# Service difficulty reports: N332UP

A list on [N332UP](https://openairdocs.org/aircraft/N332UP.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 · 120 reports

- [SDR IPXA2026042439581](https://openairdocs.org/sdr/IPXA2026042439581.md): Actuator · noisy · Apr 23, 2026 · N332UP · Boeing 76734AF · Cargo/Baggage Doors
  > NOISE DURING AFT CARGO DOOR OPERATION. I.A.W AMM 52-37-04-004-001 REV.147 AND AMM 52-37-04-404-009 REV.147 REPLACE AFT CARGO DOOR ROTARY ACTUATOR AND OPERATION CHECK, TEST RESULT WAS SATISFIED.
- [SDR IPXA2026042483757](https://openairdocs.org/sdr/IPXA2026042483757.md): Bracket · cracked · Apr 20, 2026 · N332UP · Boeing 76734AF · Leading Edge Devices
  > CRACK-BRACKET, FWD AND MID SIDE OF LT WING NR 2 SLAT INBD SEAL DOOR, REPLACED IAW AMM 57-41-56-004-001 REV 147 AND AMM 57-41-56-404-009 REV 147.
- [SDR IPXA2026042563148](https://openairdocs.org/sdr/IPXA2026042563148.md): Seal · torn · Apr 18, 2026 · N332UP · Boeing 76734AF · Spoilers
  > LEFT WING NR 6 SPOILER HAS A TORN SEAL LOCATED AT THE 3RD ATTACH POINT FROM INBD END. IAW AMM 20-11-00-910-802, REV 147, REPLACED THE SEAL.
- [SDR IPXA2026042563692](https://openairdocs.org/sdr/IPXA2026042563692.md): Hinge · worn · Apr 18, 2026 · N332UP · Boeing 76734AF · Wing, Attach Fittings
  > FOUND NR 8 TAI DOOR AFT HINGE WORN OUT. IAW AMM 57-41-58-434-044, ADJUSTED AND PERFORMED A BONDING TEST OF NR 8 TAI DOOR AFTER HINGE,RESULT WAS SATISFACTORY.
- [SDR IPXA2026042463695](https://openairdocs.org/sdr/IPXA2026042463695.md): Bearing · migrated · Apr 18, 2026 · N332UP · Boeing 76734AF · Spoilers
  > MIGRATED BEARING, RT WING T/E NR 7 SPOILER LOWER FITTING. IAW AMM27-61-02-424-023 REV.147 CONNECT RH WING NO.7 SPOILER PCA ROD END AND THE SPOILER TO FLAP CLEARANCE MEASURED CHECK SATISFIED.
- [SDR IPXA2026042263719](https://openairdocs.org/sdr/IPXA2026042263719.md): Door · chafed · Apr 18, 2026 · N332UP · Boeing 76734AF · Engine Thrust Reverser
  > CHAFED SKIN, NR 2 ENG RT THRUST REVERSER LOWER BLOWOUT DOOR L/E AREA. REFER TO FAULT: T3F18E008P5SF FOR NEW DOOR REPLACEMENT.
- [SDR IPXA2026042262880](https://openairdocs.org/sdr/IPXA2026042262880.md): Angle · cracked · Apr 18, 2026 · N332UP · Boeing 76734AF · Nacelle/Pylon Miscellaneous Structure
  > RIGHT PYLON ANGLE AT LOWER SURFACE RIGHT SIDE, BELOW AFT THRUST LINK IS CRACKED. INSTALLED NEW ANGLE I.A.W SRM 51-40-02-0G REV.95 AND BOEING DWG NO.313T2380 SH.65 REV.D AND DWG NO. 313T2380 SH.66 REV.D
- [SDR IPXA2026042263867](https://openairdocs.org/sdr/IPXA2026042263867.md): Fairing · broken · Apr 18, 2026 · N332UP · Boeing 76734AF · Engine Thrust Reverser
  > BROKEN FAIRING NR 1 ENG RT THRUST REVERSER TRANSLATING COWL FAIRING INNER 12:00 POS. ACCOMPLISHED JOB I.A.W UPS SREO-45403-REQ003 REV.1 AND SRM 51-40-02-0G REV.95 AND IPC 78-32-32 REV.96
- [SDR IPXA2026042146211](https://openairdocs.org/sdr/IPXA2026042146211.md): Seal · broken · Apr 17, 2026 · N332UP · Boeing 76734AF · Nacelle/Pylon, Main Frame
  > BROKEN-SEAL, NR 2 PYLON FAIRING PANEL 446CR SPRING SEAL. REMOVED DAMAGED SEAL IAW SRM 51-40-02-0G REV.95. INSTALL NEW SEAL IAW SRM 51-40-02-0G, REV.95, AND DWG 311T2570, SH 15, REV B.
- [SDR IPXA2026042146228](https://openairdocs.org/sdr/IPXA2026042146228.md): Door · chafed · Apr 17, 2026 · N332UP · Boeing 76734AF · Engine Thrust Reverser
  > CHAFED DOOR, NR 2 ENG RT THRUST REVERSER LWR LATCH PNL INNER AREA (REPLACE) REMOVED DAMAGE DOOR I.A.W SRM 51-40-02-0G REV.95. INSTALL NEW DOOR IAW SRM 51-40-02-0G REV.95 AND AIPC 78-31-51-03 REV.141 AND ST ENGINEERING IPC 78-32-22 REV.96 AND AMM 78-31-19-402-
- [SDR IPXA2026042146161](https://openairdocs.org/sdr/IPXA2026042146161.md): Bracket · chafed · Apr 17, 2026 · N332UP · Boeing 76734AF · Nacelle/Pylon, Main Frame
  > CHAFED BRACKET, NR 2 ENG LT CORE COWL HOLD OPEN ROD SUPPORT BRACKET. REMOVED DAMAGE BRACKET IAW SRM 51-40-02-0G, REV 95. INSTALLED A NEW BRACKET IAW SRM 51-40-02-0G, REV 95 AND CMM IPL 71-13-23, REV 47.
- [SDR IPXA2026042146248](https://openairdocs.org/sdr/IPXA2026042146248.md): Bracket · cracked · Apr 17, 2026 · N332UP · Boeing 76734AF · Engine Thrust Reverser
  > CRACK-ANGLE, NR 1 ENG RT THRUST REVERSER INNER DRAIN TUBE SUPPORT. REMOVE DAMAGE BRACKET IAW SRM 51-40-02-0G REV.95..INSTALLED A NEW BRACKET IAW SRM 51-40-02-0G, REV.95 AND IPC 78-32-52 REV.96.
- [SDR IPXA2026042428033](https://openairdocs.org/sdr/IPXA2026042428033.md): Bulb Seal · broken · Apr 16, 2026 · N332UP · Boeing 76734AF · Passenger/Crew Doors
  > AERODYNAMIC SEAL BROKEN, FORWARD LH ENTRY DOOR. INSTALL NEW SILICONE RUBBER SEAL I.A.W SRM 51-40-02-0G REV.95 AND BOEING DWG NO:141T6121 SH13 REV.B.
- [SDR IPXA2026042428172](https://openairdocs.org/sdr/IPXA2026042428172.md): Scuff Plate · dented · Apr 16, 2026 · N332UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > DENTED SCUFF PLATE, BULK CARGO DOOR CUTOUT LOWER AFT CORNER AREA. REPLACED IAW AMM 53-13-02-404-007 REV.147 TO INSTALL SCUFF PLATE. IAW AMM 53-13-02-404-007 REV.147 TO INSTALL SCUFF PLATE.
- [SDR IPXA2026042428272](https://openairdocs.org/sdr/IPXA2026042428272.md): Actuator · leaking · Apr 16, 2026 · N332UP · Boeing 76734AF · Aileron Control System
  > FOUND THE OUTBOARD SIDE PCA OF LEFT WING OUTBOARD AILERON HYDRAULIC LEAK. I.A.W AMM 27-11-49-422-028 REV.147 STEP 3.A TO 3.H(7) INSTALLED LH WING OUTBOARD AILERON OUTBOARD SIDE PCA.
- [SDR IPXA2026042227994](https://openairdocs.org/sdr/IPXA2026042227994.md): Support Angle · broken · Apr 16, 2026 · N332UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > FOUND MAIN DECK CARGO CREW ENTRY DOOR LOWER SILL DAMAGE UNDER SCUFF PLATE. (REPLACE) INSTALL NEW LLIPLAY I.A.W SRM 51-40-02-0G REV.95 AND BOEING DWG NO: 141T8310 SHEET.4 REV.H
- [SDR IPXA2026042026781](https://openairdocs.org/sdr/IPXA2026042026781.md): Guide · worn · Apr 16, 2026 · N332UP · Boeing 76734AF · Cargo Compartments
  > FOUND MAIN DECK CARGO HANDLING ROLLER BROKEN OF LATERAL GUIDE ASSY AT BS 620 LBL 66.00. IAW AMM 25-57-08-004-015 AND AMM 25-57-08-404-020 REV.147 REPLACED LATERAL GUIDE ASSY. CHECK NORMAL.
- [SDR IPXA2026042026761](https://openairdocs.org/sdr/IPXA2026042026761.md): Restraint · broken · Apr 16, 2026 · N332UP · Boeing 76734AF · Cargo Compartments
  > FOUND MAIN DECK CARGO HANDLING CL DOOR AREA RESTRAINT ASSY BROKEN AT: STA 522 BL 0.00 I.A.W AMM 25-58-03-404-031 AND AMM 25-58-03-404-017 REV.147 REPLACED CL DOOR AREA RESTRAINT ASSY TOTAL: 1 EA. CONDITION CHECK NORMAL.
- [SDR IPXA2026041828803](https://openairdocs.org/sdr/IPXA2026041828803.md): Skin · damaged · Apr 16, 2026 · N332UP · Boeing 76734AF · Trailing Edge Flaps
  > L/H WING T/E OUTBD FLAP INBD SIDE AFT CAP, WBL 355..I.A.W AMM 20-11-00-910-802 REV147 INSTALL L/H OUTBD FLAP INBD SIDE P-SEAL & RETAINER UPPER AND LOWER.
- [SDR IPXA2026041628033](https://openairdocs.org/sdr/IPXA2026041628033.md): Seal · broken · Apr 16, 2026 · N332UP · Boeing 76734AF · Passenger/Crew Doors
  > AERODYNAMIC SEAL BROKEN, FORWARD LH ENTRY DOOR. OPEN
- [SDR IPXA2026042410374](https://openairdocs.org/sdr/IPXA2026042410374.md): Scuff Plate · dented · Apr 15, 2026 · N332UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > DENTED SCUFF PLATE, BULK CARGO DOOR CUTOUT LOWER MID AREA. REPLACED IAW AMM 53-13-02-404-007 REV.147 TO INSTALL SCUFF PLATE.
- [SDR IPXA2026041711117](https://openairdocs.org/sdr/IPXA2026041711117.md): Roller · worn · Apr 15, 2026 · N332UP · Boeing 76734AF · Cargo Compartments
  > FOUND MAIN DECK CARGO HANDLING ROLLER RAIL ASSY WORN AT: STA 785 ~ STA 795 LBL 33.00, STA 797 ~ STA 807 LBL 33.00, STA 895 ~ STA 925 RBL 33. STEP 2 I.A.W AMM 25-57-05-004-001 AND AMM 25-57-05-404-006 REV.147 REPLACED ROLLER RAIL ASSY.
- [SDR IPXA2026041710726](https://openairdocs.org/sdr/IPXA2026041710726.md): Seat Track · worn · Apr 15, 2026 · N332UP · Boeing 76734AF · Fuselage, Seat/Cargo Attach Fittings
  > FOUND FIRST OFFICER SEAT TRACK ASSY WORN AT: INBOARD AFT AND INBOARD FORWARD. I.A.W AMM 25-11-01-822-095-001 REV.147 REPLACED TRACK ASSY TOTAL: 2 EA.
- [SDR IPXA2026041711106](https://openairdocs.org/sdr/IPXA2026041711106.md): Guide · broken · Apr 15, 2026 · N332UP · Boeing 76734AF · Cargo Compartments
  > FOUND MAIN DECK CARGO HANDLING LATERAL GUIDE ASSY BROKEN AT BS 500 RBL 22. REPLACED IAW AMM 25-57-08-004-015 AND AMM 25-57-08-404-020 REV.147.
- [SDR IPXA2026041710867](https://openairdocs.org/sdr/IPXA2026041710867.md): Seat Track · worn · Apr 15, 2026 · N332UP · Boeing 76734AF · Fuselage, Seat/Cargo Attach Fittings
  > FOUND CAPTAIN SEAT TRACK ASSY WORN AT: INBOARD AFT. I.A.W AMM 25-11-01-822-095-001 REV.147 REPLACED TRACK ASSY CONDITION CHECK NORMAL.
- [SDR IPXA2026041711079](https://openairdocs.org/sdr/IPXA2026041711079.md): Lock · worn · Apr 15, 2026 · N332UP · Boeing 76734AF · Cargo/Baggage Doors
  > FOUND MAIN DECK CARGO HANDLING ROLLER HOLE WORN OF LOCK ASSY AT: STA 1131 LBL 77.50 TOTAL: 1EA. I.A.W AMM 25-58-01-004-001 AND AMM 25-58-01-404-005 REV.147 REPLACED LOCK ASSY TOTAL: 1 EA.
- [SDR IPXA2026042010664](https://openairdocs.org/sdr/IPXA2026042010664.md): Stiffener · cracked · Apr 15, 2026 · N332UP · Boeing 76734AF · Fuselage Main, Longeron/Stringer
  > DURING PERFORM EO-63470-JIC002 FOUND CRACK AT NWW STA 287,RBL 25 STIFFENER. PERFORMED HEAT TREATED. REPAIRED IAW EO-63472-JIC001 REV.5 STEP 7. MAJOR REPAIR.
- [SDR IPXA2026042010700](https://openairdocs.org/sdr/IPXA2026042010700.md): Stiffener · cracked · Apr 15, 2026 · N332UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > MAJOR REPAIR. DURING PERFORM EO-63470-JIC001 FOUND CRACK AT NWW BS 287, LBL 25, STIFFENER..ACCOMPLISH THE REPAIR I.A.W UPS EO-63472-JIC001 REV5.
- [SDR IPXA2026042471246](https://openairdocs.org/sdr/IPXA2026042471246.md): Actuator · leaking · Apr 13, 2026 · N332UP · Boeing 76734AF · Aileron Control System
  > FOUND RT LCC ACTUATOR LEAKING. IAW AMM 27-11-14-424-016 REV.147 STEP 3.A TO STEP 3.F(9), INSTALLED RH WING LCCA.
- [SDR IPXA2026041772172](https://openairdocs.org/sdr/IPXA2026041772172.md): Panel · broken · Apr 13, 2026 · N332UP · Boeing 76734AF · Fuselage Main, Structure
  > FOUND MAIN DECK CARGO DADO PANEL WITH DAMAG ACCOMPLISH UPS SREO-29536-REQ002 REV.2.
- [SDR IPXA2026041472404](https://openairdocs.org/sdr/IPXA2026041472404.md): Floor Panel · damaged · Apr 13, 2026 · N332UP · Boeing 76734AF · Fuselage Floor Panel
  > MAJOR REPAIR. FOUND MAIN DECK FLOOR PANEL DAMAGED, IAW AMM 53-01-06-400-801 REV.147 INSTALLED MAIN DECK CARGO FLOOR PANEL.
- [SDR IPXA2026041472413](https://openairdocs.org/sdr/IPXA2026041472413.md): Floor Panel · damaged · Apr 13, 2026 · N332UP · Boeing 76734AF · Fuselage Floor Panel
  > MAJOR REPAIR. FOUND MAIN DECK FLOOR PANEL DAMAGE, IAW AMM 53-01-06-400-801 REV.147 INSTALLED MAIN DECK CARGO FLOOR PANEL.
- [SDR IPXA2025092972337](https://openairdocs.org/sdr/IPXA2025092972337.md): Sign · inoperative · Sep 27, 2025 · N332UP · Boeing 76734AF · Emergency Lighting
  > EMERGENCY EXIT LIGHTED SIGN BY THE COCKPIT ENTRYWAY DOOR IS INOPERATIVE. REMOVED AND REPLACED EMERGENCY CHARGER POWER SUPPLY UNIT IN REFERENCE TO AMM 33-51-07. AND ALSO REMOVED AND REPLACED EMERGENCY EXIT SIGN ASSY IN REFERENCE TO AMM 33-51-01. OPS CHECKS GOOD
- [SDR IPXA2025031385751](https://openairdocs.org/sdr/IPXA2025031385751.md): Skin · damaged · Jul 12, 2024 · N332UP · Boeing 76734AF · Trailing Edge Flaps
  > LEFT INBOARD AFT FLAP DAMAGED ON UPPER SURFACE AT APPROXIMATELY AFT OUTBOARD CORNER. COMPLETED REPAIR OF FLAP PER SRM 51-70-10-2R AND EO 90887-REQ5
- [SDR IPXA2024071941894](https://openairdocs.org/sdr/IPXA2024071941894.md): Skin · cracked · Jun 13, 2024 · N332UP · Boeing 76734AF · Nacelle/Pylon, Plate/Skin
  > LEFT PYLON HAS A CRACK ABOVE INBD SERVICE PANEL, ABOUT 1.5 INCHES LONG. MARKED. ALL REPAIR STEPS ACCOMPLISHED PER EO-90663-REQ2. LEFT ACCESS DOOR REINSTALL ADDRESSED ON T3F18E004TVDV. SHEETMETAL REPAIR IS COMPLETE.
- [SDR IPXA2024061441894](https://openairdocs.org/sdr/IPXA2024061441894.md): Skin · cracked · Jun 13, 2024 · N332UP · Boeing 76734AF · Nacelle/Pylon, Plate/Skin
  > LEFT PYLON HAS A CRACK ABOVE INBD SERVICE PANEL, ABOUT 1.5 INCHES LONG. MARKED. PERFORMED CONDUCTIVITY TEST ON CORD MATERIAL 7075 T6XXX IAW NDT 51-00-00. ALL 4 CORDS WERE CONSISTENT WITH A IAC OF 33. OPEN
- [SDR IPXA2024042918728](https://openairdocs.org/sdr/IPXA2024042918728.md): Bracket · corroded · Apr 16, 2024 · N332UP · Boeing 76734AF · Horizontal Stabilizer Structure
  > FAULT - CORROSION - BRACKET, R/H LOWER SURFACE OF UPPER RIGHT HORIZONTAL STABILIZER BOX STA 1805 (REPLACE) REMOVED DAMAGE PART I.A.W SRM 51-40-02-0G REV. 89. INSTALLED NEW PART I.A.W SRM 51-40-02-0G REV. 89. AND BOEING DWG NO. 182T7119 SH. 1 REV. D. JOB COMPL
- [SDR IPXA2024042462866](https://openairdocs.org/sdr/IPXA2024042462866.md): Angle · cracked · Apr 12, 2024 · N332UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > CRACK - ANGLE BULK CARGO COMPARTMENT LEFT AREA STA 1578 LBL 60 (REPLACE) 1. REMOVED DAMAGE PART I.A.W SRM 51-40-02-0G REV. 89. 2. INSTALLED NEW PART I.A.W SRM 51-40-02-0G REV. 89. AND BOEING DWG NO. 146T5650 SH. 5 REV. C. 3. JOB COMPLETED.
- [SDR IPXA2024041364183](https://openairdocs.org/sdr/IPXA2024041364183.md): None · none · Apr 12, 2024 · N332UP · Boeing 76734AF · Standard Practices/Structures
  > FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R. ACCOMPLISHED SDR PER E0-82173-J1C001.
- [SDR IPXA2024041964132](https://openairdocs.org/sdr/IPXA2024041964132.md): Angle · cracked · Apr 12, 2024 · N332UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > FAULT - CRACK - ANGLE BULK CARGO COMPARTMENT RIGHT AREA STA 1578 RBL 60 (REPLACE) REMOVED DAMAGE PART I.A.W SRM 51-40-02-0G REV. 89. INSTALLED NEW PART I.A.W SRM 51-40-02-0G REV. 89. AND BOEING DWG NO. 146T5650 SH. 5 REV. C. JOB COMPLETED.
- [SDR IPXA2024042246123](https://openairdocs.org/sdr/IPXA2024042246123.md): Skin · cracked · Apr 11, 2024 · N332UP · Boeing 76734AF · Wing, Plate/Skin
  > SKIN, FWD LOWER FACE OF R/H WING NO.9 SLAT L/E SKIN, NEAR INBD TRACK. (REPAIR) ACCOMPLISHED REPAIR I.A.W SRM 57-43-01-2R-2 REV. 89 AND EGAT WORK SHEET NO. 40316. REVIEWED
- [SDR IPXA2024081211321](https://openairdocs.org/sdr/IPXA2024081211321.md): Skin · dented · Aug 7, 2023 · N332UP · Boeing 76734AF · Fuselage Main, Plate/Skin
  > FUESLAGE DENT @ STA 654 +88 BETWEEN 35-36R PERFORMED PERMANENT REPAIR IAW EO-87841-REQ3.
- [SDR IPXA2023071303512](https://openairdocs.org/sdr/IPXA2023071303512.md): Door · noisy · Jul 13, 2023 · N332UP · Boeing 76734AF · Passenger/Crew Doors
  > VERY LOUD PRESSURIZATION AIR NOISE FROM MAIN ENTRY DOOR SEAL QUIT AT BETWEEN 4.0 & 5.0 PSI CABIN PRESSURE CLEANED MAIN ENTRY DOOR SEAL, PRESSURIZED A/C PER AMM 05-51-24, NO LEAKS NOTED. NO HISTORY LAST 30 DAYS, A/C OK FOR SERVICE.
- [SDR IPXA2023080898884](https://openairdocs.org/sdr/IPXA2023080898884.md): Skin · dented · May 11, 2023 · N332UP · Boeing 76734AF · Horizontal Stabilizer, Plate/Skin
  > *MAJOR REPAIR* RH HORIZONTAL STABILIZER UPPER SKIN DENT***SM40/LMX4*** COMPLETED E0-86923-REQ2. THIS CLEARS MOC 2301223.
- [SDR IPXA2023020890760](https://openairdocs.org/sdr/IPXA2023020890760.md): Indicator · not reported · Feb 8, 2023 · N332UP · Boeing 76734AF · Fuel Quantity Indicator
  > INSPECTION TYPE:NAFUEL QUANTITY INDICATOR ON OVERHEAD PANEL INTERMITTENT.PERFORMED FUEL QTY TEST PER FIM 28 41 00 815 861. NO FAULTS FOUND. SYSTEM OK. FUEL QTY INDICATION SHOWING CORRECTLY.
- [SDR IPXA2022081585251](https://openairdocs.org/sdr/IPXA2022081585251.md): Warning Message · illuminated · Aug 15, 2022 · N332UP · Boeing 76734AF · Engine Thrust Reverser
  > INSPECTION TYPE:ETOP** ETOPS FILED OPEN ** AFTER LANDING - R REV ISLN VALVE CAUTION MSG. DEFERRED PER MEL 78-31-1 PERFORMED DMP 78-31-1,DMI M788792 ASSIGNED INSTALLED PLACARD 3
- [SDR IPXA2022051382066](https://openairdocs.org/sdr/IPXA2022051382066.md): Circuit Breaker · popped · May 13, 2022 · N332UP · Boeing 76734AF · Fuel Boost Pump
  > INSPECTION TYPE:NA**SUPPLENTAL SDR** AT 1 H 43 MIN LH AFT FUEL PUMP C/B POPPED.1.R/R LH MAIN FUEL TANK AFT BOOST PUMP IAW AMM 28-22-03. 2. FUEL BOOST PUMP OPERATIONAL TEST SATIS. PN ON/OFF 5006003D/5006003S SN ON/OFF 3981/725 REF IPC 28-22-03-01-060U I
- [SDR IPXA2022050981860](https://openairdocs.org/sdr/IPXA2022050981860.md): Skin · damaged · Apr 29, 2022 · N332UP · Boeing 76734AF · Fuselage Main, Structure
  > INSPECTION TYPE:C11 LIGHTNING STRIKE DAMAGE WAS FOUND ON FUSELAGE SKIN (P/N:141T3840-77)BETWEEN STA 139 - STA 148.75, WL 224.5 - WL 216.REPAIR I.A.W 767-300F SRM 53-00-01-2R-6, REPAIR 6, REV 83.01.
- [SDR IPXA2022050881845](https://openairdocs.org/sdr/IPXA2022050881845.md): Stiffener · cracked · Apr 29, 2022 · N332UP · Boeing 76734AF · Wing Main, Frame Structure
  > INSPECTION TYPE:C11CRACK ON CENTER WING TANK STIFFENER(P/N:111T2005-8) ON STA 785.9, RBL 11.REPAIR I.A.W 767-300F SRM 57-10-10-2R-2 REPAIR 2 REV.83.01, AND UPS EO B767-5740-58151-C.
- [SDR IPXA2022050881844](https://openairdocs.org/sdr/IPXA2022050881844.md): Stiffener · cracked · Apr 29, 2022 · N332UP · Boeing 76734AF · Wing Main, Frame Structure
  > INSPECTION TYPE:C11CRACK ON CENTER WING TANK STIFFENER(P/N:111T2005-7) ON STA 785.9, LBL 11.REPAIR I.A.W 767-300F SRM 57-10-10-2R-2 REPAIR 2 REV.83.01, AND UPS EO B767-5740-58151-C.

Next page: https://openairdocs.org/aircraft/N332UP/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 = 'N332UP' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N332UP/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.