# Service difficulty reports: N340UP

A list on [N340UP](https://openairdocs.org/aircraft/N340UP.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 2 · 61 reports

- [SDR IPXA2026090361862](https://openairdocs.org/sdr/IPXA2026090361862.md): Lamp · inoperative · Sep 3, 2026 · N340UP · Boeing 76734AF · Emergency Lighting
  > L1271 EMERGENCY CEILING LT INOPERATIVE. REPLACED THE LAMP AND LIGHT TEST OK, IAW AMM 33-51-11/201.
- [SDR IPXA2026040275634](https://openairdocs.org/sdr/IPXA2026040275634.md): Jumper · damaged · Apr 1, 2026 · N340UP · Boeing 76734AF · Cargo/Baggage Doors
  > FOUND FORWARD CARGO DOOR JUMPER DAMAGED AT FWD & AFT SIDE (REPLACE)..I.A.W AMM 52-33-01-004-060 REV.147 AND AMM 52-33-01-404-061 REV.147 REPLACED FWD CARGO DOOR JUMPER AT FWD AND AFT SIDE, AND DO BONDING TEST THE RESULT WAS STATISFIED.
- [SDR IPXA2026032822628](https://openairdocs.org/sdr/IPXA2026032822628.md): Filler · broken · Mar 23, 2026 · N340UP · Boeing 76734AF · Horizontal Stabilizer Miscellaneous Structure
  > BROKEN FILLER, RT HORIZONTAL STAB TIP AFT OTBD CORNER. INSTALLED A NEW FILLER IAW SRM 51-40-02-0G, REV 94, AND DWG 189T0001, SHT 1, REV E.
- [SDR IPXA2026032822558](https://openairdocs.org/sdr/IPXA2026032822558.md): Filler · damaged · Mar 23, 2026 · N340UP · Boeing 76734AF · Horizontal Stabilizer Miscellaneous Structure
  > LIGHTNING STRIKE, FILLER, LT HORIZONTAL STAB TIP AFT OTBD CORNER. INSTALLED A NEW FILLER IAW SRM 51-40-02-0G, REV 94, AND DWG 189T0001, SHT 1, REV E.
- [SDR IPXA2026032609725](https://openairdocs.org/sdr/IPXA2026032609725.md): Bushing · missing · Mar 22, 2026 · N340UP · Boeing 76734AF · Nacelle/Pylon, Main Frame
  > FAULT- MISSING- BUSHING, NO.1 ENG L/H FAN COWL NO.2 LATCH AREA. (REPLACE). INSTALL NEW RECEIVER I.A.W SRM 51-40-02-0G REV.94 AND GOODRICH AEROSTRUCTURES CMM IPL 71-13-21 REV. 47. REVIEW COMPLETE
- [SDR IPXA2026040110702](https://openairdocs.org/sdr/IPXA2026040110702.md): Fitting · cracked · Mar 22, 2026 · N340UP · Boeing 76734AF · Fuselage Main, Structure
  > FOUND THE MAIN DECK CARGO RESTRAINT FLOOR ADAPTER FITTING WITH CRACK DAMAGE AT BS 632, BL 0, FLOOR PANEL. JOB COMPLETED AND CONDITION CHECK NORMAL. REPLACED FLOOR ADAPTER FITTING I.A.W AMM 20-11-00-910-802 REV.147 AND TORQUE BOLT TO 85 IN-LB.
- [SDR IPXA2026032712143](https://openairdocs.org/sdr/IPXA2026032712143.md): Blowout Door · chafed · Mar 22, 2026 · N340UP · Boeing 76734AF · Engine Thrust Reverser
  > CHAFED SKIN, NR 1 ENGINE, RT THRUST REVERSER BLOWOUT DOOR INNER L/E AREA. INSTALLED A NEW BLOWOUT DOOR IAW SRM 51-40-02-0G, REV 94, AIPC 78-31-51-03, REV 141, & IPC 78-32-22, REV 94.
- [SDR IPXA2026033112189](https://openairdocs.org/sdr/IPXA2026033112189.md): Angle · cracked · Mar 22, 2026 · N340UP · Boeing 76734AF · Wing Miscellaneous Structure
  > CRACKED ANGLE, LT WING LE REFUELING STATION LOWER DOOR CUTOUT INBD STOP SPRING, ACCESS PANEL 521QB. INSTALLED A NEW ANGLE IAW SRM 51-40-02-0G, REV 94, & DWG 114T2450, SH 10, REV A.
- [SDR IPXA2026033112225](https://openairdocs.org/sdr/IPXA2026033112225.md): Clamp · broken · Mar 22, 2026 · N340UP · Boeing 76734AF · Nacelle/Pylon, Main Frame
  > BROKEN CLAMP, NR 1 PYLON AFT FAIRING INNER HOLD OPEN ROD SUPPORT BRACKET AREA. INSTALLED NEW BRACKET I.A.W SRM 51-40-02-0G REV. 95. AND BOEING DWG NO.313T3349 SH.2 REV.B. AND DWG NO.313T3349 SH.3 REV.A.
- [SDR IPXA2026032810500](https://openairdocs.org/sdr/IPXA2026032810500.md): Bracket · chafed · Mar 22, 2026 · N340UP · Boeing 76734AF · Nacelle/Pylon, Main Frame
  > CHAFED BRACKET, NR 1 ENGINE LT CORE COWL INNER HOLD OPEN ROD SUPPORT BRACKET. INSTALLED A NEW BRACKET IAW SRM 51-40-02-0G, REV 94, AND CMM IPL 71-13-23, REV 47.
- [SDR IPXA2026032612126](https://openairdocs.org/sdr/IPXA2026032612126.md): Blowout Door · chafed · Mar 22, 2026 · N340UP · Boeing 76734AF · Engine Thrust Reverser
  > CHAFED SKIN, NR 2 ENGINE, RT THRUST REVERSER LWR BLOWOUT DOOR, L/E AREA. INSTALLED A NEW BLOWOUT DOOR ASSY IAW SRM 51-40-02-0G, REV 94, AND AIPC 78-31-51-03, REV 141.
- [SDR IPXA2026032711985](https://openairdocs.org/sdr/IPXA2026032711985.md): Bracket · chafed · Mar 22, 2026 · N340UP · Boeing 76734AF · Engine Thrust Reverser
  > CHAFED BRACKET, NR 2 ENG LT THRUST REVERSER LOWER CLOSURE DOOR T/E AREA. INSTALLED A NEW BRACKET IAW SRM 51-40-02-0G, REV 94, AND IPC 78-32-21, REV.94.
- [SDR IPXA2026032612437](https://openairdocs.org/sdr/IPXA2026032612437.md): Housing · stuck · Mar 22, 2026 · N340UP · Boeing 76734AF · Fuselage Main, Structure
  > STUCK - HOUSING ASSY, FWD CARGO DOOR CUTOUT AFT SIDE (REPLACE). I.A.W AMM 20-11-00-910-802 REV.147 REPLACE FWD CARGO DOOR HOUSING ASSY AT AFT SIDE CUTOUT AREA. IAW AMM 52-33-00-825-013,REV.147, CHECK THE FWD CARGO DOOR FLUSHNESS.
- [SDR IPXA2026032610644](https://openairdocs.org/sdr/IPXA2026032610644.md): Bracket · chafed · Mar 22, 2026 · N340UP · Boeing 76734AF · Nacelle/Pylon, Main Frame
  > CHAFED BRACKET, NR 2 ENGINE, LT CORE COWL HOLD OPEN ROD SUPPORT BRACKET. INSTALLED A NEW ADAPTER IAW SRM 51-40-02-0G, REV 94, & CMM IPL 71-13-23, REV 47.
- [SDR IPXA2026032610631](https://openairdocs.org/sdr/IPXA2026032610631.md): Bracket · chafed · Mar 22, 2026 · N340UP · Boeing 76734AF · Engine Thrust Reverser
  > CHAFED BRACKET, NR 1 ENG, LT THRUST REVERSER FWD LWR CLOSURE DOOR T/E AREA. NSTALLED A NEW BRACKET IAW SRM 51-40-02-0G, REV 94, & IPC 78-32-21 REV 94.
- [SDR IPXA2026032610990](https://openairdocs.org/sdr/IPXA2026032610990.md): Clamp · damaged · Mar 22, 2026 · N340UP · Boeing 76734AF · Nacelle/Pylon, Main Frame
  > DAMAGED CLAMP, NR.2 PYLON AFT FAIRING DOOR SUPPORT ROD. INSTALLED A NEW CLAMP IAW SRM 51-40-02-0G, REV 94, AND DWG 313T2303, SH 135, REV -.
- [SDR IPXA2026032612020](https://openairdocs.org/sdr/IPXA2026032612020.md): Bracket · chafed · Mar 22, 2026 · N340UP · Boeing 76734AF · Engine Thrust Reverser
  > CHAFED BRACKET, NR 2 ENG, RT THRUST REVERSER LOWER CLOSURE DOOR T/E AREA. INSTALLED A NEW BRACKET IAW SRM 51-40-02-0G, REV 94, AND IPC 78-32-22 REV 94.
- [SDR IPXA2026032611804](https://openairdocs.org/sdr/IPXA2026032611804.md): Plate · cracked · Mar 22, 2026 · N340UP · Boeing 76734AF · Nacelle/Pylon, Main Frame
  > CRACKED PLATE, NR 1 ENG LT CORE COWL INNER AFT LWR SIDE. INSTALLED A NEW PLATE IAW SRM 51-40-02-0G, REV 94, AND CMM IPL 71-13-23, REV 47.
- [SDR IPXA2026032612053](https://openairdocs.org/sdr/IPXA2026032612053.md): Bracket · chafed · Mar 22, 2026 · N340UP · Boeing 76734AF · Engine Thrust Reverser
  > CHAFED BRACKET, NR 1 ENG, RT THRUST REVERSER FWD LOWER CLOSURE DOOR T/E AREA. INSTALLED A NEW BRACKET IAW SRM 51-40-02-0G, REV 94, & IPC 78-32-22 REV.94.
- [SDR IPXA2026032612072](https://openairdocs.org/sdr/IPXA2026032612072.md): Bracket · cracked · Mar 22, 2026 · N340UP · Boeing 76734AF · Wing Miscellaneous Structure
  > CRACKED BRACKET, LT WING INBD L/E NR 6 SLAT DRIVE TORQUE TUBE SUPPORT, LES 285. INSTALL NEW BRACKET I.A.W SRM 51-40-02-0G REV.95 AND BOEING DWG NO: 114T1240 SH 6 REV: -.
- [SDR IPXA2026032612305](https://openairdocs.org/sdr/IPXA2026032612305.md): Angle · cracked · Mar 22, 2026 · N340UP · Boeing 76734AF · Nacelle/Pylon Miscellaneous Structure
  > CRACKED ANGLE, NR 1 PYLON AFT FAIRING INNER AFT BULKHEAD INBD SIDE SUPPORT ANGLE. INSTALLED A NEW ANGLE IAW SRM 51-40-02-0G, REV 94, DWG 313T2303, SHEET 131, REV-, & DWG 313T2303, SHEET 136, REV-.
- [SDR IPXA2026040197859](https://openairdocs.org/sdr/IPXA2026040197859.md): Duct · chafed · Mar 21, 2026 · N340UP · Boeing 76734AF · Nacelle/Pylon, Main Frame
  > CHAFED DUCT, NR 2 ENG R/H CORE COWL PRECOOLER OULET DUCT (REPLACE). INSTALL PRECOOLER DUCT FOR ACCESS I.A.W SRM 51-40-02-0G REV.94 AND GOODRICH AEROSTRUCTURES CMM IPL 71-13-24 REV. 50. C/W REVIEW
- [SDR IPXA2026033100868](https://openairdocs.org/sdr/IPXA2026033100868.md): Skin Panel · corroded · Mar 21, 2026 · N340UP · Boeing 76734AF · Fuselage Main, Plate/Skin
  > LOWER FUSELAGE EXTERNAL SURFACE SKIN CORRODED NEAR DRAIN HOLE AREA AT BS 1395 - 1417, S38R - 39R. ACCOMPLISHED THE REPAIR I.A.W EGAT EI NO. F2026A53M-588 SEQUENCE AÂ Â STEP
- [SDR IPXA2026032072891](https://openairdocs.org/sdr/IPXA2026032072891.md): Skin · dented · Mar 20, 2026 · N340UP · Boeing 76734AF · Trailing Edge Flaps
  > DENT - SKIN, LOWER FACE OF L/H WING T/E OUTBD FLAP INNER SKIN, NEAR OTEF STA 137 (REPAIR). REPAIR DENT ON LOWER SURFACE OF LWR PANEL ON LH WING OUTBD T/E FLAP NEAR OTEF STA 137 I.A.W. EGAT EI NO. F2026A57M-589 TRV.1 AND UPS EO-96990-REQ1 REV.1. C/W REVIEW
- [SDR IPXA2026040178486](https://openairdocs.org/sdr/IPXA2026040178486.md): Fitting · cracked · Mar 20, 2026 · N340UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > FOUND THE MAIN DECK CARGO RESTRAINT FLOOR ADAPTER FITTING WITH CRACK DAMAGE AT STA 1241 LBL 47.5, FLOOR PANEL NO. 251NFF (REPLACE). REPLACE FLOOR ADAPTER FITTING I.A.W AMM 20-11-00-910-802 REV.147 AND TORQUE BOLT TO 85 IN-LB.
- [SDR IPXA2026040178532](https://openairdocs.org/sdr/IPXA2026040178532.md): Fitting · cracked · Mar 20, 2026 · N340UP · Boeing 76734AF · Fuselage Main, Structure
  > FOUND THE MAIN DECK CARGO RESTRAINT FLOOR ADAPTER FITTING WITH CRACK DAMAGE AT BS 1373, RBL 47.5, FLOOR PANEL 252QFF. INSTALLED FLOOR PANEL 252QFF IAW AMM 53-01-06-400-801, REV.147. REPLACED FLOOR ADAPTER FITTING I.A.W AMM 20-11-00-910-802 REV.147 AND TOR
- [SDR IPXA2026033175660](https://openairdocs.org/sdr/IPXA2026033175660.md): Plate · chafed · Mar 20, 2026 · N340UP · Boeing 76734AF · Wing, Plate/Skin
  > CHAFED PLATE, FWD EDGE LOWER FACE OF LT WING INBD L/E LOWER PLATE, ISS 250.625 - ISS 256.145. INSTALLED NEW SKIN PLATE IAW SRM 51-40-02-0G, REV 94, DWG 114T1000,SH 4, REV -, DWG 114T1225, SH 6, REV -, SH 7, REV -, DWG 114T1220, SH 6, REV -, SH 7, REV -, & D
- [SDR IPXA2026040178536](https://openairdocs.org/sdr/IPXA2026040178536.md): Fitting · cracked · Mar 20, 2026 · N340UP · Boeing 76734AF · Fuselage Main, Structure
  > FOUND THE MAIN DECK CARGO RESTRAINT FLOOR ADAPTER FITTING WITH CRACK DAMAGE AT BS 676, RBL 47.5, FLOOR PANEL 232LFF. INSTALLED FLOOR PANEL 232LFF IAW AMM 53-01-06-400-801, REV 147. REPLACE FLOOR ADAPTER FITTING I.A.W AMM 20-11-00-910-802 REV.147 AND TORQUE
- [SDR IPXA2026040178528](https://openairdocs.org/sdr/IPXA2026040178528.md): Fitting · cracked · Mar 20, 2026 · N340UP · Boeing 76734AF · Fuselage Main, Structure
  > FOUND THE MAIN DECK CARGO RESTRAINT FLOOR ADAPTER FITTING WITH CRACK DAMAGE AT BS 654+44 BL 0, FLOOR PANEL 231LFF. REPLACE FLOOR ADAPTER FITTING I.A.W AMM 20-11-00-910-802 REV.147 AND TORQUE BOLT TO 85 IN-LB.
- [SDR IPXA2026040178544](https://openairdocs.org/sdr/IPXA2026040178544.md): Fitting · cracked · Mar 20, 2026 · N340UP · Boeing 76734AF · Fuselage Main, Structure
  > FOUND THE MAIN DECK CARGO RESTRAINT FLOOR ADAPTER FITTING WITH CRACK DAMAGE AT STA 1241 BL 0, FLOOR PANEL NO. 251LFF (REPLACE). REPLACE FLOOR ADAPTER FITTING IAW AMM 20-11-00-910-802 REV.147 AND TORQUE BOLT TO 85 IN-LB.
- [SDR IPXA2026032278838](https://openairdocs.org/sdr/IPXA2026032278838.md): Floor Panel · cracked · Mar 20, 2026 · N340UP · Boeing 76734AF · Fuselage Floor Panel
  > CRACKS ON THE FLOOR PANEL NO. 252UFF, AT BS 1400 - 1520, RBL 55 - 77 IN THE MAIN DECK CARGO COMPARTMENT. INSTALL THE REPLACEMENT FLOOR PANEL IAW AMM 53-01-06. COMPLETED UPS SREO-9693-REQ001 REV.4.
- [SDR IPXA2026033156373](https://openairdocs.org/sdr/IPXA2026033156373.md): Retainer · damaged · Mar 19, 2026 · N340UP · Boeing 76734AF · Wing Main, Frame Structure
  > FOUND NUTPLATE DAMAGED 1EA, PNL NO.611JB. FABRICATE RETAINER IAW DWG 114T1400, SH 3, REV F, PL REV BW, PSDL REV F AS A SAMPLE IAW GMM-MTX CH 9.08 REV 14.1 REQUIREMENT. INSTALL THE NUTPLATE TO RETAINER IAW SRM 51-40-02-0G, REV 94, & DWG 114T1400, SH 3, REV
- [SDR IPXA2026033032521](https://openairdocs.org/sdr/IPXA2026033032521.md): Actuator · faulted · Mar 18, 2026 · N340UP · Boeing 76734AF · Cargo/Baggage Doors
  > FOUND ROTARY ACTUATOR NOISE AT FWD CARGO DOOR. IAW AMM 52-33-04-004-027 REV.147 AND AMM 52-33-04-404-028 REV.147 REPLACED FWD CARGO DOOR ROTARY ACTUATOR.
- [SDR IPXA2026033132792](https://openairdocs.org/sdr/IPXA2026033132792.md): Support Angle · gouged · Jan 29, 2026 · N340UP · Boeing 76734AF · Cargo/Baggage Doors
  > UNLOAD CREW REPORTED DAMAGE TO LOWER FWD CARGO DOOR FRAME UPPER AFT CORNER. REMOVED DAMAGE SUPPORT ANGLE I.A.W SRM 51-40-02-0G REV.94. INSTALL NEW SUPPORT ANGLEI.A.W SRM 51-40-02-0G REV.94 AND BOEING DWG NO. 143T8514 SH 5 REV: A, SH 7 REV: B.
- [SDR IPXA2024032590713](https://openairdocs.org/sdr/IPXA2024032590713.md): Cylinder · corroded · Mar 15, 2024 · N340UP · Boeing 76734AF · Main Landing Gear
  > *SDR FILED OPEN* FAULT - FOUND LEFT MAIN GEAR GLAND NUT AND OUTER CYLINDER THREAD CORROSION. (EVALUATE) ACCOMPLISHED EO 89873 REQUEST DMI TO REPLACE LMLG WITHIN 30 DAYS PER EO 89873
- [SDR IPXA2024032683572](https://openairdocs.org/sdr/IPXA2024032683572.md): None · none · Mar 10, 2024 · N340UP · Boeing 76734AF · Standard Practices/Structures
  > FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R) CONDITION CHECK OK.
- [SDR IPXA2024031083572](https://openairdocs.org/sdr/IPXA2024031083572.md): None · none · Mar 10, 2024 · N340UP · Boeing 76734AF · Standard Practices/Structures
  > OPEN, FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R) COMPLETED SDR.
- [SDR IPXA2024032673650](https://openairdocs.org/sdr/IPXA2024032673650.md): Seal · worn · Mar 9, 2024 · N340UP · Boeing 76734AF · Passenger/Crew Doors
  > FOUND ENTRY DOOR AFT SIDE DOORWAY SEAL WORN (REPLACE) REVIEW COMPLETE
- [SDR IPXA2024031173650](https://openairdocs.org/sdr/IPXA2024031173650.md): Seal · worn · Mar 9, 2024 · N340UP · Boeing 76734AF · Passenger/Crew Doors
  > OPEN, FOUND ENTRY DOOR AFT SIDE DOORWAY SEAL WORN (REPLACE) OK TO WORK
- [SDR IPXA2024030479506](https://openairdocs.org/sdr/IPXA2024030479506.md): Battery · failed · Mar 4, 2024 · N340UP · Boeing 76734AF · Emergency Lighting
  > EMER LIGHT SYS TEST FAILED. REMOVED AND REPLACED EMER BATT PER AMM 33-51-07/401. OPS CHECK GOOD.
- [SDR IPXA2022042281381](https://openairdocs.org/sdr/IPXA2022042281381.md): Stiffener · cracked · Apr 17, 2022 · N340UP · Boeing 76734AF · Wing Main, Frame Structure
  > INSPECTION TYPE:C6CRACK ON CENTER WING TANK STIFFENER (P/N: 111T2008-12) ON STA 785.9, RBL 33REPAIR IA.W 767-300F SRM 57-10-10-2R-2 REPAIR 2 REV.83.00, UPS EO B767-5740-58151-C AND UPS EO B767-5720-76672-A
- [SDR IPXA2022042281380](https://openairdocs.org/sdr/IPXA2022042281380.md): Stiffener · cracked · Apr 17, 2022 · N340UP · Boeing 76734AF · Wing Main, Frame Structure
  > INSPECTION TYPE:C6CRACK ON CENTER WING TANK STIFFENER (P/N: 111T2011-6) ON STA 785.9, RBL 55REPAIR I.A.W 767-300F SRM 57-10-10-2R-2 REPAIR 2 REV.83.00, UPS EO B767-5740-58151-C AND UPS EO B767-5720-76672-A
- [SDR IPXA2019071044303](https://openairdocs.org/sdr/IPXA2019071044303.md): Fuel Cap · missing · Jul 10, 2019 · N340UP · Boeing 76734AF · Aircraft Fuel Distribution System
  > INSPECTION TYPE:INSP DUE TO WAN 2937896 AND DMI M676316 FUELING RECEPTACLE CAP. FUEL CAP ASSY INSTALLED IAW AMM 28-21-01-401 REV 127.04. THIS CLOSES DMI M676316. PLACARD REMOVED.
- [SDR IPXA2019040440760](https://openairdocs.org/sdr/IPXA2019040440760.md): Structure · punctured · Apr 3, 2019 · N340UP · Boeing 76734AF · Nacelle/Pylon, Main Frame
  > R. ENGINE COWL EXTERIOR HAS LG PUNCTURE HOLE WITH FIBERGLASS PROTRUDING FROM ENTRY HOLE. NOTICED ON PREFLIGHT WALK AROUND DAMAGE IS PROB. 4-6 INCHES LONG. 3 INCHES IN DIAMETER. ACCOMPLISHED INTERIM INSPECTION & REPAIR IAW EO. B767-7110-72129-A. DEFERRED PER
- [SDR IPXA2018110523567](https://openairdocs.org/sdr/IPXA2018110523567.md): Arming Lever · damaged · Nov 1, 2018 · N340UP · Boeing 76734AF · Emergency Equipment
  > DOOR ARMING LEVER HINGED DOOR MECHANISM WAS DAMAGED. R & R THE FWD ENTRY DOOR HINGE ASSY IAW AMM 52-12-02, PB 401, REV 124.05. OPS NORMAL.
- [SDR IPXA2018091734075](https://openairdocs.org/sdr/IPXA2018091734075.md): Cover · unsecure · Sep 14, 2018 · N340UP · Boeing 76734AF · Passenger/Crew Doors
  > CREW ENTRY DOOR ARMING COVER WILL NOT STOW. REMOVED COVER. REMOVED AND REPLACED FORWARD L1 DOOR HINGE AND HANDLE. OPS NORMAL IAW MM 52-12-02. OK FOR SERVICE.
- [SDR IPXA2017112623900](https://openairdocs.org/sdr/IPXA2017112623900.md): Floor Panel · punctured · Nov 26, 2017 · N340UP · Boeing 76734AF · Fuselage Floor Panel
  > MCD FLOOR PANEL AT POS 10, WL 200, BL 0 FWD, CTR HAS TWO HOLES IN PANEL. FABRICATED A NEW FLOOR PANEL IAW EO B767-5320-9693-I
- [SDR IPXA2017030114550](https://openairdocs.org/sdr/IPXA2017030114550.md): Skin · damaged · Feb 28, 2017 · N340UP · Boeing 76734AF · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN DAMAGED AT BS 132.5 BETWEEN STRINGERS 24 - 30R. DAMAGE MEASURES 12 INCHES CIRCUMFERENTIAL BY 2.25 INCHES FORE & AFT AND 1.5 INCHES OUTWARD DEFLECCTION, DAMAGE IS APPOX 6 INCHES FROM LOWER EDGE OF SKIN AND AT L/E. REPAIRED IAW EO B767-5330-63407
- [SDR IPXA2017022214316](https://openairdocs.org/sdr/IPXA2017022214316.md): Lamp · inoperative · Feb 19, 2017 · N340UP · Boeing 76734AF · Emergency Lighting
  > EXTERIOR EMERGENCY LIGHT FAILED ON TEST. REMOVED AND REPLACED THE LAMP, AND TESTED IAW AMM 33-51-16-201, REV 120.02. TESTED OK.
- [SDR IPXA2017013013469](https://openairdocs.org/sdr/IPXA2017013013469.md): Seal · leaking · Jan 29, 2017 · N340UP · Boeing 76734AF · Passenger/Crew Doors
  > L1 DOOR SEAL DEVELOPED A LEAK STARTING AT FL 200. LEAK CONTINUED ENTIRE FLIGHT. FOUND LOWER DOOR SEAL PULLED OUT OF RETAINER. REINSTALLED L1 DOOR SEAL IAW MM 52-09-01.

Next page: https://openairdocs.org/aircraft/N340UP/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 = 'N340UP' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N340UP/reports

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