# Service difficulty reports: N158UP

A list on [N158UP](https://openairdocs.org/aircraft/N158UP.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 4 · 166 reports

- [SDR IPXA2026102027627](https://openairdocs.org/sdr/IPXA2026102027627.md): Fitting · cracked · Oct 19, 2026 · N158UP · Airbus A300F4622R · Fuselage Main, Attach Fittings
  > NLG UPLOCK ACTUATOR FIXTURE CRACKED. INSTALLED UPLOCK FIXTURE IAW AMM 32-31-14/401 AND 20-21-12/001.
- [SDR IPXA202610051117](https://openairdocs.org/sdr/IPXA202610051117.md): Rib · cracked · Oct 2, 2026 · N158UP · Airbus A300F4622R · Wing, Rib/Bulkhead
  > CREATED TO CAPTURE ENG STATUS AND COMPLETION FOR TASK CARD T3F18E009MQ3S. ACCOMPLISH REPAIR IN ACCORDANCE WITH EO-98679-REQ1 AND STE PNA EA 300-5753-27-A4632, REV. _.
- [SDR IPXA2026101239996](https://openairdocs.org/sdr/IPXA2026101239996.md): Warning Buzzer · broken · Oct 1, 2026 · N158UP · Airbus A300F4622R · Passenger/Crew Doors
  > AVI CREW ENTRY DOOR, DOOR WARNING BUZZER (FINN: 11WN) IS BROKEN. REPLACED WARNING HORN (BUZZER) AND CARRIED OUT OPS CHECK GOOD IAW AMM 52-73-12/401.
- [SDR IPXA2026100639564](https://openairdocs.org/sdr/IPXA2026100639564.md): Panel · cracked · Oct 1, 2026 · N158UP · Airbus A300F4622R · Nacelle/Pylon, Main Frame
  > AFTER REMOVAL OF SEAL, FOUND PANEL 423BL CRACKED. INSTALLED DOUBLER ON PANEL 423BL IAW SRM 54-52-51-201-C1, PARAGRAPH D.2. STEP U, FIGURE 204.
- [SDR IPXA2026100239996](https://openairdocs.org/sdr/IPXA2026100239996.md): Warning Buzzer · broken · Oct 1, 2026 · N158UP · Airbus A300F4622R · Door Warning System
  > AVI CREW ENTRY DOOR, DOOR WARNING BUZZER (FINN: 11WN) IS BROKEN.
- [SDR IPXA2026100181758](https://openairdocs.org/sdr/IPXA2026100181758.md): Access Panel · cracked · Sep 29, 2026 · N158UP · Airbus A300F4622R · Wing, Plate/Skin
  > LEFT WING BELOW KRUGER FLAP ACCESS PANEL 513AB STRUCTURE (RING) CRACKED. INTERNAL DOUBLER WAS REMOVED AT LH WING BELOW KRUGER FLAP ACCESS PANEL 513AB IAW A300-600 SRM 51-40-21-001. INSTALLED INTERNAL DOUBLER ON LH WING BELOW KRUGER FLAP ACCESS PANEL 513AB IAW
- [SDR IPXA2026092628088](https://openairdocs.org/sdr/IPXA2026092628088.md): Angle · cracked · Sep 25, 2026 · N158UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > FR 79 R/H DURING REMOVAL "Z" PROFILE FOUND ANGLE CRACKED. INSTALLED ANGLE PER SRM TASK:51-40-21-001 PAR. 6.
- [SDR IPXA2026100508332](https://openairdocs.org/sdr/IPXA2026100508332.md): Crossbeam · broken · Sep 24, 2026 · N158UP · Airbus A300F4622R · Fuselage Main, Structure
  > MDC FR 79 R/H Y2127.6 FOUND CROSS BEAM WITH CRACK. ACCOMPLISH REPAIR IN ACCORDANCE WITH EO-98797 AND STE PNA EA 300-5318-27-A4649, REV. _.
- [SDR IPXA2026100608317](https://openairdocs.org/sdr/IPXA2026100608317.md): Crossbeam · cracked · Sep 24, 2026 · N158UP · Airbus A300F4622R · Fuselage Main, Structure
  > MDC FR 79 -Y2127.6 FOUND CROSS BEAM WITH CRACK.ACCOMPLISH REPAIR IN ACCORDANCE WITH EO-98797 AND STE PNA EA 300-5318-27-A4649, REV. _.
- [SDR IPXA2026100816052](https://openairdocs.org/sdr/IPXA2026100816052.md): Lug · broken · Sep 24, 2026 · N158UP · Airbus A300F4622R · Elevator Miscellaneous Structure
  > RIGHT ELEVATOR ATTACH FITTING NR 2 SAFETY LUG IS BROKEN. INSTALLED NEW LOCKING PLATE PER SRM 51-40-21-001, & 55-26-11-201.
- [SDR IPXA2026100650463](https://openairdocs.org/sdr/IPXA2026100650463.md): Strap · corroded · Sep 21, 2026 · N158UP · Airbus A300F4622R · Wing Miscellaneous Structure
  > RIGHT WING FIXED TRAILING EDGE LOWER SURFACE INBD SIDE JUST OUTBD OF RT FLAP HAS SKIN BULDGING WITH INTERNAL CORROSION. REMOVED LOWER SKIN PANEL (1EA) AT R/W FIXED TRAILING EDGE FOR ACCESS IAW SRM 51-40-21. INSTALLED NEW STRAP AND RE-INSTALLED LOWER SKIN PANE
- [SDR IPXA2026101639999](https://openairdocs.org/sdr/IPXA2026101639999.md): Skin · corroded · Sep 20, 2026 · N158UP · Airbus A300F4622R · Wing, Plate/Skin
  > LEFT WING UPPER SURFACE OUTBD FIXED TRAILING EDGE INBD AFT SIDE IS BULGING AROUND A FASTNER, POSSIBLE INTERNAL CORROSION. INSTALLED LANDING P/N UPA57246385200 AT LH WING IAW A300-600 SRM 51-40-21-001.
- [SDR IPXA2026100101667](https://openairdocs.org/sdr/IPXA2026100101667.md): Frame · cracked · Sep 17, 2026 · N158UP · Airbus A300F4622R · Fuselage Main, Frame
  > MAJOR REPAIR. CENTER FUSELAGE BASE FRAME FITTING FR44 LT HAS SIGNS OF CRACK. CRACK EXTENDS ENTIRE TOP SURFACE AND STOPS JUST PAST EDGE ON FWD SURFACE OF FRAME. ACCOMPLISHED REPAIR IAW EO 46789-JIC 7 AND EO-46789-REQ 6 (APPX J).
- [SDR IPXA2026100101697](https://openairdocs.org/sdr/IPXA2026100101697.md): Frame · cracked · Sep 17, 2026 · N158UP · Airbus A300F4622R · Fuselage Main, Frame
  > MAJOR REPAIR. CENTER FUSELAGE BASE FRAME FITTING FR45 LH SIDE HAS SIGNS OF CRACK. AFTER FURTHER EVALUATION FOUND CRACK LENGTH IS 0.100". ACCOMPLISHED REPAIR IAW EO 46789-JIC 7 AND EO-46789-REQ 6 (APPX J).
- [SDR IPXA2026100102772](https://openairdocs.org/sdr/IPXA2026100102772.md): Panel · cracked · Sep 17, 2026 · N158UP · Airbus A300F4622R · Nacelle/Pylon, Main Frame
  > PANEL 423BL LOWER AREA WITH 2 CRACKS. REMOVED (IEA) SEAL AND SEAL RETAINER AT PANEL 423BL IAW SRM 51-40-21. REINSTALLED SEAL AND SEAL RETAINER AT PANEL 423BL IAW SRM 51-40-21.
- [SDR IPXA2026100101699](https://openairdocs.org/sdr/IPXA2026100101699.md): Shear Tie · cracked · Sep 17, 2026 · N158UP · Airbus A300F4622R · Fuselage Internal Mounting Structure
  > MAJOR REPAIR. CENTER FUSELAGE BASE FRAME FITTING FR46 LH SIDE HAS SIGNS OF CRACK. ACCOMPLISHED EO-46789-JIC007.
- [SDR IPXA2026100102793](https://openairdocs.org/sdr/IPXA2026100102793.md): Panel · cracked · Sep 17, 2026 · N158UP · Airbus A300F4622R · Nacelle/Pylon, Plate/Skin
  > PANEL 423BL EXTERNAL SURFACE WITH A CRACK. VERIFIED RECEIVED THE REPAIRED PANEL 423BL BY WELDING ON TRAVELER # T26/1879228, NOTE: THE INSTALLATION WILL BE ACCOMPLISED ON TASKCARD: T3F18E007EGD6.
- [SDR IPXA2026100102892](https://openairdocs.org/sdr/IPXA2026100102892.md): Access Panel · cracked · Sep 17, 2026 · N158UP · Airbus A300F4622R · Nacelle/Pylon, Plate/Skin
  > PANEL 413BL, EXTERNAL SURFACE WITH A CRACK DOT 53-024. RECEIVED THE REPAIRED PANEL 413BL BY WELDING ON TRAVELER # T26/1879227, NOTE: THE INSTALLASION WILL BE ACCOMPLISED ON TASK CARD T3F18E007EGD6.
- [SDR IPXA2026092801699](https://openairdocs.org/sdr/IPXA2026092801699.md): Shear Tie · cracked · Sep 17, 2026 · N158UP · Airbus A300F4622R · Fuselage Internal Mounting Structure
  > MAJOR REPAIR. CENTER FUSELAGE BASE FRAME FITTING FR46 LT SIDE HAS SIGNS OF CRACK. ACCOMPLISHED THE FOLLOWING STEPS: 58 TO 63 IAW EO-46789-JIC007.
- [SDR IPXA2026092801667](https://openairdocs.org/sdr/IPXA2026092801667.md): Shear Tie · cracked · Sep 17, 2026 · N158UP · Airbus A300F4622R · Fuselage Internal Mounting Structure
  > MAJOR REPAIR. CENTER FUSELAGE BASE FRAME FITTING FR44 LH SIDE HAS SIGNS OF CRACK. VERIFIED C/W STEPS: 41 AND 42 OF EO-46789-JIC007 (T3F18E009P8WZ)
- [SDR IPXA2026092801697](https://openairdocs.org/sdr/IPXA2026092801697.md): Shear Tie · cracked · Sep 17, 2026 · N158UP · Airbus A300F4622R · Fuselage Internal Mounting Structure
  > MAJOR REPAIR. CENTER FUSELAGE BASE FRAME FITTING FR45 LH SIDE HAS SIGNS OF CRACK. ACCOMPLISHED ROTPROBPROBE INSPECTION IAW NTM 51-10-01 PART 6. CRACK TERMINATES AT STOP DRILL.
- [SDR IPXA2026093076928](https://openairdocs.org/sdr/IPXA2026093076928.md): Skin · corroded · Sep 16, 2026 · N158UP · Airbus A300F4622R · Wing, Plate/Skin
  > RIGHT WING OUTBOARD FIXED TRAILING EDGE WEDGE HAS 4 SPOTS OF CORROSION. REMOVED RT WING OUTBOARD FIXED TRAILING EDGE WEDGE I.A.W. A300-600 SRM 51-40-21. INSTALLED NEW SECTION PANEL TRAILING EDGE PER SRM A300-600 TASK: 51-40-21.
- [SDR IPXA2026092177194](https://openairdocs.org/sdr/IPXA2026092177194.md): Bracket · cracked · Sep 16, 2026 · N158UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > FR FROM E&E COCKPIT FLOOR STRUCTURE AT RH FR 10 HAS A CRACKED ANGLE. INSTALLED NEW ANGLE BRACKET AT E&E COCKPIT FLOOR STRUCTURE AT RH FR 10 IAW A300-600 SRM 51-40-21.
- [SDR IPXA2026092443712](https://openairdocs.org/sdr/IPXA2026092443712.md): Bracket · cracked · Sep 14, 2026 · N158UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > MAIN DECK, FLOOR BRACKET UNDER FR 79 AND Y1580 IS CRACKED. REMOVED FLOOR BRACKET WITH CRACK, IAW SRM 51-40-21. INSTALLED FLOOR BRACKET FOR MAIN DECK AT FR 79 Y1580 IAW SRM 51-40-21.
- [SDR IPXA2026092444327](https://openairdocs.org/sdr/IPXA2026092444327.md): Web · cracked · Sep 14, 2026 · N158UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > MAIN DECK, FLOOR WEB AT FR 74 AND Y2127 IS CRACKED. INSTALLED PLATE SUPPORT AT FR 74, Y2127 PER SRM 51-40-21-00A.
- [SDR IPXA2026092443777](https://openairdocs.org/sdr/IPXA2026092443777.md): Floor Support · cracked · Sep 14, 2026 · N158UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > MAIN DECK, FLOOR STRUCTURE AT FR 75 AND Y2127 IS CRACKED. INSTALLED NEW PART AT MAIN DECK, FLOOR STRUCTURE AT FR 75 AND Y2127 IAW SRM 51-40-21.
- [SDR IPXA2026101915093](https://openairdocs.org/sdr/IPXA2026101915093.md): Fitting · cracked · Sep 12, 2026 · N158UP · Airbus A300F4622R · Fuselage Main, Keel
  > LEFT KEEL BEAM AT THE LEVEL OF CONNECTING FITTING BETWEEN FR13A AND 14 IN NOSE LANDING GEAR FIGURE 3, VIEW B AND C. FOUND CRACK ON FORWARD LOWER HOLE 4 O`CLOCK POSITION FACING OUTBOARD. ACCOMPLISH THE REPAIR PER EO-98843 AND STE PNA EA 300-5312-27-A4650, REV-.
- [SDR IPXA2026101215031](https://openairdocs.org/sdr/IPXA2026101215031.md): Keelbeam · cracked · Sep 12, 2026 · N158UP · Airbus A300F4622R · Fuselage Main, Keel
  > RIGHT KEEL BEAM AT THE LEVEL OF CONNECTING FITTING BETWEEN FR13A AND 14 IN NOSE LANDING GEAR FIGURE 3, VIEW B AND C. FOUND CRACK ON FORWARD LOWER HOLE 4&9 O`CLOCK POSITION FACING OUTBOARD. REMOVED WEB BETWEEN FR 13A AND 14 R/H SIDE OF NOSE LANDING GEAR BOX IN
- [SDR IPXA2026092815031](https://openairdocs.org/sdr/IPXA2026092815031.md): Keelbeam · cracked · Sep 12, 2026 · N158UP · Airbus A300F4622R · Fuselage Main, Keel
  > MAJOR REPAIR, RIGHT KEEL BEAM AT THE LEVEL OF CONNECTING FITTING BETWEEN FR13A AND 14 IN NOSE LANDING GEAR FIGURE 3, VIEW B AND C. FOUND CRACK ON FORWARD LOWER HOLE 4&9 O`CLOCK POSITION FACING OUTBOARD. AS PER REQUEST, PERFORMED EXTERNAL HFEC SURFACE INSPECT
- [SDR IPXA2026092815093](https://openairdocs.org/sdr/IPXA2026092815093.md): Keelbeam · cracked · Sep 12, 2026 · N158UP · Airbus A300F4622R · Fuselage Main, Keel
  > MAJOR REPAIR, LEFT KEEL BEAM AT THE LEVEL OF CONNECTING FITTING BETWEEN FR13A AND 14 IN NOSE LANDING GEAR FIGURE 3, VIEW B AND C. FOUND CRACK ON FORWARD LOWER HOLE 4 O`CLOCK POSITION FACING OUTBOARD. VERIFIED REMOVAL OF L/H NLG DOOR TORQUE TUBE I.A.W. A300-6
- [SDR IPXA2026101803114](https://openairdocs.org/sdr/IPXA2026101803114.md): Skin · cracked · Sep 11, 2026 · N158UP · Airbus A300F4622R · Trailing Edge Flaps
  > RT WING, CENTER FLAP, TOP SKIN RIB FLANGE. 1 EA CRACK NOTED AT RIB 25. ACCOMPLISH REPAIR IN ACCORDANCE WITH EO-98679 AND EA 300-5753-27-A4632, REV-.
- [SDR IPXA2026092605733](https://openairdocs.org/sdr/IPXA2026092605733.md): Floor Panel · cracked · Sep 11, 2026 · N158UP · Airbus A300F4622R · Fuselage Floor Panel
  > MAIN DECK FLOOR STRUCTURE Z-PROFILE ON R/H SIDE AT FR 75 UNDER FLOOR PANEL 262PF IS CRACKED. INSTALLED Z PROFILE AT R/H SIDE AT FR 75 UNDER FLOOR PANEL 262PF PER SRM 51-40-21-001.
- [SDR IPXA2026092405633](https://openairdocs.org/sdr/IPXA2026092405633.md): Tee Angle · cracked · Sep 11, 2026 · N158UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > MAIN DECK FLOOR STRUCTURE T-PROFILE ON LT SIDE AT FR 80 IS CRACKED, INSTALLED NEW PROFILE-T I.A.W. A300-600 SRM 51-40-21.
- [SDR IPXA2026092105610](https://openairdocs.org/sdr/IPXA2026092105610.md): Profile · cracked · Sep 11, 2026 · N158UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > MAIN DECK FLOOR STRUCTURE T-PROFILE ON RT SIDE AT FR 80 IS CRACKED. INSTALLED NEW T-PROFILE SRM 51-40-21-001.
- [SDR IPXA2026092823749](https://openairdocs.org/sdr/IPXA2026092823749.md): Fairing · cracked · Sep 1, 2026 · N158UP · Airbus A300F4622R · Nacelle/Pylon, Main Frame
  > CRACK ON #1 ENG AFT LWR PYLON FAIRING, LOWER SKIN. LOWER AFT FAIRING REMOVED AND INSTALLED ON MPC 400 T3F18E007EGD6.
- [SDR IPXA2026050302068](https://openairdocs.org/sdr/IPXA2026050302068.md): Slide · no test · May 3, 2026 · N158UP · Airbus A300F4622R · Escape Slide
  > ESCAPE SLIDE FAILED LIGHT TEST. CLEANED AND TIGHTENED LOOSE PTT SWITCH. OPS CHECKS GOOD PER AMM 52-73-11.
- [SDR IPXA2026042352149](https://openairdocs.org/sdr/IPXA2026042352149.md): Slide · faulted · Apr 23, 2026 · N158UP · Airbus A300F4622R · Escape Slide
  > RED FLASHING DOOR SLIDE ARMED LIGHT IS FLASHING WITH SLIDE DISARMED PERFORMED OPERATIONAL CHECK OF EMERGENCY ESCAPE SLIDE WARNING LIGHT IN REFERENCE TO AMM 52-73-11. OPS CHECK GOOD. NO DMP. PLACARD REMOVED.
- [SDR IPXA2025081144210](https://openairdocs.org/sdr/IPXA2025081144210.md): Power Supply · inoperative · Aug 1, 2025 · N158UP · Airbus A300F4622R · Emergency Lighting
  > EMERGENCY LIGHTS POWER SUPPLY UNITS FAILED BITE CHECK -ER AMM 33-51-00-0501 REF PS1 STEP 23. C/W BITE CHECK IAW AMM 33-51-00-0501, NO FAULTS FOUND, CHECK OK AT THIS TIME
- [SDR IPXA202508044210](https://openairdocs.org/sdr/IPXA202508044210.md): Power Supply · no test · Aug 1, 2025 · N158UP · Airbus A300F4622R · Emergency Lighting
  > EMERGENCY LIGHTS POWER SUPPLY UNITS FAILED BITE CHECK -ER AMM 33-51-00-0501 REF PS1 STEP 23 C/W BITE CHECK IAW AMM 33-51-00-0501, NO FAULTS FOUND, CHECK OK AT THIS TIME
- [SDR IPXA2025031483584](https://openairdocs.org/sdr/IPXA2025031483584.md): Coupling · leaking · Mar 11, 2025 · N158UP · Airbus A300F4622R · Aircraft Fuel Distribution System
  > FUEL APPEARS TO BE MIGRATING FROM L INNER TO CENTER TANK AT 2-300LBS/HR.(1300LBS OVER 4 HR FLT.) AIRCRAFT OPERATED IN PAYLOAD, (CTR AND TRIM DEACTIVATED.) PERFORMED GVI ON LH CENTER TANK ENGINE FEED LINES IN CENTER TANK THAT GOES TO THE PUMP FOUND 2 COUPLING L
- [SDR IPXA2025031283584](https://openairdocs.org/sdr/IPXA2025031283584.md): Fuel Tank · leaking · Mar 11, 2025 · N158UP · Airbus A300F4622R · Fuel Storage
  > *SDR FILED OPEN* FUEL APPEARS TO BE MIGRATING FROM L INNER TO CENTER TANK AT 2-300LBS/HR.(1300LBS OVER 4 HR FLT.) AIRCRAFT OPERATED IN PAYLOAD, (CTR AND TRIM DEACTIVATED.) VERIFIED FUEL IS TRANSFERRING SLOWLY BETWEEN LEFT INNER TANK AND CENTER TANK USING LEFT
- [SDR IPXA2025021309682](https://openairdocs.org/sdr/IPXA2025021309682.md): Indicator · malfunctioned · Feb 12, 2025 · N158UP · Airbus A300F4622R · Door Warning System
  > CREW DOOR, WITH DOOR OPEN AND DISARMED, FOUND WARNING LIGHT (7WN) BLINKING, NO WARNING HORN. CLEANED SWITCH 13WN AND PERF ADJ TEST IAW MM 52-10-11/501 TEST NORMAL DEFERRAL CLEARED PLAC RMVD
- [SDR IPXA2025020323495](https://openairdocs.org/sdr/IPXA2025020323495.md): Transfer Sys · inoperative · Feb 1, 2025 · N158UP · Airbus A300F4622R · Aircraft Fuel Distribution System
  > A/C IN PAYLOAD MODE. CTR TANK FUEL 100# AT ENG START. STEADILY INCREASE DURING FLT + 1 HR AFTER T/O 700LBS +2 HRS=1000LBS +3HR+1250LBS CTR TANK. AT ENG. SHUTDOWN 1260 REVERSED MEL 28-28-26-1-1 AFTER REMOVAL AND REPLACEMENT OF CGCC IAW AMM 31-46-11 AND REMOVAL
- [SDR IPXA2025010295911](https://openairdocs.org/sdr/IPXA2025010295911.md): Slide · warning light · Jan 2, 2025 · N158UP · Airbus A300F4622R · Emergency Equipment
  > MAIN ENTRY DOOR L-1 SLIDE PRESSURE INDICATION IN RED BAN L-1 DOOR ESCAPE SLIDE PRESSURE INDICATIONS CHECKS GOOD IAW AMM 25-61-20.
- [SDR IPXA2024070218398](https://openairdocs.org/sdr/IPXA2024070218398.md): Warning Buzzer · inoperative · Jul 2, 2024 · N158UP · Airbus A300F4622R · Emergency Exits
  > EMERGENCY DOOR SLIDE BUZZER INOP REMOVED AND REPLACED ENTRY DOOR SLIDE WARNING BUZZER IAW AMM 52-73-12/401. OPS CHECK GOOD
- [SDR IPXA2024051574929](https://openairdocs.org/sdr/IPXA2024051574929.md): Unknown · vibration · May 15, 2024 · N158UP · Airbus A300F4622R · Fuselage Structure (General)
  > **ATB** **SDR FILED OPEN** CLIMBING THROUGH 3500 FT EXPERIENCED HIGH VIBRATION THAT SHOOK THE A/C.WE LEVELED OFF AT 6000 AND REDUCED TO GREEN DOT. VIBRATION WENT AWAY. NO ECAM OR ABNORMAL INDICATIONS. FIBER GLASS DUST CAME OUT
- [SDR IPXA2024040269813](https://openairdocs.org/sdr/IPXA2024040269813.md): Adapter · corroded · Mar 8, 2024 · N158UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > MAIN CARGO RH, FR 20, CLS ADAPTER (NEXT TO 232EF PANEL AND NEXT TO SEAT TRACK -Y1959) WITH CORROSION AND IS BROKEN. D0T 103-024 REVIEWED. REMOVED MAIN CARGO RH FR 20 CLS ADAPTER IAW A300-600 SRM 51-40-21.
- [SDR IPXA2024040339914](https://openairdocs.org/sdr/IPXA2024040339914.md): Seat Track · corroded · Mar 7, 2024 · N158UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN LEFT SIDE SEAT TRACK Y794 HAS CORROSION AT FR 82 15-07 REVIEWED. REMOVED SEAT TRACK Y852 FROM FR 78.5 TO FR82 IAW A300-600 SRM 53-10-16. LOCATED AND DRILLED SEAT TRACK IAW SRM 53-10-16 AND SRM 51-40-44.
- [SDR IPXA2024040339682](https://openairdocs.org/sdr/IPXA2024040339682.md): Seat Track · corroded · Mar 7, 2024 · N158UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN LEFT SIDE SEAT TRACK Y450 HAS CORROSION AT FR 82 15-06 REVIEWED. REMOVED SEAT TRACK Y450 FROM FR79.5 TO FR82 IAW A300-600 SRM 53-10-16. ACCOMPLISH MAJOR PERMANENT REPAIR PER SRM 53-10-16-201 PARAGRAPH 4 FIGURE 201B (REV 40).
- [SDR IPXA2024040339480](https://openairdocs.org/sdr/IPXA2024040339480.md): Seat Track · corroded · Mar 7, 2024 · N158UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN RIGHT SIDE SEAT TRACK -Y450 HAS CORROSION AT FR 82 15-03 REVIEWED. REMOVED SEAT TRACK -Y450 FROM FR78.5 TO FR82. IAW A300-600 SRM 53-10-16-201. TREATED AND PRIMED SEAT TRACK AND SPLICES. IAW A300-600 SRM 51-21-10.

Next page: https://openairdocs.org/aircraft/N158UP/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 = 'N158UP' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N158UP/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.