N130UP

Service difficulty reports · 251

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 = 'N130UP' 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 IPXA2026061951038Indication Sys · intermittentWITH SLIDE ARMED THE SLIDE LIGHTS TURN OFF AND ON INTERMITTENTLY. REPLACED 13WN LIMIT SWITCH ON L1 DOOR PER A300 AMM 52-73-13. OPS TEST PASS.Jun 19, 2026 · N130UP · Airbus A300F4622R · Door Warning SystemSDR IPXA2026050904243Annunciator · faultedMAIN ENTRY DOOR SLIDE ANNUNCIATOR ON ECAM IS ERRATICALLY / FLICKERING ON AND OFF IN FLIGHT. ACCOMPLISHED WIGGLE TEST ON CONNECTOR 13WNA, FOUND CONNECTION INTERMITTENT. REPLACED CONNECTOR 13WNA IAW ESPM 20-44-11-01. ACCOMPLISHED OPS CHECK OF SWITCH 13WN DOOR SLMay 9, 2026 · N130UP · Airbus A300F4622R · Door Warning SystemSDR IPXA2026042226341Slide · malfunctionedSLIDE ON DOOR ECAM, INDICATING SLIDE ARMED, FLASHED ON & OFF SEVERAL TIMES AFTER ARMING SLIDE. ARMED SLIDE CONFIRMED ISSUE. CYCLED POWER TO FIN 70WN IAW AMM 53-73-18 OPS CHECK GOOD. ARMED DOOR MULTIPLE TIME LIGHT REMAINED ON ECAM. REVERSED DMP, PLACARD REMOVEApr 22, 2026 · N130UP · Airbus A300F4622R · Escape SlideSDR IPXA2026010897482Gauge · failedAIR TURN BACK, NR 1 N1 & EGT GAUGE FAILURE THEN INTERMITTENT OPERATION ENG 1 FAILURE ECAM AND ENG #1 REVERSE UNLOCK ECAM. FMC REVERTED TO ENGINE OUT MODE. REPLACED #1 ENGINE LEFT FAN CASE HARNESS 21W4118 PER AMM 71-51-01/401 DUE TO D4998P LOCKING MECHANISM FAIJan 7, 2026 · N130UP · Airbus A300F4622R · Central WarningSDR IPXA2025080500763Light · inoperativeL1 EMERGENCY LIGHT ABOVE DOORWAY HAS LIGHT INOPERATIVE ON LOWER SIDE OF ASSY. REMOVED AND REPLACED LIGHT PER AMM 33-51-13. OPS CHECK OK.Aug 4, 2025 · N130UP · Airbus A300F4622R · Emergency LightingSDR IPXA2025062040113Bracket · cracked#2 ENGINE INBD T/R HOLD OPEN ACTUATOR LINE LOWER FITTING CRACKED JP-110.REMOVED AND REPLACED 01 BRACKET P/N 221-6559-501, BTCH #0004403418. IAW A300/600, SRM 51-40-21Jun 10, 2025 · N130UP · Airbus A300F4622R · Engine Thrust ReverserSDR IPXA2025062325275Precooler · crackedFAULT: APG: #2 ENGINE PRECOOLER HAS BODY CRACKS.REMOVED #2 ENGINE PRECOOLER, IAW A300-AMM 36-11-15/401.INSTALLED NEW #2 ENGINE PRECOOLER, IAW A300-AMM 36-11-15/401Jun 9, 2025 · N130UP · Airbus A300F4622R · Pneumatic Distribution SystemSDR IPXA2025062315518Strap · crackedAFT FUSELAGE INT 1EA INTERCOASTAL BETWEEN FR86-FR87 DEFORMED AT S37R. INSTALLED NEW PROFILE-L AT AFT FUSELAGE BETWEEN FR86-FR87 S37R, IAW A300-600 SRM 51-40-21.Jun 9, 2025 · N130UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2025062014520Intercostal · deformedAFT FUSELAGE INTERIOR BETWEEN FR85 - FR86 1EA INTERCOSTAL DEFORMED AT S31R. INSTALLED NEW PROFILE-L AT AFT FUSELAGE BETWEEN FR85-FR86 S31 R/H, IAW A300-600 SRM 51-40-21.Jun 9, 2025 · N130UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2025062514520Intercostal · crackedAFT FUSELAGE INTERIOR BETWEEN FR85 - FR86 1EA INTERCOASTAL DEFORMED AT S31RJun 9, 2025 · N130UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2025070697137Frame · crackedCRACK FOUND ON RH FR47 HORIZONTAL JUNCTION HOLE P.REAMED HOLE TO .593 IAW SRM-51-40-44 ALSO IN COMPLIANCE WITH EA-300-5710-27-A3997.PERFORMED ROTO ON RH FR47 HORIZONTAL JUNCTION HOLE P. WET INSTALLED BOLT IN HOLE "P" P/N EN6114V10 B# 0004403579 NUT P/N ASNA25Jun 7, 2025 · N130UP · Airbus A300F4622R · Fuselage Main, FrameSDR IPXA2025070697371Frame · crackedCRACK FOUND ON FR47 LH HORIZONTAL JUNCTION HOLE C. REAMED HOLE TO .528 IAW-A300-SRM-51-40-44 ALSO IN COMPLIANCE WITH EA-300-5710-27-A3998.PERFORMED ROTO ON LH HORIZONTAL JUNCTION HOLE C. MANUFACTURED REPAIR BUSHING ON TRAVELER # T25/1820352, REPAIR BUSHING TJun 7, 2025 · N130UP · Airbus A300F4622R · Fuselage Main, FrameSDR IPXA2025061996386Seat Track · corrodedFAULT-STR-Z200-FLOOR STRUCTURE BELOW FLOOR PANEL 232NJ, FR22 TO FR27 , Y0 RH HAVE SEVERAL SPOTS OF CORROSION. INSTALLED CLS TRACK ADAPETER AT FR 27 Y"0" USING SEALANT P/N PS 870 B2 B B# 0004362799, FASTNERS P/N HL11VF6-4 B# 0004394238, HL10VF6-5 B# 000406455,Jun 7, 2025 · N130UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2025062401415Angle · corrodedCORROSION AT FR39 FWD PIT AT HORIZONTAL PRESSURE DECK UPPER SUFACE LH/RH SIDE. INSTALLED NEW ANGLES NEW ANGLES (RETAINERS) FOR BOTH SIDES RH/LH ON SURFACE OF PRESSURE DECK FR39 IAW SRM 51-40-21.Jun 7, 2025 · N130UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2025062497939Floor Panel · brokenFLOOR PANEL 222EG BROKEN AT THE CORNER. FABRICATED FLOOR PANEL 221EG, IAW SREO-40552-REQ001.Jun 7, 2025 · N130UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2025062501415Angle · corrodedCORROSION AT FR39 FWD PIT AT HORIZONTAL PRESSURE DECK UPPER SUFACE LH/RH SIDE. DOT 140-1544 REJECT MEASUREMENT TASK MUST BE COMPLETED /CORRECTED.Jun 7, 2025 · N130UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2025062096175Adapter · corrodedMCD FLOOR STRUCTURE AREA FR34 / Y0, ADAPTER CLS CORRODED. ACCOMPLISHED E.A.#:300-5310-27-A3996, PRELIMINARY 1, STEP #11: "INSTALL 3 EACH CLS ADAPTERS AS FOLLOWING: ACCOMPLISH PERMANENT REPAIR IN ACCORDANCE WITH EO-94034-REQ1 AND VT-MAE EA 300-5310-27-A3996 REJun 7, 2025 · N130UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2025061600746Angle · crackedLH WING CENTER FLAP O/B TRAILING EDGE ANGLE BROKEN.REMOVED TRAILING EDGE ANGLE FROM L/H CENTER FLAP IAW A300-600 SRM 51-40-21.FABRICATED NEW TRAILING EDGE ANGLE FOR L/H WING CENTER FLAP IAW A300-600 SRM 51-27-00 AND UPS GMM 09.08.01.03. INSTALLED NEW ANGLE FORJun 7, 2025 · N130UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA202507180732Floor Panel · brokenMDC FLOOR PANEL 232NJ IS BROKEN REVIEWEDJun 6, 2025 · N130UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2025070280732Floor Panel · damagedMDC FLOOR PANEL 232NJ IS BROKEN. FABRICATED FLOOR PANEL 232NJ, IAW SREO-40552-REQ001.Jun 6, 2025 · N130UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2025062575431Beam · corrodedLEFT WING, UPPER SURFACE, O/B SIDE OF RIB 29, AROUND OF WICK AND BASE HAS CORROSION. DOT 103-62. INSTALLED AT Z500, STR, LH WING, UPPER SURFACE, O/B SIDE OF RIB 29 FILLER PLATE AND DOUBLER REPAIR IAW A300-600 SRM 57-30-11. REVIEWEDJun 6, 2025 · N130UP · Airbus A300F4622R · Wing Main, Frame StructureSDR IPXA2025062680732Floor Panel · damagedMDC FLOOR PANEL 232NJ IS BROKEN VERIFIED FABRICATED FLOOR PANEL 232NJ, WHIT P/N:5024N400001SS-G, BTCH: 0004055277, INSERTS P/N: G2001B-3P (56), BTCH: 0004142469 (56), P/N: G2002B-3S, BTCH: 0004370926Jun 6, 2025 · N130UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2025062060343Adapter · corrodedCLS ADAPTER EXFOLIATED WITH 100% MATERIAL LOSS AT FRAME 57.1, Y0 R/H SIDE ACCOMPLISH PERMANENT REPAIR IN ACCORDANCE WITH EO-94034-REQ1 AND VT-MAE EA 300-5310-27-A3996 REV. - .Jun 5, 2025 · N130UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2025062539189Seat Track · corrodedFR72-FR73, -Y1580.5 (PANEL 252EN AND 252KG ) SEAT TRACK HAVE CORROSION DOT 113-06. INSTALLED NEW SEAT TRACK AND NEW U-SECTION (SPLICE) AT MCD, FR72-FR73, -Y1580.5 IAW A300-600 SRM 51-40-21.Jun 4, 2025 · N130UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2025062645098Plate · dentedRIGHT HORZ STAB PANEL 342AB L/E HAS 10EA DENTS-109-VWV. INSTALLED NEW PLATE IAW SRM 51-40-21.Jun 4, 2025 · N130UP · Airbus A300F4622R · Vertical StabilizerSDR IPXA2025060933591Angle · crackedCREW DOOR, FLOOR AREA, NEAR C15A UNDER PANEL 221FF, STRIP SUPPORT HAS A CRACK DOT 103-25 INSTALED NEW ANGLE STRIP SUPPORT FOR STRUCTURE BELOW PANEL 221FF IAW A300-600 SRM 51-40-21.Jun 4, 2025 · N130UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2025060742155Crossbeam · bentCROSSBEAM AT FR 48 BETWEEN -Y450 AND -Y953 BENT. JP-110. INSTALLED NEW CROSSBEAM PART NUMBER# A5381337800001, BATCH NUMBER# 0004326890 AT FRAME 48 BETWEEN -Y 450 AND -Y 953, IAW A300-600 SRM 51-40-21, TORQUE VALUE IAW SRM 51-49-00, TABLE# 9, PAGE 6, TOOL#T976Jun 4, 2025 · N130UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2025060742207Floorbeam · bentCROSS BEAM AT FR 49 BETWEEN -Y450 AND -Y953 BENT. JP-110 VERIFIED INSTALLATION OF NEW CROSSBEAM PART NUMBER# A5381337800001, BATCH NUMBER# 0004325898 AT FRAME 49 BETWEEN -Y 450 AND -Y953, IAW A300-600 SRM 51-40-21, TORQUE VALUE IAW SRM 51-49-00 TABLE# 9,PAGE 6Jun 4, 2025 · N130UP · Airbus A300F4622R · Fuselage Main, Floor BeamSDR IPXA2025060742228Floorbeam · bentCROSSBEAM AT FR 50 BETWEEN -Y450 AND -Y953 BENT. JP-110 VERIFIED INSTALLATION OF NEW CROSSBEAM PART NUMBER A5381337800001, BATCH NUMBER# 0004325900 AT FRAME 50, BETWEEN -Y450 AND -Y953 IAW A300-600 SRM 51-40-21, TORQUE VALUE IAW SRM 51-49-00, TABLE# 9, PAGE 6Jun 4, 2025 · N130UP · Airbus A300F4622R · Fuselage Main, Floor BeamSDR IPXA2025061925543Rib · crackedMAJOR REPAIR, THE R/H CENTER FLAP ASSY HAS MULTIPLE CRACKS (2EA) AT RIB 26 AFT SIDE, IN THE TOP SKIN RIB FLANGE. ACCOMPLISHED PERMANENT REPAIR IN ACCORDANCE WITH EO-97043-REQ1 AND VT-MAE EA 300-5750-27-A4001, REV. -.Jun 3, 2025 · N130UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2025061925742Rib · crackedMAJOR REPAIR, THE LT CENTER FLAP ASSY HAS A CRACK (1EA) AT RIB 27 AFT SIDE, IN THE TOP SKIN RIB FLANGE. ACCOMPLISH REPAIR IN ACCORDANCE WITH EO-94074-REQ1 AND VT-MAE EA 300-5750-27-A4002, REV. -.Jun 3, 2025 · N130UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2025061925105Rib · crackedMAJOR REPAIR. THE RT CENTER FLAP ASSY HAS MULTIPLE CRACKS (2EA) AT RIB 13 AFT SIDE, IN THE TOP SKIN RIB FLANGE. ALL DAMAGE. ACCOMPLISHED PERMANENT REPAIR IN ACCORDANCE WITH EO-94073-REQ1 AND VT-MAE EA 300-5750-27-A4001, REV. -.Jun 3, 2025 · N130UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2025061925656Rib · crackedMAJOR REPAIR. THE RT CENTER FLAP ASSY HAS A CRACK (1EA) AT RIB 27 AFT SIDE, IN THE TOP SKIN RIB FLANGE. ALL DAMAGE. ACCOMPLISHED PERMANENT REPAIR IN ACCORDANCE WITH EO-97043-REQ1 AND VT-MAE EA 300-5750-27-A4001, REV. -.Jun 3, 2025 · N130UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2025061925522Rib · crackedMAJOR REPAIR, THE RT CENTER FLAP ASSY HAS A CRACK (1EA) AT RIB 25 AFT SIDE, IN THE TOP SKIN RIB FLANGE. ALL DAMAGE. ACCOMPLISHED PERMANENT REPAIR IN ACCORDANCE WITH EO-97043-REQ1 AND VT-MAE EA 300-5750-27-A4001, REV. -.Jun 3, 2025 · N130UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2025061925238Rib · crackedMAJOR REPAIR, THE R/H CENTER FLAP ASSY HAS A CRACK (1EA) AT RIB 16 AFT SIDE, IN THE TOP SKIN RIB FLANGE. ALL DAMAGE MARKED IN RED. ACCOMPLISHED PERMANENT REPAIR IN ACCORDANCE WITH EO-94073-REQ1 AND VT-MAE EA 300-5750-27-A4001, REV. -.Jun 3, 2025 · N130UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2025061925447Rib · crackedTHE RIGHT CENTER FLAP ASSY HAS A CRACK (1EA) AT RIB 18 AFT SIDE, IN THE TOP SKIN RIB FLANGE. ALL DAMAGE. ACCOMPLISHED PERMANENT REPAIR IN ACCORDANCE WITH EO-97043-REQ1 AND VT-MAE EA 300-5750-27-A4001, REV. -. MAJOR REPAIR.Jun 3, 2025 · N130UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2025061925247Rib · crackedTHE R/H CENTER FLAP ASSY HAS A CRACK (1EA) AT RIB 17 AFT SIDE, IN THE TOP SKIN RIB FLANGE. ALL DAMAGE. ACCOMPLISHED PERMANENT REPAIR IN ACCORDANCE WITH EO-97043-REQ1 AND VT-MAE EA 300-5750-27-A4001, REV. -. MAJOR REPAIR.Jun 3, 2025 · N130UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2025062612503Panel · crackedCRACKS AT RH WING T/E UPPER FIXED PANEL FWD OF NO.2 SPOILER. DOT NO. 17-05 NOTE: THIS FAULT IS ALREADY DEFERRED. DO NOT CLOSE. <BR>CONTACT GWC TO UNASSIGN FROM WORK PACKAGE AFTER ALL THE DOCUMENTATION AND AUDIT REQUIREMENTS ARE SATISFIED.Jun 3, 2025 · N130UP · Airbus A300F4622R · Wing, Plate/SkinSDR IPXA2025062011769Rub Strip · chafedNR 1 OUTBD. T/R AFT UPPER EDGE IS CHAFED FROM RAIN GAURD DOT#58-04 DARRYL FORD 91102506.REMOVED RUBSTRIP AT #1 OUTBD. T/R AFT UPPER EDGE, IAW A300-600 SRM 51-40-21.FABRICATED NEW RUBSTRIP, IAW GMM 09-08-01-03. MATERIAL USED: CRES SHEET P/N 321A .040SS BATCH 00Jun 3, 2025 · N130UP · Airbus A300F4622R · Engine Thrust ReverserSDR IPXA2025061225823Profile · crackedMDC FR75-77, Y1580.5 TO Y2127.5, Z ANGLE ON A CORNER OF FLOOR STR AREA, THERE IS A CRACK.REMOVED Z-PROFILE FROM MDC FR75 TO FR77 WITH CRACK IAW A300-600 SRM 51-40-21. FABRICATED Z-PROFILE USING MATERIAL 5052-H34.071, BATCH 0004399222, IAW GMM 09-08 PARAGRAPH Jun 3, 2025 · N130UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2025061924955Rib · crackedTHE R/H CENTER FLAP ASSY HAS MULTIPLE CRACKS (2EA) AT RIB 11 AFT SIDE, IN THE TOP SKIN RIB FLANGE. ALL DAMAGE MARKED IN RED. ACCOMPLISHED PERMANENT REPAIR IN ACCORDANCE WITH EO-94073-REQ1 AND VT-MAE EA 300-5750-27-A4001, REV. -. MAJOR REPAIR.Jun 3, 2025 · N130UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2025061402667Seat Track · corrodedSEAT TRACK EXFOLIATED AT FRAME 80 Y1137.1. INSTALLED SEAT TRACK AT FRAME 80 Y2127, IAW SRM 51-40-21 AND SRM 53-10-16 FIGURE 201 PAGE 207/208.Jun 2, 2025 · N130UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2025061202813Angle · crackedZ ANGLE CRACKED AT FRAME 80 ON L/H SIDE.REMOVED ANGLE CRACKED AT FRAME 80 ON L/H SIDE IAW SRM 51-40-21.LOCATED AND DRILL NEW ANGLE-T IAW A300-600 SRM 51-40-44. INSTALLED NEW ANGLE-T P/N#A5398140120100 BTCH#4403136 AT FRAME 80 ON L/H SIDE IAW SRM 51-40-21-001.Jun 2, 2025 · N130UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2025062005068Adapter · brokenCLS ADAPTER BROKEN AT FRAME 55 L/H SIDE Y 0. ACCOMPLISHED PERMANENT REPAIR IAW EO-94034-REQ1 AND VT-MAE EA 300-5310-27-A3996 REV. - . MAJOR REPAIR.Jun 2, 2025 · N130UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2025061202780Profile · crackedZ PROFILE CRACKED AT FRAME 73-75 ON L/H SIDE. INSTALLED NEW Z-PROFILE ON MCD BETWEEN FR 73 TO FR 75 L/H SIDE IAW SRM 51-40-21 AND SRM 51-76-10.Jun 2, 2025 · N130UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2025062502828Profile · crackedZ ANGLE CRACKED AT FRAME 80 ON R/H SIDE. INSTALLED NEW ANGLE-T P/N#A5398140120100 BTCH#4403136 AT FRAME 80 ON R/H SIDE IAW A300-600F SRM 51-40-21-001.Jun 2, 2025 · N130UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2025062502737Profile · crackedPROFILE CRACKED AT FRAME 73-75 ON R/H SIDE. INSTALLED NEW Z-PROFILE ON MCD BETWEEN FR 73 TO FR 75 R/H SIDE USING FASTENERS 55(EA) P/N MS20426AD5-7, BATCH 0004372118 AND SEALANT 1 (EA) P/N 04-001-0114, BATCH 0004362797, IAW SRM 51-40-21 AND SRM 51-76-10.Jun 2, 2025 · N130UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2025041510432Tensioner · disconnectedENTRY DOOR DAMPER TENSIONER FOUND DISCONNECTED ON INBOARD END. VERIFIED RIG PIN REMOVED, SPRING TENSIONER ASSY AND ATTACHMENT BOLT INSTALLED AND SECURED IAW AMM 52-10-14. OPS CHK GOOD.Apr 15, 2025 · N130UP · Airbus A300F4622R · Passenger/Crew DoorsSDR IPXA2025032332357Skin · damagedMAJOR REPAIR, L/H FORWARD FUSELAGE SECTION DAMAGE BETWEEN FR26 AND FR28 PERFORMED REPAIR IAW EO-93137-REQ1.Mar 19, 2025 · N130UP · Airbus A300F4622R · Fuselage Main, Plate/SkinSDR IPXA202503212357Skin · damagedL/H FORWARD FUSELAGE SECTION DAMAGE BETWEEN FR26 AND FR28.Mar 19, 2025 · N130UP · Airbus A300F4622R · Fuselage Main, Plate/Skin
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