# Service difficulty reports: N133UP

A list on [N133UP](https://openairdocs.org/aircraft/N133UP.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 5 · 246 reports

- [SDR IPXA2026090347689](https://openairdocs.org/sdr/IPXA2026090347689.md): Fuel · leaking · Sep 2, 2026 · N133UP · Airbus A300F4622R · Air Distribution System
  > STRONG ODOR OF JET FUEL ON THE FLIGHT DECK. IN AIR OR GROUND WITH PACKS ON WITH ENG OR APU AS BLEED SOURCE. CLEANED AREA OF THE FUEL LEAK, RAN APU FOR SEVERAL HOURS. VERIFIED NO FUEL SMELL FROM PACKS USING APU. REF MM 49-32-12-401.
- [SDR IPXA2026090247689](https://openairdocs.org/sdr/IPXA2026090247689.md): Unknown · odor · Sep 2, 2026 · N133UP · Airbus A300F4622R · Air Distribution System
  > STRONG ODOR OF JET FUEL ON THE FLIGHT DECK. IN AIR OR GROUND WITH PACKS ON WITH ENG OR APU AS BLEED SOURCE.
- [SDR IPXA2026071456799](https://openairdocs.org/sdr/IPXA2026071456799.md): Cover · broken · Jul 14, 2026 · N133UP · Airbus A300F4622R · Passenger/Crew Doors
  > SAFETY COVER FOR DOOR ARMING LEVER BROKEN & CRACKED, SHARP EDGES EXPOSED. REMOVED DAMAGED ENTRY DOOR SLIDE ARMING COVER. REPLACED ARMING COVER DOOR IAW AMM 52-10-13. OPS CHECKS GOOD.
- [SDR IPXA2026060401733](https://openairdocs.org/sdr/IPXA2026060401733.md): Valve · odor · Jun 4, 2026 · N133UP · Airbus A300F4622R · Pneumatic Distribution System
  > IN DECENT WITH NON IDLE POWER SETTING THE #1 AND #2 HP VALVES CYCLED WITH A HOT SMELL. #1 HP EVENTUALLY FAULTED AND RESET VIA THE CHECKLIST. THE CYCLING CONTINUED DURING DECENT. ON FINAL WITH #2 PACK. FOUND PNEUMATIC SYSTEM CONTROLLER 1 TO HAVE €ŒC CONTROLLE
- [SDR IPXA2025120329714](https://openairdocs.org/sdr/IPXA2025120329714.md): Button · stuck · Dec 2, 2025 · N133UP · Airbus A300F4622R · Passenger/Crew Doors
  > ON MAIN CABIN ENTERY DOOR. THE PUSH TO RELEASE BUTTON IS STUCK DOWN. DOOR WILL NOT LOCK OPEN. FREED UP PUSH TO RELEASE BUTTON AND OPS CHECK GOOD PER AMM 52-10-00-2.
- [SDR IPXA2025111229656](https://openairdocs.org/sdr/IPXA2025111229656.md): Computer · faulted · Nov 12, 2025 · N133UP · Airbus A300F4622R · Fuel Indicating System
  > EMERGENCY DECLARED, AUTO FUEL FAULT IN FLIGHT RAN QRH PROCEDURES AFTER EVALUATING FUEL QUANITY WE SAW OUTER FUEL @ 4700 REVIEWED FUEL IMBALANCE CHECK BALANCEED FUEL UPON LANDING OUTER FUEL TANK SHOWED 8200 LBS. T/S AUTO FUEL FEED FAULT PREFORMED AUTO FU
- [SDR IPXA2025103116091](https://openairdocs.org/sdr/IPXA2025103116091.md): Web · cracked · Oct 29, 2025 · N133UP · Airbus A300F4622R · Nacelle/Pylon Miscellaneous Structure
  > NR 1 PYLON AFT MEMBER BETWEEN RIB 18 AND RIB 21 CRACKED. JP-110. REMOVED AND REPLACED AFT MEMBER (WEB) IAW A300-600 SRM 51-40-21.
- [SDR IPXA2025103185179](https://openairdocs.org/sdr/IPXA2025103185179.md): Bracket · broken · Oct 27, 2025 · N133UP · Airbus A300F4622R · Fuselage Floor Panel
  > FLOOR PANEL 144FR AREA, AFT BRACKET BROKEN. SUPPORT FAIRING WAS INSTALLED IAW A300/600 SRM 51-40-21. REVIEWED
- [SDR IPXA2025103121028](https://openairdocs.org/sdr/IPXA2025103121028.md): Floor Panel · damaged · Oct 12, 2025 · N133UP · Airbus A300F4622R · Fuselage Floor Panel
  > INSP MLG W/W PANEL 147BF DELAMINATED. VERIFIED FLOOR PANEL 147BF FABRICATED IAW SREO-16407-REQ002.
- [SDR IPXA2025103104418](https://openairdocs.org/sdr/IPXA2025103104418.md): Floor Panel · debonded · Oct 10, 2025 · N133UP · Airbus A300F4622R · Fuselage Floor Panel
  > FLOOR PANEL 131 BH EDGE IS DISBONDED. FLOOR PANEL 131BH FABRICATION IS COMPLETED IAW SERO-16407-REQ002((APPX C) A300 FWD/AFT LOWER CARGO COMPARTMENT FLOOR PANEL FABRICATION (SREO)).
- [SDR IPXA2025103104517](https://openairdocs.org/sdr/IPXA2025103104517.md): Floor Panel · damaged · Oct 10, 2025 · N133UP · Airbus A300F4622R · Fuselage Floor Panel
  > FLOOR PANEL 152 M CORNER HAS BROKEN COMPOSITE. FLOOR PANEL 152MG FABRICATED IAW SREO-16407-REQ002 ((APPX C) A300 FWD/AFT LOWER CARGO COMPARTMENT FLOOR PANEL FABRICATION (SREO)).
- [SDR IPXA2025110188289](https://openairdocs.org/sdr/IPXA2025110188289.md): Deflector · cracked · Oct 10, 2025 · N133UP · Airbus A300F4622R · Wing Main, Frame Structure
  > FAULT - STR, Z500, PANEL RACK, LH WING, DEFLECTOR PANEL 572LB HAS GOUGE W/CRACK. DOT 103-1524. PROFILE WAS INSTALLED IAW A300/600 SRM 51-40-21 REVIEWED
- [SDR IPXA2025102102022](https://openairdocs.org/sdr/IPXA2025102102022.md): Seat Track · damaged · Oct 10, 2025 · N133UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN - ENLONGATED HOLE ON SEAT TRACK BTW FR79 AND FR80/82 -Y450. REMOVED SEAT TRACK BTW FR79 AND FR80/82 -Y450 IAW SRM 53-10-16 PG 207 FIGURE 201. INSTALLED NEW SEAT TRACK BTW FR79 AND FR80/82-Y450 IAW SRM 53-10-16 PAG.207, FIG. 20.
- [SDR IPXA2025101675564](https://openairdocs.org/sdr/IPXA2025101675564.md): Adapter · corroded · Oct 9, 2025 · N133UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings
  > ***SUPPLEMENTAL SDR*** FAULT: STR - Z200 - MAIN CABIN - CLS ADAPTER WITH CRACK AT FR34 BTW -Y1959 & -Y2462. INSTALLED CLS ADAPTER IAW A300 SRM 51-40-21.
- [SDR IPXA2025101475564](https://openairdocs.org/sdr/IPXA2025101475564.md): Adapter · cracked · Oct 9, 2025 · N133UP · Airbus A300F4622R · Fuselage Main, Structure
  > MAIN CABIN, CLS ADAPTER WITH CRACK AT FR34 BTW -Y1959 & -Y2462 LOCATED AND DRILLED CLS ADAPTER. IAW A300 SRM 51-40-40. REQUEST OK TO INSTALL.
- [SDR IPXA2025110459260](https://openairdocs.org/sdr/IPXA2025110459260.md): Adapter · corroded · Oct 8, 2025 · N133UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN - SEAT TRACK ADAPTER SEGMENT CLS WITH CORROSION BTW FR20 AND FR27 BTW Y1580 & Y2244. INSTALLED NEW TRACK ADAPTER CLS SEGMENT IAW A300-600 SRM 51-40-21. REVIEWED
- [SDR IPXA2025110561418](https://openairdocs.org/sdr/IPXA2025110561418.md): Adapter · corroded · Oct 8, 2025 · N133UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN - CLS ADAPTER WITH CORROSION AT FR 27 Y0 RH. INSTALED CLS ADAPTER I.A.W. A300-600 SRM 51-40-21. REVIEWED
- [SDR IPXA2025102461494](https://openairdocs.org/sdr/IPXA2025102461494.md): Adapter · corroded · Oct 8, 2025 · N133UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN - SEAT TRACK CLS ADAPTER WITH CORROSION AT FR 27 Y0 LT. INSTALLED CLS ADAPTER IAW SRM 51-40-21.
- [SDR IPXA2025102356354](https://openairdocs.org/sdr/IPXA2025102356354.md): Profile · damaged · Oct 8, 2025 · N133UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > MAIN CABIN - Z-PROFILE CRACKED BTW FR73-FR74 -Y2127.6. REMOVED Z-PROFILE IN MAIN CABIN BTW FR73-FR74 -Y 2127.6 IAW AIRBUS A300-600 SRM 51-40-21. INSTALLED NEW Z-PROFILE AT FR73-FR74 -Y2127.6 IAW AIRBUS A300-600 SRM 51-40-21.
- [SDR IPXA2025101658777](https://openairdocs.org/sdr/IPXA2025101658777.md): Adapter · corroded · Oct 8, 2025 · N133UP · Airbus A300F4622R · Fuselage Main, Structure
  > MAIN CABIN - CLS ADAPTER WITH CRACK AT FR37 BTW Y1580.5 & Y2127.5. INSTALLED CLS ADAPTER IAW A300 SRM 51-40-21.
- [SDR IPXA2025102461059](https://openairdocs.org/sdr/IPXA2025102461059.md): Hinge Fitting · corroded · Oct 8, 2025 · N133UP · Airbus A300F4622R · Engine Thrust Reverser
  > FAULT - STR Z400 - ENG #2 O/B FAN COWL, AFT ATTACH SUPPORT DAMAGED. DOT 90-038. ++REPLACED FAN COWL HINGE AT STR Z400 - ENG #2 O/B FAN COWL, AFT ATTACH SUPPORT IAW A300-600 SRM 51-40-21
- [SDR IPXA2025101655510](https://openairdocs.org/sdr/IPXA2025101655510.md): Profile · cracked · Oct 8, 2025 · N133UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > MAIN CABIN - T-PROFILE CRACKED AT FR80/82 -Y2127. REMOVED T-PROFILE IN MAIN CABIN AT FR80/82 -Y 2127. IAW SRM 51-40-21. INSTALLED. MAIN CABIN NEW T-PROFILE AT FR80/82-Y2127 IAW SRM 51-40-21 USED.
- [SDR IPXA2025102355969](https://openairdocs.org/sdr/IPXA2025102355969.md): Profile · damaged · Oct 8, 2025 · N133UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > MAIN CABIN - Z-PROFILE CRACKED AT FR75 Y2127.6. REMOVED Z-PROFILE IN MAIN CABIN AT FR75 Y 2127.6 IAW SRM 51-40-21. INSTALLED NEW Z-PROFILE AT FR75 Y2127.6 IAW SRM 51-40-21.
- [SDR IPXA2025102356317](https://openairdocs.org/sdr/IPXA2025102356317.md): Web · damaged · Oct 8, 2025 · N133UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > MAIN CABIN - WEB CRACKED BTW FR73-FR74 Y2127.6. REMOVED WEB IN MAIN CABIN BTW FR73-FR74 Y2127.6 IAW SRM 51-40-21. ++INSTALLED NEW WEB BTW FR73-FR74 Y2127.6. IAW SRM 51-40-21.
- [SDR IPXA2025102356212](https://openairdocs.org/sdr/IPXA2025102356212.md): Web · cracked · Oct 8, 2025 · N133UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > MAIN CABIN - WEB CRACKED BTW FR73-FR74 -Y2127.6. REMOVED Z-PROFILE IN MAIN CABIN BTW FR73-FR74 -Y 2127.6 IAW SRM 51-40-21. INSTALLED NEW Z-PROFILE AT FR73-FR74 -Y2127.6 IAW SRM 51-40-21.
- [SDR IPXA2025102261418](https://openairdocs.org/sdr/IPXA2025102261418.md): Adapter · corroded · Oct 8, 2025 · N133UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN - CLS ADAPTER (SEAT TRACK) WITH CORROSION AT FR 27 Y0 RH VERIFIED INSTALLATION OF CLS ADAPTER IAW SRM 51-40-21. OPEN
- [SDR IPXA2025102261494](https://openairdocs.org/sdr/IPXA2025102261494.md): Adapter · corroded · Oct 8, 2025 · N133UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN - CLS ADAPTER (SEAT TRACK) WITH CORROSION AT FR 27 Y0 LT VERIFIED INSTALLATION OF CLS ADAPTER IAW A300-600 SRM 51-40-21 (1 TUBE QTY). OPEN
- [SDR IPXA2025102158491](https://openairdocs.org/sdr/IPXA2025102158491.md): Seat Track · corroded · Oct 8, 2025 · N133UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN - SEAT TRACK WITH CORROSION AT FR67 Y0. INSTALLED NEW SEAT TRACK BTW FR66-FR67 AND FR68-69 Y0 IAW AIRBUS A300-600 SRM 53-10-16 PAG.207, FIG. 20.
- [SDR IPXA2025101555582](https://openairdocs.org/sdr/IPXA2025101555582.md): Profile · cracked · Oct 8, 2025 · N133UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > MAIN CABIN - T-PROFILE CRACKED AT FR80/82 Y2127. REMOVED T-PROFILE IN MAIN CABIN AT FR80/82 Y 2127. IAW SRM 51-40-21. INSTALLED. MAIN CABIN NEW T-PROFILE AT FR80/82 Y2127 IAW SRM 51-40-21 USED.
- [SDR IPXA2025101458777](https://openairdocs.org/sdr/IPXA2025101458777.md): Adapter · corroded · Oct 8, 2025 · N133UP · Airbus A300F4622R · Fuselage Main, Structure
  > MAIN CABIN, CLS ADAPTER WITH CRACK AT FR37 BTW Y1580.5 & Y2127.5 LOCATED AND DRILLED CLS ADAPTER. IAW A300 SRM 51-40-40. REQUEST OK TO INSTALL.
- [SDR IPXA2025101458725](https://openairdocs.org/sdr/IPXA2025101458725.md): Adapter · corroded · Oct 8, 2025 · N133UP · Airbus A300F4622R · Fuselage Main, Structure
  > ADAPTER WITH CORROSION AT FR 38 BTW Y1580.5 & Y2127.5. INSTALLED CLS ADAPTER IAW A300 SRM 51-40-21.
- [SDR IPXA2025102434573](https://openairdocs.org/sdr/IPXA2025102434573.md): Rib · cracked · Oct 7, 2025 · N133UP · Airbus A300F4622R · Trailing Edge Flaps
  > RIGHT WING, CENTER FLAP, TOP SKIN RIB FLANGE. ONE CRACK NOTED AT RIB 17. ACCOMPLISH PERMANENT REPAIR IN ACCORDANCE WITH VT-MAE EA 300-5750-27-A4183, REV. -.
- [SDR IPXA2025102434841](https://openairdocs.org/sdr/IPXA2025102434841.md): Rib · cracked · Oct 7, 2025 · N133UP · Airbus A300F4622R · Trailing Edge Flaps
  > RIGHT WING, CENTER FLAP, TOP SKIN RIB FLANGE. TWO CRACKS NOTED AT RIB 27. ACCOMPLISH PERMANENT REPAIR IAW EA 300-5750-27-A4183, REV. -.
- [SDR IPXA2025102434554](https://openairdocs.org/sdr/IPXA2025102434554.md): Rib · cracked · Oct 7, 2025 · N133UP · Airbus A300F4622R · Trailing Edge Flaps
  > RIGHT WING, CENTER FLAP, TOP SKIN RIB FLANGE. 1EA CRACK NOTED AT RIB 11. ACCOMPLISHED PERMANENT REPAIR IN ACCORDANCE WITH VT-MAE EA 300-5750-27-A4183, REV. -.
- [SDR IPXA2025102434561](https://openairdocs.org/sdr/IPXA2025102434561.md): Rib · cracked · Oct 7, 2025 · N133UP · Airbus A300F4622R · Trailing Edge Flaps
  > RIGHT WING, CENTER FLAP, TOP SKIN RIB FLANGE. 1EA CRACK NOTED AT RIB 18. ACCOMPLISH PERMANENT REPAIR IN ACCORDANCE WITH VT-MAE EA 300-5750-27-A4183, REV. -.
- [SDR IPXA2025102434775](https://openairdocs.org/sdr/IPXA2025102434775.md): Rib · cracked · Oct 7, 2025 · N133UP · Airbus A300F4622R · Trailing Edge Flaps
  > FAULT: RH WING, CENTER FLAP, TOP SKIN RIB FLANGE. 2EA CRACKS NOTED AT RIB 26. CIRCLED IN RED. ACCOMPLISH PERMANENT REPAIR IN ACCORDANCE WITH VT-MAE EA 300-5750-27-A4183, REV. -. REVIEWED
- [SDR IPXA2025102434779](https://openairdocs.org/sdr/IPXA2025102434779.md): Rib · cracked · Oct 7, 2025 · N133UP · Airbus A300F4622R · Trailing Edge Flaps
  > FAULT: RH WING, CENTER FLAP, TOP SKIN RIB FLANGE. 2EA CRACKS NOTED AT RIB 25. CIRCLED IN RED. ACCOMPLISHED PERMANENT REPAIR IN ACCORDANCE WITH VT-MAE EA 300-5750-27-A4183, REV. -. REVIEWED
- [SDR IPXA2025102838770](https://openairdocs.org/sdr/IPXA2025102838770.md): Fitting · cracked · Oct 7, 2025 · N133UP · Airbus A300F4622R · Wing Main, Frame Structure
  > CRACK FOUND AT OPEN HOLE OF LT WING FR 40 LOWER RADIUS, CRACK NOTED AT FIRST LAYER FWD LAYER, 6 O'CLOCK POSITION, CRACK DEPTH FROM FWD TO AFT AT 5MM. INSTALLED REINFORCING SKIN AND STIFFENER UNDER IAW SRM 51-40-21.
- [SDR IPXA2025101740226](https://openairdocs.org/sdr/IPXA2025101740226.md): Floor Support · cracked · Oct 7, 2025 · N133UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > CABIN FLOOR SIDE SUPPORT BETWEEN FR 38.1 AND FR38.2 LH, Y2462 CRACKED. JP-110. REMOVED SIDE FLOOR SUPPORT BTW FR38.1 AND FR38.2 LH IAW SRM 51-40-21. INSTALLED NEW SUPPORT BRACKET IAW SRM A300-600 51-40-21.
- [SDR IPXA2025103099591](https://openairdocs.org/sdr/IPXA2025103099591.md): Web · cracked · Oct 5, 2025 · N133UP · Airbus A300F4622R · Nacelle/Pylon Miscellaneous Structure
  > NR 1 PYLON RIB 3 UPPER WEB CRACKED. JP-110. INSTALLED PYLON #1 SUPPORT OF THE PRESSURE RELIEF DOOR, IAW-A300-AMM 54-52-62/401 ITEM (4).
- [SDR IPXA2025102298127](https://openairdocs.org/sdr/IPXA2025102298127.md): Support · cracked · Oct 5, 2025 · N133UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > CABIN FLOOR SIDE SUPPORT BETWEEN FR 38 AND FR38.1 LH, Y2462 CRACKED. REMOVAL FUNNEL FROM FRAME 34 TO FRAME 38 AND FROM FRAME 38 TO FRAME 38.2 IAW SRM 51-40-21 AND AIPC 25-58-04-85B. FLOOR SIDE SUPPORT WAS REMOVED FROM FR 38 TO FR 38.1 LH IAW A300-600 SRM 51-4
- [SDR IPXA2025101498133](https://openairdocs.org/sdr/IPXA2025101498133.md): Floor Support · cracked · Oct 5, 2025 · N133UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > CABIN FLOOR SIDE SUPPORT BETWEEN FR 37 AND FR38 RH, -Y2462 CRACKED. JP-110. REMOVED SIDE SUPPORT BETWEEN FR 37 AND FR 38 RH -Y2462 IAW SRM 51-40-21. SIDE SUPPORT WAS INSTALLED IAW SRM 51-40-2.
- [SDR IPXA2025102988759](https://openairdocs.org/sdr/IPXA2025102988759.md): Web · cracked · Oct 4, 2025 · N133UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT WEB AT FR54, Y1959 CRACKED. REMOVED THE WEB AT FR54, Y1959 IAW SRM 51-40-21. INSTALLED NEW WEB ANGLE AT FR54 Y1959 LH SIDE.
- [SDR IPXA2025102988782](https://openairdocs.org/sdr/IPXA2025102988782.md): Angle · cracked · Oct 4, 2025 · N133UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT WEB AT FR54, Y953 LH CRACKED. REMOVED AFT CARGO COMPARTMENT WEB AT FR54, Y953 LT IAW SRM 51-40-21. INSTALLED NEW WEB ANGLE AT FR54 7953 LH SIDE.
- [SDR IPXA2025101379065](https://openairdocs.org/sdr/IPXA2025101379065.md): Angle · cracked · Oct 3, 2025 · N133UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > AVIONICS COMPARTMNT FR9 ANGLE CRACKED AT Y950. FABRICATED AND DRILLED NEW ANGLE FITTING FROM 2024-T3.063C", B/N:0004276732. IAW SRM 53-12-15 FIG.7ITEM #80 AND UPS GMM-09.08.01.03, FOLLOW #4. INSTALLED NEW ANGLE FITTING IAW SRM 51-40-21.
- [SDR IPXA2025101379032](https://openairdocs.org/sdr/IPXA2025101379032.md): Angle · cracked · Oct 3, 2025 · N133UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > AVIONICS COMPARTMNT FR9 ANGLE CRACKED AT -Y950 JP-110. REMOVED WEB CRACKED RH SIDE IAW A300/600 SRM 51-40-21. INSTALLED NEW ANGLE FITTING IAW A300-600 SRM 51-40-21.
- [SDR IPXA2024102271179](https://openairdocs.org/sdr/IPXA2024102271179.md): Slide · unknown · Oct 22, 2024 · N133UP · Airbus A300F4622R · Escape Slide
  > AFTER SHUTDOWN SLIDE DISARMS BUT WONT DISARM TO WHERE YOU CAN INSERT THE SAFETY PIN INSTALLED EMERGENCY EVACUATION SLIDE IAW MM 25-61-21
- [SDR IPXA2023080293780](https://openairdocs.org/sdr/IPXA2023080293780.md): Door · inoperative · Aug 2, 2023 · N133UP · Airbus A300F4622R · Passenger/Crew Doors
  > INSPECTION TYPE:N/ACREW ENTRY DOOR GUST LOCK BUTTON STUCK DOWNLUBRICATED GUST LOCK BUTTON AND CHECKED DOOR OPERATION PER AMM 52 10 20. SOP CHECKS NORMAL AT THIS TIME
- [SDR IPXA2023061793461](https://openairdocs.org/sdr/IPXA2023061793461.md): Skin · gouged · Jun 17, 2023 · N133UP · Airbus A300F4622R · Nacelle/Pylon Structure
  > INSPECTION TYPE:C#2 ENGINE OB EXHAUST CONE AREA HAS A GOUGEREPAIRED AREA IAW PW SRM 54-40-00
- [SDR IPXA2023060993406](https://openairdocs.org/sdr/IPXA2023060993406.md): Fairing · cracked · Jun 7, 2023 · N133UP · Airbus A300F4622R · Fuselage Structure (General)
  > INSPECTION TYPE:C611AB OPENING HAS A CRACKREPAIRED AREA IAW SRM 53-15-63

Next page: https://openairdocs.org/aircraft/N133UP/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 = 'N133UP' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N133UP/reports

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