Boeing 767-346

Service difficulty reports · 133

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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 aircraft_model_key = '767346'
  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 IPXA2026101497479Strap · brokenBROKEN STRAP, NR 2 PYLON FWD FAIRING AFT SIDE LOWER SKIRT FAIRING LOWER SIDE. REPLACED. INSTALL NEW STRAP I.A.W SRM 51-40-02-0G REV 56. AND BOEING DWG 311T2570 SHEET 16 REV -. 2.Oct 5, 2026 · N364UP · Boeing 767346 · Nacelle/Pylon Miscellaneous StructureSDR IPXA2026101396536Former · crackedCRACK-FORMER, LT WING OUTBD L/E CAVITY CURTAIN SUPPORT, NEAR OSS 499. INSTALLED NEW FORMER I.A.W SRM 51-40-02-0G REV. 56 AND BOEING DWG NO. 114T2161 SH. 3 REV. B AND SREO-50900-REQ001 REV2.Oct 5, 2026 · N364UP · Boeing 767346 · Wing Main, Frame StructureSDR IPXA2026101296572Former · crackedCRACKED FORMER, LT WING OTBD CAVITY CURTAIN SUPPORT, NEAR OSS 648. INSTALLED NEW FORMER I.A.W SRM 51-40-02-0G REV. 56 AND BOEING DWG NO. 114T2163 SH. 3 REV. A AND SREO-50900-REQ001 REV2.Oct 5, 2026 · N364UP · Boeing 767346 · Wing Main, Frame StructureSDR IPXA2026101296488Former · crackedCRACKED BRACKET, RT WING OTBD L/E FOLDING NOSE INNER SIDE AT OSS 565, ADJUSTED NR 9 SLAT INBD SUPPORT ROD. INSTALLED NEW FORMER I.A.W SRM 51-40-02-0G REV. 56 AND DWG 114T2162 SH. 3 REV. C AND SREO-50900-REQ001 REV2. JOB COMPLETED.Oct 5, 2026 · N364UP · Boeing 767346 · Wing Main, Frame StructureSDR IPXA2026101685638Web · corrodedMAJOR REPAIR, RT PACK FWD BULKHEAD STA 785 CORRODED. ACCOMPLISHED REPAIR I.A.W EO-98914-REQ1 REV1 AND EGAT EI F2026A57M-2220 REV.2.Oct 4, 2026 · N364UP · Boeing 767346 · Fuselage Miscellaneous StructureSDR IPXA2026101387189Hinge · wornRT AFT FAIRING DOOR NR 4 HINGE WORN , NR 2 PYLON. REPAIR DAMAGE AREA I.A.W UPS EO-98882-REQ1 REV1. 2. REPLACED NEW HINGE FITTING (P/N: 313T3325U6) I.A.W SRM 51-40-02-0G REV. 56 AND BOEING DWG NO: 313T3340 SHEET 27 REV. B.Oct 4, 2026 · N364UP · Boeing 767346 · Nacelle/Pylon, Main FrameSDR IPXA2026101285892Former · crackedCRACKED FORMER, LT WING OTBD L/E CAVITY CURTAIN SUPPORT NEAR OFSS 562. INSTALLED NEW FORMER I.A.W SRM 51-40-02-0G REV. 56 AND BOEING DWG NO. 114T2162 SH. 3 REV. C AND SREO-50900-REQ001 REV2. JOB COMPLETED.Oct 4, 2026 · N364UP · Boeing 767346 · Wing Main, Frame StructureSDR IPXA2026101276376Floor Panel · crackedFOUND CRACKS ON THE FLOOR PANEL P/N 814T6542-66 IN THE MAIN DECK CARGO COMPARTMENT. I.A.W AMM 53-01-06-400-801 REV.149 INSTALLED THE MAIN DECK FLOOR PANEL. I.A.W AMM 25-57-02-404-16, AMM 25-57-05-404-006 AND AMM 25-58-04-404-015 REV.149 INSTALLED MAIN DECK CAROct 3, 2026 · N364UP · Boeing 767346 · Fuselage Floor PanelSDR IPXA2026100957455Radome · brokenBROKEN COMPOSITE , RADOME EXTERNAL 2 AREA. IAW EO-35385-JIC001, REV 4, INSTALL RADOME BOOT. I.A.W AMM 53-12-01-402-059 REV.149 INSTALL THE NOSE RADOME. CONDITION CHECK NORMAL.Oct 2, 2026 · N364UP · Boeing 767346 · Aerodynamic FairingsSDR IPXA2026081028152Bushing · migratedNR 7 SPOILER ACTUATOR , ROD END BOLT BEARING MIGRATION. REPLACED. IAW CMM:57-70-11 REV.43 REPAIR:2-1 PAGE:601 STEP:3, COMPLETED NEW BUSHING REPLACEMENT OF THE NO.7 SPOILER ACTUATOR ROD END.Aug 5, 2026 · N362UP · Boeing 767346 · SpoilersSDR IPXA2026081028158Bushing · migratedMIGRATION - BUSHING , LT WING T/E OTBD SPOILER NR 1 UPPER. I.A.W AMM 27-61-02-024-001 REV.148 DISCONNECT LT WING NR 1 SPOILER PCA ROD END. IAW CMM 57-70-51, REV.38, REPAIR 2-1, PAGE 601, STEP 2, COMPLETED NEW BUSHING REPLACEMENT OF THE NR 1 SPOILER ACTUATOR Aug 5, 2026 · N362UP · Boeing 767346 · SpoilersSDR IPXA2026080722672Cap · crackedCRACK CAP , L/H WING T/E OUTBD FLAP INBD END CAP. (REPAIR). I.A.W UPS SREO-70175-REQ001 REV. 1 PERFORM REPAIR AS BELOW. REMOVED THE CRACKED MATERIALS AND CLEANED. MEASURED DAMAGE AREA ( L : 1.1", W : 0.1", 6.5" FROM AFT EDGE , AT INBD EDGE ). BOND THE REPAAug 5, 2026 · N362UP · Boeing 767346 · Wing Miscellaneous StructureSDR IPXA2026080903490Bracket · chafedCHAFED BRACKET, NR 1 ENG LT LOWER T/R COWL FWD CLOSURE DOOR T/E ATTACHED. REMOVED DAMAGE BRACKET IAW SRM 51-40-02-0G, REV 55. INSTALLED A NEW BRACKET IAW SRM 51-40-02-0G, REV.55, AND IPC 78-32-21 REV.96.Aug 4, 2026 · N362UP · Boeing 767346 · Engine Thrust ReverserSDR IPXA2026080703836Wedge · damagedRIGHT OUTBOARD FLAP, INBOARD T/E WEDGE UPPER AND LOWER SKIN DAMAGE. (REPAIR). I.A.W UPS SREO-70175-REQ001 REV. 1 PERFORM REPAIR AS BELOW. REMOVED THE CRACK MATERIALS AND CLEANED. MEASURE THE DAMAGE AREA ( L : 0.8", W : 0.05", 6" FROM AFT EDGE , AT INBD EDGEAug 4, 2026 · N362UP · Boeing 767346 · Trailing Edge FlapsSDR IPXA2026081391163Angle · crackedCRACK-ANGLE, BULK CGO OVERHEAD M/D FLOOR BEAM STRUCTURE ATTACHED AT STA 1580 , ADJACENT RBL 70 AREA.(REPLACE) ACCOMPLISHED JOB I.A.W UPS EO-98247-REQ1 REV 1 AND SRM 51-40-02-0G REV.55 AND BOEING DWG:657T1332 SHEET 5 REV: A.Aug 3, 2026 · N362UP · Boeing 767346 · Fuselage Miscellaneous StructureSDR IPXA2026081387667Plate · wornNR 1 STRUT AFT FAIRING,INBOARD SUPPORT STIFFENER LINK PLATE BEARING WORN , BS 376.20. (REPLACE)1 ACCOMPLISHED JOB I.A.W UPS E0-98274-REQ1 REV.1 AND EGAT EI F2026A54M-1622 REV.1 AND SRM 51-40-02-0G REV.55 AND DWG 313T2303, SH.96, REV.C AND DWG 313T2303 SH.99 RAug 3, 2026 · N362UP · Boeing 767346 · Nacelle/Pylon, Main FrameSDR IPXA2026080987685Support · crackedNR 1 STRUT AFT FAIRING, INBD ZEE CRACK , BS 376.20. REMOVED DAMAGE ZEE INBD SEAL IAW SRM 51-40-02-0G, REV.55. INSTALLED NEW ZEE INBD SEAL IAW SRM 51-40-02-0G REV.55 AND DWG 313T2380, SH 48, REV -, DWG 313T2303, SH 92, REV: C, SH 93 REV: C, SH 98 REV B.Aug 3, 2026 · N362UP · Boeing 767346 · Nacelle/Pylon, Main FrameSDR IPXA2026080889776Bracket · chafedCHAFED BRACKET , NR 1 ENG RT T/R COWL LOWER FWD CLOSURE DOOR T/E ATTACHED. REMOVED DAMAGE BRACKET IAW SRM 51-40-02-0G, REV.55. INSTALLED A NEW BRACKET IAW SRM 51-40-02-0G, REV.55 AND IPC 78-32-22, REV 96.Aug 3, 2026 · N362UP · Boeing 767346 · Engine Thrust ReverserSDR IPXA2026080889497Former · crackedRIGHT WING OUTBOARD L/E NOSE FORMER CRACK , OSS 499 (NR 8 SLAT OUTBOARD SEAL DOOR UPPER AREA). REMOVED DAMAGE FORMER IAW SRM 51-40-02-0G, REV 55. INSTALLED A NEW FORMER IAW SRM 51-40-02-0G, REV 55 AND DWG 114T2161, SH 3, REV B, AND SREO-50900-REQ001, REV Aug 3, 2026 · N362UP · Boeing 767346 · Wing Main, Frame StructureSDR IPXA2026080789540Skin · debondedDISBOND - SKIN , LT WING T/E OUTBD FLAP INBD LWR. (REPAIR). IAW SRM 57-53-01-2R-1 REFER TO SRM 51-70-07-0G-0 REV.55. PERFORM REPAIR AS BELOW STEP:1.1 REMOVED THE DISBOND MATERIALS AND CLEANED. MEASURE THE DAMAGE SIZE AND LOCATION (L:4.5", W:2", 1.3" FROM AFAug 3, 2026 · N362UP · Boeing 767346 · Trailing Edge FlapsSDR IPXA2026080877850Channel · crackedCRACKED CHANNEL, NR 1 PYLON RT AFT FAIRING TRAILING EDGE NUTPLATE BRACKET. (REPLACE) REMOVED DAMAGE CHANNEL IAW SRM 51-40-02-0G, REV.55. FABRICATE CHANNEL (P/N: 313T2380-741) IAW DWG 313T2380, SH 57, REV-; PL REV BJ; PSDL REV C AS A SAMPLE IAW GMM-MTX CH 9.08Aug 2, 2026 · N362UP · Boeing 767346 · Nacelle/Pylon Miscellaneous StructureSDR IPXA2026080875370Angle · crackedCRACK - ANGLE, BULK CGO COMPT CEILING AREA, BS 1577, LBL 74 OUTBD SIDE. (REPLACE). REMOVED DAMAGE ANGLE IAW SRM 51-40-02-0G, REV.55. INSTALL NEW ANGLE I.A.W SRM 51-40-02-0G REV.55 AND BOEING DWG NO. 657T1332 SH 5 REV: A .Aug 2, 2026 · N362UP · Boeing 767346 · Fuselage Miscellaneous StructureSDR IPXA2026080875315Angle · crackedCRACKED ANGLE, BULK CGO COMPT CEILING AREA, BS 1577, LBL 74 INBD SIDE. (REPLACE) FABRICATE ANGLE IAW DWG 657T1338 SH 3 REV-; PL REV.- AS A SAMPLE IAW GMM-MTX 9.08, REV: 17 REQUIREMENT. INSTALLED FABRICATED ANGLE IAW SRM 51-40-02-0G REV.55, AND DWG 657T1332,Aug 2, 2026 · N362UP · Boeing 767346 · Fuselage Miscellaneous StructureSDR IPXA2026081368122Angle · damagedENLARGE HOLE - FITTING, NO.1 PYLON R/H AFT FAIRING DOOR NO.2 HINGE UPPER SIDE CONNECTION. (REPLACE).INSTALL FABRICATE ANGLE (P/N: 313T3310-889) I.A.W SRM 51-40-02-0G REV.55 AND DWG 313T2310 SH 42 REV: B, 313T2310 SH 36 REV: A, 313T2310 SH 38 REV: A.Aug 1, 2026 · N362UP · Boeing 767346 · Nacelle/Pylon Miscellaneous StructureSDR IPXA2026072237841Bracket · chafedCHAFED BRACKET, NR 2 ENG RT CORE COWL OPEN ROD HOLD BRACKET. REMOVED DAMAGE BRACKETS IAW SRM 51-40-02-0G, REV 55. INSTALLED NEW BRACKETS IAW SRM 51-40-02-0G, REV 55, AND CMM IPL 71-13-24, REV 51.Jul 19, 2026 · N363UP · Boeing 767346 · Nacelle/Pylon Miscellaneous StructureSDR IPXA2026072835996Drain Mast · crackedCRACKED MAST, NR 1 ENG LWR DRAIN MAST. IAW AMM 71-71-01-024-001-H00, REV 148, AND AMM 71-71-01-424-005-H00, REV.148, REPLACED THE DRAIN MAST OF NR 1 ENGINE.Jul 19, 2026 · N363UP · Boeing 767346 · Nacelle/Pylon, Main FrameSDR IPXA2026072035996Drain Mast · crackedCRACKED MAST, NR1 ENG LWR DRAIN MAST. (REPLACE)Jul 19, 2026 · N363UP · Boeing 767346 · Engine (Turbine/Turboprop)SDR IPXA2026072422572Skin · crackedCRACKED NR 2 PYLON FAIRING PANEL 447 ELX. ACCOMPLISH THE REPAIR IAW SRM 54-52-70-2R-4, REV 55, AND EGAT WORK SHEET 60557.Jul 18, 2026 · N363UP · Boeing 767346 · Nacelle/Pylon, Plate/SkinSDR IPXA2026072223130Support · crackedCRACKED SUPPORT, LEFT HORIZONTAL STAB BODY SEAL 313CLX LAST ONE FITTING. INSTALLED NEW SUPPORT IAW SRM 51-40-02-0G, REV 55, AND DWG 182T7119, SHT 1, REV D.Jul 18, 2026 · N363UP · Boeing 767346 · Horizontal Stabilizer Miscellaneous StructureSDR IPXA2026072223167Support · crackedCRACK SUPPORT, RIGHT HORIZONTAL STABILIZER BODY SEAL NO.314CRX LAST ONE FITTING. INSTALLED NEW SUPPORT IAW SRM 51-40-02-0G, REV 55, AND DWG 182T7119 SH 1, REV D.Jul 18, 2026 · N363UP · Boeing 767346 · Horizontal Stabilizer Miscellaneous StructureSDR IPXA2026072223255Seal · crackedCRACKED ZEE SEAL, NR 1 PYLON LT AFT FAIRING DOOR CUTOUT LWR, AFT SEAL AREA. INSTALLED FABRICATED ZEE SEAL IAW SRM 51-40-02-0G, REV 55, AND DWG 313T2380, SHT 68, REV A, & DWG 313T2303, SH 90, REV C, & SB 767-54-0109, REV 2.Jul 18, 2026 · N363UP · Boeing 767346 · Nacelle/Pylon, Main FrameSDR IPXA2026072707922Floor Panel · delaminatedTHE FLOOR PANEL IN THE AFT CARGO COMPARTMENT IS DELAMINATED. IAW AMM 53-01-05-404-004, REV 148, INSTALLED THE FLOOR PANEL. CONDITION CHKD NORMAL.Jul 17, 2026 · N363UP · Boeing 767346 · Fuselage Floor PanelSDR IPXA2026072204865Retainer · brokenMISSING ZEE SEAL , NR 2 ENG RT AFT FAIRING LOWER AFT AREA. INSTALLED NEW ZEE SEAL IAW SRM 51-40-02-0G, REV 55, AND DWG NR 313T2380 SH. 68 REV. A.Jul 17, 2026 · N363UP · Boeing 767346 · Nacelle/Pylon Miscellaneous StructureSDR IPXA2026071803780Angle · crackedTHE BULK CARGO INBD ANGLE AT BS 1578, LBL 80 CRACKED. REMOVED DAMAGE ANGLE IAW SRM 51-40-02-0G, REV 55. INSTALLED FABRICATED ANGLE IAW SRM 51-40-02-0G, REV 55, AND DWG 657T1332, SHEET 5, REV A.Jul 17, 2026 · N363UP · Boeing 767346 · Fuselage Miscellaneous StructureSDR IPXA2026071807167Angle · crackedTHE BULK CARGO OUTBOARD ANGLE AT BS 1578 LBL 80 IS CRACKED. INSTALLED NEW ANGLE IAW SRM 51-40-02-0G, REV 55, AND DWG 657T1332, SHT 5, REV A.Jul 17, 2026 · N363UP · Boeing 767346 · Fuselage Miscellaneous StructureSDR IPXA2026072889610Splice Plate · brokenBROKEN SPLICE PLATE, UPPER FACE OF LT WING INBD T/E UPPER FIXED PANEL, WBL 127. INSTALLED NEW SPLICE PLATE IAW SRM 51-40-02-0G, REV 55, AND DWG 113T1900, SHT 1, REV C, AND DWG 113T1603, SHT 1. REV B.Jul 16, 2026 · N363UP · Boeing 767346 · Wing Main, Frame StructureSDR IPXA2026072889321Channel · corrodedLEFT APU DOOR HAS LIGHT CORROSION AT INBD INTERNAL SIDE. ACCOMPLISHED CORROSION DAMAGE REPAIR IAW EO-98128-REQ1, REV1, AND DWG 148T6551, SHEET 3, REV B. JOB COMPLETED.Jul 16, 2026 · N363UP · Boeing 767346 · Auxiliary Power Unit (APU) DoorsSDR IPXA2026072485434Fitting · crackedCRACKED FITTING, NR 1 ENG LT T/R FWD TORQUE BOX UPR ACTUATOR FITTING CRACK. INSTALLED NEW FITTING IAW SRM 51-40-02-0G, REV 55, AND IPC 78-32-21, REV 96.Jul 16, 2026 · N363UP · Boeing 767346 · Engine Thrust ReverserSDR IPXA2026072289584Beam · crackedCRACKED BEAM, NR 2 ENG RT AFT FAIRING LOWER BEAM AFT AREA. NSTALLED NEW BEAM IAW SRM 51-40-02-0G, REV 55, SB 767-54-0109, REV 1, DWG 313T2380, SHT 88, REV A, DWG 313T2303, SHT 90, REV C, DWG 313T2303, SHT 94, REV C, & DWG 313T2303, SHT 95, REV C.Jul 16, 2026 · N363UP · Boeing 767346 · Nacelle/Pylon Miscellaneous StructureSDR IPXA2026072051088Battery Pack · no testFOUND EMERGENCY BATTERY PACK FAILED TO ILLUMINATE FOR 15 MINUTES. IAW AMM 33-51-07-022-001, AND 33-51-07-422-012, REV 148. REPLACED EMERGENCY LIGHT BATTERY PACK.Jul 14, 2026 · N363UP · Boeing 767346 · Emergency LightingSDR IPXA2026071551088Battery Pack · inoperativeFOUND EMERGENCY BATTERY PACK FAILS TO ILLUMINATE FOR 15 MINUTES. (REPLACE).Jul 14, 2026 · N363UP · Boeing 767346 · Emergency LightingSDR IPXA2026070190225Cowling · crackedNR 1 ENG INLET COWL LIP CRACKED BETWEEN 11 AND 1 O'CLOCK POSITIONS. INSTALLED NR 1 ENGINE INLET COWL IAW AMM 71-11-01.Jun 27, 2026 · N362UP · Boeing 767346 · Nacelle/Pylon, Main FrameSDR IPXA202606290225Skin · crackedNR 1 ENG INLET COWL LIP CRACKED BETWEEN 11 AND 1 O'CLOCK POSITIONS REMOVED #1 ENGINE INLET IAW AMM 71-11-01Jun 27, 2026 · N362UP · Boeing 767346 · Nacelle/Pylon, Plate/SkinSDR IPXA2026062280159Battery · inoperativeEMERGENCY LIGHTS BATTERY DEPLETED. EMERGENCY LIGHTS BATTERY REPLACED BY SERVICEABLE. IAW AMM 33-51-07/401 REV 148. OPERATIONAL TEST C/O O.K.Jun 21, 2026 · N362UP · Boeing 767346 · Emergency LightingSDR IPXA2026061535378Skin · debondedFAULT - DISBOND - SKIN , INBD EDGE OF L/H WING T/E OUTBD FLAP T/E UPPER SKIN , WBL 355. I.A.W CMM 57-53-51 REV 39 REMOVE THE RETAINER AND SEAL. REMOVE THE DISBOND MATERIALS AND CLEAN. BOND THE REPAIR PLIES WITH RESIN CURED AT 200°F FOR 220 MINUTES WITH MINIMUJun 6, 2026 · N397UP · Boeing 767346 · Trailing Edge FlapsSDR IPXA2026061235691Skin · debondedFAULT - DEBONDED SKIN , LOWER FACE OF LT WING T/E OTBD FLAP WEDGE LOWER SKIN , WS 663. IAW SRM 57-53-01-2R-1 REFER TO SRM 51-70-06-0G-0 REV. 55 PERFORM REPAIR AS BELOW STEP : 1.REMOVE THE DISBOND MATERIALS AND CLEAN. MEASURE THE DAMAGE SIZE AND LOCATION ( DIJun 6, 2026 · N397UP · Boeing 767346 · Trailing Edge FlapsSDR IPXA2026061235713Skin · debondedDEBONDED SKIN , FORWARD FACE OF LT WING T/E OUTBD FLAP L/E SKIN , WBL 420. REMOVE THE DISBOND MATERIALS AND CLEAN. MEASURE THE DAMAGE SIZE AND LOCATION ( DIA : 1", 5.4" FROM LOWER EDGE, 67" FROM INBD EDGE ). BONDED THE REPAIR PLIES WITH RESIN CURED AT 150°F FJun 6, 2026 · N397UP · Boeing 767346 · Trailing Edge FlapsSDR IPXA2026040281014Apu · inoperativeEMERGENCY DECLARED DESCENDING THRU APPROXIMATELY 11000, APT FAULTS, APU AUTO SHUTDOWN RESULTING IN SINGLE ELECTRICAL SOURCE. RAN QRT ,APU CAME BACK UP ONLINE. PREVIOUS RESET APU GENERATOR SO WE DID NOT ATTEMPT A SECOND PER FIM 24-20 TASK 805, REPLACED APU GCU Apr 1, 2026 · N396UP · Boeing 767346 · APU Core EngineSDR IPXA2026030569928Pawl · inoperativeFOUND CREW ENTRY DOOR EXTERNAL HANDLE PAWL DAMAGED. IAW AMM 52-11-26-004-001, REV 147, AND AMM 52-11-26-404-003, REV 147, REPLACED THE CREW ENTRY DOOR EXTERNAL HANDLE PAWL.Feb 6, 2026 · N396UP · Boeing 767346 · Passenger/Crew DoorsSDR IPXA202602069928Pawl · damagedFOUND CREW ENTRY DOOR EXTERNAL HANDLE PAWL DAMAGED. (REPLACE) OPENFeb 6, 2026 · N396UP · Boeing 767346 · Passenger/Crew Doors
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