# Service difficulty reports: N313UP

A list on [N313UP](https://openairdocs.org/aircraft/N313UP.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 · 177 reports

- [SDR IPXA2026041371289](https://openairdocs.org/sdr/IPXA2026041371289.md): Fitting · none · Apr 13, 2026 · N313UP · Boeing 76734AF · Wing Main, Frame Structure
  > NR 2 WING STRUT SUPPORT CLEVIS FITTING FREEZE PLUG - PERMANENT REPAIR. CONDITION CHECK NORMAL. PAPER FINAL CHECK OK.
- [SDR IPXA2026041575356](https://openairdocs.org/sdr/IPXA2026041575356.md): Bushing · migrated · Apr 7, 2026 · N313UP · Boeing 76734AF · Wing Main, Frame Structure
  > MIGRATED BUSHING, RT WING T/E NR 8 SPOILER MID LWR. IAW CMM:57-70-11, REV 42, REPAIR 2-1, PAGE 601 - 602 STEP 3, COMPLETED THE REPLACEMENT OF BUSHING.
- [SDR IPXA2026041070344](https://openairdocs.org/sdr/IPXA2026041070344.md): Seal · cracked · Apr 7, 2026 · N313UP · Boeing 76734AF · Nacelle/Pylon, Main Frame
  > NR 1 ENG FAIRING PANEL 436CR SPRING SEAL CRACKED. INSTALL NEW STRIP SEAL I.A.W SRM 51-40-02-0G REV.94 AND BOEING DWG NO:311T2570 SH 1 REV.N
- [SDR IPXA2026041669415](https://openairdocs.org/sdr/IPXA2026041669415.md): Depressor · deformed · Apr 7, 2026 · N313UP · Boeing 76734AF · Cargo/Baggage Doors
  > DEFORMED DEPRESSOR SILL, FORWARD CARGO DOOR CUTOUT AREA AFTER SIDE. INSTALL NEW DEPRESSOR SEAL I.A.W SRM 51-40-02-0G REV.94 AND BOEING DWG NO:143T8540 SH1 REV.B AND BOEING DWG NO:143T8540 SH2 REV.B.
- [SDR IPXA2026041172897](https://openairdocs.org/sdr/IPXA2026041172897.md): Skin · bulged · Apr 7, 2026 · N313UP · Boeing 76734AF · Trailing Edge Flaps
  > SKIN, R/H WING T/E OUTBD FLAP INBD LWR. PERFORMED NDT/UT FOR THE REWORKED AREA & PLUS 2" HEATED AREA IAW NDT MANUAL PART 1 51-01-01 REV 143.
- [SDR IPXA2026040958846](https://openairdocs.org/sdr/IPXA2026040958846.md): Seal · broken · Apr 6, 2026 · N313UP · Boeing 76734AF · Nacelle/Pylon, Main Frame
  > NO.2 PYLON, RT FAIRING PANEL 446CR SEAL BROKEN INSTALLED NEW SEAL I.A.W SRM 51-40-02-0G REV. 94 AND BOEING DWG NO. 311T2570 SH. 1 REV. N.
- [SDR IPXA2026041159269](https://openairdocs.org/sdr/IPXA2026041159269.md): Hinge · worn · Apr 6, 2026 · N313UP · Boeing 76734AF · Nacelle/Pylon, Main Frame
  > NR 2 PYLON L/H PRSOV ACCESS DWR. INSTALLED NEW HINGE I.A.W SRM 51-40-02-0G REV. 94, BOEING DWG NO. 311T1064 SH. 1 REV. G AND BOEING DWG NO. 311T1064 SH. 2 REV. E.
- [SDR IPXA2026041658143](https://openairdocs.org/sdr/IPXA2026041658143.md): Floorbeam · cracked · Apr 6, 2026 · N313UP · Boeing 76734AF · Fuselage Main, Floor Beam
  > CRACK, ANGLE FLOORBEAM BS 246, RBL 38. ACCOMPLISHED REPAIR I.A.W UPS EO-97146-REQ1 REV1.
- [SDR IPXA2026041458575](https://openairdocs.org/sdr/IPXA2026041458575.md): Strut · cracked · Apr 6, 2026 · N313UP · Boeing 76734AF · Wing Main, Frame Structure
  > CRACKED STRUT, RT WING L/E PANEL NR 621SB, OTBD, OSS 694. Â INSTALLED NEW STRUT I.A.W SRM 51-40-02-0G REV. 94 AND BOEING DWG NO. 114T2214 SH 1 REV. B, 112T2000 SH 13 REV. B.
- [SDR IPXA2026041259154](https://openairdocs.org/sdr/IPXA2026041259154.md): Bracket · chafed · Apr 6, 2026 · N313UP · Boeing 76734AF · Nacelle/Pylon, Main Frame
  > CHAFED BRACKET, NR 1 ENG LT CORE COWL HOLD OPEN ROD SUPPORT BRACKET. INSTALLED NEW BRACKET IAW SRM 51-40-02-0G, REV 94, AND CMM IPL 71-13-23, REV 47.
- [SDR IPXA2026041259005](https://openairdocs.org/sdr/IPXA2026041259005.md): Bracket · chafed · Apr 6, 2026 · N313UP · Boeing 76734AF · Nacelle/Pylon, Main Frame
  > CHAFED BRACKET, NR 1 ENGINE RT CORE COWL HOLD OPEN ROD SUPPORT BRACKET. INSTALLED NEW BRACKET IAW SRM 51-40-02-0G, REV 94, AND CMM IPL 71-13-24, REV 50.
- [SDR IPXA2026041159001](https://openairdocs.org/sdr/IPXA2026041159001.md): Stiffener · cracked · Apr 6, 2026 · N313UP · Boeing 76734AF · Engine Thrust Reverser
  > CRACKED STIFFENER, NR 1 ENG RT THRUST REVERSER FWD TORQUE BOX SUPPORT STIFFENER NEAR 2:00 POS. INSTALL A NEW STIFFENER IAW SRM 51-40-02-0G, REV 94, AND AIPC 78-31-00-60, REV 141.
- [SDR IPXA2026041158718](https://openairdocs.org/sdr/IPXA2026041158718.md): Stiffener · cracked · Apr 6, 2026 · N313UP · Boeing 76734AF · Engine Thrust Reverser
  > CRACKED STIFFENER, NR 1 ENG RT THRUST REVERSER. FWD TORQUE BOX SUPPORT STIFFENER NEAR 1:00 POS. INSTALLED A NEW STIFFENER IAW SRM 51-40-02-0G, REV 94 & AIPC 78-31-00-60, REV 141.
- [SDR IPXA2026041058741](https://openairdocs.org/sdr/IPXA2026041058741.md): Channel · cracked · Apr 6, 2026 · N313UP · Boeing 76734AF · Nacelle/Pylon Miscellaneous Structure
  > CRACKED CHANNEL, NR 2 ENG AFT FAIRING PANEL 447DB INNER AREA. INSTALLED A NEW CHANNEL IAW SRM 51-40-02-0G REV.94, & DWG 313T3360, SH 42, REV E.
- [SDR IPXA2026041059158](https://openairdocs.org/sdr/IPXA2026041059158.md): Floor Panel · delaminated · Apr 6, 2026 · N313UP · Boeing 76734AF · Fuselage Floor Panel
  > FLOOR PANEL IN THE AFT CARGO COMPARTMENT IS DELAMINATED. REPAIRED IAW SRM 53-00-50-2R-0, REV 94. CHECKED SATISFACTORY.
- [SDR IPXA2026041346666](https://openairdocs.org/sdr/IPXA2026041346666.md): Rub Strip · cracked · Apr 5, 2026 · N313UP · Boeing 76734AF · Nacelle/Pylon Miscellaneous Structure
  > NR 2 ENG LT CORE COWL INNER T/E UPPER RUB STRIP. INSTALLED NEW STRIP IAW SRM 51-40-02-0G REV. 94 AND CMM IPL 71-13-23 REV. 47.
- [SDR IPXA2026041447390](https://openairdocs.org/sdr/IPXA2026041447390.md): Structure · cracked · Apr 5, 2026 · N313UP · Boeing 76734AF · Wing Main, Frame Structure
  > CRACKED CHORD, RT WING L/E PNL 621HB MID AREA OSS 531. INSTALLED NEW CHORD I.A.W SRM 51-40-02-0G REV. 94 AND BOEING DWG NO: 114T2206 SH 1REV. B.
- [SDR IPXA2026041047733](https://openairdocs.org/sdr/IPXA2026041047733.md): Floor Panel · delaminated · Apr 5, 2026 · N313UP · Boeing 76734AF · Fuselage Floor Panel
  > THE FLOOR PANEL IN THE AFT CARGO COMPARTMENT IS DELAMINATED. REPAIRED IAW SRM 53-00-50-2R-0, REV 94.
- [SDR IPXA2026041047753](https://openairdocs.org/sdr/IPXA2026041047753.md): Floor Panel · delaminated · Apr 5, 2026 · N313UP · Boeing 76734AF · Fuselage Floor Panel
  > THE FLOOR PANEL IN THE AFT CARGO COMPARTMENT IS DELAMINATED. REPAIRED IAW SRM 53-00-50-2R-0 REV. 94.
- [SDR IPXA2026041047769](https://openairdocs.org/sdr/IPXA2026041047769.md): Floor Panel · delaminated · Apr 5, 2026 · N313UP · Boeing 76734AF · Fuselage Floor Panel
  > THE FLOOR PANEL IN THE AFT CARGO COMPARTMENT IS DELAMINATED. IAW SRM 53-00-50-2R-0, REV 94, PERFORMED A BOND THE REPAIR OF PLIES WITH RESIN CURED AT 170°F FOR 2 HRS WITH A MINIMUM VACUUM OF 20 IN/HG.
- [SDR IPXA2026041047239](https://openairdocs.org/sdr/IPXA2026041047239.md): Floor Panel · delaminated · Apr 5, 2026 · N313UP · Boeing 76734AF · Fuselage Floor Panel
  > THE FLOOR PANEL IN THE AFT CARGO COMPARTMENT IS DELAMINATED. REPAIRED IAW SRM 53-00-50-2R-0, REV 94.
- [SDR IPXA2026040746687](https://openairdocs.org/sdr/IPXA2026040746687.md): Bracket · cracked · Apr 5, 2026 · N313UP · Boeing 76734AF · Wing, Attach Fittings
  > L/H WING INBD L/E CAVITY TORQUE TUBE SUPPORT BRACKET CRACKED. INSTALLED NEW BRACKET IAW SRM 51-40-02-0G, REV 94, AND DWG 114T1240, SHT 2, REV E.
- [SDR IPXA2026040746494](https://openairdocs.org/sdr/IPXA2026040746494.md): Angle · cracked · Apr 5, 2026 · N313UP · Boeing 76734AF · Nacelle/Pylon Miscellaneous Structure
  > CRACKED CLIP, NR 2 PYLON AFT LWR FAIRING INNER NUT FRAME OUTBD SIDE SUPPORT CLIP. INSTALLED NEW CLIP IAW SRM 51-40-02-0G, REV 94 AND DWG 313T3380, SHT 3, REV F.
- [SDR IPXA2026040746727](https://openairdocs.org/sdr/IPXA2026040746727.md): Clamp · cracked · Apr 5, 2026 · N313UP · Boeing 76734AF · Nacelle/Pylon Miscellaneous Structure
  > CRACKED CLAMP, NR 2 ENG AFT FAIRING DOOR SUPPORT ROD STOW AREA. INSTALLED NEW CLAMP IAW SRM 51-40-02-0G REV. 94 AND DWG 313T3349, SH. 2 REV. B.
- [SDR IPXA2026041535922](https://openairdocs.org/sdr/IPXA2026041535922.md): Tee Fitting · cracked · Apr 4, 2026 · N313UP · Boeing 76734AF · Nacelle/Pylon, Main Frame
  > CRACKED TEE FITTING, NR 1 PYLON AFT FAIRING INNER OUTBD LWR TEE CRACK. INSTALLED NEW TEE IAW SRM 51-40-02-0G, REV 94, AND DWG 313T2380, SHT 7, REV H, AND EO NO:EO-97048-REQ1, REV.1 & SB 767-54-0109, REV 1.
- [SDR IPXA2026041536044](https://openairdocs.org/sdr/IPXA2026041536044.md): Seal · cracked · Apr 4, 2026 · N313UP · Boeing 76734AF · Nacelle/Pylon Miscellaneous Structure
  > CRACKED ZEE, NR 2 PYLON RT FAIRING DOOR AFT LWR CUTOUT AREA. INSTALLED NEW ZEE IAW SRM 51-40-02-0G, REV.94, AND DWG 313T2380, SHT 10, REV K AND DWG 313T2380, SHT 9, REV G AND SB 767-54-0109 REV.1
- [SDR IPXA2026041635932](https://openairdocs.org/sdr/IPXA2026041635932.md): Rub Strip · broken · Apr 4, 2026 · N313UP · Boeing 76734AF · Nacelle/Pylon Miscellaneous Structure
  > BROKEN STRIP, NR 1 ENG NOSE COWL T/E RT UPPER WEAR STRIP. INSTALLED NEW STRIP I.A.W SRM 51-40-02-0G REV. 94 AND GOODRICH CMM IPL 71-11-16 REV. 54. AND AMM INTRODUCTION SIP REV.147.
- [SDR IPXA2026041637268](https://openairdocs.org/sdr/IPXA2026041637268.md): Floorbeam · corroded · Apr 4, 2026 · N313UP · Boeing 76734AF · Fuselage Main, Floor Beam
  > CORROSION DAMAGE ON UPPER CHORD OF FLOOR BEAM AT STA 246 NEAR RBL 30 (EVALUATE) REVIEWED PER GMM-MTX 09.05.01.09. ACCOMPLISHED REPAIR I.A.W EO-97113-REQ1 REV1 AND EGAT EI F2026A53M-685 REV.2. MAJOR REPAIR
- [SDR IPXA2026041435847](https://openairdocs.org/sdr/IPXA2026041435847.md): Plate · cracked · Apr 4, 2026 · N313UP · Boeing 76734AF · Fuselage Main, Structure
  > THE FORWARD CARGO SIDE GUIDE RAIL TIE PLATE AT LT BS 566 IS CRACKED. REPLACED. INSTALLED FABRICATE TIE PLATE IAW SRM 51-40-02-0G, REV 94, AND DWG 452T2003, SHT 24, REV D.
- [SDR IPXA2026041235947](https://openairdocs.org/sdr/IPXA2026041235947.md): Bracket · cracked · Apr 4, 2026 · N313UP · Boeing 76734AF · Nacelle/Pylon Miscellaneous Structure
  > CRACKED, NR 2 PYLON AFT LWR FAIRING INNER DRAIN TUBE SUPPORT BRACKET. INSTALLED A NEW BRACKET IAW SRM 51-40-02-0G, REV 94, & DWG 272T0333, SHT 8, REV -.
- [SDR IPXA2026041035897](https://openairdocs.org/sdr/IPXA2026041035897.md): Channel · cracked · Apr 4, 2026 · N313UP · Boeing 76734AF · Nacelle/Pylon Miscellaneous Structure
  > CRACKED, NR 1 PYLON AFT FAIRING PNL NR 437DB INNER CHANNEL AREA. INSTALLED A NEW CHANNEL IAW SRM 51-40-02-0G, REV 94, AND DWG 313T3360, SHT 42, REV E.
- [SDR IPXA2026041035962](https://openairdocs.org/sdr/IPXA2026041035962.md): Bulkhead · cracked · Apr 4, 2026 · N313UP · Boeing 76734AF · Nacelle/Pylon, Bulkhead/Firewall
  > CRACKED BULKHEAD, NR 1 PYLON AFT FAIRING PANEL NR.437DB INNER NEW AREA. INSTALL NEW BULKHEAD IAW SRM 51-40-02-0G, REV 94, AND DWG 313T3360, SHT 42, REV E.
- [SDR IPXA2026041518128](https://openairdocs.org/sdr/IPXA2026041518128.md): Winglet · damaged · Apr 3, 2026 · N313UP · Boeing 76734AF · Wing Main, Frame Structure
  > R/H WING OUTBD AREA WINGLET. (REPAIR) REPAIR LIGHTNING STRIKE DAMAGE ON FASTENER HOLE OF RH WINGLET LOWER SKIN I.A.W. UPS EO-97110-REQ1 REV.1 AND EGAT EI NO. F2026A57M-668 REV.0
- [SDR IPXA2026041517950](https://openairdocs.org/sdr/IPXA2026041517950.md): Handle · worn · Apr 3, 2026 · N313UP · Boeing 76734AF · Passenger/Crew Doors
  > THE PAWL BEHIND THE CREW ENTRY DOOR EXTERNAL HANDLE IS WORN. (REPLACE) REPLACED THE PAWL I.A.W AMM 52-11-26-004-001 REV.148 AND AMM 52-11-26-404-003 REV.148,
- [SDR IPXA2026041317026](https://openairdocs.org/sdr/IPXA2026041317026.md): Floorbeam · corroded · Apr 3, 2026 · N313UP · Boeing 76734AF · Fuselage Main, Floor Beam
  > FOUND MAIN DECK FLOOR BEAM FITTING CORROSION. INSTALLED FABRICATED FILLER IAW SRM 51-40-02-0G, REV 94, AND DWG 146T5650, SHEET 5, REV C.
- [SDR IPXA2026040317950](https://openairdocs.org/sdr/IPXA2026040317950.md): Pawl · worn · Apr 3, 2026 · N313UP · Boeing 76734AF · Passenger/Crew Doors
  > THE PAWL BEHIND THE CREW ENTRY DOOR EXTERNAL HANDLE IS WORN. (REPLACE)
- [SDR IPXA2026041091568](https://openairdocs.org/sdr/IPXA2026041091568.md): Seat Track · worn · Apr 2, 2026 · N313UP · Boeing 76734AF · Fuselage, Seat/Cargo Attach Fittings
  > FOUND SEAT TRACK ASSY INBOARD FWD OF CAPTAIN SEAT WORN. REPLACED THE SEAT TRACK ASSY IAW AMM 25-11-01-822-095-001, REV 147.
- [SDR IPXA2026030586411](https://openairdocs.org/sdr/IPXA2026030586411.md): Sensor · false indication · Jan 27, 2026 · N313UP · Boeing 76734AF · Door Warning System
  > L1 DOOR EICAS MESSAGE CLIMBING THROUGH 5000 FT. PRESSURIZATION REMAINED NORMAL. REPLACED DOOR CLOSED SENSOR IAW AMM 52-71-01-964-211. DMP REVERSED. DEFERRAL CLEARED. GOOD TO CLOSE
- [SDR IPXA2026012786411](https://openairdocs.org/sdr/IPXA2026012786411.md): Warning Message · illuminated · Jan 27, 2026 · N313UP · Boeing 76734AF · Passenger/Crew Doors
  > LEFT FWD ENTRY DOOR EICAS MSG CLIMBING THROUGH 5000 FT. PRESSURIZATION REMAINED NORMAL. DEFERRED PER MEL 52-71-1-1A
- [SDR IPXA2025092645526](https://openairdocs.org/sdr/IPXA2025092645526.md): Latch · faulted · Sep 25, 2025 · N313UP · Boeing 76734AF · Passenger/Crew Doors
  > COVER FOR YELLOW ENTRY DOOR LATCH PROTRUDES OUT AND WILL NOT CLOSE. DEFERRED MAIN ENTRY/SERVICE DOOR ARMING LEVER HINGED COVERS IAW MEL 52-11-2.
- [SDR IPXA2024070994662](https://openairdocs.org/sdr/IPXA2024070994662.md): Handle · detached · Jun 30, 2024 · N313UP · Boeing 76734AF · Passenger/Crew Doors
  > CREW DOOR HANDLE FELL OFF. R&R DOOR HANDLE ESCUTCHEON DOOR ACCESS AND FWD ENTRY DOOR HINGE ASSY REF AMM 52-12-02/401. THIS CLEARS MEL 52-11-2. PLACARDS REMOVED. OKAY FOR SERVICE.
- [SDR IPXA2024063094662](https://openairdocs.org/sdr/IPXA2024063094662.md): Handle · detached · Jun 30, 2024 · N313UP · Boeing 76734AF · Passenger/Crew Doors
  > CREW DOOR HANDLE FELL OFF. DEFERRING PER MEL 52-11-2 PLACARD INSTALLED. OPEN
- [SDR IPXA2024032147565](https://openairdocs.org/sdr/IPXA2024032147565.md): Skin · corroded · Mar 19, 2024 · N313UP · Boeing 76734AF · Fuselage Main, Plate/Skin
  > FAULT - CORROSION ON FUSELAGE SKIN BETWEEN STA 1395-STA 1417, S-38R-S-39R. (REPAIR). PERFORMED FPI INSPECTION AT TRIM AREA PER SOPM 20-20-02 TO CONFIRM CORROSION FREE CONDITION,RESULT:NO CORROSION WAS FOUND REVIEW COMPLETE
- [SDR IPXA2024030138141](https://openairdocs.org/sdr/IPXA2024030138141.md): Floor Panel · broken · Mar 1, 2024 · N313UP · Boeing 76734AF · Fuselage Floor Panel
  > *MAJOR REPAIR* FAULT - FOUND MAIN DECK CARGO FLOOR PANEL BROKEN, PANEL NO.231AFF P/N: 143T5876-78 (REPLACE) FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.2. CONDITION CHECK IS SATISFACTORY. REVIEWED
- [SDR IPXA2024030138116](https://openairdocs.org/sdr/IPXA2024030138116.md): Floor Panel · broken · Mar 1, 2024 · N313UP · Boeing 76734AF · Fuselage Floor Panel
  > *MAJOR REPAIR* FAULT - FOUND MAIN DECK CARGO FLOOR PANEL BROKEN, PANEL NO.231FFF, P/N: 143T5876-85 (REPLACE) FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.2. CONDITION CHECK IS SATISFACTORY.
- [SDR IPXA2024031397889](https://openairdocs.org/sdr/IPXA2024031397889.md): Strap · cracked · Feb 28, 2024 · N313UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > FOUND CRACK AT STA 1725.5 STR-7R BULKHEAD OUTER CHORD STRAP. ACCOMPLISHED REPAIR I.A.W EO-24301-REQ002 REV.5 AND EO-24301-JIC003 REV.3 AND EO-89771-REQ1 REV.1 AND EGAT EI NO.F2024A53M-612 REV.1 AND EGAT WORK SHEET NO.40222
- [SDR IPXA2024031197280](https://openairdocs.org/sdr/IPXA2024031197280.md): Access Panel · cracked · Feb 28, 2024 · N313UP · Boeing 76734AF · Wing, Plate/Skin
  > FOUND RH WING LOWER OUTBOARD MAIN FUEL PUMP ACCESS CRACK (REPLACE) 1.I.A.W AMM 20-11-00-910-802 REV.141 REPLACED THE ACCESS PANEL. COND CHECK NORMAL. ATTACHMENT ARE UPLOADED
- [SDR IPXA2024030700729](https://openairdocs.org/sdr/IPXA2024030700729.md): Angle · leaking · Feb 28, 2024 · N313UP · Boeing 76734AF · Fuselage Structure (General)
  > ANGLE CRACKED BULK CARGO COMPARTMENT RIGHT AREA STA 1578 LBL 60 (REPLACE) ACCOMPLISHED MAIN DECK CARGO ACCESS DADO PANEL AND FLOOR PANEL OK TO INSTALL CHECK,AND ACCESS FLOOR PANEL SEALANT REMOVE CHECK NORMAL.
- [SDR IPXA2024030700671](https://openairdocs.org/sdr/IPXA2024030700671.md): Angle · cracked · Feb 28, 2024 · N313UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > CRACKED ANGLE STA 246, LBL 49. FABRICATE P/N(141T5146-16) PER BOEING DWG NO.:141T5146 SH 15 REV."B";PL REV."F";PSDL REV."-" AND ORIGINAL PART AS A SAMPLE I.A.W. GMM-MTX CH 9.08 REV 6B REQUIREMENT INSTALLED FABRICATED PARTS I.A.W SRM 51-40-02-0G REV.88 AND BO
- [SDR IPXA2024030500756](https://openairdocs.org/sdr/IPXA2024030500756.md): Angle · cracked · Feb 28, 2024 · N313UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > CRACKED ANGLE BULK CARGO COMPARTMENT RIGHT AREA STA 1578 RBL 60 (REPAIR) 1. REMOVED DAMAGE PARTS I.A.W SRM 51-40-02-0G REV.88 2. INSTALLED NEW PARTS I.A.W SRM 51-40-02-0G REV.88 AND BOEING DWG NO: 146T5650 SH 5 REV.C. I.A.W AMM 25-57-05-404-006 AND AMM 25-58-

Next page: https://openairdocs.org/aircraft/N313UP/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 = 'N313UP' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N313UP/reports

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