIALS USED: SEALANT P/N 04-001-0109, BATCH #0004371367, SOLID RIVETS 36 EACH P/N NAS1Apr 13, 2025 · N125UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2025042989085Seat Track · corrodedFAULT: STR-Z200 MDC FLOOR STRUCTURE UNDER FLOOR PANEL 262FM FR80/-Y794.3 SEAT TRACK CORRODED. DOT 11-024.REMOVED CORROSION ON SEAT TRACK AT FR 80/-Y953 IAW A300-600F SRM 51-74-10.REMOVED SEAT TRACK AT MDC FLOOR STRUCTURE UNDER FLOOR PANEL 262FM FR80/-Y794.3, IApr 13, 2025 · N125UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2025050289249Support · crackedFLOOR STRUCTURE RH SIDE BETWEEN FR73/74 WEB SUPPORT UNDER SURFACE CRACKED. DOT 11-030.REMOVED SUPPORT UNDER MDC FLOOR STRUCTURE RH SIDE BETWEEN FR73/74 IAW A300-600 SRM 51-40-21.TREATED AND PRIMED NEW PART SHEAR WED IAW A300-600 SRM 51-21-10. APPLIED TOPCOATApr 13, 2025 · N125UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2025050193756Seat Track · corrodedMDC FLOOR, SEAT TRACK IN Y450 ON PANEL 251VF HAVE CORROSION DOT 07-116 VERIFIED INSTALLATION OF NEW SEAT TRACK SECTION IN Y450 BETWEEN FR63 AND FR66 IAW SRM 53-10-16 PARAGRAPH 4 FIGURE 201 PAGE 207/208 AND SRM 51-40-21 . OPENApr 13, 2025 · N125UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2025041588630Seat Track · corrodedMDC FLOOR STRUCTURE FR79/-Y450 UNDER FLOOR PANEL 262EM SEAT TRACK CORRODED. DOT 11-023. VERIFIED REMOVAL OF CORROSION ON SEAT TRACK IAW A300-600F SRM 51-74-10. ORIGINAL MATERIAL THICKNESS .535", MATERIAL LOSS .021", MATERIAL LEFT .514". THE LOSS IS IN LIMITS Apr 13, 2025 · N125UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2025052383032Floor Support · crackedMDC COMPARTMENT AFT AREA FLOOR PANEL 261HM HAS A SUPPORT CRACKED. DOT 11-020. REMOVED AND REPLACED FLOOR SUPPORT ANGLE (PROFILE) FRAME 80 RH PNL 261 HM IAW A300-600 SRM 51-40-21. ANGLE P/N: A5398140120000 BATCH:0004390460. RIVETS P/N: MS20470AD5-5 .BATCH:00043Apr 12, 2025 · N125UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2025052383131Frame · crackedMDC, BETWEEN FR74 AND FR73, LH SIDE, UNDER FLOOR STRUCTURE FRAME HAS A CRACK BETWEEN 2 RIVETS. INSTALLED NEW SHEAR WEB I.A.W A300-600 SRM 51-40-21.Apr 12, 2025 · N125UP · Airbus A300F4622R · Fuselage Main, FrameSDR IPXA2025052383072Floor Support · crackedMDC, BETWEEN FR 78 AND FR 77, LH SIDE, FLOOR STRUCTURE FRAME HAS 2EA CRACKS. DOT 23-002. NEW WEB HAS BEEN INSTALLED IAW A300-600 SRM 51-40-21 AND ALSO THE INTERFAY SEALING HAVE BEEN RESTORED BETWEEN THE SURFACES IAW A300-600 SRM 51-76-10. MATERIALS USED: SEALApr 12, 2025 · N125UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
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