# Service difficulty reports: N134UP

A list on [N134UP](https://openairdocs.org/aircraft/N134UP.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 8 · 355 reports

- [SDR IPXA2026013048711](https://openairdocs.org/sdr/IPXA2026013048711.md): Longeron · cracked · Jan 30, 2026 · N134UP · Airbus A300F4622R · Nacelle/Pylon, Longeron/Stringer
  > NR 1 PYLON LOWER AFT FAIRING 475AL FWD LONGERON HAS A CRACK AT FWD EDGE. STOP DRILLED CRACK 1.85" AFT OF LONGERON CRACK IAW A300 SRM 54-55-51 TABLE 101 SH 1 (F2). ++INSTALLED REPAIR ANGLE AT UPPER LONGERON USING FASTNERS P/N MS20470DD5-5 B# 0004403526 AND MS20
- [SDR IPXA2026021236278](https://openairdocs.org/sdr/IPXA2026021236278.md): Frame · cracked · Jan 29, 2026 · N134UP · Airbus A300F4622R · Nacelle/Pylon, Frame/Spar/Rib
  > NR 1 ENGINE LOWER AFT FAIRING 475AL FORWARD SKIN ASSY LH FWD FRAME HAS A CRACK. REMOVED DOUBLER P/N 221-0081-244 IAW A300-600, SRM 51-40-21. REMOVED FORWARD RIB DUE TO CRACK IAW A300-600 SRM 51-40-21. INSTALLED L/H FWD FRAME ASSY USING FASTNERS NAS1097DD6 B#
- [SDR IPXA2026021200615](https://openairdocs.org/sdr/IPXA2026021200615.md): Rib · cracked · Jan 14, 2026 · N134UP · Airbus A300F4622R · Wing, Rib/Bulkhead
  > LT WING 475AL HAS CRACKED RIB 7TH FROM FWD END AT BOTTOM-QC 109-VWV REMOVED CRACKED RIB ON 475AL PANEL IAW A300-600F SRM 51-40-21. INSTALLED RIB 7 AND DOUBLER AT RIB 7 USING FASTNERS P/N NAS1097DD-6 B# 0004244840, P/N MS20426DD5-7 B# 0004372118 IAW A300-600-SR
- [SDR IPXA2026021200748](https://openairdocs.org/sdr/IPXA2026021200748.md): Angle · damaged · Jan 14, 2026 · N134UP · Airbus A300F4622R · Nacelle/Pylon Miscellaneous Structure
  > 475AL HAS MISSING HALF L ANGLE AT BOTTOM OF 7TH RIB FROM FWD END. REMOVED L ANGLE IAW SRM 51-40-21, WHEN REMOVING FOUND LOWER LONGERON WITH CRACK INSTALLED PANEL 475AL IAW AMM 54-55-00/401
- [SDR IPXA2026021107234](https://openairdocs.org/sdr/IPXA2026021107234.md): Angle · cracked · Jan 14, 2026 · N134UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > RH FRAME 47 OF CWB LOWER ANGLE FITTING; CRACK INDICATION NOTED AT HOLE H IN ALL LAYERS. ACCOMPLISHED NDT ROTO INSPECTION OF HOLE H IAW NTM 51-10-01 PART 6. CRACK INDICATION NOTED. T95868 ACCOMPLISH REPAIR IN ACCORDANCE WITH EO-96345-REQ1 AND VT-MAE EA 300-57
- [SDR IPXA2026021107176](https://openairdocs.org/sdr/IPXA2026021107176.md): Angle · cracked · Jan 14, 2026 · N134UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > RH FR47 OF CWB LOWER ANGLE FITTING; CRACK INDICATION NOTED AT HOLE Z IN ALL LAYERS. VERIFIED ACCOMPLISHED NDT ROTO INSPECTION ON HOLE Z ON ALL LAYERS IAW STEP 20. OF E.A.300-5710-27-A4292 PRELIMINARY 4 AND NTM 51-10-01 PART 6, AND THE INTERNAL FITTING LAYER I
- [SDR IPXA2026021059710](https://openairdocs.org/sdr/IPXA2026021059710.md): Skin · bulged · Jan 12, 2026 · N134UP · Airbus A300F4622R · Wing, Plate/Skin
  > RIGHT WING T/E UPPER FIXED PANEL OTBD OF OTBD FLAP, T/E WEDGE HAS SPOTS OF BULGING SKIN POSSIBLY CORROSION, FROM 1ST TO 3RD STATIC WICK. INSTALLED NEW PART SECTION PANEL TRAILING EDGE RH WING UPPER, IAW SRM 51-40-21.
- [SDR IPXA2026013155972](https://openairdocs.org/sdr/IPXA2026013155972.md): Intercostal · bent · Jan 11, 2026 · N134UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > AGING ACFT INSPECTION- INTERCOSTAL JUST AFT OF AFT ACCESSORY ENTRY DOOR IS DAMAGED, BENT. INSTALLED STRAP INTERCOSTAL IAW SRM 51-40-21.
- [SDR IPXA2026033045598](https://openairdocs.org/sdr/IPXA2026033045598.md): Adapter · corroded · Jan 10, 2026 · N134UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > MAIN CABIN FLOOR STRUCTURE, FR 30 Y0 CLS ADAPTER HAS CORROSION. RESTORED SURFACE PROTECTION IAW SRM 51-21-10 & SRM 51-75-10-201. MAJOR REPAIR.
- [SDR IPXA2026011945658](https://openairdocs.org/sdr/IPXA2026011945658.md): Adapter · cracked · Jan 10, 2026 · N134UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > MAIN CABIN FLOOR STRUCTURE, FR 19 BETWEEN -Y1959 AND -Y 2462 CLS ADAPTER CRACKED. DOT 28-46. REMOVED CLS ADAPTER ON FR 19 BETWEEN -Y1959 AND -Y 2462 IAW A300-600 SRM 51-40-21. INSTALLED NEW CLS ADAPTER IAW SRM51-40-21.
- [SDR IPXA2026011335756](https://openairdocs.org/sdr/IPXA2026011335756.md): Web · cracked · Jan 10, 2026 · N134UP · Airbus A300F4622R · Nacelle/Pylon, Main Frame
  > DURING REMOVAL OF #2 ENGINE INLET COWL AFT BLKHEAD COVER PLATE LH SIDE NEAR AMBIENT PRESS LINE MORE CRAKS FOUND AT UNDERNEATH. INSTALLED NEW WEB I.A.W. A300-600 NACELLE SRM 54-10-00. REVIEWED
- [SDR IPXA2026012623290](https://openairdocs.org/sdr/IPXA2026012623290.md): Support · corroded · Jan 9, 2026 · N134UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > MCD FLOOR, LT SIDE, FRAME 27, UNDER PANEL 231SG, UNDER CLS ADAPTER HAS CORROSION. THE NEW CLS ADAPTER SUPPORT WAS INSTALLED IAW SRM 51-40-21. REVIEWED
- [SDR IPXA2026020328654](https://openairdocs.org/sdr/IPXA2026020328654.md): Skin · out of limits · Jan 9, 2026 · N134UP · Airbus A300F4622R · Wing, Plate/Skin
  > CUSTOMER FINDINGS-FAULT-STR-ZONE 500 TRAILING EDGE OF OUTBOARD LEFT WING, UPPER SURFACE NEAR THE TRAILING EDGE STATIC WICKS ON THE FIXED TRAILING EDGE HAS BULGING SKIN.DOT AA009 REVIEWED
- [SDR IPXA2026020823535](https://openairdocs.org/sdr/IPXA2026020823535.md): Adapter · corroded · Jan 9, 2026 · N134UP · Airbus A300F4622R · Fuselage Main, Structure
  > MCD FLOOR, LH SIDE, BTWN FRAME 22 TO 24 AND BTWN Y2462 TO Y1959 SEAT TRACKS, FLOOR HAS CORROSION (APPROX 3 PLACES). DOT 103-96. VERIFIED ACCOMPLISHED REPAIR IN ACCORDANCE WITH EO-96299-REQ1 AND VT-MAE EA 300-5313-27-A4281, REV. -.
- [SDR IPXA2026021023309](https://openairdocs.org/sdr/IPXA2026021023309.md): Seat Track · corroded · Jan 9, 2026 · N134UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings
  > MCD FLOOR, LH SIDE, BTWN FRAME 26 TO 27, Y1959 SEAT TRACK HAS CORROSION. DOT 103-82. REPAIRED SEAT TRACK BETWEEN FR26 AND FR29, Y+1959 (LH), P/N B53774175208, PER SRM 53-10-16-201 PARAGRAPH 4 FIGURE 201. INSTALLED SEAT TRACK AND U-SECTION SPLICE FITTING IAW A
- [SDR IPXA2026020227094](https://openairdocs.org/sdr/IPXA2026020227094.md): Adapter · corroded · Jan 9, 2026 · N134UP · Airbus A300F4622R · Fuselage Main, Structure
  > MAJOR REPAIR, MDC FLOOR, FR 55, Y0, RT CLS ADAPTER CORRODED. ACCOMPLISHED EA 300-5316-27-A4270, PRELIMINARY 1, STEP 13. INSTALLED THE CLS ADAPTER IAW SRM 51-40-21. ACCOMPLISHED PERMANENT REPAIR IAW EO-96237-REQ1 & VT-MAE EA 300-5316-27-A4270, REV-.
- [SDR IPXA2026020222905](https://openairdocs.org/sdr/IPXA2026020222905.md): Adapter · corroded · Jan 9, 2026 · N134UP · Airbus A300F4622R · Fuselage Main, Structure
  > MAJOR REPAIR, MCD FLOOR, LT SIDE, FRAME 29 ADJACENT TO Y0 SEAT TRACK, CLS HAS CORROSION. DOT 103-71 ACCOMPLISHED E.A 300-5314-27-A4271 PRELIMINARY 1 STEP 9 RESTORE SURFACE AND PAINT SCHEME ACCORDING TO SRM 51-23-10 AND 51-75-10. ACCOMPLISHED PERMANENT REPAI
- [SDR IPXA2026012634694](https://openairdocs.org/sdr/IPXA2026012634694.md): Seat Track · corroded · Jan 9, 2026 · N134UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings
  > MDC SEAT TRACK -Y2127.5 CORRODED SECTION BETWEEN FR72 AND FR73 RH SIDE. REMOVED SEAT TRACK FROM FR 70 TO FR 74 AT -Y2127 IAW SRM-53-10-16. INSTALLED SEAT TRACK AT FR 71 TO FR 74 AT -Y2127 IAW SRM-53-10-16.
- [SDR IPXA2026020223560](https://openairdocs.org/sdr/IPXA2026020223560.md): Floor Panel · damaged · Jan 9, 2026 · N134UP · Airbus A300F4622R · Fuselage Floor Panel
  > MCD FLOOR PANEL BTWN FRAME 19 TO 22, Y1456 TO Y953 BROKEN TWO PLACES & A SPOT OF EXTERNAL SURFACE MISSING. FABRICATED A NEW FLOOR PANEL 241MJ IAW SREO-16407-REQ001.
- [SDR IPXA2026012723222](https://openairdocs.org/sdr/IPXA2026012723222.md): Floor Panel · damaged · Jan 9, 2026 · N134UP · Airbus A300F4622R · Fuselage Floor Panel
  > MCD FLOOR PANEL 231WG, LOWER SURFACE CRACKED. FABRICATED FLOOR PANEL 231KJ COMPLETED IAW SREO-16407-REQ001, APPX B.
- [SDR IPXA2026020228383](https://openairdocs.org/sdr/IPXA2026020228383.md): Web · cracked · Jan 9, 2026 · N134UP · Airbus A300F4622R · Wing Miscellaneous Structure
  > ATTACH WEB LOCTD INBD OF LT WING OTBD FLAP, INBD FLAP CARRIAGE, DIRECLY NEXT TO LT WING NR 5 SPOILER INBD ATTACH POINT CRACKED AT THE UPPR FWD CORNER. REMOVED ATTACH WEB LOCTD INBD OF LT WING OUTBD FLAP, INBD FLAP CARRIAGE, DIRECLY NEXT TO LT WING NR 5 SPOILE
- [SDR IPXA2026012223577](https://openairdocs.org/sdr/IPXA2026012223577.md): Pressure Web · corroded · Jan 9, 2026 · N134UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > MCD FLOOR, LH SIDE, BTWN FRAME 19 TO 22 AND BTWN Y1456 TO Y953 SEAT TRACKS, UNDER PANEL, FLOOR HAS CORROSION (APPROX 4 PLACES). REMOVED PRESSURE WEB IAW SRM 51-40-21. INSTALLED NEW PRESSURE WEB AT BTWN FRAME 19 TO 22 AND BTWN Y1456 TO Y953 IAW SRM 51-40-21.
- [SDR IPXA2026020313618](https://openairdocs.org/sdr/IPXA2026020313618.md): Support Beam · damaged · Jan 8, 2026 · N134UP · Airbus A300F4622R · Fuselage Main, Structure
  > MAIN CARGO COMPARTMENT DOOR SUPPORT STRUCTURE, BETWEEN FR 27-28 HAS (1EA) HOLE DRILLED NEXT TO HI-LOCK.
- [SDR IPXA2026020313524](https://openairdocs.org/sdr/IPXA2026020313524.md): Attach Angle · cracked · Jan 8, 2026 · N134UP · Airbus A300F4622R · Wing, Attach Fittings
  > TWO POSSIBLE CRACKS FOUND ON LEFT WING FWD SPAR AFT FACE LOWER ATTACH ANGLE AFT OF #3 SLAT INBD OF #10 SLAT DRIVE LINK. FABRICATED NEW ANGLE AND FILLER, IAW SRM 51-26-10 AND SRM 51-70-10. INSTALED FILLER, REPAIR ANGLE AND 3EA SPLICES AT ON LEFT WING FWD SPAR
- [SDR IPXA2026020610312](https://openairdocs.org/sdr/IPXA2026020610312.md): Panel · cracked · Jan 8, 2026 · N134UP · Airbus A300F4622R · Nacelle/Pylon, Plate/Skin
  > NR 1 PYLON-TOP OF PYLON FWD END UNDER PANEL 413BL IS A CRACK IN PANEL ATTACH RIB-QC 109-VWV. REPAIR DOUBLER INSTALLED IAW A300-600F SRM51-40-21. REVIEWED
- [SDR IPXA2026012714694](https://openairdocs.org/sdr/IPXA2026012714694.md): Floor Panel · cracked · Jan 8, 2026 · N134UP · Airbus A300F4622R · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL 262 DM CRACKED. FABRICATED THE FLOOR PANEL 262DM IAW SREO-16407-REQ001. APPX B.
- [SDR IPXA2026020995338](https://openairdocs.org/sdr/IPXA2026020995338.md): Rib · cracked · Jan 7, 2026 · N134UP · Airbus A300F4622R · Nacelle/Pylon, Frame/Spar/Rib
  > FAULT-STR-Z400 #2 ENG PYLON ON RIB 3A BRACKET HAS A CRACK ON MARKED AREA DOT 115-037. DEFERRED IN ERROR. PERMANENT REPAIR COMPLETED ON EO-96449-REQ1 [T3F18E0088TX1]. ACCOMPLISHED THE CATEGORY B REPAIR PER EO-96449-REQ1.
- [SDR IPXA2026020297816](https://openairdocs.org/sdr/IPXA2026020297816.md): Adapter · corroded · Jan 7, 2026 · N134UP · Airbus A300F4622R · Fuselage Main, Structure
  > CLS ADAPTER WITH CORROSION AT FR54.3 Y/0 L/H SIDE. DOT 06648-04. ACCOMPLISHED PERMANENT REPAIR IN ACCORDANCE WITH EO-96231-REQ1 AND VT-MAE EA 300-5316-27-A4266 REV.-.
- [SDR IPXA2026020297850](https://openairdocs.org/sdr/IPXA2026020297850.md): Adapter · corroded · Jan 7, 2026 · N134UP · Airbus A300F4622R · Fuselage Main, Structure
  > MAJOR REPAIR, CLS ADAPTER CORRODED AT FR 55 Y/0 LT SIDE. ACCOMPLISHED EA 300-5316-27-A4270, PRELIMINARY 1, STEP 13. INSTALLED THE CLS ADAPTER IAW SRM 51-40-21. ACCOMPLISHED PERMANENT REPAIR IAW EO-96237-REQ1 & VT-MAE EA 300-5316-27-A4270, REV-.
- [SDR IPXA2026020298010](https://openairdocs.org/sdr/IPXA2026020298010.md): Adapter · corroded · Jan 7, 2026 · N134UP · Airbus A300F4622R · Fuselage Main, Structure
  > MAJOR REPAIR, CLS ADAPTER WITH CORROSION AT FR 61 Y/0 LT SIDE. ACCOMPLISHED EA 300-5317-27-A4265, REV -, PRELIMINARY 1, STEP 13. INSTALLED THE CLS ADAPTER IAW SRM 51-40-21. ACCOMPLISHED PERMANENT REPAIR IAW EO-96228-REQ 1 & VT-MAE EA 300-5317-27-A4265, REV
- [SDR IPXA2026020298032](https://openairdocs.org/sdr/IPXA2026020298032.md): Adapter · corroded · Jan 7, 2026 · N134UP · Airbus A300F4622R · Fuselage Main, Structure
  > MAJOR REPAIR. CLS ADAPTER WITH CORROSION AT FR 62 Y/0 LT SIDE. PERFORMED EA 300-5317-27-A4265 REV -, PRELIMINARY 1, STEP 16. ACCOMPLISHED PERMANENT REPAIR IAW EO-96228-REQ1 & VT-MAE EA 300-5317-27-A4265 REV -.
- [SDR IPXA2026020297886](https://openairdocs.org/sdr/IPXA2026020297886.md): Adapter · corroded · Jan 7, 2026 · N134UP · Airbus A300F4622R · Fuselage Main, Structure
  > MAJOR REPAIR, CLS ADAPTER WITH CORROSION AT FR54.2 Y/0 LT SIDE. ACCOMPLISHED EA 300-5316-27-A4266, PRELIMINARY 1, STEP 14. APPLIED CORROSION PREVENTIVE COMPOUND ON AFFECTED AREA IAW SRM 51-23-20 AND EO-2780-REQ001. ACCOMPLISHED PERMANENT REPAIR IAW EO-9623
- [SDR IPXA2026020297834](https://openairdocs.org/sdr/IPXA2026020297834.md): Adapter · corroded · Jan 7, 2026 · N134UP · Airbus A300F4622R · Fuselage Main, Structure
  > MAJOR REPAIR. CLS ADAPTER WITH CORROSION AT FR57.1 Y/0 RT SIDE..ACCOMPLISHED EA 300-5316-27-A4266, REV -, PRELIMINARY 1, STEP 13. INSTALLED CLS ADAPTER IAW SRM 51-40-21. ACCOMPLISHED PERMANENT REPAIR IAW EO-96231-REQ1 AND VT-MAE EA 300-5316-27-A4266.
- [SDR IPXA2026020297968](https://openairdocs.org/sdr/IPXA2026020297968.md): Adapter · corroded · Jan 7, 2026 · N134UP · Airbus A300F4622R · Fuselage Main, Structure
  > MAJOR REPAIR, CLS ADAPTER WITH CORROSION AT FR 32 Y/0 L/H SIDE. DOT 06648-08. REMOVED ADAPTER CLS ON FR63 BTW -Y1959 & -Y2462 IAW A300-600 SRM 51-40-21. INSTALLED CLS ADAPTER FR63 -Y1959 -Y2462 IAW A300-600 SRM 51-40-21.
- [SDR IPXA2026020297958](https://openairdocs.org/sdr/IPXA2026020297958.md): Adapter · corroded · Jan 7, 2026 · N134UP · Airbus A300F4622R · Fuselage Main, Structure
  > MAJOR REPAIR, CLS ADAPTER WITH CORROSION AT FR 32 Y/0 RT SIDE. ACCOMPLISHED EA 300-5314-27 A4264, PRELIMINARY 1, STEP 13, INSTALLED CLS ADAPTER IAW DRAWING B53774150 AT FR 32 YO RT IAW SRM 51-40-21. ACCOMPLISH PERMANENT REPAIR IAW EO-96227-REQ1 AND VT-MAE
- [SDR IPXA2026020297922](https://openairdocs.org/sdr/IPXA2026020297922.md): Adapter · corroded · Jan 7, 2026 · N134UP · Airbus A300F4622R · Fuselage Main, Structure
  > MAJOR REPAIR, CLS ADAPTER WITH CORROSION AT FR 34 Y/0 R/H SIDE. ACCOMPLISHED E.A 300-5314-27 A4264 PRELIMINARY 1 STEP 13 INSTALL CLS ADAPTER IAW DRAWING B53774150 AT FR34 YO RT LOCATIONS IAW SRM 51-40-21. ACCOMPLISHED PERMANENT REPAIR IAW EO-96227-REQ1 A
- [SDR IPXA2026020298123](https://openairdocs.org/sdr/IPXA2026020298123.md): Adapter · corroded · Jan 7, 2026 · N134UP · Airbus A300F4622R · Fuselage Main, Structure
  > MAJOR REPAIR, CLS ADAPTER WITH CORROSION AT FR 33 Y/0 R/H SIDE. ACCOMPLISHED E.A 300-5314-27 A4264 PRELIMINARY 1 STEP 13 INSTALL CLS ADAPTER PER DRAWING B53774150 AT FR33 YO RH LOCATINS IAW SRM 51-40-21. ACCOMPLISHED PERMANENT REPAIR IAW EO-96227-REQ1 AND
- [SDR IPXA2026020298006](https://openairdocs.org/sdr/IPXA2026020298006.md): Adapter · corroded · Jan 7, 2026 · N134UP · Airbus A300F4622R · Fuselage Main, Structure
  > MAJOR REPAIR. CLS ADAPTER WITH CORROSION AT FR 28 Y/0 L/H SIDE. ACCOMPLISHED EA#300-5314-27-A4264 PRELIMINARY 1 STEP 9 RESTORE SURFACE AND PAINT SCHEME ACCORDING TO SRM 51-23-10 AND 51-75-10. ACCOMPLISHED PERMANENT REPAIR IAW EO-96227-REQ1 AND VT-MAE EA 3
- [SDR IPXA2026020297992](https://openairdocs.org/sdr/IPXA2026020297992.md): Adapter · corroded · Jan 7, 2026 · N134UP · Airbus A300F4622R · Fuselage Main, Structure
  > MAJOR REPAIR. CLS ADAPTER WITH CORROSION AT FR 28 Y/0 R/H SIDE. ACCOMPLISHED E.A 300-5314-27 A4264 PRELIMINARY 1 STEP 13 INSTALL CLS ADAPTER PER AIRBUS DRAWING B53774150 AT FR 28 YO RH LOCATINS IAW SRM 51-40-21. ACCOMPLISHED PERMANENT REPAIR IAW EO-96227
- [SDR IPXA2026020297812](https://openairdocs.org/sdr/IPXA2026020297812.md): Adapter · corroded · Jan 7, 2026 · N134UP · Airbus A300F4622R · Fuselage Main, Structure
  > MAJOR REPAIR. CLS ADAPTER WITH CORROSION AT FR57.1 Y/0 L/H SIDE. DOT 06648-02. ACCOMPLISHED E.A. 300-5316-27-A4266 REV -, PRELIMINARY 1, STEP 13. INSTALLED CLS ADAPTER IAW A300-600 SRM 51-40-21. ACCOMPLISHED PERMANENT REPAIR IAW EO-96231-REQ1 AND VT-MAE EA 3
- [SDR IPXA2026012880090](https://openairdocs.org/sdr/IPXA2026012880090.md): Spar Web · cracked · Jan 7, 2026 · N134UP · Airbus A300F4622R · Wing Spar
  > LEFT WING, LOWER SURFACE, NR 3 SPOILER, INBD SIDE, AFT REAR SPAR WEB DEFORMED. FABRICATED AND DRILLED A NEW WEB IAW SRM 51-40-44, SRM 51-27-11, SRM 51-26-00 AND GMM 09-08-01-04. INSTALLED THE NEW WEB IAW SRM 51-40-21.
- [SDR IPXA2026011997722](https://openairdocs.org/sdr/IPXA2026011997722.md): Adapter · corroded · Jan 7, 2026 · N134UP · Airbus A300F4622R · Fuselage Main, Structure
  > CLS ADAPTER CORRODED AT FR36 RT, UNDER FLOOR PANEL 242KF. REMOVED THE CLS ADAPTER AT FR36 IAW SRM 51-40-21. INSTALLED A NEW CLS ADAPTER IAW SRM 51-40-21.
- [SDR IPXA2026012196338](https://openairdocs.org/sdr/IPXA2026012196338.md): Rub Strip · cracked · Jan 7, 2026 · N134UP · Airbus A300F4622R · Engine Thrust Reverser
  > NUMBER 2 ENGINE O/B T/R WHERE METAL FIRE SEAL MAKES CONTACT HAS A HOLE IN THE CORNER. WEAR ANGLE AND RUBSTRIP O/B T/R REMOVED IAW A300-600F SRM51-40-21. WEAR ANGLE AND RUBSTRIP INSTALLED IAW SRM51-40-21.
- [SDR IPXA2026021176316](https://openairdocs.org/sdr/IPXA2026021176316.md): Skin · dented · Jan 6, 2026 · N134UP · Airbus A300F4622R · Wing, Plate/Skin
  > FAULT-STR-ZONE 500. LH WING LEADING EDGE TIP HAS (1EA) DENT. DOT 28-02 ACCOMPLISHED PERMANENT REPAIR IN ACCORDANCE WITH EO-96373-REQ1 AND VT-MAE EA 300-5730-27-A4299, REV. -.
- [SDR IPXA2026021066324](https://openairdocs.org/sdr/IPXA2026021066324.md): Support Angle · cracked · Jan 6, 2026 · N134UP · Airbus A300F4622R · Wing Miscellaneous Structure
  > RIGHT WING UPPER FIXED PANEL SUPPORT CHANNEL ABOVE THE NR 6 FLAP TRACK HAS DAMAGED HOLE. INSTALLED SUPPORT ANGLE IAW SRM A300-600 51-40-21. REVIEWED
- [SDR IPXA2026011363640](https://openairdocs.org/sdr/IPXA2026011363640.md): Rib · cracked · Jan 6, 2026 · N134UP · Airbus A300F4622R · Trailing Edge Flaps
  > LEFT WING, CENTER FLAP, TOP SKIN RIB FLANGE, 1 CRACK INDICATION NOTED AT RIB 27. CIRCLED IN RED. PERFORM TRAILING EDGE BOTTOM SKIN CUT OUT DOWNSTREAM OF THE REAR SPAR BETWEEN RIB 25 AND RIB 25A AS PER FIGURE 2 SHEET 2 AND GUIDELINES PER SRM 57-50-00 PARAGRAPF
- [SDR IPXA2026011563643](https://openairdocs.org/sdr/IPXA2026011563643.md): Rib · cracked · Jan 6, 2026 · N134UP · Airbus A300F4622R · Wing, Rib/Bulkhead
  > MAJOR REPAIR, LT WING, CENTER FLAP, TOP SKIN RIB FLANGE, 1 CRACK INDICATION NOTED AT RIB 13. CIRCLED IN RED. REMOVE RIB 25 STIFFENER A57960437205 BETWEEN STRINGER 2.8 AND REAR SPAR BY APPLICATION OF AN INCISION MIDWAY EXISTING FASTENER POSITIONS AS PER FIGU
- [SDR IPXA2026011563588](https://openairdocs.org/sdr/IPXA2026011563588.md): Rib · cracked · Jan 6, 2026 · N134UP · Airbus A300F4622R · Trailing Edge Flaps
  > MAJOR REPAIR, RT WING, CENTER FLAP, TOP SKIN RIB FLANGE, 1 CRACK INDICATION NOTED AT RIB 25. CIRCLED IN RED. AUDIT COMPLETED
- [SDR IPXA2026011563596](https://openairdocs.org/sdr/IPXA2026011563596.md): Rib · cracked · Jan 6, 2026 · N134UP · Airbus A300F4622R · Trailing Edge Flaps
  > MAJOR REPAIR, RT WING, CENTER FLAP, TOP SKIN RIB FLANGE, TWO CRACK INDICATIONS NOTED AT RIB 26. PERFORM 2X BOTTOM SKIN CUT OUTS IN AREA ENCLOSED BY RIB-26- RIB27, STRINGER 2.2- REAR SPAR. ++ACCOMPLISHED REPAIR IN ACCORDANCE WITH EO-96208-REQ1 AND VT-MAE EA 30
- [SDR IPXA2026011563560](https://openairdocs.org/sdr/IPXA2026011563560.md): Rib · cracked · Jan 6, 2026 · N134UP · Airbus A300F4622R · Trailing Edge Flaps
  > MAJOR REPAIR, RT WING, CENTER FLAP, TOP SKIN RIB FLANGE, 1 CRACK INDICATION NOTED AT RIB 27. ACCOMPLISHED PERMANENT REPAIR IN ACCORDANCE WITH EO-96209-REQ1 AND VT-MAE EA 300-5753-27-A4259, REV. -.

Next page: https://openairdocs.org/aircraft/N134UP/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 = 'N134UP' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N134UP/reports

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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.