# Service difficulty reports: N147UP

A list on [N147UP](https://openairdocs.org/aircraft/N147UP.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 7 · 338 reports

- [SDR IPXA2026091835366](https://openairdocs.org/sdr/IPXA2026091835366.md): Support Fitting · cracked · Sep 1, 2026 · N147UP · Airbus A300F4622R · Horizontal Stabilizer Miscellaneous Structure
  > AFTER LT HORIZONTAL LEADING EDGE 331AB SUPPORT BRACKET REMOVAL, FOUND 1EA FITTING WITH CRACK. INSTALLATION OF NEW SUPPORT, FITTING AT L/H HORIZONTAL LEADING EDGE 331AB IAW SRM 51-40-21.
- [SDR IPXA2026100214982](https://openairdocs.org/sdr/IPXA2026100214982.md): Support Bracket · missing · Aug 31, 2026 · N147UP · Airbus A300F4622R · Wing Miscellaneous Structure
  > LH WING LEADING EDGE INSIDE OF ACCESS PANEL 512KB CAMLOC SUPPORT BRACKET IS MISSING P/N: 244-16 (QTY 01). INSTALLED NEW RETAINER P/N A5724183600251 AT Z500 / LH WING LEADING EDGE INSIDE OF ACCESS PANEL 512KB: I.A.W. A300-600 SRM 51-40-21-001
- [SDR IPXA2026092117554](https://openairdocs.org/sdr/IPXA2026092117554.md): Stiffener · cracked · Aug 25, 2026 · N147UP · Airbus A300F4622R · Leading Edge Devices
  > RIGHT WING, KRUEGER FLAP MOVABLE VANE, CRACK UNDER TEFLON STOP BASE. INSPECTED AND VERIFIED INSTALLATION OF STIFFENER ON RT WING KRUEGER FLAP MOVABLE VANE IAW SRM 51-40-21.
- [SDR IPXA2026100228085](https://openairdocs.org/sdr/IPXA2026100228085.md): Stiffener · cracked · Aug 17, 2026 · N147UP · Airbus A300F4622R · Leading Edge Devices
  > L/H WING, KRUEGER FLAP MOVABLE VANE, CRACK UNDER TEFLON STOP BASE. DOT 73-176. INSTALLED STIFFENER AND REINSTALLED COVER SEAL + FITTING IAW A300 SRM 51-40-21. REVIEWED
- [SDR IPXA2026092805259](https://openairdocs.org/sdr/IPXA2026092805259.md): Plate · out of limits · Aug 15, 2026 · N147UP · Airbus A300F4622R · Nacelle/Pylon, Main Frame
  > FAIRING 475AL, FWD UPPER I/B SIDE, 3EA FASTENER HOLES ELONGATED AND STRUCTURE BENT AND WITH CHAFFING. DOT 73-155. VERIFIED REMOVAL AND REPLACEMENT OF THE PLATE ON FAIRING 475AL, FWD UPPER I/B SIDE IAW A300-600 SRM 51-40-21.
- [SDR IPXA2026092905418](https://openairdocs.org/sdr/IPXA2026092905418.md): Support · cracked · Aug 15, 2026 · N147UP · Airbus A300F4622R · Nacelle/Pylon, Main Frame
  > PANEL RACK, FAIRING 475AL, FWD WEB WITH CRACK. DOT 73-169. REMOVED AND REPLACED NEW SUPPORT P/N 221-0081-53 BATCH:0004506588 ON FAIRING 475AL, FWD WEB. IAW A300-600 SRM 51-40-21 REVIEWED.
- [SDR IPXA2026100200616](https://openairdocs.org/sdr/IPXA2026100200616.md): Plate · cracked · Aug 15, 2026 · N147UP · Airbus A300F4622R · Wing, Landing Gear Attach Fittings
  > AGING AIRCRAFT INSPECTION-FAULT-AVI-ZONE 100 RIGHT MAIN LANDING GEAR SERVICE LIGHT, LOCATED DIRECTLY ABOVE THE SIDE BRACE HAS A CRACKED FIXTURE. AA011. NEW PLATE MOUNTING WAS INSTALLED IAW A300-600 SRM 51-40-21. REVIEWED
- [SDR IPXA2026092805342](https://openairdocs.org/sdr/IPXA2026092805342.md): Rib · cracked · Aug 15, 2026 · N147UP · Airbus A300F4622R · Aerodynamic Fairings
  > FAIRING 475AL, FWD I/B RIB CRACK. REMOVED AND REPLACED NEW RIB ON FAIRING 475AL, FWD I/B IAW SRM 51-40-21.
- [SDR IPXA2026091780741](https://openairdocs.org/sdr/IPXA2026091780741.md): Frame · damaged · Aug 14, 2026 · N147UP · Airbus A300F4622R · Fuselage Main, Frame
  > RIGHT WING FR 47 UPPER RADIUS BRACKET HAS ELONGATED HOLES. INSTALLATION OF SPLICE AND SPAR CONTROLLED IN THE EO-18290-JIC004.
- [SDR IPXA2026090991849](https://openairdocs.org/sdr/IPXA2026090991849.md): Floor Panel · damaged · Aug 14, 2026 · N147UP · Airbus A300F4622R · Fuselage Floor Panel
  > MAJOR REPAIR. MCD FLOOR PANEL 242DN IS BROKEN. FLOOR PANEL 242DN IS FABRICATED IAW SREO-16407-REQ001 (APPX B) A300 MAIN DECK CARGO COMPARTMENT FLOOR PANEL FABRICATION.
- [SDR IPXA2026090987132](https://openairdocs.org/sdr/IPXA2026090987132.md): Floor Panel · broken · Aug 14, 2026 · N147UP · Airbus A300F4622R · Fuselage Floor Panel
  > MAJOR REPAIR. MCD FLOOR PANEL 231WG IS BROKEN. THE FLOOR PANEL 231WG WAS FABRICATED IAW SREO-16407-REQ001 (APPX B) A300 MAIN DECK CARGO COMPARTMENT FLOOR PANEL FABRICATION.
- [SDR IPXA2026090987296](https://openairdocs.org/sdr/IPXA2026090987296.md): Floor Panel · broken · Aug 14, 2026 · N147UP · Airbus A300F4622R · Fuselage Floor Panel
  > MAJOR REPAIR. MCD FLOOR PANEL 231VG IS BROKEN. PANEL 231VG IS FABRICATED IAW SREO-16407-REQ001 (APPX B) MAIN DECK CARGO COMPARTMENT FLOOR PANEL FABRICATION.
- [SDR IPXA2026090494048](https://openairdocs.org/sdr/IPXA2026090494048.md): Support Fitting · cracked · Aug 14, 2026 · N147UP · Airbus A300F4622R · Horizontal Stabilizer Miscellaneous Structure
  > HORIZONTAL STAB, R/H LOWER APRON ATTACH AREA, #10 BRACKET, WITH CRACK. REMOVED #10 BRACKET, HORIZONTAL STAB, R/H LOWER IAW A300-600 SRM 51-40-21-001. REPLACED APRON FITTING SUPPORT P/N A5517160320251 AT R/H LOWER APRON ATTACH AREA, #10 BRACKET IAW SRM 51-40
- [SDR IPXA2026092874261](https://openairdocs.org/sdr/IPXA2026092874261.md): Web · cracked · Aug 13, 2026 · N147UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > AVIONICS COMPARTMENT, CEILING AREA, BTW FR 10 AND FR 11, Y953, WEB BROKEN. INSTALLED WEB AT AVIONIC COMPARTMENT, CEILING AREA, BTW FR 10 AND FR 11, Y953 IAW A300-600 SRM 51-40-21.
- [SDR IPXA2026092874251](https://openairdocs.org/sdr/IPXA2026092874251.md): Bracket · broken · Aug 13, 2026 · N147UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > AVIONICS COMPARTMENT, CEILING AREA, FR 10, Y953, AFT BRACKET BROKEN. INSTALLED BRACKET AT AVIONIC COMPARTMENT, CEILING AREA, FR 10, Y953 IAW SRM 51-40-21.
- [SDR IPXA2026082873757](https://openairdocs.org/sdr/IPXA2026082873757.md): Shear Tie · cracked · Aug 13, 2026 · N147UP · Airbus A300F4622R · Fuselage Internal Mounting Structure
  > CENTER FUSELAGE BASE FRAME FITTING, FR 45, STR 37R HAS EVIDENCE OF CRACK. VERIFIED ACCOMPLISHED REPAIR IN ACCORDANCE WITH EO-98669-REQ1 AND STE PNA EA 300-5710-27-A4617, REV. _.
- [SDR IPXA2026100654735](https://openairdocs.org/sdr/IPXA2026100654735.md): Adapter · corroded · Aug 12, 2026 · N147UP · Airbus A300F4622R · Fuselage Main, Structure
  > MAIN DECK FLOOR STRUCTURE, CLS AT FR 30 BETWEEN Y0 & -Y450 HAS CORROSION. INSTALLED NEW CLS ADAPTER FR30, BTW Y0 AND -Y450 IAW SRM 51-40-21.
- [SDR IPXA2026100654025](https://openairdocs.org/sdr/IPXA2026100654025.md): Adapter · corroded · Aug 12, 2026 · N147UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > MDC, CLS AT FR36, BTW Y0 AND Y450 IS CORRODED. VERIFIED INSTALLATION OF NEW CLS ADAPTER AT FR36 BTW Y0 AND Y450 IAW SRM 51-40-21-001.
- [SDR IPXA2026100654726](https://openairdocs.org/sdr/IPXA2026100654726.md): Floorbeam · corroded · Aug 12, 2026 · N147UP · Airbus A300F4622R · Fuselage Main, Floor Beam
  > MAIN DECK FLOOR STRUCTURE, CLS AT FR 34 BETWEEN Y0 & -Y450 HAS CORROSION INSTALLED NEW CLS ADAPTER P/N UP-B53774136200 IAW A300-600 SRM 51-40-21-001.
- [SDR IPXA2026100654057](https://openairdocs.org/sdr/IPXA2026100654057.md): Adapter · corroded · Aug 12, 2026 · N147UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings
  > MDC, CLS AT FR34, BTW Y0 AND Y450 IS CORRODED. VERIFIED INSTALLATION OF NEW CLS ADAPTER AT FR34, BTW Y0 AND Y450 IAW SRM 51-40-21-001.
- [SDR IPXA2026100654048](https://openairdocs.org/sdr/IPXA2026100654048.md): Adapter · corroded · Aug 12, 2026 · N147UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings
  > MDC, CLS AT FR35, BTW Y0 AND Y450 IS CORRODED. VERIFIED INSTALLATION OF NEW CLS ADAPTER A TFR35 BTW Y0 AND Y450 IAW SRM 51-40-21-001.
- [SDR IPXA2026100653905](https://openairdocs.org/sdr/IPXA2026100653905.md): Adapter · corroded · Aug 12, 2026 · N147UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings
  > MDC, CLS ADAPTER AT FR38.1, BTW Y0 AND Y450 IS EXFOLIATED. VERIFIED INSTALLATION OF NEW CLS ADAPTER AT FR38.1, BTW Y0 AND Y450 IAW SRM 51-40-21-001.
- [SDR IPXA2026100652275](https://openairdocs.org/sdr/IPXA2026100652275.md): Adapter · corroded · Aug 12, 2026 · N147UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK, RH FR35, Y0 CLS ADAPTER HAS CORROSION IN 2EA SPOTS. VERIFIED INSTALLATION OF NEW CLS ADAPTER AT RH FR35, Y0 IAW A300- SRM 51-40-21-001
- [SDR IPXA2026100652219](https://openairdocs.org/sdr/IPXA2026100652219.md): Adapter · corroded · Aug 12, 2026 · N147UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK, RH FR38.1, Y0 CLS ADAPTER IS DAMAGED, VERIFIED INSTALLATION OF NEW CLS ADAPTER AT RH FR38.1 Y0 IAW SRM 51-40-21-001.
- [SDR IPXA2026082154325](https://openairdocs.org/sdr/IPXA2026082154325.md): Seat Track · corroded · Aug 12, 2026 · N147UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings
  > MAJOR REPAIR, MDC SEAT TRACK, BTWN FR 30 - 31, Y450, HAD 2 SPOTS OF CORROSION AT L/H LATERAL FACE. REPAIRED IAW SRM 53-10-16-16-201, PAGE207 & 208, FIG 201,REV 43.
- [SDR IPXA2026082154505](https://openairdocs.org/sdr/IPXA2026082154505.md): Seat Track · corroded · Aug 12, 2026 · N147UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings
  > MAJOR REPAIR, MDC SEAT TRACK, FR 28 - 31, Y2462, HAD FOUR SPOTS OF CORROSION AT R/H SIDE. REPAIRED IAW SRM 53-10-16-201 PARAGRAPH 4 FIGURE 201,REV 43. THIS IS A CATEGORY A REPAIR AND NO FURTHER ACTION IS REQUIRED.
- [SDR IPXA2026101454460](https://openairdocs.org/sdr/IPXA2026101454460.md): Seat Track · corroded · Aug 12, 2026 · N147UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings
  > MAJOR REPAIR, MAIN DECK SEAT TRACK, EVIDENCE OF CORROSION IN SEVERAL SPOTS AT -Y1959 BETWEEN FR 31 & 27. IAW SRM 53-10-16-201,REV 43, PAGE 207/208, FIGURE 201. INSTALLED SEAT TRACK AT -Y1959, BTW FR22 AND FR 32.
- [SDR IPXA2026092454797](https://openairdocs.org/sdr/IPXA2026092454797.md): Adapter · corroded · Aug 12, 2026 · N147UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > MAIN DECK FLOOR STRUCTURE, CLS ADAPTER PLATE AT FR 27 BETWEEN Y0 & Y450 HAS EVIDENCE OF CORROSION. INSTALLED NEW CLS ADAPTER TRACK AND CLS ADAPTER ON MAIN DECK FLOOR STRUCTURE AT FR 27 BETWEEN Y0 AND Y450 IAW SRM 51-40-21. REVIEWED
- [SDR IPXA2026092554466](https://openairdocs.org/sdr/IPXA2026092554466.md): Adapter · broken · Aug 12, 2026 · N147UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > MDC FLOOR, FR 33, BTW Y1959 AND Y2462, CLS ADAPTER BROKEN. INSTALLED NEW CLS ADAPTER AT Z200 - MDC FLOOR, FR 33, BTW Y1959 AND Y2462, IAW SRM 51-40-21-001.
- [SDR IPXA2026092553975](https://openairdocs.org/sdr/IPXA2026092553975.md): Adapter · corroded · Aug 12, 2026 · N147UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > MDC, CLS AT FR37, BTW Y1959 AND Y2462 IS CORRODED. DOT 23-052 SURFACE PROTECTION RESOTORED OF CLS ADAPTER STR - Z200 - MDC FLOOR, FR 37, BTW Y1959 AND Y2462 I.A.W SRM 51-21-10-001 AND SRM 51-75-10-201. EWIS PROTECTION REMOVED I.A.W ESPM 20-54-50-02.
- [SDR IPXA2026092454842](https://openairdocs.org/sdr/IPXA2026092454842.md): Seat Track · corroded · Aug 12, 2026 · N147UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK FLOOR STRUCTURE, CLS ADAPTER PLATE AT FR 26 BETWEEN Y0 & Y450 HAS EVIDENCE OF CORROSION. INSTALLED 1EA NEW CLS ADAPTER TRACK, 5EA CLS ADAPTER AND 2EA SPLICE ON MAIN DECK FLOOR STRUCTURE AT FR20 TO FR26 BETWEEN Y0 AND Y450 IAW A300-600 SRM 51-40-21.
- [SDR IPXA2026092654275](https://openairdocs.org/sdr/IPXA2026092654275.md): Bracket · chafed · Aug 12, 2026 · N147UP · Airbus A300F4622R · Passenger/Crew Doors
  > CREW DOOR AFT EDGE LOWER BRACKET IS CHAFED REMOVED AND REPLACED BRACKET IN CREW DOOR AFT EDGE LOWER. IAW A300-600 SRM 51-40-21-001 AND SRM52-11-00-001. REVIEWED
- [SDR IPXA2026092354797](https://openairdocs.org/sdr/IPXA2026092354797.md): Adapter · corroded · Aug 12, 2026 · N147UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > MAIN DECK FLOOR STRUCTURE, CLS ADAPTER PLATE AT FR 27 BETWEEN Y0 & Y450 HAS EVIDENCE OF CORROSION (DOT 64-201) VERIFIED NEW CLS ADAPTERS TRACKS AND CLS ADAPTERS INSTALLATION AT FR 27 PER SRM 51-40-21
- [SDR IPXA2026091354568](https://openairdocs.org/sdr/IPXA2026091354568.md): Bracket · corroded · Aug 12, 2026 · N147UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > MDC FLOOR, BTW FR 28 AND 29, BTW Y1959 AND Y2462, THRUST BRACKET WITH CORROSION. INSTALLED NEW BRACKET THRUST AT STR - Z200 - MDC FLOOR, BTW FR 28 AND 29 BTW Y1959 AND Y2462, I.A.W. A300-600 SRM 51-40-21.
- [SDR IPXA2026091354585](https://openairdocs.org/sdr/IPXA2026091354585.md): Thrust Bracket · corroded · Aug 12, 2026 · N147UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > MDC FLOOR, BTW FR 27 AND 28, BTW Y1959 AND Y2462, TRUST BRACKET WITH CORROSION. VERIFIED REMOVED EWIS PROTECTION IAW ESPM PG BLK 20-54-50-0. INSTALLED NEW BRACKET THRUST. MDC FLOOR, BTW FR 27 AND 28, BTW Y1959 AND Y2462, IAW SRM 51-40-21.
- [SDR IPXA2026100632273](https://openairdocs.org/sdr/IPXA2026100632273.md): Adapter · corroded · Aug 11, 2026 · N147UP · Airbus A300F4622R · Fuselage Main, Structure
  > MAIN DECK FLOOR STRUCTURE, AT FR 62 Y0, CLS ADAPTER HAS CORROSION. INSTALLATION OF NEW CLS ADAPTER AT FR 62 Y0 I.AW. A300-600 SRM 51-40-21-001.
- [SDR IPXA2026100632272](https://openairdocs.org/sdr/IPXA2026100632272.md): Adapter · corroded · Aug 11, 2026 · N147UP · Airbus A300F4622R · Fuselage Main, Structure
  > MAIN DECK FLOOR STRUCTURE, AT FR 58 Y0, CLS ADAPTER HAS CORROSION. INSTALLATION OF NEW CLS ADAPTER AT MD FLOOR STRUCTURE AT FR58 Y0 IAW SRM 51-40-21-001,
- [SDR IPXA2026100632726](https://openairdocs.org/sdr/IPXA2026100632726.md): Adapter · corroded · Aug 11, 2026 · N147UP · Airbus A300F4622R · Fuselage Main, Structure
  > MDC FLOOR, FR 60, Y0 R/H CLS ADAPTER WITH CORROSION. VERIFIED INSTALLATION OF NEW CLS ADAPTER AT FR 60, Y0 R/H I.AW. SRM 51-40-21-001. INSTALLATION OF NEW CLS ADAPTER AT FR 60, Y0 R/H I.AW. A300-600 SRM 51-40-21-001. VERIFIED PARTS MARKING IAW UPS GMM 09-08.
- [SDR IPXA2026100632694](https://openairdocs.org/sdr/IPXA2026100632694.md): Adapter · corroded · Aug 11, 2026 · N147UP · Airbus A300F4622R · Fuselage Main, Structure
  > MDC FLOOR, FR 65, Y0 R/H CLS ADAPTER WITH CORROSION. VERIFIED CLS ADAPTER INSTALLATION PER SRM 51-40-21-001
- [SDR IPXA2026100632584](https://openairdocs.org/sdr/IPXA2026100632584.md): Adapter · corroded · Aug 11, 2026 · N147UP · Airbus A300F4622R · Fuselage Main, Structure
  > MDC FLOOR, FR 66, Y0 R/H CLS ADAPTER WITH CORROSION. INSTALLED NEW CLS ADAPTER AT Z200 - MDC FLOOR, FR 66, Y0 R/H.P/N UPA53275455201.TRAVELER # T26/1875628.I.A.W A300-600 SRM 51-40-21-001.
- [SDR IPXA2026100632573](https://openairdocs.org/sdr/IPXA2026100632573.md): Adapter · corroded · Aug 11, 2026 · N147UP · Airbus A300F4622R · Fuselage Main, Structure
  > MDC FLOOR, FR 75, L/H SIDE OF -Y1580.5, CLS ADAPTER WITH CORROSION ON BASE. INSTALLED NEW CLS ADAPTER AT Z200 - MDC FLOOR, FR 75, L/H SIDE OF -Y1580.5. I.A.W A300-600 SRM 51-40-21-001.
- [SDR IPXA2026100632700](https://openairdocs.org/sdr/IPXA2026100632700.md): Seat Track · corroded · Aug 11, 2026 · N147UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings
  > MAJOR REPAIR, MDC SEAT TRACK, BTWN FR 65 & 66, Y0, CORRODED. LOCATED AND DRILLED.
- [SDR IPXA2026100132589](https://openairdocs.org/sdr/IPXA2026100132589.md): Seat Track · corroded · Aug 11, 2026 · N147UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings
  > MAJOR REPAIR, MDC FLOOR, BTW FR 71 & 72, -Y1456, SEAT TRACK CORRODED AT R/H LATERAL FACE. LOCATED AND DRILLED A SPLICE SEAT TRACK AND SPLICE UNION IAW SRM 53-10-16, FIG 201, AND SRM 51-40-44.
- [SDR IPXA2026090532016](https://openairdocs.org/sdr/IPXA2026090532016.md): Support · cracked · Aug 11, 2026 · N147UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > MAIN DECK FLOOR STRUCTURE, AT FR 74 AND 75 LH SIDE, Z-PROFILE HAS CRACKS (2EA SPOTS). INSTALLED NEW T-PROFILE IN MAIN DECK FLOOR STRUCTURE, AT FR 74 AND 75 LH SIDE. IAW SRM 51-40-21-001 AND SRM 53-18-18-001.
- [SDR IPXA2026092127542](https://openairdocs.org/sdr/IPXA2026092127542.md): Support · cracked · Aug 11, 2026 · N147UP · Airbus A300F4622R · Aerodynamic Fairings
  > LEFT FR 47 HORIZONTAL JUNCTION AREA. CRACK INDICATION NOTED AT HOLE "P" IN ALL LAYERS. VERIFIED E.A.#300-5710-27-A4579, PRELIMINARY 4, STEP 56. VERIFIED UPS EO-68606-JIC001 INSTRUCTIONS COMPLETED (T3F18E002MT2B).
- [SDR IPXA2026092127516](https://openairdocs.org/sdr/IPXA2026092127516.md): Support · cracked · Aug 11, 2026 · N147UP · Airbus A300F4622R · Aerodynamic Fairings
  > LEFT FR47 HORIZONTAL JUNCTION AREA. CRACK INDICATION NOTED AT HOLE "D" IN ALL LAYERS. VERIFIED E.A.#300-5710-27-A4579, PRELIMINARY 4, STEP 56. VERIFIED UPS EO-68606-JIC001 INSTRUCTIONS COMPLETED (T3F18E002MT2B).
- [SDR IPXA2026092127471](https://openairdocs.org/sdr/IPXA2026092127471.md): Support · cracked · Aug 11, 2026 · N147UP · Airbus A300F4622R · Aerodynamic Fairings
  > LEFT FR 47, HORIZONTAL JUNCTION AREA. CRACK INDICATION NOTED AT HOLE B IN ALL LAYERS. VERIFIED E.A.#300-5710-27-A4579, PRELIMINARY 4, STEP 56. VERIFIED UPS EO-68606-JIC001 INSTRUCTIONS COMPLETED (T3F18E002MT2B).
- [SDR IPXA2026090432523](https://openairdocs.org/sdr/IPXA2026090432523.md): Seat Track · corroded · Aug 11, 2026 · N147UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings
  > MDC FLOOR, FR 80, -Y450, SEAT TRACK WITH CORROSION. VERIFIED APPLICATION OF SURFACE PROTECTION COATS IAW SRM 51-75-10. AND GMM 04.02 VERIFIED REMOVAL OF EWIS PROTECTION IAW ESPM 20-54-50-02.
- [SDR IPXA2026090332495](https://openairdocs.org/sdr/IPXA2026090332495.md): Seat Track · corroded · Aug 11, 2026 · N147UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings
  > MDC FLOOR, FR 80, Y0, SEAT TRACK WITH CORROSION. VERIFIED APPLICATION OF SURFACE PROTECTION COATS IAW A300-600 SRM 51-75-10. AND UPS GMM 04.02 VERIFIED REMOVAL OF EWIS PROTECTION IAW A300-600 ESPM 20-54-50-02.
- [SDR IPXA2026090331979](https://openairdocs.org/sdr/IPXA2026090331979.md): Seat Track · corroded · Aug 11, 2026 · N147UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK FLOOR STRUCTURE, AT FR 80 SEAT TRACK Y450 HAD CORROSION (2EA SPOTS). INSTALLATION OF SPLICE SEAT TRACK 2EA P\N: R5327049020000 BTCH: 0004506809 AND SEAT TRACK 1EA P\N: R5307007120200 BTCH: 0004479769, IAW A300-600 SRM 51-40-21 AND SRM 53-10-16. AND

Next page: https://openairdocs.org/aircraft/N147UP/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 = 'N147UP' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N147UP/reports

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