N339UP

Service difficulty reports · 56

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR IPXA2026020384940Floor Panel · corrodedFOUND MAIN DECK FLOOR PANEL CORRODED, BS 1601, RBL 33. INSTALLED FLOOR PANEL IAW AMM 20-11-00-910-802, REV 147.Jan 20, 2026 · N339UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA2026020385077Cargo Track · corrodedFOUND 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.Jan 20, 2026 · N339UP · Boeing 76734AF · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2025080729838Fce · faultedAIR 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 (MAug 6, 2025 · N339UP · Boeing 76734AF · Leading Edge Slat Position Indicating SystemSDR IPXA2024121958268A/C Pack · odorLEFT 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 OPDec 12, 2024 · N339UP · Boeing 76734AF · Cabin Cooling SystemSDR IPXA2024072611426Warning Message · false activation**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 NOTEDJul 26, 2024 · N339UP · Boeing 76734AF · Trailing Edge Flap Control SystemSDR IPXA2024013128494Skin · debondedFAULT - 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.Jan 19, 2024 · N339UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA2024013128280Rib · crackedFAULT - 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.88Jan 19, 2024 · N339UP · Boeing 76734AF · Nacelle/Pylon, Frame/Spar/RibSDR IPXA2024013128251Access Panel · crackedFAULT - 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.88Jan 19, 2024 · N339UP · Boeing 76734AF · Nacelle/Pylon, Main FrameSDR IPXA2024013128068Panel · crackedFAULT - 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.88Jan 19, 2024 · N339UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA2024012228068Panel · damaged*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 Jan 19, 2024 · N339UP · Boeing 76734AF · Wing Main, Frame StructureSDR IPXA2024012228251Support · cracked*SDR FILED OPEN* FAULT - CRACK - RIB, NO.1 PYLON INSIDE OF MID TORQUE BOX SUPPORT, CAN ACCESS FROM PANEL #436AR (REPLACE) OK TO WORKJan 19, 2024 · N339UP · Boeing 76734AF · Nacelle/Pylon Miscellaneous StructureSDR IPXA2024012228494Skin · debonded*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.Jan 19, 2024 · N339UP · Boeing 76734AF · Wing, Plate/SkinSDR IPXA2024012228280Support · cracked*SDR FILED OPEN* FAULT - CRACK - RIB, NO.1 PYLON INSIDE OF MID TORQUE BOX SUPPORT, CAN ACCESS FROM PANEL #436AL (REPLACE) OK TO WORKJan 19, 2024 · N339UP · Boeing 76734AF · Nacelle/Pylon Miscellaneous StructureSDR IPXA2024012227720Cap · crackedFAULT - 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 INBOARJan 19, 2024 · N339UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA2024012227663Skin · damagedFAULT - 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 Jan 19, 2024 · N339UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA2024013145304Liner · missing**SUPPLEMENTAL SDR**FAULT - FOUND ENTRY DOOR FORWARD DOORWAY LINING TRIM MISSING (REPLACE) C/W REVIEW INSTALLED NEW DOOR LINING I.A.W AMM 52-12-02-004-001Jan 16, 2024 · N339UP · Boeing 76734AF · Passenger/Crew DoorsSDR IPXA2024011745304Liner · unknownFOUND ENTRY DOOR FORWARD DOORWAY LINING TRIM MISSING (REPLACE) OK TO WORKJan 16, 2024 · N339UP · Boeing 76734AF · Passenger/Crew DoorsSDR IPXA2024011636099Stiffener · crackedFAULT - 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 SRMJan 15, 2024 · N339UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR IPXA2023071059404Escape Rope · looseCAPT SIDE EMERGENCY ESCAPE ROPE CHASE PANEL IS LOOSE FIXED PER AMM 25-61-02-201Jul 9, 2023 · N339UP · Boeing 76734AF · Emergency EquipmentSDR IPXA2022102487418Fan · vibrationATB, 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 72Oct 22, 2022 · N339UP · Boeing 76734AF · Engine (Turbine/Turboprop)SDR IPXA2022022479365Stiffener · noneINSPECTION 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.Feb 18, 2022 · N339UP · Boeing 76734AF · Wing Main, Frame StructureSDR IPXA2022022479364Floor Panel · noneINSPECTION 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-IFeb 18, 2022 · N339UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR IPXA2021102975440Seal · noneINSPECTION 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 Oct 29, 2021 · N339UP · Boeing 76734AF · Passenger/Crew DoorsSDR IPXA2021021765784Battery Pack · inoperativeINSPECTION 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.Feb 17, 2021 · N339UP · Boeing 76734AF · Emergency LightingSDR IPXA2021012764978Retainer · damagedINSPECTION 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 52-0Jan 26, 2021 · N339UP · Boeing 76734AF · Fuselage Main, FrameSDR IPXA2020120863218Transmitter · malfunctionedINSPECTION 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 ACDec 7, 2020 · N339UP · Boeing 76734AF · Trailing Flap Position Indicating SystemSDR IPXA2020102261573Warning Message · illuminatedINSPECTION 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 INSTOct 20, 2020 · N339UP · Boeing 76734AF · Door Warning SystemSDR IPXA2020051155128Skin · damagedINSPECTION 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.May 10, 2020 · N339UP · Boeing 76734AF · AileronsSDR IPXA2020051055129Skin · damagedINSPECTION 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 CORMay 10, 2020 · N339UP · Boeing 76734AF · AileronsSDR IPXA2018121756948Control Panel · inoperativeEMERGENCY LIGHTS BACK GROUND PLATE LIGHTS INOPERATIVE. R & R EMERGENCY LIGHTS CONTROL PANEL IAW MM 33-51-08-4, OPS CHECKED GOOD.Dec 15, 2018 · N339UP · Boeing 76734AF · Emergency LightingSDR IPXA2018121737001Control Panel · inoperativeEMERGENCY LIGHTS SWITCH BACKLIGHTS INOP. R&R EMER LIGHTS CONTROL PANEL IAW MM 31-51-08-4. OPS CK GOOD.Dec 11, 2018 · N339UP · Boeing 76734AF · Emergency LightingSDR IPXA2018022126729Skin · dentedINSPECTION TYPE: C4, SKIN DENTED BS 451, STRINGER 25 - 26R. REPAIRED IAW SRID 3-4105366013 AND EO B767-5330-67377-A.Feb 4, 2018 · N339UP · Boeing 76734AF · Fuselage Main, Plate/SkinSDR IPXA2017012113040Pbe · contaminatedCOCKPIT PBE MOISTURE INDICATOR SHOWS WHITE. REMOVED AND REPLACED THE PBE. SECURED IN HOLDER.Jan 21, 2017 · N339UP · Boeing 76734AF · Emergency EquipmentSDR IPXA2017010912538Cover · brokenCREW ENTRY DOOR ARMING LEVER HINGE COVER MISSING HINGE IS BROKEN. R&R HINGE COVER ASSY IAW AMM 20-00-00.Jan 7, 2017 · N339UP · Boeing 76734AF · Passenger/Crew DoorsSDR IPXA2016041101942Floor Panel · damagedMAIN CARGO DECK FLOOR PANEL POSITION 8L HAS A DAMAGE TO UPPER SKIN. REPAIRED IAW EO B767-5320-9693-IApr 11, 2016 · N339UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA2016041101943Floor Panel · damagedFLOOR PANEL 5/5 RT HAS DAMAGE UPPER SKIN. REPAIRED IAW EO B767-5320-9693-I.Apr 11, 2016 · N339UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA2016041001900Floor Panel · dentedFLOOR PANEL 12L DENT APPROXIMATELY 1", LOCATION 8" FROM EDGE. REPAIRED IAW SRM 53-00-50-2R, REV 64.Apr 10, 2016 · N339UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA2015060689894Cover Plate · malfunctionedMAIN ENTRY ARMING HINGE COVER WILL NOT STOW. BLOCKING EGRESS. R & R COVER IAW SRM 51-40-02.Jun 6, 2015 · N339UP · Boeing 76734AF · Passenger/Crew DoorsSDR IPXA2015050288543Blower · inoperativeCAPTAINS 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.May 1, 2015 · N339UP · Boeing 76734AF · Air Distribution FanSDR IPXA2015042688390Floor Panel · puncturedMAIN CARGO DECK FLOOR PANEL, PN 141T5856-13 HAS MULTIPLE DAMAGES TO UPPER SKIN AND PANEL EDGE FABRICATED REPLACEMENT PANEL IAW EO B767-5320-9693H.Apr 26, 2015 · N339UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA2015021685969Shutoff Valve · inoperativeINSPECTION TYPE: E, TOP WAN NR 2253636, ACCOMPLISHED SEE LP 823263, ITEM 2.Feb 13, 2015 · N339UP · Boeing 76734AF · Pneumatic Distribution SystemSDR IPXA2014102784720Placard · deterioratedF/O EMERGENCY EXIT PULL PLACARD IS DETERIORATED. R & R THE PLACARD IAW AMM 20-10-12.Oct 26, 2014 · N339UP · Boeing 76734AF · Placards and MarkingsSDR IPXA2014061383290Flap System · false indicationEMERGENCY 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.Jun 12, 2014 · N339UP · Boeing 76734AF · Trailing Edge Flap Control SystemSDR IPXA2014060283176Power Supply · inoperativeEMERGENCY LIGHTS POWER SUPPLY INOPERATIVE. REPLACED EMERGENCY LIGHTS POWER SUPPLY WRT 33-51-07. OPS CHECKED OK.May 31, 2014 · N339UP · Boeing 76734AF · Emergency LightingSDR IPXA2014060283175Lamp · inoperativeEMERGENCY LIGHT ON LT SIDE FUSELAGE INOPERATIVE. REPLACED LAMP. OPS CHECKED OK IAW MM 33-51-16.May 31, 2014 · N339UP · Boeing 76734AF · Emergency LightingSDR IPXA2013122301111Transmitter · inoperativeAIR 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.Dec 21, 2013 · N339UP · Boeing 76734AF · Trailing Flap Position Indicating SystemSDR IPXA2672256Floor Panel · brokenINSPECTION 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.Mar 12, 2012 · N339UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA2672231Wedge · damagedINSPECTION 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-Mar 7, 2012 · N339UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA2672230Skin · dentedINSPECTION 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 OMar 7, 2012 · N339UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA1669044Floorboard · damagedINSPECTION 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 ASep 4, 2011 · N339UP · Boeing 76734AF · Fuselage Floor Panel
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