# Service difficulty reports: N339UP

A list on [N339UP](https://openairdocs.org/aircraft/N339UP.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 · 56 reports

- [SDR IPXA2026020384940](https://openairdocs.org/sdr/IPXA2026020384940.md): Floor Panel · corroded · Jan 20, 2026 · N339UP · Boeing 76734AF · Fuselage Floor Panel
  > FOUND MAIN DECK FLOOR PANEL CORRODED, BS 1601, RBL 33. INSTALLED FLOOR PANEL IAW AMM 20-11-00-910-802, REV 147.
- [SDR IPXA2026020385077](https://openairdocs.org/sdr/IPXA2026020385077.md): Cargo Track · corroded · Jan 20, 2026 · N339UP · Boeing 76734AF · Fuselage, Seat/Cargo Attach Fittings
  > FOUND MAIN DECK CARGO TRACK CORRODED, BS 1601, RBL 11 IN THE AFT BULK CARGO BAY.. INSTALLED FABRICATED CARGO TRACK IAW SRM 51-40-02-0G.
- [SDR IPXA2025080729838](https://openairdocs.org/sdr/IPXA2025080729838.md): Fce · faulted · Aug 6, 2025 · N339UP · Boeing 76734AF · Leading Edge Slat Position Indicating System
  > AIR TURN BACK, LE SLAT DISAGREE. PERFORMED FSEU BITE PER FIM 27-51 FT 809. FOUND EXISTING FAULT MSG: LVR RVDT 2 MISRIG WITH FAULT CODE 27-51023. ALSO PREVIOUS LEG FAULT 0. FOUND MSG: LE SLATS SEE FIM WITH FAULT CODE: 27-81045. PERFORMED POSITION RVDT #2 (M
- [SDR IPXA2024121958268](https://openairdocs.org/sdr/IPXA2024121958268.md): A/C Pack · odor · Dec 12, 2024 · N339UP · Boeing 76734AF · Cabin Cooling System
  > LEFT PACK IS DISCHARGING FOULSMELL. DEBRIEFED INBOUND CREW, REPORTING FOUL SMELL NOT BEING PRESENT ON GROUND OR FLIGHT. NO OIL/GLYCOL CONTAMINATION FOUND, REACTIVATED LH PACK. RAN LH PACK SEPARATELY SEVERAL TIMES WITH APU AIR, NO FOUL SMELL NOTICEABLE. ALSO OP
- [SDR IPXA2024072611426](https://openairdocs.org/sdr/IPXA2024072611426.md): Warning Message · false activation · Jul 26, 2024 · N339UP · Boeing 76734AF · Trailing Edge Flap Control System
  > **EMERGENCY DECLARED**ON FINAL APPROACH, WHEN ON G/S, SELECTED FLAPS 20 DG, TE FLAP DISAGREE EICAS MESSAGE SPEED 180KTS, ALT 3500-. PERFORMED GA, RAN THE QRH PROCEDURE. USED ALT TE SWITCH AND LANDED FLAPS 20. C/W FIM 27-51 809, BITE CHECK FSCU, NO FAULTS NOTED
- [SDR IPXA2024013128494](https://openairdocs.org/sdr/IPXA2024013128494.md): Skin · debonded · Jan 19, 2024 · N339UP · Boeing 76734AF · Leading Edge Devices
  > FAULT - DISBOND SKIN, LH WING LE NO.4 SLAT INBD TE CORNER. (REPAIR) C/W REVIEW. ADJUSTMENT AND OPERATIONAL TEST OF THE LH WING NO.4 SLAT. I.A.W AMM 27-88-01-722-028 REV.141 STEP G(16) TO STEP H COMPLETED LE SLAT SYSTEM OPERATIONAL TEST, RESULT WAS SATISFIED.
- [SDR IPXA2024013128280](https://openairdocs.org/sdr/IPXA2024013128280.md): Rib · cracked · Jan 19, 2024 · N339UP · Boeing 76734AF · Nacelle/Pylon, Frame/Spar/Rib
  > FAULT - CRACK - RIB, NO.1 PYLON INSIDE OF MID TORQUE BOX SUPPORT, CAN ACCESS FROM PANEL #436AL (REPLACE) C/W REVIEW REMOVED DAMAGE PART I.A.W SRM 51-40-02-0G REV.88.INSTALLED NEW PART I.A.W SRM 51-40-02-0G REV.88
- [SDR IPXA2024013128251](https://openairdocs.org/sdr/IPXA2024013128251.md): Access Panel · cracked · Jan 19, 2024 · N339UP · Boeing 76734AF · Nacelle/Pylon, Main Frame
  > FAULT - CRACK - RIB, NO.1 PYLON INSIDE OF MID TORQUE BOX SUPPORT, CAN ACCESS FROM PANEL #436AR (REPLACE) REVIEWED REMOVED DAMAGE PARTS I.A.W SRM 51-40-02-0G REV.88.INSTALLED NEW PARTS I.A.W SRM 51-40-02-0G REV.88
- [SDR IPXA2024013128068](https://openairdocs.org/sdr/IPXA2024013128068.md): Panel · cracked · Jan 19, 2024 · N339UP · Boeing 76734AF · Leading Edge Devices
  > FAULT - CRACK PNL, LH WING NO.4 SLAT LOWER CLOSEOUT PNL UNDER OUTBD AUX TRACK. (REPAIR) REVIEWED REMOVED CLOSURE PANEL AT NO.4 SLAT I.A.W SRM 51-40-02-0G REV.88
- [SDR IPXA2024012228068](https://openairdocs.org/sdr/IPXA2024012228068.md): Panel · damaged · Jan 19, 2024 · N339UP · Boeing 76734AF · Wing Main, Frame Structure
  > *SDR FILED OPEN* FAULT - CRACK PNL, LH WING NO.4 SLAT LOWER CLOSEOUT PNL UNDER OUTBD AUX TRACK. (REPAIR) PER B767 NDT MANUAL PART 1, 51-01-01 & PART 4, 51-00-02, REV.136 TO PERFORM NDT/UT FOR THE POST REPAIRED AREA INCLUDED THE AREA WAS HOT PLUS WITHIN 6" ALL
- [SDR IPXA2024012228251](https://openairdocs.org/sdr/IPXA2024012228251.md): Support · cracked · Jan 19, 2024 · N339UP · Boeing 76734AF · Nacelle/Pylon Miscellaneous Structure
  > *SDR FILED OPEN* FAULT - CRACK - RIB, NO.1 PYLON INSIDE OF MID TORQUE BOX SUPPORT, CAN ACCESS FROM PANEL #436AR (REPLACE) OK TO WORK
- [SDR IPXA2024012228494](https://openairdocs.org/sdr/IPXA2024012228494.md): Skin · debonded · Jan 19, 2024 · N339UP · Boeing 76734AF · Wing, Plate/Skin
  > *SDR FILED OPEN* *MAJOR REPAIR* FAULT - DISBOND SKIN, LH WING LE NO.4 SLAT INBD TE CORNER. (REPAIR) 1.OK TO INSTALL CHECK SATISFIED.<BR>2.I.A.W. AMM 27-81-02-424-099 REV.141 STEP 1.A TO 1.H(15) INSTALL NO.4 SLAT OF THE LH WING LEADING EDGE.
- [SDR IPXA2024012228280](https://openairdocs.org/sdr/IPXA2024012228280.md): Support · cracked · Jan 19, 2024 · N339UP · Boeing 76734AF · Nacelle/Pylon Miscellaneous Structure
  > *SDR FILED OPEN* FAULT - CRACK - RIB, NO.1 PYLON INSIDE OF MID TORQUE BOX SUPPORT, CAN ACCESS FROM PANEL #436AL (REPLACE) OK TO WORK
- [SDR IPXA2024012227720](https://openairdocs.org/sdr/IPXA2024012227720.md): Cap · cracked · Jan 19, 2024 · N339UP · Boeing 76734AF · Trailing Edge Flaps
  > FAULT - CRACK, LH WING OUTBD FLAP END CAP. (REPAIR). PERFORMED NDT/UT FOR REWORKED AREA PLUS 6'' AROUND HEATED AREA I.A.W. 767 NTM PART1 51-01-01 REV:136. RESULT:NO DEFECT FOUND. 1.REMOVE THE DAMAGE MATERIALS (L:0.3", W:0.05", AT LEFT HAND OUTBOARD FLAP INBOAR
- [SDR IPXA2024012227663](https://openairdocs.org/sdr/IPXA2024012227663.md): Skin · damaged · Jan 19, 2024 · N339UP · Boeing 76734AF · Trailing Edge Flaps
  > FAULT - CHIP SKIN, LH WING INBD MAIN FLAP OUTBD UPR SEAL LE AREA. (REPAIR). 1. REMOVE THE UNWANTED MATERIALS AND CLEAN AT LEFT HAND WING INBOARD MAIN FLAP OUTBOARD UPPER SEAL LEADING EDGE AREA. AND TRIM OUT THE DAMAGE AS REQUIRED, KEEP A MINIMUM 0.5 IN CORNER
- [SDR IPXA2024013145304](https://openairdocs.org/sdr/IPXA2024013145304.md): Liner · missing · Jan 16, 2024 · N339UP · Boeing 76734AF · Passenger/Crew Doors
  > **SUPPLEMENTAL SDR**FAULT - FOUND ENTRY DOOR FORWARD DOORWAY LINING TRIM MISSING (REPLACE) C/W REVIEW INSTALLED NEW DOOR LINING I.A.W AMM 52-12-02-004-001
- [SDR IPXA2024011745304](https://openairdocs.org/sdr/IPXA2024011745304.md): Liner · unknown · Jan 16, 2024 · N339UP · Boeing 76734AF · Passenger/Crew Doors
  > FOUND ENTRY DOOR FORWARD DOORWAY LINING TRIM MISSING (REPLACE) OK TO WORK
- [SDR IPXA2024011636099](https://openairdocs.org/sdr/IPXA2024011636099.md): Stiffener · cracked · Jan 15, 2024 · N339UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > FAULT - CRACK WING CENTER TANK FRONT SPAR STIFFENER AT STA 785.9 RBL 11 (REPAIR) THIS REPAIR IS CLASSIFIED AS MAJOR. ACCOMPLISH THE REPAIR PER SRM 57-10-10-2R-2 AND SUBTASK T3F18E003SH3X. MARK THE FAULT WITH FLIGHT SAFETY IMPACT. ACCOMPLISHED REPAIR I.A.W SRM
- [SDR IPXA2023071059404](https://openairdocs.org/sdr/IPXA2023071059404.md): Escape Rope · loose · Jul 9, 2023 · N339UP · Boeing 76734AF · Emergency Equipment
  > CAPT SIDE EMERGENCY ESCAPE ROPE CHASE PANEL IS LOOSE FIXED PER AMM 25-61-02-201
- [SDR IPXA2022102487418](https://openairdocs.org/sdr/IPXA2022102487418.md): Fan · vibration · Oct 22, 2022 · N339UP · Boeing 76734AF · Engine (Turbine/Turboprop)
  > ATB, DURING CLIMBOUT LEFT ENGINE N2 FAN VIBE DISPLAYED 5.0 WITH SIGNIFICANT VIBRATION AND NOISE ON FLIGHT DECK. CONFIRMED BIRDSTRIKE TO LEFT ENGINE. REF LOGPAGE 41181 ITEM2 AND LOGPAGE 411882 ITEM 1 FOR REQUIRED INSPECTIONS.BLENDED BLADES #27 & 28 IAW AMM 72
- [SDR IPXA2022022479365](https://openairdocs.org/sdr/IPXA2022022479365.md): Stiffener · none · Feb 18, 2022 · N339UP · Boeing 76734AF · Wing Main, Frame Structure
  > INSPECTION TYPE:C6CRACK ON CENTER WING TANK STIFFENER(P/N:111T2011-6) ON STA 785.9, RBL 55.REPAIR I.A.W 767-300F SRM 57-10-10-2R-2 REPAIR 2 REV.82.01 AND UPS EO B767-5730-58151-C AND B767-5720-76672-A.
- [SDR IPXA2022022479364](https://openairdocs.org/sdr/IPXA2022022479364.md): Floor Panel · none · Feb 18, 2022 · N339UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C6DAMAGE ON M/D CARGO FLOOR PANEL AT STA 850, RBL 11-LBL11.FABRICATE THE REPLACEMENT FLOOR PANEL PER EO NO. B767-5320-9693-I
- [SDR IPXA2021102975440](https://openairdocs.org/sdr/IPXA2021102975440.md): Seal · none · Oct 29, 2021 · N339UP · Boeing 76734AF · Passenger/Crew Doors
  > INSPECTION TYPE:NACLIMBING OUT OF FL200 A VERY LOUD HISSING SOUND CAME FROM NEAR FWD ENTRY DOOR. SOUND REMAINED CONSTANT. NO PRESSURIZATION ISSUES NOTED.FOUND DOOR SEAL OF FWD ENTRY DOOR SEPARATING FROM RETAINER GROOVE AT BOTTOM OF FWD ENTRY DOOR. REINSTALLED
- [SDR IPXA2021021765784](https://openairdocs.org/sdr/IPXA2021021765784.md): Battery Pack · inoperative · Feb 17, 2021 · N339UP · Boeing 76734AF · Emergency Lighting
  > INSPECTION TYPE: NA EMERGENCY LTS INOP. REMOVED AND REPLACED EMERGENCY LT BATTERY PACK IAW MM 33-51-07 OPS CK NORMAL IPC 33-51-07-32 20J.
- [SDR IPXA2021012764978](https://openairdocs.org/sdr/IPXA2021012764978.md): Retainer · damaged · Jan 26, 2021 · N339UP · Boeing 76734AF · Fuselage Main, Frame
  > INSPECTION TYPE: N/A CLIMBING THRU 17000FT A VERY LOUD POP WAS HEARD, FOLLOWED BY LOUD HISSING SOUND COMING FROM THE BOTTOM OF MAIN CABIN DOOR. CABIN ALT REMAINED STEADY, FOUND SEAL OUT OF RETAINER. REINSTALLED SEAL AT BOTTOM OF MAIN CABIN DOOR, IAW AMM 52-0
- [SDR IPXA2020120863218](https://openairdocs.org/sdr/IPXA2020120863218.md): Transmitter · malfunctioned · Dec 7, 2020 · N339UP · Boeing 76734AF · Trailing Flap Position Indicating System
  > INSPECTION TYPE: NA, EMERGENCY DECLARED-NO EQUIPMENT USED. TRAILING EDGE DISAGREE ON APPROACH WHEN SELECTING FLAPS 5 DEG TO 20 DEG. QRH PROCEDURE COMPLETED. TRAILING EDGE ALTN SYSTEM USED PER QRH. FLAPS OPERATED NORMALLY VIA ALTN SYSTEM. NORMAL LANDING AC
- [SDR IPXA2020102261573](https://openairdocs.org/sdr/IPXA2020102261573.md): Warning Message · illuminated · Oct 20, 2020 · N339UP · Boeing 76734AF · Door Warning System
  > INSPECTION TYPE: N/A ATB EMERGENCY DECLARED. LANDING UNEVENTFUL. CLIMBING OUT AT 11000 CABIN ALTITUDE HORN, LIGHT AND EICAS MESSAGE THEN CABIN ALTITUDE AUTO AND FINALLY MAIN CARGO DOOR LIGHT AND EICAS MESSAGE. FOUND MAIN DECK CARGO COMPT SAFELY NET NOT INST
- [SDR IPXA2020051155128](https://openairdocs.org/sdr/IPXA2020051155128.md): Skin · damaged · May 10, 2020 · N339UP · Boeing 76734AF · Ailerons
  > INSPECTION TYPE:N/ALH WING INBOARRD AILERON LOWER SKIN DAMAGE RE: EO B767-5750-76127-B. NON-BALANCED SURFACE PER ENGINEERING.SANDED DAMAGED AREAS. REMOVED DAMAGE. INSTALLED NEW CORE AND REPAIR PLYS. COMPLETED REPAIR IAW EO B767-5750-76127-C.
- [SDR IPXA2020051055129](https://openairdocs.org/sdr/IPXA2020051055129.md): Skin · damaged · May 10, 2020 · N339UP · Boeing 76734AF · Ailerons
  > INSPECTION TYPE:N/A **SUPPLEMENTAL SDR** (CLOSED) LEFT WING INBOARD AILERON LOWER SKIN DAMAGE. THIS IS A MAJOR REPAIR TRANSFERRED TO NON-ROUTINE CARD # 663200 DM 0557813 05-08-20Y. SANDED DAMAGED AREAS PER SRM 51-70-17. REMOVED DAMAGED SKIN & FABRICATED COR
- [SDR IPXA2018121756948](https://openairdocs.org/sdr/IPXA2018121756948.md): Control Panel · inoperative · Dec 15, 2018 · N339UP · Boeing 76734AF · Emergency Lighting
  > EMERGENCY LIGHTS BACK GROUND PLATE LIGHTS INOPERATIVE. R & R EMERGENCY LIGHTS CONTROL PANEL IAW MM 33-51-08-4, OPS CHECKED GOOD.
- [SDR IPXA2018121737001](https://openairdocs.org/sdr/IPXA2018121737001.md): Control Panel · inoperative · Dec 11, 2018 · N339UP · Boeing 76734AF · Emergency Lighting
  > EMERGENCY LIGHTS SWITCH BACKLIGHTS INOP. R&R EMER LIGHTS CONTROL PANEL IAW MM 31-51-08-4. OPS CK GOOD.
- [SDR IPXA2018022126729](https://openairdocs.org/sdr/IPXA2018022126729.md): Skin · dented · Feb 4, 2018 · N339UP · Boeing 76734AF · Fuselage Main, Plate/Skin
  > INSPECTION TYPE: C4, SKIN DENTED BS 451, STRINGER 25 - 26R. REPAIRED IAW SRID 3-4105366013 AND EO B767-5330-67377-A.
- [SDR IPXA2017012113040](https://openairdocs.org/sdr/IPXA2017012113040.md): Pbe · contaminated · Jan 21, 2017 · N339UP · Boeing 76734AF · Emergency Equipment
  > COCKPIT PBE MOISTURE INDICATOR SHOWS WHITE. REMOVED AND REPLACED THE PBE. SECURED IN HOLDER.
- [SDR IPXA2017010912538](https://openairdocs.org/sdr/IPXA2017010912538.md): Cover · broken · Jan 7, 2017 · N339UP · Boeing 76734AF · Passenger/Crew Doors
  > CREW ENTRY DOOR ARMING LEVER HINGE COVER MISSING HINGE IS BROKEN. R&R HINGE COVER ASSY IAW AMM 20-00-00.
- [SDR IPXA2016041101942](https://openairdocs.org/sdr/IPXA2016041101942.md): Floor Panel · damaged · Apr 11, 2016 · N339UP · Boeing 76734AF · Fuselage Floor Panel
  > MAIN CARGO DECK FLOOR PANEL POSITION 8L HAS A DAMAGE TO UPPER SKIN. REPAIRED IAW EO B767-5320-9693-I
- [SDR IPXA2016041101943](https://openairdocs.org/sdr/IPXA2016041101943.md): Floor Panel · damaged · Apr 11, 2016 · N339UP · Boeing 76734AF · Fuselage Floor Panel
  > FLOOR PANEL 5/5 RT HAS DAMAGE UPPER SKIN. REPAIRED IAW EO B767-5320-9693-I.
- [SDR IPXA2016041001900](https://openairdocs.org/sdr/IPXA2016041001900.md): Floor Panel · dented · Apr 10, 2016 · N339UP · Boeing 76734AF · Fuselage Floor Panel
  > FLOOR PANEL 12L DENT APPROXIMATELY 1", LOCATION 8" FROM EDGE. REPAIRED IAW SRM 53-00-50-2R, REV 64.
- [SDR IPXA2015060689894](https://openairdocs.org/sdr/IPXA2015060689894.md): Cover Plate · malfunctioned · Jun 6, 2015 · N339UP · Boeing 76734AF · Passenger/Crew Doors
  > MAIN ENTRY ARMING HINGE COVER WILL NOT STOW. BLOCKING EGRESS. R & R COVER IAW SRM 51-40-02.
- [SDR IPXA2015050288543](https://openairdocs.org/sdr/IPXA2015050288543.md): Blower · inoperative · May 1, 2015 · N339UP · Boeing 76734AF · Air Distribution Fan
  > CAPTAINS EVAS BLOWER DOES NOT RUN WITH TEST TOOL REF TC 25-069-00. R & R CAPTAINS EVAS AMM 25-69-00-000-801C3, 25-60-00-400-801C3 TESTS NORMAL IAW TC 25-069-00, IPC 25-60-00-90, ITEM - 001.
- [SDR IPXA2015042688390](https://openairdocs.org/sdr/IPXA2015042688390.md): Floor Panel · punctured · Apr 26, 2015 · N339UP · Boeing 76734AF · Fuselage Floor Panel
  > MAIN CARGO DECK FLOOR PANEL, PN 141T5856-13 HAS MULTIPLE DAMAGES TO UPPER SKIN AND PANEL EDGE FABRICATED REPLACEMENT PANEL IAW EO B767-5320-9693H.
- [SDR IPXA2015021685969](https://openairdocs.org/sdr/IPXA2015021685969.md): Shutoff Valve · inoperative · Feb 13, 2015 · N339UP · Boeing 76734AF · Pneumatic Distribution System
  > INSPECTION TYPE: E, TOP WAN NR 2253636, ACCOMPLISHED SEE LP 823263, ITEM 2.
- [SDR IPXA2014102784720](https://openairdocs.org/sdr/IPXA2014102784720.md): Placard · deteriorated · Oct 26, 2014 · N339UP · Boeing 76734AF · Placards and Markings
  > F/O EMERGENCY EXIT PULL PLACARD IS DETERIORATED. R & R THE PLACARD IAW AMM 20-10-12.
- [SDR IPXA2014061383290](https://openairdocs.org/sdr/IPXA2014061383290.md): Flap System · false indication · Jun 12, 2014 · N339UP · Boeing 76734AF · Trailing Edge Flap Control System
  > EMERGENCY DECLARED, FLAPS INDICATE SPLIT WITHOUT EICAS MESSAGE. CYCLED CIRCUIT BREAKER, INDICATOR NORMAL. OPS FLAPS IAW MM 27-51-00-201 WITHOUT PROBLEMS NO INDICATION DISCREPENCIES OR EICAS MESSAGE NOTED, NO HISTORY LAST 30 DAYS.
- [SDR IPXA2014060283176](https://openairdocs.org/sdr/IPXA2014060283176.md): Power Supply · inoperative · May 31, 2014 · N339UP · Boeing 76734AF · Emergency Lighting
  > EMERGENCY LIGHTS POWER SUPPLY INOPERATIVE. REPLACED EMERGENCY LIGHTS POWER SUPPLY WRT 33-51-07. OPS CHECKED OK.
- [SDR IPXA2014060283175](https://openairdocs.org/sdr/IPXA2014060283175.md): Lamp · inoperative · May 31, 2014 · N339UP · Boeing 76734AF · Emergency Lighting
  > EMERGENCY LIGHT ON LT SIDE FUSELAGE INOPERATIVE. REPLACED LAMP. OPS CHECKED OK IAW MM 33-51-16.
- [SDR IPXA2013122301111](https://openairdocs.org/sdr/IPXA2013122301111.md): Transmitter · inoperative · Dec 21, 2013 · N339UP · Boeing 76734AF · Trailing Flap Position Indicating System
  > AIR TURNBACK DUE TO FLAP ASSEMETRY INDICATION. LT T/E FLAP INDICATOR STAYED AT 15 DEGREES AND THE RT WENT TO 5 DEGREES. DETERMINED THAT THE FLAP SPLIT WAS INDICATION ONLY. R & R LEFT FLAP NR 1 POSITION TRANSMITTER IAW AMM 27-517-45. OPS CHECKED GOOD.
- [SDR IPXA2672256](https://openairdocs.org/sdr/IPXA2672256.md): Floor Panel · broken · Mar 12, 2012 · N339UP · Boeing 76734AF · Fuselage Floor Panel
  > INSPECTION TYPE: C, MAIN DECK FLOOR PANEL NR 241AFF BROKEN AT BS 761, RBL 1. L X W=1"X1" ON UPPER SKIN AND CORE;L X W=1.2"X1" ON LOWER SKIN CUT OUT THE DAMAGE AREA WITH L X W=1.25"X1.25". REPAIR IAW REV:52, SRM 53-00-50 REPAIR GENERAL, FIG 201 PARA 4 E.
- [SDR IPXA2672231](https://openairdocs.org/sdr/IPXA2672231.md): Wedge · damaged · Mar 7, 2012 · N339UP · Boeing 76734AF · Trailing Edge Flaps
  > INSPECTION TYPE: C, LEFT WING OTBD T/E FLAP HAS PUNCTURE (2"X1")ON L/E. LOCATED 2' OTBD OF INBD EDGE ON THE L/E. REMOVE THE EXISTING INTERIM REPAIR FOR SIZE L X W=5.1"X2.5". PERFORM THE REPAIR IAW REV:52,767-300F, SRM 57-53-01, REPAIR 1, TABLE I AND SRM 51-
- [SDR IPXA2672230](https://openairdocs.org/sdr/IPXA2672230.md): Skin · dented · Mar 7, 2012 · N339UP · Boeing 76734AF · Trailing Edge Flaps
  > INSPECTION TYPE: C, DENTED SKIN, LT WING OTBD FLAP LOWER SKIN DENTS AT OTEF STA 250 AND OTEF STA 263.5. DENT WITH DELAMINATION DIMENSION L X W X D=2.2"X2.1"X0.020" AT OTEF STA 250 AND THE OTHER DENT WITH DELAMINATION DIMENSION L X W X D=2.0"X1.54"X0.020" AT O
- [SDR IPXA1669044](https://openairdocs.org/sdr/IPXA1669044.md): Floorboard · damaged · Sep 4, 2011 · N339UP · Boeing 76734AF · Fuselage Floor Panel
  > INSPECTION TYPE:MX POS 4 FLOORBOARD MCD CENTER INTERIM REPAIR 2 INCH HOLES 16 INCHES AFT OF CENTERLINE IDENTIFIED PANEL FROM POSITION 4. PN 143T5876-98 IAW EO B767-5320-969 APPENDIX H. FABRICATED A REPLACEMENT PANEL BY CUTTING OUT A NEW PANEL FROM A402H A

Next page: https://openairdocs.org/aircraft/N339UP/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 = 'N339UP' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N339UP/reports

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