# Service difficulty reports: N169UP

A list on [N169UP](https://openairdocs.org/aircraft/N169UP.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 3 · 127 reports

- [SDR IPXA2026092487635](https://openairdocs.org/sdr/IPXA2026092487635.md): Cabin Press Sys · faulted · Sep 23, 2026 · N169UP · Airbus A300F4622R · Cabin Pressure Control System
  > IN DESCENT AT ABOUT 6000 FT WE RECIEVED CAB PRESS ADV, VS ON CAB PRESS PAGE WAS AT 1500 FT/MIN A NOTICEABLE HISSING SOUND FROM CAPTAINS SIDE OF COCKPIT AND NOTICEABLE EAR POPS FOR CAPT AND FO PERFORMED INSP/CHECK OF PREFORMED SEAL CAPT. SLIDING WINDOW PER AMM
- [SDR IPXA2026092387635](https://openairdocs.org/sdr/IPXA2026092387635.md): Cabin Pressure · low pressure · Sep 23, 2026 · N169UP · Airbus A300F4622R · Cabin Pressure Control System
  > DURING DESCENT AT ABOUT 6000 FT, RECIEVED CABIN PRESSURE ADV, VS ON CABIN PRESSURE PAGE WAS AT 1500 FT/MIN A NOTICEABLE HISSING SOUND FROM CAPTAINS SIDE OF COCKPIT AND NOTICEABLE EAR POPS FOR CAPT AND FO.
- [SDR IPXA2026040278578](https://openairdocs.org/sdr/IPXA2026040278578.md): Rib · cracked · Mar 14, 2026 · N169UP · Airbus A300F4622R · Spoilers
  > UPON FURTHER INSPECTION OF DAMAGED LEFT WING #5 SPOILER ACCESS DOOR, FOUND UNDERLYING STRUCTURAL DAMAGE TO SPOILER HINGE. INSTALLED NEW "RIB JACK ABX 148-625" AT LEFT WING #5 SPOILER IAW A300-600 SRM 51-40-21-001.
- [SDR IPXA2025063037463](https://openairdocs.org/sdr/IPXA2025063037463.md): Smoke Warning · false activation · Jun 26, 2025 · N169UP · Airbus A300F4622R · Smoke Detection
  > AVIONICS SMOKE ECAM ON CLIMB OUT. NO SMOKE DETECTED. ECAM OCCURED TWO MORE TIMES ON DESCENT. NO SMOKE DETECTED THROUGHOUT THE FLIGHT TROUBLESHOT IAW A300 TSM 26-15-00 FIG. 102 SHEET 1. REMOVED AND REPLACED SMOKE DETECTORS 11WA AND 13WA IAW A300 AMM 26-15-1
- [SDR IPXA2025020737215](https://openairdocs.org/sdr/IPXA2025020737215.md): Sensor · faulted · Feb 7, 2025 · N169UP · Airbus A300F4622R · Pitot/Static Anti-Ice System
  > **ATB** IMMEDIATELY AFTER TAKEOFF, RECEIVED CAPTAIN PITOT HEAT FAULT. RAN ECAM/QRH PROCEDURE AND IT WOULD NOT RECOVER. PERFORMED INSULATION TEST PER AMM 30-31-00/501. INSULATION TEST GOOD. PER TSM 30-31-00/101 FIG 103, RELAY 75DA REQUIRES REPLACEMENT. R/R RELA
- [SDR IPXA2024120386082](https://openairdocs.org/sdr/IPXA2024120386082.md): Bracket · cracked · Dec 2, 2024 · N169UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > FWD CARGO FR 38.2 HAS 4(EA) CRACKED BEAM SUPPORT. INSTALLED NEW BRACKETS IAW SRM 51-40-20.
- [SDR IPXA2024113024730](https://openairdocs.org/sdr/IPXA2024113024730.md): Web · cracked · Nov 27, 2024 · N169UP · Airbus A300F4622R · Nacelle/Pylon Miscellaneous Structure
  > #1 PYLON LOWER AFT AREA WEB P/N A54515063206 IS CRACKED. INSTALLED NEW WEB AT PYLON #1 LOWER IAW A300-600, SRM 51-40-21, WITH FASTENER: RIVET SOLID P/N:MS2615-4M5, BATCH# 0004090312, CR3523-4-04, BATCH# 0004176917, IAD 41R54610328 AND SRM 54-54-11 AND SRM 51-
- [SDR IPXA2024112724730](https://openairdocs.org/sdr/IPXA2024112724730.md): Web · cracked · Nov 27, 2024 · N169UP · Airbus A300F4622R · Nacelle/Pylon Miscellaneous Structure
  > NR 1 PYLON LOWER AFT AREA WEB P/N A54515063206 IS CRACKED APPROVED.
- [SDR IPXA2024120460569](https://openairdocs.org/sdr/IPXA2024120460569.md): Nut Plate · damaged · Nov 23, 2024 · N169UP · Airbus A300F4622R · Wing, Control Surface Attach Fittings
  > RH WING INTERNERAL KRUEGER FLAP AREA HAS A NUTPLATE STRIP WITH MISSING CHUNK. INSTALLED NUT PLATE STRIP IN RH WING INTERNAL KRUEGER FLAP IAW SRM 51-40-21 P/N MS20470AD5-4 BATCH#0004130107.
- [SDR IPXA2024112560569](https://openairdocs.org/sdr/IPXA2024112560569.md): Nut Plate · damaged · Nov 23, 2024 · N169UP · Airbus A300F4622R · Leading Edge Devices
  > RH WING INTERNERAL KRUEGER FLAP AREA HAS A NUTPLATE STRIP WITH MISSING CHUNK GIVEN OK TO INSTALL STEP # 10.
- [SDR IPXA2024120483595](https://openairdocs.org/sdr/IPXA2024120483595.md): Insulation · missing · Nov 14, 2024 · N169UP · Airbus A300F4622R · Passenger/Crew Doors
  > CREW DOOR: INSULATION PLATES MISSING ON TOP OF CREW DOOR. INSTALLED INSULATION AT THE TOP OF THE CREW DOOR USING PN: DAN381H10 BATCH: 0004342850 AND PN: 1357 BATCH: 0004333962 IAW AMM25-00-00/801.
- [SDR IPXA2024111583595](https://openairdocs.org/sdr/IPXA2024111583595.md): Plate · missing · Nov 14, 2024 · N169UP · Airbus A300F4622R · Passenger/Crew Doors
  > **SDR FILED OPEN** CREW DOOR: INSULATION PLATES MISSING ON TOP OF CREW DOOR APPROVED.
- [SDR IPXA2024112079444](https://openairdocs.org/sdr/IPXA2024112079444.md): Adapter · corroded · Oct 26, 2024 · N169UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK FLOOR SEAT TRACK Y0 CENTER CLS ADAPTER HAS CORROSION DOT 108-03, CM-108. ACCOMPLISH PERMANENT REPAIR PER EO-92003-REQ1 REV. 1.
- [SDR IPXA2024112967766](https://openairdocs.org/sdr/IPXA2024112967766.md): Rib · cracked · Oct 25, 2024 · N169UP · Airbus A300F4622R · Nacelle/Pylon, Frame/Spar/Rib
  > PYLON #1 RIB 18, PANEL 475AL SUPPORT O/B HAS A CRACK.
- [SDR IPXA2024120438050](https://openairdocs.org/sdr/IPXA2024120438050.md): Skin · no discrepancy · Oct 24, 2024 · N169UP · Airbus A300F4622R · Standard Practices/Structures
  > FWD CREW DOOR NEED INTERNAL SKIN CLEANING AND CIC. 89-471. CLEANED AREA IAW AMM 12-21-12. CIC APPLIED ON ORIGINATING TASK CARD# T3F18E002PX4W.
- [SDR IPXA2024112726460](https://openairdocs.org/sdr/IPXA2024112726460.md): Support · cracked · Oct 24, 2024 · N169UP · Airbus A300F4622R · Nacelle/Pylon Miscellaneous Structure
  > PYLON #1 PRECOOLER UPPER PANEL AREA, FWD PANEL SUPPORT HAS A CRACK. DOT 28-28. INSTALLED NEW #1 PYLON PRECOOLER WEB IAW SRM 51-40-21 P/NA54612419200 BATCH# 0004341019 P/N MS206156M4 BATCH# 0004302637 P/N CCR264SS3-4 BATCH# 0004335024.
- [SDR IPXA2024103013519](https://openairdocs.org/sdr/IPXA2024103013519.md): Fan Cowl · cracked · Oct 24, 2024 · N169UP · Airbus A300F4622R · Turbine Engine Reduction Gear
  > FAULT STR-460 ENGINE #2, FAN CORE RH-REAR SIDE W/CRACK NEXT TO P2/T2 ELBOW LINE COUPLING (3' POSITION); DOT 117-025, JR-117. INSTELLED NEW WEB IAW A300 PRATT & WHITNEY 54-10-00. PN: CR3553-6-5, BN: 0004267593, PN: CR3522-6-5, BN: 0004292846. INSTALLED COVER AN
- [SDR IPXA2024110216569](https://openairdocs.org/sdr/IPXA2024110216569.md): Web · cracked · Oct 24, 2024 · N169UP · Airbus A300F4622R · Nacelle/Pylon, Main Frame
  > ENGINE #1 RIGHT REAR NOSE COWL P2T2 ELBOW, SHOWS A CRACK EVIDENCE. DOT 75-047 HA-75. INSTALLED LINE AND COVER IAW A300 AMM 73-24-06/401 T95888.
- [SDR IPXA2024110216565](https://openairdocs.org/sdr/IPXA2024110216565.md): Web · cracked · Oct 24, 2024 · N169UP · Airbus A300F4622R · Nacelle/Pylon, Main Frame
  > ENGINE #1 LEFT REAR NOSE COWL P2T2 ELBOW, SHOWS A CRACK EVIDENCE. DOT 75-46 HA-75. INSTALLED LINE AND COVER IAW A300 AMM 73-24-06/401 T95888.
- [SDR IPXA2024102538050](https://openairdocs.org/sdr/IPXA2024102538050.md): Skin · dirty · Oct 24, 2024 · N169UP · Airbus A300F4622R · Passenger/Crew Doors
  > FAULT - FWD CREW DOOR NEED INTERNAL SKIN CLEANING AND CIC. 89-471 APPROVED FOR CLEANING. CIC IS PART OF ORIGINATING TASK.
- [SDR IPXA2024111101593](https://openairdocs.org/sdr/IPXA2024111101593.md): Floorboard · gouged · Oct 23, 2024 · N169UP · Airbus A300F4622R · Fuselage Floor Panel
  > MAIN DECK: MAIN DECK FLOOR PANEL 232SG HAS GOUGE DOT 6999-02. REPAIRED FLOOR PANEL 232SG USING PN:04-009-0146 BATCH: 0004333424 IAW SREO-42721-REQ001.
- [SDR IPXA2024110101522](https://openairdocs.org/sdr/IPXA2024110101522.md): Floor Panel · gouged · Oct 23, 2024 · N169UP · Airbus A300F4622R · Fuselage Floor Panel
  > MAIN DECK: MAIN DECK FLOOR PANEL 232NJ HAS DAMAGE DOT 6999-01. REPAIRED FLOOR PANEL 232NJ USING PN: 04-009-0146 BATCH: 0004333424 IAW SREO- 42721- REQ001.
- [SDR IPXA2024103110990](https://openairdocs.org/sdr/IPXA2024103110990.md): Web · cracked · Oct 23, 2024 · N169UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > UNDER PANEL 212HP WEB AND ANGLE AT -Y953/FR10 CRACKED. DOT: 101-11 TG-101. INSTALLED NEW ANGLE UNDER PANEL 212HP AT Y-953/FR 10 I.A.W. A300-600 S.R.M. 51-40-21. REVIEWED.
- [SDR IPXA2024103003563](https://openairdocs.org/sdr/IPXA2024103003563.md): Floor Panel · damaged · Oct 23, 2024 · N169UP · Airbus A300F4622R · Fuselage Floor Panel
  > FWD CARGO COMPARTMENT FLOOR PANEL 131SG HAS MATERIAL LOSE. DOT 28-20. REPAIRED FLOOR PANEL 131SG USING PN: 04-009-0146 BATCH: 0004333424 IAW SREO-42721-REQ001. REVIEWED.
- [SDR IPXA2024103003555](https://openairdocs.org/sdr/IPXA2024103003555.md): Floor Panel · damaged · Oct 23, 2024 · N169UP · Airbus A300F4622R · Fuselage Floor Panel
  > FAULT-COMPST-ZONE 100. FWD CARGO COMPARTMENT FLOOR PANEL 131GE HAS MATERIAL LOSE. DOT 28-19. REPAIRED FLOOR PANEL 131GE USING PN: 04-009-0146 BATCH: 0004333424 IAW SREO-42721-REQ001. REVIEWED.
- [SDR IPXA2024103101710](https://openairdocs.org/sdr/IPXA2024103101710.md): Floor Panel · cracked · Oct 23, 2024 · N169UP · Airbus A300F4622R · Fuselage Floor Panel
  > MAIN DECK FLOOR PANEL 251WJ IS CRACKED DOT 6999-04. FABRICATED MAIN DECK FLOOR PANEL 251WJ USING MATERIALS P/N:5024N00001SS-G BATCH#:0000096292, INSERTS:G2001B-3P BATCH#:0004326496 G2002A-3S BATCH#:0004318237 I.A.W. SREO-16407-REQ001.
- [SDR IPXA2024103003591](https://openairdocs.org/sdr/IPXA2024103003591.md): Floor Panel · damaged · Oct 23, 2024 · N169UP · Airbus A300F4622R · Fuselage Floor Panel
  > FWD CARGO COMPARTMENT FLOOR PANEL 132SG HAS MATERIAL LOSE. DOT 28-21. REPAIRED FLOOR PANEL 132SG USING PN: 04-009-0146 BATCH: 0004333424 IAW SREO-42721-REQ001. REVIEWED.
- [SDR IPXA2024103111466](https://openairdocs.org/sdr/IPXA2024103111466.md): Angle · cracked · Oct 23, 2024 · N169UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > UNDER PANEL 211HP ANGLE CREACKED AT Y953/FR 10 DOT101-15 TG-101. INSTALLED NEW ANGLE UNDER PANEL 211HP AT Y953/FR 10 I.A.W. A300-600 S.R.M. 51-40-21. REVIEWED.
- [SDR IPXA2024102801522](https://openairdocs.org/sdr/IPXA2024102801522.md): Floor Panel · damaged · Oct 23, 2024 · N169UP · Airbus A300F4622R · Fuselage Floor Panel
  > MAIN DECK: MAIN DECK FLOOR PANEL 232NJ HAS DAMAGE DOT 6999-01 REJECTED. MAJOR REPAIR.
- [SDR IPXA2024102801593](https://openairdocs.org/sdr/IPXA2024102801593.md): Floor Panel · gouged · Oct 23, 2024 · N169UP · Airbus A300F4622R · Fuselage Floor Panel
  > *SDR FILED OPEN*, MAIN DECK: MAIN DECK FLOOR PANEL 232SG HAS GOUGE. MAJOR REPAIR.
- [SDR IPXA2024111357868](https://openairdocs.org/sdr/IPXA2024111357868.md): Floor Support · cracked · Oct 21, 2024 · N169UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > AFT LOWER CARGO AT FR 54 L/H MIDDLE O/B FLOOR SUPPORT BRACKET IS CRACKED. DOT 60-007. INSTALLED NEW SUPPORT WITH P/N MS20470AD5-12 B/N0004235393 IAW SRM 51-40-21.
- [SDR IPXA2024120337570](https://openairdocs.org/sdr/IPXA2024120337570.md): Panel · cracked · Oct 19, 2024 · N169UP · Airbus A300F4622R · Wing Main, Frame Structure
  > CUT OUT UNDER PANEL 513AB IS CRACKED. DOT 101-01 TG-101. INSTALLED DOUBLERS IAW A300-600 SRM 51-40-21 WITH FASTENERS P/N:MS20426AD4-4, BATCH# 0004249215,NUT PLATE P/N: MS21060-3,BATCH:0004177915.
- [SDR IPXA2024102432320](https://openairdocs.org/sdr/IPXA2024102432320.md): Bracket · corroded · Oct 19, 2024 · N169UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > AFT CARGO FR 54 RH SIDE CEILING PANEL SUPPORT CORRODED DOT 07586-01 REVIEWED. VENDOR CLOSED SDR WITHOUT QC AUDIT AND MMX-REP AUDIT. INSTALLED NEW SUPPORT IAW A300 SRM 51-40-21. PN: CCR264553-04, BN: 00043311647, PN: ABS0337-01A, BN: 0004326080.
- [SDR IPXA2024102332372](https://openairdocs.org/sdr/IPXA2024102332372.md): Bracket · cracked · Oct 19, 2024 · N169UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > AFT CARGO FR 54 RH SIDE MOST O/B PANEL SUPPORT CRACKED 07586-02. INSTALLED NEW ANGLE IAW SRM 51-40-21 HILOCK HL110VF6-5, BATCH:4237615 P/N:3D0006-3 BATCH:0004273630.
- [SDR IPXA2024102332408](https://openairdocs.org/sdr/IPXA2024102332408.md): Bracket · cracked · Oct 19, 2024 · N169UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > AFT CARGO FR 54 RH SIDE SECOND MOST O/B PANEL SUPPORT CRACKED DOT 07586-03. INSTALLED NEW BRACKET IAW SRM 51-40-21.
- [SDR IPXA2024102432532](https://openairdocs.org/sdr/IPXA2024102432532.md): Profile · corroded · Oct 19, 2024 · N169UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > AFT CARGO FR 58 HORIZONTAL CEILING SUPPORTS LH TO RH HAS 8(EA) SPOTS OF CORROSION AROUND FASTENER HOLES DOT 07586-08. INSTALLED NEW HORIZONTAL CEILING SUPPORTS AT AFT CARGO FR58 IAW SRM 51-40-21.
- [SDR IPXA2023061393434](https://openairdocs.org/sdr/IPXA2023061393434.md): Warning Buzzer · inoperative · Jun 11, 2023 · N169UP · Airbus A300F4622R · Passenger/Crew Doors
  > INSPECTION TYPE:NAEVAC SLIDE WARNING BUZZER BROKEN IN HALFR&R ESCAPE SLIDE WARNING BUZZER IAW AMM 52-73-12. OPS TEST GOOD.
- [SDR IPXA2022120288622](https://openairdocs.org/sdr/IPXA2022120288622.md): Door · inoperative · Dec 1, 2022 · N169UP · Airbus A300F4622R · Landing Gear Doors
  > DIVERSION ON GEAR RETRACTION, NOSE GEAR DOOR DID NOT CLOSE, ECAM AND FRDC CW INFLT DIV TO SDF. REMOVED AND REPLACED THE RT FWD NOSE DOOR COVER FITTING IAW AMM 32-22-11-501 PERFORMED NOSE BEAR OPERATION IAW A300 32-31-00. OPS CHECKED GOOD.
- [SDR IPXA2022062783544](https://openairdocs.org/sdr/IPXA2022062783544.md): Engine · abnormal · Jun 26, 2022 · N169UP · Airbus A300F4622R · Powerplant System
  > INSPECTION TYPE:NADURING #2 ENGINE START AT MAX MOTOR (23%) #2 FUEL LEVER WOULD NOT MOVE OUT OF CUTOFF POSITION. FUEL WAS NEVER ADDED AND START WAS ABORTEDPERFROMED 3 ENGINE STARTS / STOPS CYCLES IAW AMM 71-00-00-0501. ALL OPS CHECK GOOD. RUNS WERE PERFROMED A
- [SDR IPXA2022062483452](https://openairdocs.org/sdr/IPXA2022062483452.md): Bracket · cracked · Jun 24, 2022 · N169UP · Airbus A300F4622R · Wing, Attach Fittings
  > INSPECTION TYPE:A300SUPPORT FITTING CRACKED AT ATTATCH POINT BEHIND DEFLECTOR PANEL 572LBREMOVED AND REPLACED IAW SRM 51-40-21
- [SDR IPXA2022062483460](https://openairdocs.org/sdr/IPXA2022062483460.md): Crossbeam · broken · Jun 24, 2022 · N169UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:1C/3E AND E COMPARTMENT UNDER FLOORRBOARDS 121 FT HAS A WIRE SUPPORT BROKEN.ACCOMPLISHED REPAIRED PER SRM 51-70-10 FIG.29
- [SDR IPXA2022062483444](https://openairdocs.org/sdr/IPXA2022062483444.md): Angle · cracked · Jun 24, 2022 · N169UP · Airbus A300F4622R · Fuselage Main, Structure
  > INSPECTION TYPE:1CRH KRUGER FLAP WING AREA HAS A CRACK ON INNER BRACKET/ANGLE DOT 90-36REMOVED AND REPLACED IAW SRM 51-40-21
- [SDR IPXA2021112976421](https://openairdocs.org/sdr/IPXA2021112976421.md): Apu · faulted · Nov 25, 2021 · N169UP · Airbus A300F4622R · APU Cowling/Containment
  > INSPECTION TYPE:N/A**DIVERSION**EMERG DEC'D**A/C LANDED W/OUT INCIDENT** ON CLIMBOUT GEN #2 FAULTED PERFORMED ECAM/QRH PROC, STARTED APU, APU FAILED PERFORMED DIVERSION TO MDT.DEFERRED #2 IDG IAW MEL 24-11-01-1. PLACARD INSTALLED, DMP C/W. CHECKED & SERVICED #
- [SDR IPXA2021071371609](https://openairdocs.org/sdr/IPXA2021071371609.md): Switch · stuck · Jul 13, 2021 · N169UP · Airbus A300F4622R · Emergency Lighting
  > INSPECTION TYPE:NAEMERGENCY LIGHTING STUCK IN THE ON POSITIONPERFORMED OPERATIONAL TEST OF EMERGENCY LIGHTS IAW AMM 33-51-00-0501. OPS CHECK GOOD AT THIS TIME
- [SDR IPXA2020042254517](https://openairdocs.org/sdr/IPXA2020042254517.md): Skin · delaminated · Apr 21, 2020 · N169UP · Airbus A300F4622R · Wing, Plate/Skin
  > INSPECTION TYPE:SEGLT WING FIXED T/E O/B OF #6 FLAP FAIRING DELAM ON SKIN - 2 AREASREPAIR PER EA# 300-5750-27-A2440 REV -
- [SDR IPXA2020042254516](https://openairdocs.org/sdr/IPXA2020042254516.md): Skin · delaminated · Apr 21, 2020 · N169UP · Airbus A300F4622R · Wing, Plate/Skin
  > INSPECTION TYPE:SEGLT WING FIXED T/E O/B OF #6 FLAP FAIRING DELAM ON SKIN - 2 AREASREPAIR PER EA# 300-5750-27-A2440 RE -
- [SDR IPXA2020041554272](https://openairdocs.org/sdr/IPXA2020041554272.md): Seat Track · corroded · Apr 15, 2020 · N169UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE:SEGMCD SEAT TRACK BET FR79-FR80 -Y794.3(R/H) CORROSIONREPAIRED IAW A300-600 SRM REV33 53-10-16 FIG 201
- [SDR IPXA2020041554271](https://openairdocs.org/sdr/IPXA2020041554271.md): Seat Track · corroded · Apr 15, 2020 · N169UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE:SEGMCD SEAT TRACK BET FR79-FR80 @ Y794.3(L/H) HAS CORROSIONREPLACE (REPAIRED) IAW A300-600 SRM REV 33 53-10-16 FIG 201
- [SDR IPXA2020041554270](https://openairdocs.org/sdr/IPXA2020041554270.md): Seat Track · corroded · Apr 15, 2020 · N169UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE:SEGMCD SEAT TRACK BET FR79-FR80 @ -Y1137.1 (R/H) CORROSIONREPAIRED IAW A300-600 SRM REC33 53-10-16 FIG 201
- [SDR IPXA2020041554223](https://openairdocs.org/sdr/IPXA2020041554223.md): Angle · bent · Apr 14, 2020 · N169UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:SEGFWD CARGO CUT OUT, CLOSE OUT ANGLE HAS NICKS AND IS BENTREMOVED AND REPLACE ANGLE (NEW) IAW SRM-51-40-21.

Next page: https://openairdocs.org/aircraft/N169UP/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 = 'N169UP' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N169UP/reports

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