# Service difficulty reports: N142UP

A list on [N142UP](https://openairdocs.org/aircraft/N142UP.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 · 287 reports

- [SDR IPXA2026090755372](https://openairdocs.org/sdr/IPXA2026090755372.md): Skin · dented · Jul 31, 2026 · N142UP · Airbus A300F4622R · Fuselage Main, Plate/Skin
  > MAJOR REPAIR. DENT ON LEFT SIDE OF FUSELAGE JUST AFT OF LAV SERVICE DOOR REPAIRED IAW EO-98195-REQ2.
- [SDR IPXA2026011406798](https://openairdocs.org/sdr/IPXA2026011406798.md): Warning Light · inoperative · Jan 14, 2026 · N142UP · Airbus A300F4622R · Door Warning System
  > ON PREFLIGHT, L1 RED WARNING LIGHT DOES NOT ILLUMINATE WHEN TESTED. BUZZER DOES SOUND. FOUND ASPSU WITH RED LIGHT DISPLAYED ON UNIT POSITION. REMOVED AND REPLACED APSU 70WN AND OPERATION CHECKS GOOD IAW AMM 52-73-18/401. THIS CLEARS DMI, PLACARD REMOVED. NO DM
- [SDR IPXA2026011546798](https://openairdocs.org/sdr/IPXA2026011546798.md): Indicator · no test · Jan 14, 2026 · N142UP · Airbus A300F4622R · Door Warning System
  > ON PREFLIGHT, L1 RED WARNING LIGHT DOES NOT ILLUMINATE WHEN TESTED. BUZZER DOES SOUND. DEFERRED AS PER MEL 52-73-01-1. PLACARD INSTALLED. NO DMP REQ.
- [SDR IPXA2025093098082](https://openairdocs.org/sdr/IPXA2025093098082.md): Bracket · cracked · Sep 29, 2025 · N142UP · Airbus A300F4622R · Wing, Attach Fittings
  > DURING ACCOMPLISHING OF T.C T3F18E007GZC1 FOUND 1EA HYDRAULIC CASE DRAIN LINES SUPPORT BRACKET CRACKED INSIDE ACCESS PANEL 675AB. REMOVED SUPPORT BRACKET IAW SRM 51-40-21. FABRICATED NEW PPORT BRACKET I.A.W A300-600 SRM 57-51-11.INSTALLED NEW BRACKET IAW
- [SDR IPXA2025092036861](https://openairdocs.org/sdr/IPXA2025092036861.md): Skin Panel · cracked · Sep 16, 2025 · N142UP · Airbus A300F4622R · Wing, Plate/Skin
  > RIGHT WING INBD FIXED T/E IS CRACKED AT FASTNER HOLE. INSTALLED SKIN PANEL AT UPEER AND LOWER R/H WING T/E FIXED INBD USING FASTNERS P/N CR3212-4-03 B# 0004279987 150 EA AND P/N MS20426AD4 B# 0004361884 10 EA IAW A300-600-SRM-51-40-21 AND A300-600-IPC-75-51-1
- [SDR IPXA2025092043577](https://openairdocs.org/sdr/IPXA2025092043577.md): Support Bracket · damaged · Aug 30, 2025 · N142UP · Airbus A300F4622R · Wing Main, Frame Structure
  > FAULT-Z600-APG-RH WING ACCESS PANEL 672PB CHAFFING ON VERTICAL SUPPORT BRACKET DOT 55-060. INSTALLED RIB ATTACHMENT ON RH WING ACCESS PANEL 672PB IAW A300-600 SRM 51-40-21. REVIEWED
- [SDR IPXA2025091706569](https://openairdocs.org/sdr/IPXA2025091706569.md): Attach Bracket · cracked · Aug 28, 2025 · N142UP · Airbus A300F4622R · Horizontal Stabilizer Miscellaneous Structure
  > RIGHT HORIZONTAL STAB UPPER CLOSE OUT ATTACH BRACKET IS CRACKED, INSTALLED R/H HORIZONTAL STABILIZER FRONT APRON IAW AMM 55-15-11/401.
- [SDR IPXA2025092275064](https://openairdocs.org/sdr/IPXA2025092275064.md): Retainer · gouged · Aug 27, 2025 · N142UP · Airbus A300F4622R · Wing Main, Frame Structure
  > LEFT WING FAIRING 533AT SEAL RETAINER HAS A GOUGE. 33-009. INSTALLED NEW SEAL RETAINER ON FAIRING 533AT IAW SRM 51-40-21 AND SRM 51-40-23. REVIEWED
- [SDR IPXA2025091978349](https://openairdocs.org/sdr/IPXA2025091978349.md): Floor Panel · damaged · Aug 27, 2025 · N142UP · Airbus A300F4622R · Fuselage Floor Panel
  > FWD. CARGO PIT FLOORBOARD PANEL#132MG RT. CENTER EDGE DAMAGE. VERIFIED FABRICATIN OF FLOOR PANEL 132MG. IAW SREO-16407-REQ002 ((APPX C).
- [SDR IPXA2025091978207](https://openairdocs.org/sdr/IPXA2025091978207.md): Floor Panel · damaged · Aug 27, 2025 · N142UP · Airbus A300F4622R · Fuselage Floor Panel
  > FWD. CARGO PIT FLOORBOARD PANEL #131DE LH. CORNERS DAMAGED DOT#58-20 DARRYL FORD 91102506. FABRICATED/ INSTALL FLOOR PANEL 131DE, P/N B5327052700000 IAW A300 SREO-16407-REQ002 ((APPX C).
- [SDR IPXA2025090682238](https://openairdocs.org/sdr/IPXA2025090682238.md): Floorbeam · cracked · Aug 27, 2025 · N142UP · Airbus A300F4622R · Fuselage Main, Floor Beam
  > MDC FLOOR, FR 80, BTW -Y1221.2 AND -Y1580.5, CORNER FLOOR SUPPORT CRACKED. INSTALLED NEW PART IAW SRM 51-40-21 WITH FASTENERS.
- [SDR IPXA2025090682210](https://openairdocs.org/sdr/IPXA2025090682210.md): Floorbeam · cracked · Aug 27, 2025 · N142UP · Airbus A300F4622R · Fuselage Main, Floor Beam
  > MDC FLOOR, FR 80, BTW Y1221.2 AND Y1580.5, CORNER FLOORBEAM CRACKED. PROFILE T WAS INSTALLED IAW SRM 51-40-21.
- [SDR IPXA2025092671560](https://openairdocs.org/sdr/IPXA2025092671560.md): Adapter · corroded · Aug 26, 2025 · N142UP · Airbus A300F4622R · Fuselage Main, Structure
  > CORROSION FOUND ON SEAT TRACK ADAPTER BTW FR 21 AND FR 27 AT 4 PLACES, NEXT TO ADAPTERS CLS, Y0 -2". INSTALLED NEW SEAT TRACK ADAPTER BETWEEN FR 21 TO FR 27 AND Y-2 IAW SRM 51-20-21.
- [SDR IPXA2025092671370](https://openairdocs.org/sdr/IPXA2025092671370.md): Adapter · corroded · Aug 26, 2025 · N142UP · Airbus A300F4622R · Fuselage Main, Structure
  > CORROSION FOUND ON SEAT TRACK ADAPTER BTW FR 21 AND FR 27 AT 4 PLACES, NEXT TO ADAPTERS CLS. Y0 +2". INSTALLED A NEW SEAT TRACK ADAPTER BETWEEN FR 21 TO FR 27 AND Y+2 IAW SRM 51-20-21.
- [SDR IPXA2025092565497](https://openairdocs.org/sdr/IPXA2025092565497.md): Profile · chafed · Aug 26, 2025 · N142UP · Airbus A300F4622R · Wing Miscellaneous Structure
  > LEFT WING FAIRING 34AT HAS CHAFING ON FWD ATTACH ANGLE 109, INSTALLED NEW PROFILE ON FAIRING 534AT IAW AIRBUS SRM 51-40-21 & SRM 51- 40-23.
- [SDR IPXA2025092358524](https://openairdocs.org/sdr/IPXA2025092358524.md): Support Plate · cracked · Aug 26, 2025 · N142UP · Airbus A300F4622R · Wing Main, Frame Structure
  > PANEL 575AB SUPPORT PLATE CRACKED. DOT NO. 17-48.INSTALLED SUPPORT PLATE, IAW SRM 51-40-21. VERIFIED ACCOMPLISHMENT OF REPAIR IAW EO-95135-REQ1 AND VT-MAE EA 300-5751-27-A4146, REV.
- [SDR IPXA2025091964060](https://openairdocs.org/sdr/IPXA2025091964060.md): Floor Panel · damaged · Aug 26, 2025 · N142UP · Airbus A300F4622R · Fuselage Floor Panel
  > AFT CARGO FLOOR PANEL 151QF HAS DAMAGED EDGES. FABRICATION OF FLOOR PANEL 151QF, IAW SREO-16407-REQ002 ((APPX C). PANEL WILL BE INSTALLED ACCORDING TO CARD NO T3F18E006P978.
- [SDR IPXA2025091970836](https://openairdocs.org/sdr/IPXA2025091970836.md): Floor Panel · damaged · Aug 26, 2025 · N142UP · Airbus A300F4622R · Fuselage Floor Panel
  > FWD CARGO FLOOR PANEL 132MG HAS DAMAGE IN 10 PLACES. SH 91148554 VERIFIED FABRICATION OF FLOOR PANEL 132MG, IAW SREO-16407-REQ002 ((APPX C).
- [SDR IPXA2025090663534](https://openairdocs.org/sdr/IPXA2025090663534.md): Bracket · cracked · Aug 26, 2025 · N142UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT WEB AT FR54, Y0, CRACKED. JP-110. INSTALLED NEW BRACKET IN STR-ZONE 150- AFT CARGO COMPARTMENT WEB AT FR54, Y0, I.A.W. SRM 51-40-21 WITH SEALANT,
- [SDR IPXA2025090663530](https://openairdocs.org/sdr/IPXA2025090663530.md): Bracket · cracked · Aug 26, 2025 · N142UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > AFT CARGO WEB AT FR54, Y1959, CRACKED. JP-110. INSTALLED NEW BRACKET IN STR-ZONE 150-AFT CARGO WEB AT FR54, Y1959, I.A.W. A300-600 SRM 51-40-21 WITH SEALANT.
- [SDR IPXA2025090657922](https://openairdocs.org/sdr/IPXA2025090657922.md): Skin · corroded · Aug 26, 2025 · N142UP · Airbus A300F4622R · Wing, Plate/Skin
  > LEFT WING TIP UPPER SURFACE BONDING STRIP AFT END CORRODED. DOT NO. 17-35. INSTALLED 1 EA FILLER 1 EA DOUBLER 1 MOUNTING STATIC DISCHARGE IAW SRM 51-40-21.
- [SDR IPXA2025091850638](https://openairdocs.org/sdr/IPXA2025091850638.md): Bracket · cracked · Aug 25, 2025 · N142UP · Airbus A300F4622R · Fuselage, Stabilizer Attach Fittings
  > -EXT TAIL-L/H SIDE WHERE FUSELAGE AND TAIL MEET-ANGLE CRACKED FOR UPPER APRON(333AT)-109 VWV 91195430. INSTALLED L/H HORIZONTAL STABILIZER LEADING EDGE 331AB IAW A300-600 AMM 55-12-11/401. REVIEWED
- [SDR IPXA2025091739173](https://openairdocs.org/sdr/IPXA2025091739173.md): Bracket · cracked · Aug 24, 2025 · N142UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > E&E COMPARTMENT, RIB 10, -Y953, SUPPORT ANGLE WITH EVIDENCE OF CRACK. INSTALLED NEW SUPPORT ANGLE AT Z100 E&E COMPARTMENT, RIB 10, -Y953. IAW SRM 51-75-10. REVIEWED
- [SDR IPXA2025091739164](https://openairdocs.org/sdr/IPXA2025091739164.md): Bracket · cracked · Aug 24, 2025 · N142UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > E&E COMPARTMENT, RIB 10, Y953, SUPPORT ANGLE CRACK. INSTALLED NEW SUPPORT ANGLE AT E&E COMPARTMENT, RIB 10, Y953. IAW A300-600 SRM 51-75-10.
- [SDR IPXA202509025671](https://openairdocs.org/sdr/IPXA202509025671.md): Hinge Fitting · cracked · Aug 23, 2025 · N142UP · Airbus A300F4622R · Fuselage, Door Hinge
  > PIANO HINGE FITTING OF MDC DOOR HAS CRACK/DAMAGE IN HOLE [19F] BOTTOM LAYERS, 5`CLOCK POSITION. FASTENER IS INSTALLED IAW TASK CARD MXP-531355-02-1-233-JIC (SDI - PIANO HINGE FITTINGS OF MDC DOOR ON FUSELAGE AND DOOR INCLUDING SURROUNDING STRUCTURE) REVIEWED
- [SDR IPXA2025082925599](https://openairdocs.org/sdr/IPXA2025082925599.md): Hinge · cracked · Aug 23, 2025 · N142UP · Airbus A300F4622R · Fuselage, Door Hinge
  > PIANO HINGE FITTING OF MDC DOOR HAS CRACK IN HOLE [10D] BOTTOM LAYER. FASTENER IS INSTALLED IAW TASK CARD MXP-531355-02-1-233-JIC. SDI - PIANO HINGE FITTINGS OF MDC DOOR ON FUSELAGE AND DOOR INCLUDING SURROUNDING STRUCTURE.
- [SDR IPXA2025092606949](https://openairdocs.org/sdr/IPXA2025092606949.md): Rib · cracked · Aug 22, 2025 · N142UP · Airbus A300F4622R · Trailing Edge Flaps
  > LEFT WING CENTER FLAP, TOP SKIN RIB FLANGE, 2 CRACKS NOTED AT RIB11. CIRCLED IN RED.ACCOMPLISHED THE REPAIR IN ACCORDANCE WITH EO-94890-REQ1 AND VT-MAE EA 300-5750-27-A4108.
- [SDR IPXA2025092607053](https://openairdocs.org/sdr/IPXA2025092607053.md): Rib · cracked · Aug 22, 2025 · N142UP · Airbus A300F4622R · Trailing Edge Flaps
  > LEFT WING CENTER FLAP, TOP SKIN RIB FLANGE, 1 CRACK NOTED AT RIB15. CIRCLED IN RED.ACCOMPLISHED THE REPAIR IN ACCORDANCE WITH EO-94890-REQ1 AND VT-MAE EA 300-5750-27-A4108.
- [SDR IPXA2025092607057](https://openairdocs.org/sdr/IPXA2025092607057.md): Rib · cracked · Aug 22, 2025 · N142UP · Airbus A300F4622R · Trailing Edge Flaps
  > LEFT WING CENTER FLAP, TOP SKIN RIB FLANGE, 1 CRACK NOTED AT RIB19. CIRCLED IN RED.ACCOMPLISHED THE REPAIR IN ACCORDANCE WITH EO-94890-REQ1 AND VT-MAE EA 300-5750-27-A4108.
- [SDR IPXA2025092607061](https://openairdocs.org/sdr/IPXA2025092607061.md): Rib · cracked · Aug 22, 2025 · N142UP · Airbus A300F4622R · Trailing Edge Flaps
  > LEFT WING CENTER FLAP, TOP SKIN RIB FLANGE, 1 CRACK NOTED AT RIB25. CIRCLED IN RED.ACCOMPLISHED THE REPAIR IN ACCORDANCE WITH EO-94890-REQ1 AND VT-MAE EA 300-5750-27-A4108.
- [SDR IPXA2025092607301](https://openairdocs.org/sdr/IPXA2025092607301.md): Rib · cracked · Aug 22, 2025 · N142UP · Airbus A300F4622R · Trailing Edge Flaps
  > RIGHT WING CENTER FLAP, TOP SKIN RIB FLANGE, TWO CRACKS NOTED AT RIB 25. ACCOMPLISHED PERMANENT REPAIR IAW EO-94891-REQ1 AND EA 300-5750-27-A4107, REV -.
- [SDR IPXA2025101307330](https://openairdocs.org/sdr/IPXA2025101307330.md): Rib · cracked · Aug 22, 2025 · N142UP · Airbus A300F4622R · Trailing Edge Flaps
  > RIGHT WING CENTER FLAP, TOP SKIN RIB FLANGE, TWO CRACKS NOTED AT RIB 27. ACCOMPLISHED PERMANENT REPAIR IAW EO-94891-REQ1 AND EA 300-5750-27-A4107, REV -.
- [SDR IPXA2025092607320](https://openairdocs.org/sdr/IPXA2025092607320.md): Rib · cracked · Aug 22, 2025 · N142UP · Airbus A300F4622R · Trailing Edge Flaps
  > MAJOR REPAIR, RT WING CENTER FLAP, TOP SKIN RIB FLANGE, TWO CRACKS NOTED AT RIB 26. ACCOMPLISHED PERMANENT REPAIR IAW EO-94891-REQ1 AND EA 300-5750-27-A4107, REV. -.
- [SDR IPXA2025092607221](https://openairdocs.org/sdr/IPXA2025092607221.md): Rib · cracked · Aug 22, 2025 · N142UP · Airbus A300F4622R · Trailing Edge Flaps
  > MAJOR REPAIR, RT WING CENTER FLAP, TOP SKIN RIB FLANGE, TWO CRACKS NOTED AT RIB 13. ACCOMPLISHED PERMANENT REPAIR IAW EO-94891-REQ1 AND EA 300-5750-27-A4107, REV. -.
- [SDR IPXA2025092607255](https://openairdocs.org/sdr/IPXA2025092607255.md): Rib · cracked · Aug 22, 2025 · N142UP · Airbus A300F4622R · Trailing Edge Flaps
  > MAJOR REPAIR. RT WING CENTER FLAP, TOP SKIN RIB FLANGE, ONE CRACK NOTED AT RIB18. ACCOMPLISHED PRMANENT REPAIR IAW EO-94891-REQ1 AND EA 300-5750-27-A4107, REV. -.
- [SDR IPXA2025091909183](https://openairdocs.org/sdr/IPXA2025091909183.md): Floor Panel · damaged · Aug 22, 2025 · N142UP · Airbus A300F4622R · Fuselage Floor Panel
  > FWD CARGO FLOOR PANEL 131DE HAS EDGE DAMAGE 4". SH 91148554. FABRICATED/ INSTALLED FLOOR PANEL 131DE, P/N B5327052700000 IAW A300 SREO-16407-REQ002 ((APPX C).
- [SDR IPXA2025091908647](https://openairdocs.org/sdr/IPXA2025091908647.md): Floor Panel · damaged · Aug 22, 2025 · N142UP · Airbus A300F4622R · Fuselage Floor Panel
  > AFT CARGO FLOOR PANEL 151QF HAS 2 PLACES 5" OF EDGE DAMAGE. SH 91148554 VERIFIED FABRICATION OF FLOOR PANEL 151QF, P/N B5327053100000<BR>IAW A300 SREO-16407-REQ002 ((APPX C) PANEL WILL BE INSTALLED ACCORDING TO CARD NO T3F18E006P978.
- [SDR IPXA2025091007301](https://openairdocs.org/sdr/IPXA2025091007301.md): Rib · cracked · Aug 22, 2025 · N142UP · Airbus A300F4622R · Wing, Rib/Bulkhead
  > MAJOR REPAIR. RT WING CENTER FLAP, TOP SKIN RIB FLANGE, 2 CRACKS NOTED AT RIB25. CIRCLED IN RED. REVIEWED
- [SDR IPXA2025091007330](https://openairdocs.org/sdr/IPXA2025091007330.md): Rib · cracked · Aug 22, 2025 · N142UP · Airbus A300F4622R · Trailing Edge Flaps
  > MAJOR REPAIR, RT WING CENTER FLAP, TOP SKIN RIB FLANGE, 2 CRACKS NOTED AT RIB27.
- [SDR IPXA2025091907221](https://openairdocs.org/sdr/IPXA2025091907221.md): Rib · cracked · Aug 22, 2025 · N142UP · Airbus A300F4622R · Trailing Edge Flaps
  > MAJOR REPAIR, RT WING CENTER FLAP, TOP SKIN RIB FLANGE, 2 CRACKS NOTED AT RIB13.
- [SDR IPXA2025091507320](https://openairdocs.org/sdr/IPXA2025091507320.md): Rib · cracked · Aug 22, 2025 · N142UP · Airbus A300F4622R · Trailing Edge Flaps
  > RIGHT WING CENTER FLAP, TOP SKIN RIB FLANGE, HAD 2 CRACKS AT RIB 26. COMPLIED WITH STEP 33 OF EA 300-5750-27-A4107, PRELIMINARY 1.
- [SDR IPXA2025090913704](https://openairdocs.org/sdr/IPXA2025090913704.md): Floorbeam · damaged · Aug 22, 2025 · N142UP · Airbus A300F4622R · Fuselage Main, Floor Beam
  > MAIN DECK-RT SIDE FR51 CROSSBEAM BENT (Y-953 TO Y-450)-109 VWV 91195430 ACCOMPLISHED JOB IAW SREO-75878-REQ001 ((APPX B) TASK CARD:T3F18E007A68T.
- [SDR IPXA2025092089259](https://openairdocs.org/sdr/IPXA2025092089259.md): Adapter · corroded · Aug 21, 2025 · N142UP · Airbus A300F4622R · Fuselage Main, Structure
  > MAJOR REPAIR, CORROSION ON CLS ADAPTER FR76 Y1580.5. ACCOMPLISHED A PERMANENT REPAIR IAW EO-95063-REQ1 AND EA 300-5318-27-A4106 REV. -.
- [SDR IPXA2025092090275](https://openairdocs.org/sdr/IPXA2025092090275.md): Adapter · corroded · Aug 21, 2025 · N142UP · Airbus A300F4622R · Fuselage Main, Structure
  > MAJOR REPAIR, CORROSION FOUND ON CLS FR60 Y0 + 3" LT, ACCOMPLISHED REPAIR IAW EO-95062-REQ1 AND EA 300-5317-27-A4104 REV. -.
- [SDR IPXA2025092090261](https://openairdocs.org/sdr/IPXA2025092090261.md): Adapter · corroded · Aug 21, 2025 · N142UP · Airbus A300F4622R · Fuselage Main, Structure
  > MAJOR REPAIR, CORROSION FOUND ON CLS FR63 Y0 + 3", LT. ACCOMPLISHED PERMANENT REPAIR IAW EO-95062-REQ1 AND EA 300-5317-27-A4104 REV. -..
- [SDR IPXA2025091990000](https://openairdocs.org/sdr/IPXA2025091990000.md): Seat Track · corroded · Aug 21, 2025 · N142UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings
  > MAJOR REPAIR, CORROSION FOUND ON SEAT TRACK FLANGE FR 30, Y2462, TWO LOCATIONS. INSTALLED A NEW SEAT TRACK SECTION Y2462 TO FR 30 IAW SRM 51-40-21 AND SRM 53-10-16 PARAGRAPH 4 (FIGURE 201) PAGE 205/206.
- [SDR IPXA2025091789967](https://openairdocs.org/sdr/IPXA2025091789967.md): Seat Track · corroded · Aug 21, 2025 · N142UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings
  > MAJOR REPAIR, CORROSION FOUND ON SEAT TRACK FLANGE FR 30 Y1959, TWO LOCATIONS. SEAT TRACK WAS INSTALLED IAW SRM 51-40-21 AND SRM 53-10-16.
- [SDR IPXA2025092090347](https://openairdocs.org/sdr/IPXA2025092090347.md): Adapter · corroded · Aug 21, 2025 · N142UP · Airbus A300F4622R · Fuselage Main, Structure
  > MAJOR REPAIR, CORROSION FOUND ON CLS FR 33 Y0 + 3" RT, ACCOMPLISHED PERMANENT REPAIR IAWEO-95061-REQ1 AND EA 300-5314-27-A4103 REV. -.
- [SDR IPXA2025083089022](https://openairdocs.org/sdr/IPXA2025083089022.md): Seat Track · corroded · Aug 21, 2025 · N142UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings
  > MAJOR REPAIR, CORROSION ON SEAT TRACK Y0 BTW FR79 AND FR80/82 NEW SEAT TRACK SECTION Y0 BTW FR79-FR80 HAS BEEN INSTALLED IAW SRM 53-10-16 PARAGRAPH 4 PAGE 204 FIGURE 201 AND SRM 51-40-21.
- [SDR IPXA2025090289057](https://openairdocs.org/sdr/IPXA2025090289057.md): Seat Track · corroded · Aug 21, 2025 · N142UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings
  > MAJOR REPAIR, CORROSION ON SEAT TRACK Y794.3 BTW FR 79 AND FR 80- 82, NEW SEAT TRACK SECTION WAS INSTALLED IAW SRM 51-40-21 AND SRM 53-10-16 PARAGRAPH 4 FIGURE 201.

Next page: https://openairdocs.org/aircraft/N142UP/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 = 'N142UP' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N142UP/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.