# Service difficulty reports: N320UP

A list on [N320UP](https://openairdocs.org/aircraft/N320UP.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 · 185 reports

- [SDR IPXA2026090120360](https://openairdocs.org/sdr/IPXA2026090120360.md): Battery Pack · no test · Aug 31, 2026 · N320UP · Boeing 76734AF · Emergency Lighting
  > DURING PDC, FOUND EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK IAW AMM 33-51-07. OPS CHECK GOOD.
- [SDR IPXA2026062990060](https://openairdocs.org/sdr/IPXA2026062990060.md): Indicator · stuck · Jun 27, 2026 · N320UP · Boeing 76734AF · Trailing Flap Position Indicating System
  > EMERGENCY DECLARED, FLAP INDICATOR DISAGREE,RAN QRH CHECKLIST.RT TE PLAP INDICATOR EVENTUALLY UNSTUCK REMOVED AND REPLACED FLAP INDICATOR AS PER AMM 27-58-02, OPS TEST OK
- [SDR IPXA2026050519564](https://openairdocs.org/sdr/IPXA2026050519564.md): Collar · cracked · Apr 22, 2026 · N320UP · Boeing 76734AF · Nacelle/Pylon Miscellaneous Structure
  > CRACKED COLLAR, NR 2 PYLON AFT LWR FAIRING AFT FRAME OTBD SIDE FWD SURFACE. INSTALLED NEW COLLAR IAW SRM 51-40-02-0G, REV 95, & DWG 313T3380, SH 3, REV F.
- [SDR IPXA2026050519511](https://openairdocs.org/sdr/IPXA2026050519511.md): Collar · cracked · Apr 22, 2026 · N320UP · Boeing 76734AF · Nacelle/Pylon Miscellaneous Structure
  > CRACKED COLLAR, NR 1 PYLON AFT FAIRING AFT BULKHEAD FWD CHANNEL INBD SIDE TOTAL 2 EA. INSTALLED NEW COLLAR IAW SRM 51-40-02-0G, REV 95, & DWG 313T3380, SH 3, REV F.
- [SDR IPXA2026043020504](https://openairdocs.org/sdr/IPXA2026043020504.md): Bracket · broken · Apr 22, 2026 · N320UP · Boeing 76734AF · Leading Edge Devices
  > FOUND RT WING NR 12 SLAT OTBD SIDE MAIN TRACK SKEW DETECTION BRACKET BROKEN. REPLACED IAW AMM 27-81-34-404-014, REV 147, INSTALLED RT WING NR 12 SLAT OTBD SIDE MAIN TRACK SKEW DETECTION BRACKET.
- [SDR IPXA2026050222041](https://openairdocs.org/sdr/IPXA2026050222041.md): Ring · cracked · Apr 22, 2026 · N320UP · Boeing 76734AF · Engine Thrust Reverser
  > FOUND ENG-1 RT THRUST REVERSER CASCADE SUPPORT RING CRACK AT 9 O'CLOCK. REFERENCED TASK T3F18E008RMGN INSTALLED THE T/R, FAN COWL AND ACCOMPLISHED THE INSTALLATION TEST.
- [SDR IPXA2026050119808](https://openairdocs.org/sdr/IPXA2026050119808.md): Angle · cracked · Apr 22, 2026 · N320UP · Boeing 76734AF · Engine Thrust Reverser
  > FAULT - CRACK - ANGLE, NO.2 ENG L/H T/R DRAIN TUBE SUPPORT BRACKET. (REPLACE) INSTALL NEW BRACKET I.A.W SRM 51-40-02-0G REV.95 AND ST ENGINEERING IPC 78-32-51 REV.96
- [SDR IPXA2026050119881](https://openairdocs.org/sdr/IPXA2026050119881.md): Pan · broken · Apr 22, 2026 · N320UP · Boeing 76734AF · Leading Edge Devices
  > BROKEN - PAN - SEAL, R/H WING SLAT NO.7 OUTBD SIDE. IAW PL 114T3200 REV. W DWG 114T3200 SHEET 3 REV. A & AMM 20-11-00-910-802 REV. 147 TO INSTALL THE SEAL PAN PN: 114T3187-2.
- [SDR IPXA2026042619384](https://openairdocs.org/sdr/IPXA2026042619384.md): Channel · chafed · Apr 22, 2026 · N320UP · Boeing 76734AF · Engine Thrust Reverser
  > CHAFING - CHANNEL, NO. 1 ENG L/H T/R AFT LWR FAIRING L/E AREA (REPLACE) INSTALL NEW CHANNEL I.A.W SRM 51-40-02-0G REV.95 AND ST ENGINEERING IPC 78-32-01 REV.96
- [SDR IPXA2026050119905](https://openairdocs.org/sdr/IPXA2026050119905.md): Clamp · broken · Apr 22, 2026 · N320UP · Boeing 76734AF · Passenger/Crew Doors
  > BROKEN - CLAMP, CREW ENTRY DOOR UPPER CUTOUT AREA. (REPLACE) I.A.W SWPM 20-10-12 REV.91 REPLACED CLAMP AT CREW ENTRY UPPER CUTOUT AREA AND CONDITION CHECK NORMAL.
- [SDR IPXA2026042819227](https://openairdocs.org/sdr/IPXA2026042819227.md): Seal · broken · Apr 22, 2026 · N320UP · Boeing 76734AF · Nacelle/Pylon Miscellaneous Structure
  > BROKEN SEAL, NR 1 PYLON FAIRING PANEL NR 436 CR SPRING SEAL BROKEN. INSTALLED A NEW SEAL STRIP IAW SRM 51-40-02-0G, REV 95, AND DWG 311T2570, SHT 14, REV -.
- [SDR IPXA2026042619261](https://openairdocs.org/sdr/IPXA2026042619261.md): Rub Strip · chafed · Apr 22, 2026 · N320UP · Boeing 76734AF · Nacelle/Pylon Miscellaneous Structure
  > CHAFED STRIP, NR 1 ENG RT CORE COWL INNER AFT UPPER STRIP CHAFING. INSTALLED A NEW WEAR STRIP IAW SRM 51-40-02-0G, REV.95, AND CMM IPL 71-13-24 REV. 50
- [SDR IPXA2026042619281](https://openairdocs.org/sdr/IPXA2026042619281.md): Door · chafed · Apr 22, 2026 · N320UP · Boeing 76734AF · Engine Thrust Reverser
  > CHAFED EDGE, NR 2 ENG RT T/R BLOW OUT DOOR L/E AREA. INSTALL WITH DOOR ASSY IAW SRM 51-40-02-0G, REV 95, AND AIPC 78-31-51-03, REV 141 AND IPC 78-32-22 REV.96 AND AMM 78-31-19-402-008-H00, REV 147.
- [SDR IPXA2026042619249](https://openairdocs.org/sdr/IPXA2026042619249.md): Door · chafed · Apr 22, 2026 · N320UP · Boeing 76734AF · Engine Thrust Reverser
  > CHAFED DOOR, NR 1 ENG RT T/R LWR BLOW OUT DOOR L/E AREA. INSTALL WITH DOOR ASSY I.A.W SRM 51-40-02-0G REV.95 AND BOEING AIPC 78-31-51-03 REV. 141 AND ST ENGINEERING IPC 78-32-22 REV.96 AND AMM TASK 78-31-19-402-008-H00 REV: 147
- [SDR IPXA2026042619321](https://openairdocs.org/sdr/IPXA2026042619321.md): Adapter · chafed · Apr 22, 2026 · N320UP · Boeing 76734AF · Nacelle/Pylon Miscellaneous Structure
  > CHAFED BRACKET, NR 1 ENG RT CORE COWL HOLD OPEN ROD SUPPORT BRACKET. INSTALL NEW BRACKET I.A.W SRM 51-40-02-0G REV.95 AND GOODRICH AEROSTRUCTURES CMM IPL 71-13-24 REV. 50
- [SDR IPXA2026042619349](https://openairdocs.org/sdr/IPXA2026042619349.md): Bracket · chafed · Apr 22, 2026 · N320UP · Boeing 76734AF · Nacelle/Pylon Miscellaneous Structure
  > CHAFED BRACKET, NR 1 ENG LT CORE COWL HOLD OPEN ROD SUPPORT BRACKET. INSTALL NEW BRACKET I.A.W SRM 51-40-02-0G REV.95 AND GOODRICH AEROSTRUCTURES CMM IPL 71-13-23 REV. 47
- [SDR IPXA2026042821802](https://openairdocs.org/sdr/IPXA2026042821802.md): Scuff Plate · dented · Apr 22, 2026 · N320UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > DENTED SCUFF PLATE, LOWER SIDE OF BULK CARGO DOOR CUTOUT. IAW AMM 53-13-02-404-007, REV 147, TO INSTALL BULK CARGO DOOR SCUFF PLATE CENTER.
- [SDR IPXA2026042618157](https://openairdocs.org/sdr/IPXA2026042618157.md): Seal · broken · Apr 22, 2026 · N320UP · Boeing 76734AF · Engine Thrust Reverser
  > BROKEN SEAL, NR 1 ENG LT TRANSLATING COWL AFT LWR FAIRING INNER AREA. INSTALLED A NEW SEAL IAW SRM 51-40-02-0G, REV 95, AND IPC 78-32-31, REV 96.
- [SDR IPXA2026042619433](https://openairdocs.org/sdr/IPXA2026042619433.md): Bracket · chafed · Apr 22, 2026 · N320UP · Boeing 76734AF · Engine Thrust Reverser
  > CHAFED BRACKET, NR 2 ENG, RT T/R CLOSURE DOOR T/E AREA. INSTALLED NEW BRACKET I.A.W SRM 51-40-02-0G REV.95 AND IPC 78-32-22 REV.96
- [SDR IPXA2026042619452](https://openairdocs.org/sdr/IPXA2026042619452.md): Bracket · chafed · Apr 22, 2026 · N320UP · Boeing 76734AF · Engine Thrust Reverser
  > CHAFED BRACKET, NR 1 ENG LT T/R LWR CLOSURE DOOR T/E AREA. INSTALL NEW BRACKET IAW SRM 51-40-02-0G REV.95 AND IPC 78-32-21 REV.96
- [SDR IPXA2026042621792](https://openairdocs.org/sdr/IPXA2026042621792.md): Seal · frayed · Apr 22, 2026 · N320UP · Boeing 76734AF · Engine Thrust Reverser
  > FRAYED SEAL, NR 1 ENG LT TRANSLATING COWL AFT LWR FAIRING INNER AREA. REMOVED DAMAGE SEAL IAW SRM 51-40-02-0G, REV 95,
- [SDR IPXA2026042621981](https://openairdocs.org/sdr/IPXA2026042621981.md): Longeron · chafed · Apr 22, 2026 · N320UP · Boeing 76734AF · Nacelle/Pylon, Longeron/Stringer
  > CHAFED LONGERON, NR 1 ENG RT CORE COWL AFT LWR INNER CHORD EDGE AREA. INSTALLED A NEW LONGERON IAW SRM 51-40-02-0G REV.95 AND CMM IPL 71-13-24, REV 50.
- [SDR IPXA2026042320504](https://openairdocs.org/sdr/IPXA2026042320504.md): Slat Track · damaged · Apr 22, 2026 · N320UP · Boeing 76734AF · Leading Edge Devices
  > FOUND RT WING NO.12 SLAT OTBD SIDE MAIN TRACK SKEW DETECTION BRACKET BROKEN.
- [SDR IPXA2026042219905](https://openairdocs.org/sdr/IPXA2026042219905.md): Clamp · broken · Apr 22, 2026 · N320UP · Boeing 76734AF · Passenger/Crew Doors
  > BROKEN CLAMP, CREW ENTRY DOOR UPPER CUTOUT AREA.
- [SDR IPXA2026050202306](https://openairdocs.org/sdr/IPXA2026050202306.md): Splice Plate · deformed · Apr 21, 2026 · N320UP · Boeing 76734AF · Wing Main, Frame Structure
  > LEFT WING AT LEADING EDGE SPAR AREA LWR PANEL ATTACH STRUCTURE AT NR 1 SLAT INBD DRIVE MOTOR LINK IS DEFORMED. REPAIR DAMAGE AREA IAW SRM 57-41-01-2R-4, REPAIR 4, REV 95, AND WORK SHEET 60290.
- [SDR IPXA2026050202373](https://openairdocs.org/sdr/IPXA2026050202373.md): Splice Plate · deformed · Apr 21, 2026 · N320UP · Boeing 76734AF · Wing Main, Frame Structure
  > LEFT WING AT LEADING EDGE SPAR AREA LWR PANEL ATTACH STRUCTURE AT NR 2 SLAT OUTBD DRIVE MOTOR LINK IS DEFORMED. REPAIR DAMAGE AREA IAW SRM 57-41-01-2R-4, REPAIR 4, REV.95 AND WORK SHEET 60291.
- [SDR IPXA2026050202651](https://openairdocs.org/sdr/IPXA2026050202651.md): Frame · chafed · Apr 21, 2026 · N320UP · Boeing 76734AF · Nacelle/Pylon, Frame/Spar/Rib
  > NR 1 PYLON AFT LEFT SIDE FRAME WAS CHAFED. REPAIR DAMAGE AREA IAW EO-97331-REQ1 REV 1 AND EI F2026A54M-937 REV. 0.
- [SDR IPXA2026043002803](https://openairdocs.org/sdr/IPXA2026043002803.md): Angle · bent · Apr 21, 2026 · N320UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > FAULT - BENT ANGLE IN LOWER FORWARD CARGO COMPARTMENT CEILING AT STA 478-500, RBL 80 (NO.6623) (AGING AIRRCAFT INSPECTION) INSTALL NEW CLIP-ANGLE I.A.W SRM 51-40-02-0G REV.95 AND BOEING DWG NO. 143T8550 SH 4 REV: -
- [SDR IPXA2026043002883](https://openairdocs.org/sdr/IPXA2026043002883.md): Depressor · bent · Apr 21, 2026 · N320UP · Boeing 76734AF · Fuselage Main, Structure
  > FAULT - AFT LOWER CARGO DOOR SEAL DEPRESSOR BENT AT LOWER AFT CORNER (NO.6625) (AGING AIRCRAFT INSPECTION) INSTALL NEW DEPRESSOR SEAL I.A.W SRM 51-40-02-0G REV.95 AND BOEING DWG NO. 146T8575 SH 1 REV: A, SH 2 REV: A
- [SDR IPXA2026043003364](https://openairdocs.org/sdr/IPXA2026043003364.md): Depressor · gouged · Apr 21, 2026 · N320UP · Boeing 76734AF · Fuselage Main, Structure
  > GOUGED DEPRESSOR SEAL AT MAIN DECK CGO DOOR CUTOUT AREA FWD SIDE STA 492 2EA (REPLACE) INSTALLED MAIN DECK CARGO DOOR DEPRESSOR SEAL AT FWD SIDE I.A.W AMM 20-10-00-910-802 REV.147.<
- [SDR IPXA2026042700943](https://openairdocs.org/sdr/IPXA2026042700943.md): Fairing · cracked · Apr 21, 2026 · N320UP · Boeing 76734AF · Trailing Edge Flaps
  > CRACKED FAIRING, INBD SIDE FWD EDGE OF LT WING NR 3 FLAP TRACK AFT FAIRING. IAW AMM 51-21-10-307-020, REV 147, REPAINTED AREA. I.A.W AMM 27-51-15-424-029 REV 147 INSTALL NO.3 FLAP AFT FAIRING. CONDITION CHECK NORMAL.
- [SDR IPXA2026042601924](https://openairdocs.org/sdr/IPXA2026042601924.md): Angle · cracked · Apr 21, 2026 · N320UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > CRACKED ANGLE AT BULK CARGO, BS 1578, LBL 78, INBD. INSTALL NEW ANGLE I.A.W SRM 51-40-02-0G REV.95 AND BOEING DWG NO. 146T5650 SH 5 REV: C
- [SDR IPXA2026042601951](https://openairdocs.org/sdr/IPXA2026042601951.md): Angle · cracked · Apr 21, 2026 · N320UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > CRACKED ANGLE, BULK CARGO BS 1578, LBL 78 OTBD. REMOVED THE DAMAGED ANGLE IAW SRM 51-40-02-0G, REV 95. INSTALLED A NEW ANGLE IAW SRM 51-40-02-0G, REV 95, AND DWG 146T5650, SHT 5, REV C.
- [SDR IPXA2026042803406](https://openairdocs.org/sdr/IPXA2026042803406.md): Seal · broken · Apr 21, 2026 · N320UP · Boeing 76734AF · Nacelle/Pylon Miscellaneous Structure
  > BROKEN SEAL, NR 2 PYLON RT FAIRING PANEL 446CR. INSTALLED A NEW SEAL STRIP IAW SRM 51-40-02-0G, REV 95, & DWG 311T2570, SHT 14, REV -.
- [SDR IPXA2026042803562](https://openairdocs.org/sdr/IPXA2026042803562.md): Angle · cracked · Apr 21, 2026 · N320UP · Boeing 76734AF · Nacelle/Pylon Miscellaneous Structure
  > CRACKED ANGLE, NR 1 PYLON AFT FAIRING AFT BULKHEAD INNER INBD. INSTALLED A NEW ANGLE IAW SRM 51-40-02-0G, REV 95, AND DWG 313T3380, SHT 3, REV F.
- [SDR IPXA2026042803602](https://openairdocs.org/sdr/IPXA2026042803602.md): Angle · cracked · Apr 21, 2026 · N320UP · Boeing 76734AF · Nacelle/Pylon Miscellaneous Structure
  > CRACKED ANGLE, NR 2 PYLON AFT LWR FAIRING AFT FRAME OUTBD SIDE SUPPORT ANGLE. INSTALLED A NEW ANGLE IAW SRM 51-40-02-0G, REV 95, AND DWG 313T3380, SHT 3, REV F.
- [SDR IPXA2026042803621](https://openairdocs.org/sdr/IPXA2026042803621.md): Seal · broken · Apr 21, 2026 · N320UP · Boeing 76734AF · Nacelle/Pylon Miscellaneous Structure
  > BROKEN SEAL, NR 2 PYLON LT FAIRING PANEL 446CL AREA. INSTALLED A NEW SEAL STRIP IAW SRM 51-40-02-0G, REV 95, & DWG 311T2570, SHT 14, REV -.
- [SDR IPXA2026042604547](https://openairdocs.org/sdr/IPXA2026042604547.md): Angle · cracked · Apr 21, 2026 · N320UP · Boeing 76734AF · Wing Miscellaneous Structure
  > CRACKED ANGLE, LT WING L/E REFUELINGS STATION LOWER DOOR CUTOUT INBD STOP SPRING, ACCESS PANEL NR 521QB. INSTALLED A NEW ANGLE IAW SRM 51-40-02-0G, REV 95, & DWG 114T2450, SHT 1, REV J.
- [SDR IPXA2026042703429](https://openairdocs.org/sdr/IPXA2026042703429.md): Fireshield · chafed · Apr 21, 2026 · N320UP · Boeing 76734AF · Nacelle/Pylon, Main Frame
  > CHAFED FIRESHIELD, NR 1 PYLON FAIRING PANEL 436BL INNER PLATE. INSTALLED A NEW FIRESHIELD IAW SRM 51-40-02-0G, REV 95, AND DWG 311T2570, SH 14, REV -.
- [SDR IPXA2026042703484](https://openairdocs.org/sdr/IPXA2026042703484.md): Fireshield · chafed · Apr 21, 2026 · N320UP · Boeing 76734AF · Nacelle/Pylon, Main Frame
  > CHAFED FIRESHIELD, NR 2 PYLON LT FAIRING PANEL 446BL. INSTALLED A NEW FIRESHIELD IAW SRM 51-40-02-0G, REV 95, AND DWG 311T2570, SH 14, REV -.
- [SDR IPXA2026042703493](https://openairdocs.org/sdr/IPXA2026042703493.md): Angle · cracked · Apr 21, 2026 · N320UP · Boeing 76734AF · Nacelle/Pylon Miscellaneous Structure
  > CRACK, NR 1 PYLON AFT FAIRING AFT BULKHEAD INNER OUTBD ANGLE CRACKED. INSTALLED A NEW CLIP IAW SRM 51-40-02-0G, REV 95, AND DWG 313T3380, SH 3, REV F.
- [SDR IPXA2026042604137](https://openairdocs.org/sdr/IPXA2026042604137.md): Bracket · cracked · Apr 21, 2026 · N320UP · Boeing 76734AF · Nacelle/Pylon Miscellaneous Structure
  > CRACKED BRACKET, NR 2 PYLON AFT LWR FAIRING INBD SIDE DRAIN TUBE SUPPORT BRACKET. INSTALL NEW BRACKET IAW SRM 51-40-02-0G, REV 95, AND DWG 272T0333, SH 8, REV A.
- [SDR IPXA2026042604261](https://openairdocs.org/sdr/IPXA2026042604261.md): Guard · chafed · Apr 21, 2026 · N320UP · Boeing 76734AF · Passenger/Crew Doors
  > CHAFED QUARD, MEC DOOR CUTOUT RT AREA. INSTALLED A NEW GUARD IAW SRM 51-40-02-0G, REV 95, AND DWG 141T6300, SH 1, REV J.
- [SDR IPXA2026050282674](https://openairdocs.org/sdr/IPXA2026050282674.md): Skin Panel · corroded · Apr 20, 2026 · N320UP · Boeing 76734AF · Fuselage Main, Plate/Skin
  > MAJOR REPAIR, CORROSION-FUSELAGE SKIN IMMEDIATELY SURROUNDING THE DRAIN VALVE AT STA 1410 BETWEEN S-38R AND S-39R. (REPAIR) INSTALLED BULK CARGO FLOOR PANEL IAW AMM 53-01-05-404-004 REV.1472. CONDITION CHECK NORMAL.
- [SDR IPXA2026042185805](https://openairdocs.org/sdr/IPXA2026042185805.md): Skin · debonded · Apr 20, 2026 · N320UP · Boeing 76734AF · Trailing Edge Flaps
  > DEBONDED SKIN, INBD EDGE LOWER FACE OF LT WING T/E, OTBD FLAP LOWER SKIN, WBL 355. IAW CMM 57-53-51, REV 38, AND AMM 20-11-00-910-802 REV 147 INSTALLED THE OTBD FLAP INBD UPPER AND LOWER SIDE SEAL WITH RETAINER.
- [SDR IPXA2026042974070](https://openairdocs.org/sdr/IPXA2026042974070.md): Pca · leaking · Apr 19, 2026 · N320UP · Boeing 76734AF · Rudder Tab Control System
  > FAULT- FOUND THE LOWER RUDDER PCA LEAK. (REPLACE) AMM 27-21-02-422-038 REV 147 STEP 5A TO 5H INSTALL LOWER RUDDER PCA
- [SDR IPXA2026042673479](https://openairdocs.org/sdr/IPXA2026042673479.md): Support Bracket · cracked · Apr 19, 2026 · N320UP · Boeing 76734AF · Wing Miscellaneous Structure
  > FAULT- CRACK- TORQUE TUBE SUPPORT BRACKET, RH WING INBD LE COMPARTMENT. INSTALL NEW BRACKET IAW SRM 51-40-02-0G, REV 95, AND DWG 114T1240, SH 4, REV D.
- [SDR IPXA2026050262860](https://openairdocs.org/sdr/IPXA2026050262860.md): Hinge Fitting · cracked · Apr 18, 2026 · N320UP · Boeing 76734AF · Spoilers
  > CRACKED FITTING, RT WING NR 10 SPOILER SUPPORT FITTING WS 638. REPLACED IAW AMM 27-61-01-424-019, REV 147, STEP 3A, TO 3H (11) INSTALLED NR 10 SPOILER.
- [SDR IPXA2026043063775](https://openairdocs.org/sdr/IPXA2026043063775.md): Skin · cracked · Apr 18, 2026 · N320UP · Boeing 76734AF · Wing, Plate/Skin
  > DURING PERFORM J/C: MXP-57-117-00-1-JIC, FOUND LEFT WING LOWER SKIN NEAR RIB 32, WSTA 1018.2 SKIN CRACKED. ACCOMPLISHED JOB I.A.W UPS EO-97334-REQ1 REV1 2.
- [SDR IPXA2026042160589](https://openairdocs.org/sdr/IPXA2026042160589.md): Roller · worn · Apr 18, 2026 · N320UP · Boeing 76734AF · Cargo Compartments
  > FAULT - FOUND MAIN DECK CARGO HANDLING SHAFT OF ROLLER RAIL ASSY WORN TOTAL: 2EA AT STA 456 ~ STA 500 LBL 77.50, LBL 55.50. I.A.W AMM 25-57-05-004-001 AND AMM 25-57-05-404-006 REV.147 REPLACED ROLLER RAIL ASSY.

Next page: https://openairdocs.org/aircraft/N320UP/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 = 'N320UP' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N320UP/reports

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