# Service difficulty reports: N130UP

A list on [N130UP](https://openairdocs.org/aircraft/N130UP.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 6 · 251 reports

- [SDR IPXA2026061951038](https://openairdocs.org/sdr/IPXA2026061951038.md): Indication Sys · intermittent · Jun 19, 2026 · N130UP · Airbus A300F4622R · Door Warning System
  > WITH 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.
- [SDR IPXA2026050904243](https://openairdocs.org/sdr/IPXA2026050904243.md): Annunciator · faulted · May 9, 2026 · N130UP · Airbus A300F4622R · Door Warning System
  > MAIN 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 SL
- [SDR IPXA2026042226341](https://openairdocs.org/sdr/IPXA2026042226341.md): Slide · malfunctioned · Apr 22, 2026 · N130UP · Airbus A300F4622R · Escape Slide
  > SLIDE 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 REMOVE
- [SDR IPXA2026010897482](https://openairdocs.org/sdr/IPXA2026010897482.md): Gauge · failed · Jan 7, 2026 · N130UP · Airbus A300F4622R · Central Warning
  > AIR 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 FAI
- [SDR IPXA2025080500763](https://openairdocs.org/sdr/IPXA2025080500763.md): Light · inoperative · Aug 4, 2025 · N130UP · Airbus A300F4622R · Emergency Lighting
  > L1 EMERGENCY LIGHT ABOVE DOORWAY HAS LIGHT INOPERATIVE ON LOWER SIDE OF ASSY. REMOVED AND REPLACED LIGHT PER AMM 33-51-13. OPS CHECK OK.
- [SDR IPXA2025062040113](https://openairdocs.org/sdr/IPXA2025062040113.md): Bracket · cracked · Jun 10, 2025 · N130UP · Airbus A300F4622R · Engine Thrust Reverser
  > #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 51-40-21
- [SDR IPXA2025062325275](https://openairdocs.org/sdr/IPXA2025062325275.md): Precooler · cracked · Jun 9, 2025 · N130UP · Airbus A300F4622R · Pneumatic Distribution System
  > FAULT: 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 36-11-15/401
- [SDR IPXA2025062315518](https://openairdocs.org/sdr/IPXA2025062315518.md): Strap · cracked · Jun 9, 2025 · N130UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > AFT 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.
- [SDR IPXA2025062014520](https://openairdocs.org/sdr/IPXA2025062014520.md): Intercostal · deformed · Jun 9, 2025 · N130UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > AFT 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.
- [SDR IPXA2025062514520](https://openairdocs.org/sdr/IPXA2025062514520.md): Intercostal · cracked · Jun 9, 2025 · N130UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > AFT FUSELAGE INTERIOR BETWEEN FR85 - FR86 1EA INTERCOASTAL DEFORMED AT S31R
- [SDR IPXA2025070697137](https://openairdocs.org/sdr/IPXA2025070697137.md): Frame · cracked · Jun 7, 2025 · N130UP · Airbus A300F4622R · Fuselage Main, Frame
  > CRACK 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 ASNA25
- [SDR IPXA2025070697371](https://openairdocs.org/sdr/IPXA2025070697371.md): Frame · cracked · Jun 7, 2025 · N130UP · Airbus A300F4622R · Fuselage Main, Frame
  > CRACK 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 T
- [SDR IPXA2025061996386](https://openairdocs.org/sdr/IPXA2025061996386.md): Seat Track · corroded · Jun 7, 2025 · N130UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings
  > FAULT-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,
- [SDR IPXA2025062401415](https://openairdocs.org/sdr/IPXA2025062401415.md): Angle · corroded · Jun 7, 2025 · N130UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > CORROSION 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.
- [SDR IPXA2025062497939](https://openairdocs.org/sdr/IPXA2025062497939.md): Floor Panel · broken · Jun 7, 2025 · N130UP · Airbus A300F4622R · Fuselage Floor Panel
  > FLOOR PANEL 222EG BROKEN AT THE CORNER. FABRICATED FLOOR PANEL 221EG, IAW SREO-40552-REQ001.
- [SDR IPXA2025062501415](https://openairdocs.org/sdr/IPXA2025062501415.md): Angle · corroded · Jun 7, 2025 · N130UP · Airbus A300F4622R · Fuselage Main, Structure
  > CORROSION AT FR39 FWD PIT AT HORIZONTAL PRESSURE DECK UPPER SUFACE LH/RH SIDE. DOT 140-1544 REJECT MEASUREMENT TASK MUST BE COMPLETED /CORRECTED.
- [SDR IPXA2025062096175](https://openairdocs.org/sdr/IPXA2025062096175.md): Adapter · corroded · Jun 7, 2025 · N130UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > MCD 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 RE
- [SDR IPXA2025061600746](https://openairdocs.org/sdr/IPXA2025061600746.md): Angle · cracked · Jun 7, 2025 · N130UP · Airbus A300F4622R · Trailing Edge Flaps
  > LH 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 FOR
- [SDR IPXA202507180732](https://openairdocs.org/sdr/IPXA202507180732.md): Floor Panel · broken · Jun 6, 2025 · N130UP · Airbus A300F4622R · Fuselage Floor Panel
  > MDC FLOOR PANEL 232NJ IS BROKEN REVIEWED
- [SDR IPXA2025070280732](https://openairdocs.org/sdr/IPXA2025070280732.md): Floor Panel · damaged · Jun 6, 2025 · N130UP · Airbus A300F4622R · Fuselage Floor Panel
  > MDC FLOOR PANEL 232NJ IS BROKEN. FABRICATED FLOOR PANEL 232NJ, IAW SREO-40552-REQ001.
- [SDR IPXA2025062575431](https://openairdocs.org/sdr/IPXA2025062575431.md): Beam · corroded · Jun 6, 2025 · N130UP · Airbus A300F4622R · Wing Main, Frame Structure
  > LEFT 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. REVIEWED
- [SDR IPXA2025062680732](https://openairdocs.org/sdr/IPXA2025062680732.md): Floor Panel · damaged · Jun 6, 2025 · N130UP · Airbus A300F4622R · Fuselage Floor Panel
  > MDC 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: 0004370926
- [SDR IPXA2025062060343](https://openairdocs.org/sdr/IPXA2025062060343.md): Adapter · corroded · Jun 5, 2025 · N130UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > CLS 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. -.
- [SDR IPXA2025062539189](https://openairdocs.org/sdr/IPXA2025062539189.md): Seat Track · corroded · Jun 4, 2025 · N130UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings
  > FR72-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.
- [SDR IPXA2025062645098](https://openairdocs.org/sdr/IPXA2025062645098.md): Plate · dented · Jun 4, 2025 · N130UP · Airbus A300F4622R · Vertical Stabilizer
  > RIGHT HORZ STAB PANEL 342AB L/E HAS 10EA DENTS-109-VWV. INSTALLED NEW PLATE IAW SRM 51-40-21.
- [SDR IPXA2025060933591](https://openairdocs.org/sdr/IPXA2025060933591.md): Angle · cracked · Jun 4, 2025 · N130UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > CREW 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.
- [SDR IPXA2025060742155](https://openairdocs.org/sdr/IPXA2025060742155.md): Crossbeam · bent · Jun 4, 2025 · N130UP · Airbus A300F4622R · Fuselage Main, Structure
  > CROSSBEAM 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#T976
- [SDR IPXA2025060742207](https://openairdocs.org/sdr/IPXA2025060742207.md): Floorbeam · bent · Jun 4, 2025 · N130UP · Airbus A300F4622R · Fuselage Main, Floor Beam
  > CROSS 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 6
- [SDR IPXA2025060742228](https://openairdocs.org/sdr/IPXA2025060742228.md): Floorbeam · bent · Jun 4, 2025 · N130UP · Airbus A300F4622R · Fuselage Main, Floor Beam
  > CROSSBEAM 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 6
- [SDR IPXA2025061925543](https://openairdocs.org/sdr/IPXA2025061925543.md): Rib · cracked · Jun 3, 2025 · N130UP · Airbus A300F4622R · Trailing Edge Flaps
  > MAJOR 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. -.
- [SDR IPXA2025061925742](https://openairdocs.org/sdr/IPXA2025061925742.md): Rib · cracked · Jun 3, 2025 · N130UP · Airbus A300F4622R · Trailing Edge Flaps
  > MAJOR 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. -.
- [SDR IPXA2025061925105](https://openairdocs.org/sdr/IPXA2025061925105.md): Rib · cracked · Jun 3, 2025 · N130UP · Airbus A300F4622R · Trailing Edge Flaps
  > MAJOR 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. -.
- [SDR IPXA2025061925656](https://openairdocs.org/sdr/IPXA2025061925656.md): Rib · cracked · Jun 3, 2025 · N130UP · Airbus A300F4622R · Trailing Edge Flaps
  > MAJOR 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. -.
- [SDR IPXA2025061925522](https://openairdocs.org/sdr/IPXA2025061925522.md): Rib · cracked · Jun 3, 2025 · N130UP · Airbus A300F4622R · Trailing Edge Flaps
  > MAJOR 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. -.
- [SDR IPXA2025061925238](https://openairdocs.org/sdr/IPXA2025061925238.md): Rib · cracked · Jun 3, 2025 · N130UP · Airbus A300F4622R · Trailing Edge Flaps
  > MAJOR 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. -.
- [SDR IPXA2025061925447](https://openairdocs.org/sdr/IPXA2025061925447.md): Rib · cracked · Jun 3, 2025 · N130UP · Airbus A300F4622R · Trailing Edge Flaps
  > THE 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.
- [SDR IPXA2025061925247](https://openairdocs.org/sdr/IPXA2025061925247.md): Rib · cracked · Jun 3, 2025 · N130UP · Airbus A300F4622R · Trailing Edge Flaps
  > THE 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.
- [SDR IPXA2025062612503](https://openairdocs.org/sdr/IPXA2025062612503.md): Panel · cracked · Jun 3, 2025 · N130UP · Airbus A300F4622R · Wing, Plate/Skin
  > CRACKS 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.
- [SDR IPXA2025062011769](https://openairdocs.org/sdr/IPXA2025062011769.md): Rub Strip · chafed · Jun 3, 2025 · N130UP · Airbus A300F4622R · Engine Thrust Reverser
  > NR 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 00
- [SDR IPXA2025061225823](https://openairdocs.org/sdr/IPXA2025061225823.md): Profile · cracked · Jun 3, 2025 · N130UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > MDC 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
- [SDR IPXA2025061924955](https://openairdocs.org/sdr/IPXA2025061924955.md): Rib · cracked · Jun 3, 2025 · N130UP · Airbus A300F4622R · Trailing Edge Flaps
  > THE 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.
- [SDR IPXA2025061402667](https://openairdocs.org/sdr/IPXA2025061402667.md): Seat Track · corroded · Jun 2, 2025 · N130UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings
  > SEAT 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.
- [SDR IPXA2025061202813](https://openairdocs.org/sdr/IPXA2025061202813.md): Angle · cracked · Jun 2, 2025 · N130UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > Z 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.
- [SDR IPXA2025062005068](https://openairdocs.org/sdr/IPXA2025062005068.md): Adapter · broken · Jun 2, 2025 · N130UP · Airbus A300F4622R · Fuselage Main, Structure
  > CLS 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.
- [SDR IPXA2025061202780](https://openairdocs.org/sdr/IPXA2025061202780.md): Profile · cracked · Jun 2, 2025 · N130UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > Z 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.
- [SDR IPXA2025062502828](https://openairdocs.org/sdr/IPXA2025062502828.md): Profile · cracked · Jun 2, 2025 · N130UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > Z 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.
- [SDR IPXA2025062502737](https://openairdocs.org/sdr/IPXA2025062502737.md): Profile · cracked · Jun 2, 2025 · N130UP · Airbus A300F4622R · Fuselage Main, Structure
  > PROFILE 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.
- [SDR IPXA2025041510432](https://openairdocs.org/sdr/IPXA2025041510432.md): Tensioner · disconnected · Apr 15, 2025 · N130UP · Airbus A300F4622R · Passenger/Crew Doors
  > ENTRY 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.
- [SDR IPXA2025032332357](https://openairdocs.org/sdr/IPXA2025032332357.md): Skin · damaged · Mar 19, 2025 · N130UP · Airbus A300F4622R · Fuselage Main, Plate/Skin
  > MAJOR REPAIR, L/H FORWARD FUSELAGE SECTION DAMAGE BETWEEN FR26 AND FR28 PERFORMED REPAIR IAW EO-93137-REQ1.
- [SDR IPXA202503212357](https://openairdocs.org/sdr/IPXA202503212357.md): Skin · damaged · Mar 19, 2025 · N130UP · Airbus A300F4622R · Fuselage Main, Plate/Skin
  > L/H FORWARD FUSELAGE SECTION DAMAGE BETWEEN FR26 AND FR28.

Next page: https://openairdocs.org/aircraft/N130UP/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/aircraft/N130UP/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.