N342UP

Service difficulty reports · 41

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 = 'N342UP' 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 IPXA2026091176660Seal · leakingENTRY DOOR POTENTIAL SEAL LEAK , LEAKING NOISE MOST OF THE FLIGHT ALL ALTITUDES, SOUND APPEARS TO COME FROM BOTTOM OF DOOR FOUND SEALANT MISSING FROM SEAMS IN SILL PLATE. REPLACED SEALANT. PRESSURIZED A/C AND FOUND NO MORE LEAKAGE/NOISE FROM CREW ENTRY DOOR.Sep 10, 2026 · N342UP · Boeing 76734AF · Passenger/Crew DoorsSDR IPXA2026091076660Seal · leakingENTRY DOOR POTENTIAL SEAL LEAK , LEAKING NOISE MOST OF THE FLIGHT ALL ALTITUDES, SOUND APPEARS TO COME FROM BOTTOM OF DOOR PRESSURE CHECK ENTRY DOOR IAW AMM 05-51-24. FOUND LEAK COMING FROM THE BOTTOM OF THE DOOR.Sep 10, 2026 · N342UP · Boeing 76734AF · Passenger/Crew DoorsSDR IPXA2026060872758Test Button · inoperativeWHEEL WELL FIRE DETECTION TEST DOESN'T WORK WHEN TEST BUTTON IN FLIGHTDECK PRESSED. T/S CARRIED OUT IAW FIM 26-17 FAULT TREE 803 REV. 148. FOUND WHEELWELL FIRE TEST BUTTON U/S. FIRE/OVERHEAT TEST PANEL REPLACED IAW AMM 26-11-01 PB. 401 REV. 148. POST INSTALLAJun 8, 2026 · N342UP · Boeing 76734AF · Detection SystemSDR IPXA2025102829407Flap · damagedBIRD STRIKE DAMAGE TO RIGHT WING OUTBOARD FLAP LEADING EDGE. COMPLETED REPAIR TO LEADING EDGE PANEL PER SRM 51-70-05-0G-0 ALL STEPS OF REPAIR COMPLETE. REPAIR PLIES INSTALLED AND CURED. REAPPLIED PROTECTIVE COATINGS AND PERFORM POST REPAIR REQUIREMENTS. INSTAOct 24, 2025 · N342UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA2025102429407Flap · damagedBIRD STRIKE DAMAGE TO RIGHT WING OUTBOARD FLAP LEADING EDGE. REMOVED PANEL 666AT AND ROUTED TO SHEET METAL SHOP FOR REPAIR.Oct 24, 2025 · N342UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA2025062264991Fmc · faultedATB FMC LOCKED UP WITH STBY ONE MSG PRESENT (FULL WRITEUP IN FAULT DESCRIPTION). + PERFORMED TROUBLE SHOOTING REF B767 FIM 34-61 FAULT TREE 854,NO FAULTS FOUND.REMOVED AND REPLACED L/H FMC REFB767AMM 34-61-01 9 (PRECAUTIONARY) OPS CHECK GOOD ATT.Jun 22, 2025 · N342UP · Boeing 76734AF · Flight Management Computing Hardware SystemSDR IPXA2025020716359None · noneADD SDR FOR EO-82173-JIC001 (FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF STA 1725.5 BETWEEN S-36L AND S-36R) [T3F18E0013XJ0] ACCOMPLISHED SDR. REVIEWED.Feb 7, 2025 · N342UP · Boeing 76734AF · Standard Practices/StructuresSDR IPXA2025020220164Skin · debondedDISBOND PNL, RT WING NR 8 L/E SLAT INBD, SIDE INNER UPPER WEDGE. INST THE EXT DBLR WITH FILM ADHESIVE & CURE IAW SRM 51-70-10-2R-0 PARA 18 & 20. PERFORMED NDT/UT FOR REWORKED AREA & 8" FROM WHERE EDGES OF HEAT BLANKET, IAW NDT MANUAL PT1 51-01-01 & 51-04-00 RFeb 1, 2025 · N342UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA2025020491420Angle · crackedFOUND THE ANGLE CRACK AT STA 1578 RBL 80 INBOARD IN BULK CARGO COMPARTMENT RIGHT AREA. (REPLACE). REMOVED DAMAGE PARTS I.A.W SRM 51-40-02-0G REV.91. INSTALL NEW PARTS I.A.W SRM 51-40-02-0G REV.91 AND BOEING DWG NO. 146T5650 SHEET 5 REV:C. JOB COMPLETED.Jan 26, 2025 · N342UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR IPXA2025020491290Angle · crackedFOUND THE ANGLE CRACK AT STA 1578 RBL 80 OUTBOARD IN BULK CARGO COMPARTMENT RIGHT AREA. (REPLACE). REMOVED DAMAGE PARTS I.A.W SRM 51-40-02-0G REV.91. INSTALL NEW PARTS I.A.W SRM 51-40-02-0G REV.91 AND BOEING DWG NO. 146T5650 SHEET 5 REV:C. JOB COMPLETED. I.A.WJan 26, 2025 · N342UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR IPXA2025020491462Angle · crackedFOUND THE ANGLE CRACK AT STA 1578 LBL 80 OUTBOARD IN BULK CARGO COMPARTMENT LEFT AREA. (REPLACE). REMOVED DAMAGE PARTS I.A.W SRM 51-40-02-0G REV.91 INSTALL NEW PARTS I.A.W SRM 51-40-02-0G REV.91 AND BOEING DWG NO. 146T5650 SHEET 5 REV:C. JOB COMPLETED. I.A.W AJan 26, 2025 · N342UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR IPXA2025013192484Floor Panel · damagedFOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE, P/N: 146T5869-65 PANEL NO: 251JFF STA 1197+22~STA 1197+110 LBL 55~LBL 77. (REPAIR). FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4. I.A.W AMM 25-57-05-404-006 AND AMM 25-58-01-404-005 REV.144 INSTALLED MJan 26, 2025 · N342UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA2025013192466Floor Panel · damagedFOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE, P/N: 146T5869-9 PANEL NO: 241KFF STA 1197+22~STA 1197+110 LBL 77~LBL 88. (REPAIR). FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4. I.A.W AMM 25-57-05-404-006, AMM 25-58-04-404-015 AND AMM 25-58-01-404-00Jan 26, 2025 · N342UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA2025013192454Floor Panel · damagedFOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE, P/N: 145T5876-68 PANEL NO: 241AFF STA 731~STA 834 LBL 11~RBL 11. (REPAIR). FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4. I.A.W AMM 25-57-05-404-006, AMM 25-58-01-404-005 AND AMM 25-58-03-404-004 REV.14Jan 26, 2025 · N342UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA2025013192451Floor Panel · damagedFOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE, P/N: 146T5869-135 PANEL NO: 251XFF STA 1440~STA 1540 LBL 77.5~LBL 54.75. (REPAIR). FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4. I.A.W AMM 25-57-05-404-006, AMM 25-58-04-404-015, AMM 25-58-01-404-005 AJan 26, 2025 · N342UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA202403040049Pitot Head · damagedLUZ DE CAPT PITOT ENCENDIDA DESPUES DEL ARRANQUE DE MOTORES, PROBETA DE TUBO PITOT DEL CAPITAN DAÑADA CAPT PITOT LIGHT ON AFTER STARTING, PITOT TUBE DAMAGED.Feb 21, 2024 · N342UP · Boeing 76734AF · Pitot/Static Anti-Ice SystemSDR IPXA2023012690278Floorbeam · damagedINSPECTION TYPE:C6, DAMAGE ON M/D CARGO FLOORBEAM, BS 246, LBL 53. FABRICATED A REPLACEMENT IAW DWG 141T5146 SH 15 REV B, PL REV F AND PSDL REV-. REPLACED IAW SRM 51-40-02-0G-0 REV. 85.01.Jan 13, 2023 · N342UP · Boeing 76734AF · Fuselage Main, Floor BeamSDR IPXA2022112888472Seal · detachedINSPECTION TYPE:N/ACREW ENTRY DOOR SEAL MAKES VERY LOUD HISSING NOISE IN FLIGHT.PRESSURISATION OKAYFOUND CREW ENTRY DOOR BOTTOM SEAL DETACHED SECURED AND CLEANED DOOR SEAL PER AMM 52-09-01-424-019 FOUND SATISNov 28, 2022 · N342UP · Boeing 76734AF · Passenger/Crew DoorsSDR IPXA2021121777022Apu · faultedINSPECTION TYPE:N/ASUPPLEMENTAL SDR**DIVERSION**EMERG DECLARED**A/C LANDED W/OUT INCIDENT**APU FAULT AT FL 390 DIVERTED TO STL. DEFERRED PER MEL 49-11-1A ASSIGNED M766577REPLACED APU COOLING FAN AMM 49-51-03-401 AND APU OIL COOLER AMM 49-27-09-404-011. OPS & LDec 16, 2021 · N342UP · Boeing 76734AF · APU Cowling/ContainmentSDR IPXA2020051355257Tire · damagedINSPECTION TYPE:N/A** EMERGENCY DECLARED ** THE FIRE TRUCKS FOLOWED THE A/C TO THE RAMP & THE FIRE CHIEF DETERMINED IT WAS SAFE TO TAXI TO THE GATE & FOLLOWED THE AIRCRAFT TO THE GATE ** # 7 MLG TIRE HEATSHIELD DAMAGED.R & R'D # 7 MAIN WHEEL ASSY IAW MM 32-45May 12, 2020 · N342UP · Boeing 76734AF · TireSDR IPXA2020051155077Control Module · inoperativeINSPECTION TYPE:N/AHYDRAULIC POWER CAME ON PRIOR TO ENGINE START ON PUSHBACK, BOTH YOKES WENT 3/4 FULL LEFT TURN FOR NO REASON. A/P OFF.R/R AILERON RUDDER TRIM AILERON CONTROL MODULE PER AMM 27-21-23-022-001 & 27-21-23-422-007 OPS TEST AILERON & AILERON TRIM CMay 7, 2020 · N342UP · Boeing 76734AF · Rudder Tab Control SystemSDR IPXA2019091046567Battery Pack · dischargedINSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS INOP. R&R BATT PACK PER AMM 33-51-07 OPS CHK GOOD. ESR: IPC 33-51-07-32.Sep 10, 2019 · N342UP · Boeing 76734AF · Emergency LightingSDR IPXA2019040864843Bulb · inoperativeEXTERIOR EMERGENCY LIGHT INOP. REPLACED THE BULB IAW AMM 33-51-16-962-001 OPS CKS OKApr 6, 2019 · N342UP · Boeing 76734AF · Emergency LightingSDR IPXA2019012338207Skin Panel · brokenINSPECTION TYPE:C4 BROKEN ON LOWER SKIN PANEL OF RT WING INBD AFT FLAP NEAR IFS 119.75. REPAIR IAW SRM 57-53-01 REPAIR 1, SRM 51-70-10 REPAIR 2, SRM 51-70-10 GENERAL, SRM 51-70-03 GENERAL, REV.73.01Jan 13, 2019 · N342UP · Boeing 76734AF · Wing, Plate/SkinSDR IPXA2019011837983Floor Panel · damagedINSPECTION TYPE:C4 DAMAGE ON M/D CARGO FLOOR PANEL AT STA 834-STA 930, LBL 11 - RBL 11, PNL NR 241FFF. FABRICATE THE REPLACEMENT FLOOR PANEL PER EO NR B767-5320-9693-I.Jan 13, 2019 · N342UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA2019010737587Light · inoperativeINSPECTION TYPE:N/A EXTERIOR EMERGENCY LIGHT INOP. R&R LAMP W/ REF TO AMM. 33-51-16. LIGHT OPERATES NORMAL P/N ON/OFF 767.Dec 8, 2018 · N342UP · Boeing 76734AF · Emergency LightingSDR IPXA2016062605049Floor Panel · puncturedMCD FLOOR PANEL PUNCTURED POSITION 2R, FABRICATED NEW PANEL IAW EO B767-5320-9693-I.Jun 26, 2016 · N342UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA2015120896506Fire Loop · malfunctionedRIGHT ENGINE FIRE LOOP 1 STATUS MESSAGE. REPLACED THE RT FWD LOWER FIRE LOOP DETECTOR IAW AMM 26-11-02 AND TESTED NORMAL.Dec 7, 2015 · N342UP · Boeing 76734AF · Fire DetectionSDR IPXA2015032287255Skin · damagedDURING MAJOR MAINTENANCE VISIT NR 6749, FOUND DENT ON SKIN, BULK CARGO DOOR OUTER SURFACE, STA 1447, BETWEEN S-23L AND S-24 L/E, EVALUATED DAMAGE IAW SRM 52-30-01-1A-1, FIG 101, REF: TAIL VI, REV 61.00 INFORMATION SUBMITTED FOR ADM, DENT WITHIN ALLOWABLE DAMAGMar 21, 2015 · N342UP · Boeing 76734AF · Cargo/Baggage DoorsSDR IPXA2014011001250Lamp · inoperativeEXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP.Jan 7, 2014 · N342UP · Boeing 76734AF · Emergency LightingSDR IPXA2014010201191Latch · brokenCAPTAIN'S OVERHEAD ESCAPE ROPE DOOR LATCH INOPERATIVE. OVERHEAD PANEL ASSY R & R IAW AMM TASK 25-1 4-02. ROPE INSTALLED IAW AMM TASK 25-61-02-682-001, REV 110, 02.Dec 29, 2013 · N342UP · Boeing 76734AF · Emergency EquipmentSDR IPXA3680327Floor Panel · damagedFLOOR PANEL DAMAGED. REPAIRED IAW SRM 53-00-50.Sep 21, 2013 · N342UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA3677437Skin · dentedINSPECTION TYPE:C01, A DENT WAS FOUND ON LT WING NR 3 SLAT UPPER SURFACE OF WEDGE AREA. DAMAGE SIZE IS MEASURED AS 1.75"(LENGTH) X 1.5"(WIDTH) X 0.031"(DEPTH) AT OSS 807. REPAIRED IAW SRM 57-43-02, REPAIR 1 AND 51-70-10, REPAIR 4, FIG 201, REV 55.Mar 4, 2013 · N342UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA3677436Skin · dentedINSPECTION TYPE:C01, A DENT WAS FOUND ON LT WING NR 3 SLAT UPPER SURFACE OF WEDGE AREA. DAMAGE SIZE MEASURED AS 0.88" (LENGTH) X 0.62"(WIDTH) X 0.025" (DEPTH) AT OS S 804.5 REPAIR IAW SRM 57-43-02, REPAIR 1 AND 51-70-10, REPAIR 4, FIG 201, REV 55.Mar 4, 2013 · N342UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA3677435Skin · dentedINSPECTION TYPE:C01, A DENT WAS FOUND ON LT WING NR 3 SLAT UPPER SURFACE OF WEDGE AREA. DAMAGE SIZE MEASURED AS 0.62" (LENGTH) X 0.55" (WIDTH) X 0.012"(DEPTH) AT OSS 805.5 REPAIRED IAW SRM 57-43-02, REPAIR 1 AND 51-70-10, REPAIR 4, FIG 201, REV 55.Mar 4, 2013 · N342UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA3677434Skin · dentedA DENT WAS FOUND ON LT WING NR 3 SLAT UPPER SURFACE OF WEDGE AREA. DAMAGE SIZE IS MEASURED AS 0.78" (LENGTH) X 0.55" (WIDTH) X 0.012" (DEPTH) AT OSS 801.5. REPAIR IAW 767-300F SRM 57-43-02, REPAIR 1 AND 51-70-10, REPAIR 4, FIG 201, REV 55.Mar 4, 2013 · N342UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA3677431Wedge · dentedINSPECTION TYPE:C01, LT WING NR 3 SLAT T/E WEDGE ASSY UPPER SKIN DENTED AT OSS 819. DAMAGE SIZE IS MEASURED AS 1.0" (LENGTH) X 0.66"(WIDTH) X 0.013"(DEPTH) AND THE CUT OUT IS MEASURED AS 1" DIAMETER. REPAIR IAW SRM 57-43-02, REPAIR 1 AND 51-70-10, REPAIR 4 FIMar 4, 2013 · N342UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA2676466Floor Panel · dentedMAIN CARGO DECK FLOOR PANEL POS NR 12L OTBD HAS DENT CENTER OF PANEL. REPAIRED IAW SRM 53-00-50-2R.Dec 15, 2012 · N342UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA2672017Floor Panel · damagedMAIN CARGO FLOOR PANEL HAS A 3" BY 1" HOLE AT POS 6/7 PANEL CENTER, IDENTIFIED PANEL FROM POS 6/7 CENTER AS PN 145T5876-60 IAW EO B767-5320-9693H. FABRICATED A REPLACEMENT PANEL FROM A402H ACCOMPLISHED PARA B, STEP 5 & 6 REF EO B767-5320--9693-H.Mar 4, 2012 · N342UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA2672016Floor Panel · damagedMAIN CARGO COMPARTMENT FLOOR PANEL HAS A 3" BY 1" HOLE AT POSITION 4/5 CENTER PANEL 31" AFT OF POS 4. IDENTIFIED PANEL FROM POSITION 4/5 CENTER AS PN 143T5876-112 IAW EO B767-5320-9693 H. FABRICATED A REPLACEMENT PANEL FROM A402H ACCOMPLISHED PARA B, STEP 5 &Mar 4, 2012 · N342UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA2672015Floor Panel · damagedMAIN CARGO COMPARTMENT FLOOR PANEL HAS A .5" DIAMETER HOLE AT POSITION 4/5 CENTER PANEL, 59" FWD FROM POS 4. IDENTIFIED PANEL FROM POS 4/5 CENTER AS PN 143T5876-112 IAW EO B767-5320-9693H, FABRICATED A REPL PANEL FROM A402H ACCOMPLISHED PARA B STEP 5&6 REF EOMar 4, 2012 · N342UP · Boeing 76734AF · Fuselage Floor Panel
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