N127UP

Service difficulty reports · 194

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 = 'N127UP' 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 IPXA2026101512243Skin · dentedLOWER FUSELAGE, BTWN FR 51 TO 52, LH SIDE, NEXT TO MLG DOOR CUTOUT, EXTERNAL SURFACE, SKIN HAS A DENT W/ GOUGE. ACCOMPLISH PERMANENT REPAIR IN ACCORDANCE WITH EO-98862-REQ1 AND STE PNA EA 300-5315-27-A4660, REV-.Oct 6, 2026 · N127UP · Airbus A300F4622R · Fuselage Main, Plate/SkinSDR IPXA2026102161735Fitting · out of limitsHOLE N HOLE SIZES MEASURES DIFFERENT FROM THE EO-90930-REQ2 REV 4; FWD FITTING .3780", SPLICE .2840, AFT FITTING .3780". ACCOMPLISHED THE REPAIR PER EO-98948-REQ1 AND EA 300-5710-27-A4658, REV. _.Oct 2, 2026 · N127UP · Airbus A300F4622R · Wing Main, Frame StructureSDR IPXA2026102161645Fitting · out of limitsHOLE M HOLE SIZES MEASURES DIFFERENT FROM THE EO-90930-REQ2 REV 4; FWD FITTING .4530", SPLICE .3070, AFT FITTING .4580". ACCOMPLISHED THE REPAIR PER EO-98948-REQ1 AND EA 300-5710-27-A4658, REV. _.Oct 2, 2026 · N127UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2026102161581Fitting · out of limitsHOLE L HOLE SIZES MEASURES DIFFERENT FROM THE EO-90930-REQ2 REV 4; FWD FITTING .3830", SPLICE .2810, AFT FITTING .3840". ACCOMPLISHED THE REPAIR PER EO-98948-REQ1 AND EA 300-5710-27-A4658, REV. _.Oct 2, 2026 · N127UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2026102161504Fitting · out of limitsHOLE H HOLE SIZES MEASURES DIFFERENT FROM THE EO-90930-REQ2 REV 4; SPLICE .3480, AFT FITTING .4050".ACCOMPLISHED THE REPAIR PER EO-98948-REQ1 AND EA 300-5710-27-A4658, REV. _.Oct 2, 2026 · N127UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2026082400675Test Unit · faultedASPSU TEST UNIT FAULT LIGHT ILLUMINATED WHEN BITE TESTED. REPLACED ASPSU IAW AMM 52-73-18/401. OPS CHECK GOOD, NO FURTHER DEFECTS NOTED.Aug 21, 2026 · N127UP · Airbus A300F4622R · DoorsSDR IPXA2026081438198Pump · low pressureEMERGENCY DECLARED. GREEN ENG HYD PUMP 2 LO PRESSURE FOLLOWED ECAM ,SELECTED OFF , RESULTED IN LOSS OF GREEN HYD FLUID RESULTED IN GREEN HYD FALURE. NUMBER 2 GREEN ENGINE DRIVEN HYDRAULIC PUMP REPLACEMENT COMPLETE IAW AMM 29-11-31. OPS CHECK, LEAK CHECKS GOAug 12, 2026 · N127UP · Airbus A300F4622R · Hydraulic Pump (Electric/Engine), MainSDR IPXA2026081238198Pump · low pressureEMERGENCY DECLARED, GREEN ENG HYD PUMP 2 LOW PRESSURE FOLLOWED ECAM ,SELECTED OFF , RESULTED IN LOSS OF GREEN HYD FLUID RESULTED IN GREEN HYD FALURE.Aug 12, 2026 · N127UP · Airbus A300F4622R · Hydraulic Pump (Electric/Engine), MainSDR IPXA2026062307338Door · bindingMAIN CABIN DOOR HARD TO CLOSE. FLIGHT CREW NOTED TO MX UPON ARRIVAL THAT THE L1 DOOR FUNCTIONS NORMALLY. OPENED & CLOSED L1 DOOR NUMEROUS TIMES PER A300 AMM 52-10-00. NO ABNORMAL RESISTANCE NOTED. ARMED & DISARMED SLIDE MULTIPLE TIMES PER A300 AMM 52-73-00. NOJun 23, 2026 · N127UP · Airbus A300F4622R · Passenger/Crew DoorsSDR IPXA2026061720384Computer · faultedDURING GEAR EXTENSION ECAM FWS-CRT AMBER CAUTION NOT AVAIL, ENG 1, LG WHEEL, ATS FUEL AFT TRANSFER NA, LEFT BRAKES KEEP SHOOTING UP TO ABOVE 300 C. A/C NORMAL WITH HANDLING SO LANDED. AIRCRAFT RETURNED TO FULL CAT STATUS.Jun 17, 2026 · N127UP · Airbus A300F4622R · Landing Gear SystemSDR IPXA2025072931607Slide · rupturedWHILE WORKING D/D MEL-L1 DOOR SLIDE, FOUND DOOR DAMPER PRESS LOW, AND DIAPHRAGM RUPTURED. VERIFIED ALL LOCKOUT PINS REMOVED FROM DOOR DAMPNER AND ALL OPS CHECKS GOOD IAW AMM 52-10-14Jul 26, 2025 · N127UP · Airbus A300F4622R · Escape SlideSDR IPXA2025072252379Arming Lever · faultedUNABLE TO ARM DOOR. DMP C/W.Jul 22, 2025 · N127UP · Airbus A300F4622R · Passenger/Crew DoorsSDR IPXA2025070105651Slide · no discrepancyUNABLE TO ARM SLIDE AFTER CLOSING DOOR ADJUSTED GIRT BAR ASSEMBLY REF AMM 25-61-21. DOOR OPERATES CORRECTLY AT THIS TIME. DEFERRAL CLEARED PLACARDS REMOVED.Jul 1, 2025 · N127UP · Airbus A300F4622R · Escape SlideSDR IPXA2025052074149Fitting · dirtyPILOT REPORTS L1 DOOR SLIDE WOULD NOT ARM AT DEPARTURE. INSPECTED DOOR, CLEANED GIRT BAR FLOOR ATTACHMENT POINTS, OPS CHECK GOOD W/ SLIDE INDICATION ON ECAM. AMM 52-10-11May 20, 2025 · N127UP · Airbus A300F4622R · Emergency EquipmentSDR IPXA2025021322729Bottle · low pressureL1 DOOR SLIDE LOW PRESSURE. REVERSED DMP 52-11-01-2-3, REPLACED DOOR SLIDE ASSEMBLY IAW AMM 25-61-21-401 DEFERRAL CLEARED PLACARD REMOVED. ACCOMPLISHED RII STEPS PER GMM 04-02.Feb 13, 2025 · N127UP · Airbus A300F4622R · Escape SlideSDR IPXA2024072637979Rib · crackedLH CENTER FLAP CRACK RIB 25 ACCOMPLISH REPAIR IN ACCORDANCE WITH EO-90495-REQ1 AND VT-MAE EA 300-5750-27-A3607, REV. -. REVIEWEDJun 13, 2024 · N127UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2024061737979Rib · crackedLEFTCENTER FLAP CRACKED RIB 25.Jun 13, 2024 · N127UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2024072376565Fitting · cracked*SUPPLEMENTAL SDR* FAULT: FWD CREW DOOR AFT LOWER FITTING HAS A CRACK REMOVED AND REPLACED LOWER FITTING CRACK FWD CREW DOOR IAW AMM 52-10-31/401 P/N A5211038420401 BATCH 0004293554. REVIEWEDJun 3, 2024 · N127UP · Airbus A300F4622R · Passenger/Crew DoorsSDR IPXA2024060476565Stop Fitting · crackedFWD CREW DOOR AFT LOWER FITTING STOP CRACKED. OPENJun 3, 2024 · N127UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2024062873248Bulkhead · damaged8 HOLES ON REAR PRESSURE BULKHEAD APU BLEED AIR CUT OUT HAVE DAMAGE. CLEANED 3 EA HOLES IAW SRM 51-40-44 ON APU BLEED AIR CUT OUT. ROTO PERFORMED ON 1 HOLE AT BOTTOM OF THE APU BLEED AIR CUTOUT. NO INDICATIONS FOUND. IAW NTM 51-10-01.May 27, 2024 · N127UP · Airbus A300F4622R · APU Cowling/ContainmentSDR IPXA2024062345856Frame · crackedDAMAGE FOUND IN TOP HOLE, & CRACK FOUND IN MIDDLE HOLE ON FR40 LH UPPER TENSION BOLTS. CLEANED HOLES TOP HOLE AND MIDDLE HOLE ON FR 40 UPPER TENSION BOLT LH SIDE I.A.W. A300-600 SRM 51-73-10.May 24, 2024 · N127UP · Airbus A300F4622R · Fuselage Main, FrameSDR IPXA2024072208143Frame · damagedDAMAGE FOUND IN HOLES (A, B, C, D, E, F, P) ON FR47 RH HORIZONTAL JUNCTION. AREAS MARKED IN RED. ACCOMPLISHED THE REPAIR PER UPS EO: EO-90872-REQ1 AND VT MAE FINAL EA 300-5710-27-A3621 REV. -.May 22, 2024 · N127UP · Airbus A300F4622R · Fuselage Main, FrameSDR IPXA2024061365489Rib · crackedTHE R/H CENTER FLAP ASSY, HAS A CRACK (1EA) AT RIB LOCATION 26, AFT SIDE. INSTALLED DOUBLER. IAW A300-600 SRM 51-40-21 AND SRM 57-50-00 REVIEWEDMay 20, 2024 · N127UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2024061336460Structure · crackedTHE L/H CENTER FLAP ASSY, HAS MULTIPLE CRACKS (2EA) AT RIB LOCATION 27, AFT SIDE. ACCOMPLISHED REPAIR IN ACCORDANCE WITH EO-90495-REQ1 AND VT-MAE EA 300-5750-27-A3607, REV. -. JOB COMPLETE. VERIFIED. REVIEWEDMay 17, 2024 · N127UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2024061336422Rib · crackedTHE L/H CENTER FLAP ASSY, HAS A CRACK (1EA) AT RIB LOCATION 26, AFT SIDE. ACCOMPLISHED REPAIR IN ACCORDANCE WITH EO-90495-REQ1 AND VT-MAE EA 300-5750-27-A3607, REV. -. JOB COMPLETE. VERIFIED. REVIEWEDMay 17, 2024 · N127UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2024061336403Rib · crackedTHE L/H CENTER FLAP ASSY, HAS A CRACK (1EA) AT RIB LOCATION 25, AFT SIDE. ACCOMPLISH REPAIR IN ACCORDANCE WITH EO-90495-REQ1 AND VT-MAE EA 300-5750-27-A3607, REV. -.May 17, 2024 · N127UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2024062810799Skin · damagedMDC DOOR AFT MIDDLE FUSELAGE SKIN WITH DAMAGE REMOVED NEGLIGIBLE SURFACE DISCREPANCY BY HAND WITH SCOTCH BRITE THAT WAS NOTED IN PAINT SURFACE ONLY IAW SRM 51-73-11 AND NO MATERIAL LOSS WAS NOTED. OK TO TREAT AND PRIME. RESTORED SURFACE PROTECTION IAW SRM 51-2May 16, 2024 · N127UP · Airbus A300F4622R · Fuselage Main, Plate/SkinSDR IPXA2024062860200Hinge · damagedDAMAGE FOUND IN HOLES ON MIDDLE HINGE. STEEL (14D) ALUMINIUM (12F, 13F, 15F). CLEANED HOLE (14D AND 15F) IAW SRM 51-73-10 AND REAMING HOLES (12F AND 13F) SIZE .281 IAW SRM 51-40-21. ROTO INSPECTION PERFORMED IAW NTM 51-10-01 PT 6. ALL HOLES ARE DEFECT FREE.May 14, 2024 · N127UP · Airbus A300F4622R · Fuselage, Door HingeSDR IPXA2024062760200Hinge · damagedDAMAGE FOUND IN HOLES ON MIDDLE HINGE. STEEL (14D) ALUMINIUM (12F, 13F, 15F). OPENMay 14, 2024 · N127UP · Airbus A300F4622R · Fuselage Structure (General)SDR IPXA2024062742586Web · crackedAGING ACFT INSP.- FRAME WEB BETWEEN FRAME 86L AND 87L IN AFT ACCESORY COMPT. ARE BENT AND CRACKED. DOT AA025. INSTALLED FRAME WEB BETWEEN FRAME 86 & 87 LH STGR 34 IAW SRM 51-40-21 P/N:CR3213-5-02, BTCH:0004070310. APPLIED CIC AT FRAME WEB BETWEEN FR 86 & 87 LHMay 13, 2024 · N127UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2024070830033Floorbeam · crackedFAULT STR FUSELAGE RH SIDE BETWEEN (Y= -450 TO Y= -953) FR 50 CROOSBEAM CROKED DOT 108-120. INSTALLED NEW CROSSBEAN IAW SRM 51-40-21 AND APPLIED CIC IAW EO NO:M-5100-2780-L. REVIEWEDMay 12, 2024 · N127UP · Airbus A300F4622R · Fuselage Main, Floor BeamSDR IPXA2024070830019Floorbeam · crackedFAULT STR FUSELAGE RH SIDE BETWEEN (Y= -450 TO Y= -953 FR 51 CROOSBEAM BROKEN DOT 108-119. VERIFIED CROSSBEAM REPLACEMENT AND INSTALLATION PER IAW A300-600 SRM 51-40-21. REVIEWEDMay 12, 2024 · N127UP · Airbus A300F4622R · Fuselage Main, Floor BeamSDR IPXA2024072425041Splice · crackedDAMAGE FOUND IN HOLES (A, E, L, M, AND N) CRACK/DAMAGE FOUND IN HOLE (H) ON FR47 LH SPLICE FITTING. AREAS MARKED IN RED. ACCOMPLISHED THE REPAIR PER EO-90930-REQ1 AND EA 300-5315-27-A3616 REV. -. JOB COMPLETE. REVIEWEDMay 11, 2024 · N127UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2024062923528Access Panel · crackedL/H WING ACCESS PANEL 577DT HAS A COMPOSITE CRACK ON THE INNER SIDE. DOT 110/01. REPAIRED CRACKED AREA IAW AMM A300 53-15-63/801 PARA C.2.A-F. 08-010 (EA 934) BATCH 4271892.May 11, 2024 · N127UP · Airbus A300F4622R · Wing, Plate/SkinSDR IPXA2024062707930Structure · crackedCRACKS/DAMAGE FOUND IN ALL 3 HOLES ON FR40 RH UPPER TENSION BOLTS. TOP HOLE (3 SMALL CRACKS IN 1ST LAYER) MIDDLE HOLE (PITTED CORROSION AT START OF HOLE) BOTTOM HOLE (CRACK AT START OF HOLE). ACCOMPLISHED REPAIR IN ACCORDANCE WITH EO-90914-REQ1 AND VT-MAE EA 3May 10, 2024 · N127UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2024062789486Floor Support · crackedAFT CARGO FR 54 L/H O/B HAS A CRACKED FLOOR SUPPORT BRACKET. INSTALLED FLOOR SUPPORT FR 54/LH IAW 51-40-21 A300-600. REVIEWEDMay 9, 2024 · N127UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2024062788979Floor Support · crackedAFT CARGO FLOOR SUPPORT R/H MIDDLE AT FR 54 IS CRACKED. APPLIED TOP COAT ON FLOOR SUPPORT I.A.W. SRM 51-75-10, AND INSTALLED FLOOR SUPPORT I.A.W. SRM 51-40-20. REVIEWEDMay 9, 2024 · N127UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2024072669041Seal · tornCREW ENTRY DOOR SEAL AFT MIDDLE AREA HAS TORN COVERING IN SEVERAL PLACES DOT47-03 REMOVED AND REPLACED MAIN ENTRY DOOR SEAL IAW AMM 52-10-18/401 T95749. P/N F521813562000. BATCH 0004290380. REVIEWEDMay 8, 2024 · N127UP · Airbus A300F4622R · Passenger/Crew DoorsSDR IPXA2024050969041Seal · torn**SDR FILED OPEN**FAULT CREW ENTRY DOOR SEAL AFT MIDDLE AREA HAS TORN COVERING IN SEVERAL PLACES DOT47-03May 8, 2024 · N127UP · Airbus A300F4622R · Passenger/Crew DoorsSDR IPXA2024070855351Nose Cowl · crackedENGINE #2 NOSE COWL FRON SIDE, LIP WITH CRACK IN POSITION 10 HRS, APROX 0,5 INCH DOT 108-110. INSTALLED DOUBLER AND FILLER ON AREA OF #2 NOSE COWL FRONT SIDE, I.A.W. PWA SRM 54-10-00, FIGURE 204.May 7, 2024 · N127UP · Airbus A300F4622R · Turbine Engine Air Inlet SectionSDR IPXA2024072335114Bulkhead · corrodedFAULT FWD CARGO COMPT AFT BULKHEAD FR39 UPPER TOP AREAS HAS 3 AREAS OF EXFOLIATING CORROSION MARKED WITH RED TAPE DOT 47-01 ACCOMPLISHED PERMANENT REPAIR PER EO-90839-REQ1 AND EA 300-5315-27-A3601 REV. -. JOB COMPLETE. REVIEWEDMay 6, 2024 · N127UP · Airbus A300F4622R · Fuselage Main, BulkheadSDR IPXA2023071793669Apu · inoperativeINSPECTION TYPE:NA*DIVERSION* DURING CRUISE APU AUTO SHUTDOWN APU OIL QTY BELOW MIN INDICATED. DIVERT TO BIL DUE ENG 2 B SYSTEM IGN DIVERT 1205Z AND APU REQ PER MELFOUND LOOSE B NUT ON LINE FOM OIL PUMP OUTLET. TIGHTENED PER AMM 49-90-00. LINE NUT OPS CHECKED Jul 14, 2023 · N127UP · Airbus A300F4622R · Airborne Auxiliary Power Unit (APU) SystemSDR IPXA2023011289822Lamp · inoperativeEMERGENCY "EXIT" SIGN HAS 3 EA LAMPS INOPRELAMPED & OPS NORMAL W/REF TO MM 33-51-00 PB 0501Jan 11, 2023 · N127UP · Airbus A300F4622R · Emergency LightingSDR IPXA2023010389546Brake Assy · malfunctionedBTB: 1250 PULSATING BRAKES AT VARIOUS TAXI SPEED. BRAKES HIGHER THAN NORMAL TEMPPILOTS NOTED BRAKES 5 AND 6 TEMP HIGH. INSPECTED BRAKES 5 AND 6. NO DISCREPANCIES NOTED WHEN JACKED AND OPS CHECKED FOIUND 040 FAULT ON BSCU. REMOVED AND REPLACED BSCU IAW A300 AMMDec 27, 2022 · N127UP · Airbus A300F4622R · Landing Gear Brake SystemSDR IPXA2022110487837Warning Light · inoperativeINSPECTION TYPE:NA*SUPPLEMENTAL SDR* EVACUATION SLIDE WARNING SYSTEM LIGHT INOP. DEFERRED WARNING LIGHT IAW MEL 52-73-01-1. PLACARD INSTALLED. NIL DMP. C/N M794640 ASSIGNED.R/R ASPSU OUTBD BATTERY & INBD BATTERY REF AMM 52-73-11 PB 0401. SYSTEM OPS NORMAL. THINov 3, 2022 · N127UP · Airbus A300* · Door Warning SystemSDR IPXA2021112076176None · noneINSPECTION TYPE:NACANNOT PREFLIGHT THE ESCAPE SLIDE, PRESSURE GAUGE IS NOT VISIBLE IN THE SLIDE PACK HOUSING WINDOW.R/R DOOR SLIDE PER MM 25-61-21-0401. THIS CLEARS M763622.Nov 20, 2021 · N127UP · Airbus A300F4622R · Emergency ExitsSDR IPXA2021110475596None · noneINSPECTION TYPE:NA** SUPPLEMENTAL SDR ** THE DOOR SLIDE DOES NOT SHOW ARMED ON ECAM WITH DOOR CLOSED AND SLIDE IN ARMED POSITION. DEFERED PER MEL 52-30-04, PLACARD INSTALLED.FOUND CONNECTOR 13WN-A UNPLUGGED. RECONNECTED PLUG OPS CHECK PER 52-73-00-0001 PARA8. Nov 2, 2021 · N127UP · Airbus A300F4622R · Passenger/Crew DoorsSDR IPXA2021102975450Frame · crackedINSPECTION TYPE:SEGFUSELAGE FRAME FOOT FITTING LH SIDE FRAME 44, IS CRACKED AT AREA 1.ACCOMPLISHED REPAIR PER APPENDIX J OF EO A300-5310-46789-GOct 29, 2021 · N127UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2021102975449Frame · crackedINSPECTION TYPE:SEGFUSELAGE FRAME FOOTING AT LH SIDE FRAME 45, IS CRACKED AT AREA 1ACCOMPLISHED REPAIR PER APPENDIX J OF EO. A300-5310-46789-GOct 29, 2021 · N127UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2021102975448Frame · crackedINSPECTION TYPE:SEGFUSELAGE FRAME FOOT FITTING AT LH SIDE FRAME 46 IS CRACKED AT AREA 1.ACCOMPLISHED REPAIR PER APPENDIX K OF EO. A600-5310-46789-G.Oct 29, 2021 · N127UP · Airbus A300F4622R · Fuselage Main, Structure
Back to N127UP