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 IPXA2025051283131Web · crackedMDC, BETWEEN FR74 AND FR73, LH SIDE, UNDER FLOOR STRUCTURE FRAME HAS A CRACK BETWEEN 2 RIVETS. DOT 23-003 VERIFIED INSTALL STEP 15Apr 12, 2025 · N125UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2025050182776Seat Track · damagedFAULT-STR-Z200-MDC FLOOR STRUCTURE, BETWEEN FR 79 AND FR 78, BEHIND PANEL 261AH, HAS A STRUCTURE DRILLED OUT. DOT 23-001.PERFORMED CUTOUT OF OUTBOARD FLANGE BETWEEN FR 78 AND FR 79 AT TRACK Y1580. MEASURES 1.90" WIDE BY .900" INBOARD IAW A300-600-SRM-53-10-16 Apr 12, 2025 · N125UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2025043081558Floor Panel · brokenFAULT-INTERIORS-ZONE200-MAIN CABIN: FLOORBOARD 241ZH BROKEN. DOT NO. 17-27.FABRICATED MDC FLOOR PANEL 241ZH I.A.W. SREO-16407-REQ001, MATERIAL USED P/N: 5024N400001SS-G BTCH:0004055277, PAINT P/N:34655-526A-RS65 BTCH:0004326906.Apr 12, 2025 · N125UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2025050283072Floor Support · cracked-MDC, BETWEEN FR 78 AND FR 77, LH SIDE, FLOOR STRUCTURE FRAME HAS 2EA CRACKS. DOT 23-002 SDR COMPLETEDApr 12, 2025 · N125UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2025042983138Floor Panel · brokenFAULT-COMP-Z200-MDC FLOOR PANEL 261JM IS BROKEN. DOT 23-006. VERIFIED FABRICATION OF MDC FLOOR PANEL 261JM I.A.W. SREO-16407-REQ001, MATERIAL USED P/N: 5024N400001SS-G BTCH:0004055277, PAINT P/N: 34655-526A-RS65 BTCH: 0004326906, CUP#: 02-012-176, PLUG P/N:GApr 12, 2025 · N125UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2025043083032Floor Support · cracked**SDR FILED OPEN** MDC COMPARTMENT AFT AREA FLOOR PANEL 261HM HAS A SUPPORT CRACKED. DOT 11-020 VERIFIED REMOVAL/ REPLACEMENT OF FLOOR SUPPORT ANGLE (PROFILE) FRAME 80 RH PNL 261 HMApr 12, 2025 · N125UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2025052368348Rib · cracked**SUPPLEMENTAL SDR** FAULT: L/H WING, CENTER FLAP TOP SKIN AND RIB FLANGE 27A HAS (1) CRACK INDICATION AND HAS BEEN MARKED IN RED. ACCOMPLISH REPAIR IN ACCORDANCE WITH EO-93428-REQ1 AND VT-MAE EA 300-5750-27-A3891, REV. -. REVIEWEDApr 11, 2025 · N125UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2025052368187Rib · crackedR/H WING, CENTER FLAP TOP SKIN AND RIB FLANGE 27A HAS (2) CRACK INDICATION AND HAS BEEN MARKED IN RED. INSTALLED NEW ANGLE FOR R/H WING, CENTER FLAP TOP SKIN AND RIB FLANGE 27 FLANGER REPAIR BETWEEN STRINGER 2.6 AND STRINGER 2.7 AND 2.8 AND REAR SPART IAW A30Apr 11, 2025 · N125UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2025052368253Rib · crackedL/H WING, CENTER FLAP TOP SKIN AND RIB FLANGE 26A HAS (1) CRACK INDICATION AND HAS BEEN MARKED IN RED. ACCOMPLISHED WHIT E.A 300-5750-27-A3891 PRELIMINRY 1 AND INSTALLED DOUBLER AT CENTER FLAP LH IN ACCORDANCE WHIT SRM 57-50-00 AND MATERIAL USED 2024T3 0.05Apr 11, 2025 · N125UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2025052368088Rib · crackedR/H WING, CENTER FLAP TOP SKIN AND RIB FLANGE 26A HAS (1) CRACK INDICATION AND HAS BEEN MARKED IN READ. ACCOMPLISH PERMANENT REPAIR IN ACCORDANCE WITH EO-93431-REQ1 AND VT-MAE EA 300-5750-27-A3892, REV. -. REVIEWEDApr 11, 2025 · N125UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2025050666899Floor Support · corrodedFLOOR SUPPORT AT Y953, FR11 TO FR15A CORRODED AT MANY LOCATIONS DOT# 110-33 JP-110 VERIFIED INSTALLATION OF NEW FLOOR SUPPORT PART NUMBER BAC1505-100590, BATCH NUMBER 0004389085 IAW SRM51-40-21, MATERIAL INFO: SEALANT PS870-B1/2, BATCH NUMBER 0004371367, COLLApr 11, 2025 · N125UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2025050866959Floor Support · corrodedFLOOR SUPPORT AT Y1456, FR11 TO FR15A CORRODED AT MANY LOCATIONS DOT# 110-34 JP-110. INSTALLED NEW FLOOR SUPPORT PART NUMBER BAC1505-100590 IAW SRM 51-40-21, MATERIAL INFO: SEALANT PS870-B1/2, BATCH NUMBER 0004371367, HI-LOKS PART NUMBER EN6115K3-4,BATCH NUMBApr 11, 2025 · N125UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2025050666878Floor Support · corrodedFLOOR SUPPORT AT Y730, FR11 TO FR14 CORRODED AT MANY LOCATIONSApr 11, 2025 · N125UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2025050666971Floor Support · corrodedFLOOR SUPPORT AT Y1959, FR12A TO FR17 CORRODED AT MANY LOCATIONS DOT# 110-35 JP-110. NSTALLED NEW FLOOR SUPPORT PART NUMBER A53613033212, BATCH NUMBER 0004389085, SEALANT PART NUMBER PS870-B1/2, BATCH NUMBER 4371367, IAW SRM 51-40-21.Apr 11, 2025 · N125UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2025042668348Rib · crackedL/H WING, CENTER FLAP TOP SKIN AND RIB FLANGE 27A HAS (1) CRACK INDICATION AND HAS BEEN MARKED IN RED. VERIFIED SERVICE DIFFICULTY REPORT HAS BEEN INITIATED. COMPLIED WITH STEP 20 OF E.A 300-5750-27-A3891 PRELIMINRY 1. OPENApr 11, 2025 · N125UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2025042668088Rib · crackedR/H WING, CENTER FLAP TOP SKIN AND RIB FLANGE 26A HAS (1) CRACK INDICATION AND HAS BEEN MARKED IN READ. VERIFIED SERVICE DIFFICULTY REPORT HAS BEEN INITIATED.COMPLIED WITH STEP 20 OF E.A 300-5750-27-A3892 PRELIMINRY 1. OPENApr 11, 2025 · N125UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2025042668253Rib · crackedL/H WING, CENTER FLAP TOP SKIN AND RIB FLANGE 26A HAS (1) CRACK INDICATION AND HAS BEEN MARKED IN RED. VERIFIED SERVICE DIFFICULTY REPORT HAS BEEN INITIATED. COMPLIED WITH STEP 20 OF E.A 300-5750-27-A3891 PRELIMINRY 1. OPENApr 11, 2025 · N125UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2025042668187Rib · crackedR/H WING, CENTER FLAP TOP SKIN AND RIB FLANGE 27A HAS (2) CRACK INDICATION AND HAS BEEN MARKED IN RED. VERIFIED SERVICE DIFFICULTY REPORT HAS BEEN INITIATED.COMPLIED WITH STEP 20 OF E.A 300-5750-27-A3892 PRELIMINRY 1. OPENApr 11, 2025 · N125UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2025042668077Rib · crackedSDR FILED OPEN. R/H WING, CENTER FLAP TOP SKIN AND RIB FLANGE 27F HAS (1) CRACK INDICATION AND HAS BEEN MARKED IN READ. VERIFIED SERVICE DIFFICULTY REPORT HAS BEEN INITIATED.COMPLIED WITH STEP 20 OF E.A 300-5750-27-A3892 PRELIMINRY 1.Apr 11, 2025 · N125UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2025052928479Stiffener · corroded#1 PYLON INTERNAL LOWER SPAR, LIGHT SURFACE CORROSION, AS SEEN THROUGH SIDE PANEL# 415ALApr 10, 2025 · N125UP · Airbus A300F4622R · Nacelle/Pylon Miscellaneous StructureSDR IPXA2025051238636Ceiling Panel · cracked*** SDR FILED OPEN *** FAULT-STR-ZONE 100-FWD CARGO 132LC HAS 3 DENTS AROUND 3 HOLES-DOT 109-94 VWV 5430 AUDIT COMPLETEDApr 10, 2025 · N125UP · Airbus A300F4622R · Passenger Compartment EquipmentSDR IPXA2025052521090Web · crackedRT WING INBD LEADING EDGE WEB CRACKED NEAR RIB 2.Apr 9, 2025 · N125UP · Airbus A300F4622R · Wing Miscellaneous StructureSDR IPXA2025040877267Warning Horn · no testNOSE LANDING GEAR HORN FAILS TO ACTIVATE WHEN PERFORMING OPS TEST OF OVERBOARD VALVE FAULT WARNING APPROVED.Apr 7, 2025 · N125UP · Airbus A300F4622R · Central WarningSDR IPXA2025040279850Lamp · inoperativeLAVATORY EMERGENCY LIGHT INOPERATIVE RELAMPED OPERATING NORMALLY OK FOR SERVICE REF 33-51-00Apr 1, 2025 · N125UP · Airbus A300F4622R · Emergency LightingSDR IPXA2025031314983Indication Sys · malfunctioned*DIVERSION* ENG 2/ENGINE ADV LOW OIL PRESSURE (CONDITION BOTH OIL PRESSURE GAUGE AND ECAM NOT CONFIRMED BY OIL PRESSURE LOCAL WARNING, R/R ENGINE #2 PRESURE INDICATOR PER AMM 79-33-21 OPS CHECK GOODMar 13, 2025 · N125UP · Airbus A300F4622R · Engine Oil Indicating SystemSDR IPXA2025020772580Door · damagedLOAD REPORTS BUG NET ON K LOADER MADE CONTACT WITH THE MAIN CARGO DOOR.. UPON INSPECTION FOUND 5 OF 8 INDICATOR FLAGS DAMAGED. (FWD TO AFT 1,2,4,7,8). REPLACED DAMAGED LOCKING INDICATORS REF AMM 52-36-23/401. OSD: 2/5/2025Feb 4, 2025 · N125UP · Airbus A300F4622R · Cargo/Baggage DoorsSDR IPXA202501272390Life Vest · missingCOCKPIT OBSERVER/JUMPSEAT LIFE VEST IS NOT FOUND IN COCKPIT (FOUND MISSING ON PSM CHECK) PLACED NEW LIFE VEST INTO COCKPIT PER LOCATION DESCRIPTION LISTED IN THE A 300 PSM CHECK. MXP-PSM-025000-01-1-999-JIC. (FOR MAINTENIX PURPOSES REMOVED PART INFORMATION FJan 27, 2025 · N125UP · Airbus A300F4622R · Life JacketSDR IPXA2024121018615Slide · out of positionSLIDE LEVER WOULD NOT DISARM AFTER SEVERAL ATTEMPTS. LEVER WOULD 3/4 OF THE WAY AND €ŒSTICK€? MECHANIC JUMPSEATER WAS ABLE TO MANIPULATE THE SLIDE ENOUGH TO GET THE LEVER TO €ŒDISARM€? CLEANED AND LUBRICATED GIRT BAR SLIDERS AND FLOOR FITTINGS REF AMM 52-1Dec 10, 2024 · N125UP · Airbus A300F4622R · Escape SlideSDR IPXA2024062623390Plug · missingCREW ENTRY DOOR EXTERNAL HANDLE MISSING PLUG. INSTALLED PLUG IAW AMM 52-10-20Jun 26, 2024 · N125UP · Airbus A300F4622R · Passenger/Crew DoorsSDR IPXA2024011794754Bottle · low pressureDOOR EMG. ASSIST PRESSURE LOW SERVICED ENRTRY DOOR EMERGENCY OPERATION CYLINDER PER AMM 52-10-14-301.Jan 17, 2024 · N125UP · Airbus A300F4622R · Emergency EquipmentSDR IPXA2023120882157Unknown · unknownCABIN DOOR ACTUATOR PRESSURE IS LOW. SERVICED CABIN DOOR ACTUATOR IAW AMM 52-10-14Dec 8, 2023 · N125UP · Airbus A300F4622R · Passenger/Crew DoorsSDR IPXA2023082494005A/C Pack · odorINSPECTION TYPE:NAAFTER T/O WE NOTICED A BURNING SMELL LIKE OIL COMING FROM THE GASPER VENTS FROM PACK1 / PACK2 DEFERRED NO SMOKE JUST ODOR SMELL WENT AWAY AROUND 5000'ACCOMPLISHED @2 ENG RUN W/R/T AMM 71-00-00-0201. RAN #1 PACK W/R/T AMM 21-51-00-0501. OPS GOAug 23, 2023 · N125UP · Airbus A300F4622R · Cabin Cooling SystemSDR IPXA2022120788783Mechanism · lack of lubeAFTER PARKING, DOOR SLIDE WOULD NOT DISARM. REMOVED FWD DOOR LINING MM 52-10-13-401, LUBRICATED SLIDE ARM MECHANISM IAW MM 52-10-30-601 SLIDE ARMS AND DISARMS WITH NO BINDING MM 25-61-20-601 (4).Dec 7, 2022 · N125UP · Airbus A300F4622R · Passenger/Crew DoorsSDR IPXA2022120788799Mechanism · lack of lubeINSPECTION TYPE:NAAFTER PARKING DOOR SLIDE WOULD NOT DISARM, SEE PAGE 477510 AND 477516. DEFERRED MAIN ENTRY DOOR SLIDE PER MEL 52-11-01-2-3. M797137 CREATED, PLACARD INSTALLED DMP C.W. REMOVED FWD DOOR LINING MM 52-10-13-401 LUBED SLIDE ARM MECHANISM PER MM Dec 6, 2022 · N125UP · Airbus A300F4622R · Emergency EquipmentSDR IPXA2022120788769Mechanism · lack of lubeINSPECTION TYPE:NAAFTER PARKING SLIDE ARM HANDLE WOULD NOT MOVE TO DISARM POSITIONLUBED SLIDE ARM MECHANISM PER MM 12-22-52-0001 OPS CHECK GOOD PER MM 52-10-30-601Dec 6, 2022 · N125UP · Airbus A300F4622R · Passenger/Crew DoorsSDR IPXA2022120388641Slide Channel · fodMAIN DOOR WON'T DISARM, CYCLED DISARM/ARM LEVEL SERVERAL TIMES FOUND DEBRIS STUCK ON ARM SLIDES UNDER DOOR FOR ILLEG CLEANED DEBRIS OUT AND OPS CHECK GOOD. REF AMM A300 52-10-30Dec 2, 2022 · N125UP · Airbus A300F4622R · Passenger/Crew DoorsSDR IPXA2022112988550Lever · bindingAFTER BLOCKING - DOOR SLIDE LEVER TOOK SEVERAL ATTEMPTS TO DISARM, COULD NOT DUPLICATE. NO HISTORY. CHECK SYS IAW MM 25-61-20-0501 ADJ/TEST OPS CK OK. RTS. HISTORY STARTEDNov 28, 2022 · N125UP · Airbus A300F4622R · Emergency EquipmentSDR IPXA2022102487433Door · bindingMAIN CABIN CREW ENTRY DOOR DIFFICULT TO CLOSE FROM THE INSIDE. PERFORMED INSPECT/CHECK OF LH CREW ENTRY DOOR IAW AMM 52-00-00. OPS CHECK GOODOct 21, 2022 · N125UP · Airbus A300F4622R · Passenger/Crew DoorsSDR IPXA2022100786919Panel · corrodedINSPECTION TYPE:SEG, PANEL 414ER HAS CORROSION AROUND SCREW HOLES.CUT OUT DAMAGE INSTALLED FILLER AND DOUBLER IAW SRM 54-52-51-FIG 201.Oct 7, 2022 · N125UP · Airbus A300F4622R · Nacelle/Pylon, Plate/SkinSDR IPXA2022100786918Door · corrodedINSPECTION TYPE:SEG, LOWER FWD EXTERNAL FUSE TOILET SERVICE PANEL 121DL HAS CORROSION INNER AND OUTER SURFACE.DOOR/PANEL WAS FOUND TO BE OUT OF LIMITS DOOR WAS REMOVED AND REPLACED IAW SRM 51-40-21Oct 2, 2022 · N125UP · Airbus A300F4622R · Fluid Service DoorsSDR IPXA2022100686904Panel · wornINSPECTION TYPE:SEG#2 PYLON PANEL 423CL 2EA FASTENER HOLE CUT OUT WORN2EA AREAS WAS CUTOUT FILLERS AND A DOUBLER WAS INSTALLED IAW SRM 54-52-51 FIG 201Oct 2, 2022 · N125UP · Airbus A300F4622R · Nacelle/Pylon, Plate/SkinSDR IPXA2022100686903Panel · wornINSPECTION TYPE:SEG, #2 PYLON PANEL 424CR 2EA FASTENER HOLE CUT OUT WORN2EA AREAS WAS CUTOUT FILLERS AND DOUBLER WAS INSTALLED IAW SRM 54-52-51 FIG 201Oct 2, 2022 · N125UP · Airbus A300F4622R · Nacelle/Pylon, Plate/SkinSDR IPXA2022081185145Flap · vibrationINSPECTION TYPE:N/A** ATB ** EMERGENCY DECLARED ** LANDED SUCCESSFULLY ** DURING CLIMBOUT ACCELERATING THRU 280 KIAS, ACFT BEGAN CONTINOUS VIBRATION UNTIL SPEED BELOW 280 KIAS. ALL INDICATIONS NORMAL. ATTEMPTED CLIMB AGAIN VIBRATION RESUMED.PERFORMED TROUBLESHAug 10, 2022 · N125UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2022031179986Light · inoperativeON PREFLIGHT SLIDE ARMED LIGHT DOES NOT ILLUMINATE BUZZER WORKS. RESET C/B'S ACCOMPLISHED LIGHT CHECK W/R/T AMM 52-73-00-0501. OPS CHECK GOOD.Mar 11, 2022 · N125UP · Airbus A300F4622R · Passenger/Crew DoorsSDR IPXA2021083073300Handle · inoperativeAIR TURNBACK ON DEPARTURE THE LANDING GEAR HANDLE WOULD ONLY MOVE TO THE UNLOCK POSITION. GEAR WOULD NOT RETRACT. WE RAN THE CHECKLIST AND PUT THE GEAR BACK IN THE DOWN POSITION. NO OTHER INDICATIONS THE #1 PITCH TRIM PADDLE ALSO KICKED OFF. WOULD NOTFOUND C/BAug 28, 2021 · N125UP · Airbus A300F4622R · Landing Gear SelectorSDR IPXA2021061670655Warning Message · false activationINSPECTION TYPE:NACABIN DOOR OPEN AND DOOR WARNING HORN ECOM INDICATION COME ON DURING CLIMB - NO PRESSURE LOSSPERFORMED TEST PER AMM 52-10-11-0501. DOS OPERATES SMOOTHLY AND DOOR EICAM MESSAGE. OPS CK GOOD. OK TO CONTINUE NO RECENT HISTORYJun 16, 2021 · N125UP · Airbus A300F4622R · Door Warning SystemSDR IPXA2021012164731Seal · leakingINSPECTION TYPE: NA, EMERGENCY DECLARED, NO EQUIPMENT USED. LANDING UNEVENTFUL. ON APPROACH, FLAPS 15/0 ECAM HYD BLUE RSVR LOW AIR PRESS, BLUE RSVR LOW LEVEL. BLUE QTY INDICATION LOW. REPLACED NR 1 ENGINE BLUE SYS HYD PUMP REAR DRIVE SEAL, PER AMM 72-65-07Jan 20, 2021 · N125UP · Airbus A300F4622R · Hydraulic Pump (Electric/Engine), MainSDR IPXA2021011364405Warning Light · inoperativeINSPECTION TYPE: NA SDR FILED OPEN. CREW ENTRY DOOR WARNING LIGHT INOPERABLE. BUZZER WORKS. DEFERRED CREW ENTRY N DOOR WARNING LIGHT, IAW MEL 52-73-01-1. PLACARD INSTALLED, A/C OK TO CONTINUE.Jan 12, 2021 · N125UP · Airbus A300F4622R · Passenger/Crew DoorsSDR IPXA2020100961115Warning Message · false activationINSPECTION TYPE: N/A SMOKE, AVIONICS SMOKE WARNING CAME ON/OFF ABOUT 6 TIMES. THE LAST TIME IT STAYED ON EVEN AFTER SHUTDOWN. CREW C/W SNIFFER TEST, WHICH WAS NEGATIVE. WENT INTO AVIONICS COMPARTMENT, NO SMELL OF SMOKE. BITE SYSTEM TEST ON FIRE MODULE PASSOct 8, 2020 · N125UP · Airbus A300F4622R · Smoke DetectionSDR IPXA2020080758758Floor Panel · damagedFWD CARGO FWD FLOOR PANEL 131MG WAS DAMAGED. FABRICATED A NEW FLOOR PANEL IAW SREO A300-5320-16407-E.Aug 7, 2020 · N125UP · Airbus A300F4622R · Fuselage Floor Panel
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