Boeing 767-323

Service difficulty reports · 8,544

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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 = '767323'
  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 NACA2022010400003Control Unit · unknownREPLACE WINDOW HEAT CONTROL UNIT RH SIDE. REMOVED AND REPLACED RH M-192 WINDOW HEAT CONTROL UNIT OPS CHECK GOOD. REF B767 AMM 30-4101. PART IS DTO POOL AND HAS BEEN EXCHANGED OUT, NO HOUR INFO AVAILABLE.Jan 4, 2022 · N399CM · Boeing 767323 · Windshield/Door Rain/Ice RemovalSDR NACA2022010400002Not Reported · not reportedAPU AUTOSHUTDOWN DURING TOWING. ACCOMPLISHED ECU TEST, NO FAULTS. APU TESTS OK IAW AMM 49-61-05Jan 4, 2022 · N351CM · Boeing 767323 · APU Cowling/ContainmentSDR NACA2021010400001Not Reported · not reportedAPU WOULD NOT START AFTER LANDING IN MIA - FAULT LIGHT, TRIED TWICE. PERFORMED FIM 49-11 FAULT TREE 958, NO FAULTS APPEAR ON TEST.Jan 4, 2022 · N379CX · Boeing 767323 · APU Cowling/ContainmentSDR NACA2022010300006Not Reported · not reportedIDLE DISAGREE AFTER LANDING. CORRECTIVE ACTION SAME AS NACA2022010300005: FOUND PRV CONTROLLER SENSE LINE CHAFING, REMOVED AND REPLACED PRV CONTROLLER SENSE LINE IAW AMM 20-10-01 AND OPS CHECK NORMAL IAW AMM 78-31-00Jan 3, 2022 · N379CX · Boeing 767323 · Pneumatic Distribution SystemSDR NACA2022010300005Not Reported · not reportedRIGHT REVERSER DID NOT STOW AFTER LANDING. NOTE: RTL WOULD NOT ADVANCE FORWARD AFTER LANDING. REVERSER LIGHT WAS GREEN AND ONLY WHEN IT BECAME AMBER DID TL ADVANCE FAILED. FOUND PRV CONTROLLER SENSE LINE CHAFING, REMOVED AND REPLACED PRV CONTROLLER SENSE LINE Jan 3, 2022 · N379CX · Boeing 767323 · Pneumatic Distribution SystemSDR NACA2022010300004Not Reported · not reportedRIGHT DUCT PRESSURE @5 PSI, LEFT @ 20 PSI. PERFORMED FIM 78-34 FAULT TREE 810 AND FOUND NORMAL.Jan 3, 2022 · N379CX · Boeing 767323 · Pneumatic Distribution SystemSDR NACA2022010300003Not Reported · not reportedAPU FAULT ON START IN MIA. FIM 49-11 FAULT TREE 958 NO FAULTS, TESTS OKJan 3, 2022 · N379CX · Boeing 767323 · APU Cowling/ContainmentSDR NACA2022010300002Not Reported · not reportedLEFT AFT FUEL PUMP STUCK ON INTERMITTENT. PERFORMED OPS CHECK PER AMM 28-22-00, NO FAULTS NOTED. OK FOR ETOPS 180Jan 3, 2022 · N321CM · Boeing 767323 · Fuel Boost PumpSDR NACA2022010300001Valve · unknownLEFT ENG TAI VALVE (SIC). REPLACED LEFT ENGINE TAI VALVE PER AMM 30-21-03, BOTH OPS AND LEAK CHECKS OK. AC REMAINS ETOPS 180. DTO POOL PART EXCHANGED OUT, NO HOURS INFORMATION IN SYSTEM.Jan 3, 2022 · N399CM · Boeing 767323 · Air Intake Anti/De-Ice SystemSDR MK1Y202201025None · noneTHE ENGINEERING ORDER PROVIDES DETAILED INSTRUCTIONS FOR THE REPAIR OF THE FUSELAGE MAIN FRAME INNER CHORD TRANSITION RADII LOCATED ON THE RIGHT SIDE OF B767-300 AIRCRAFT THAT HAVE TYPE III OVER WING EXIT DOOR. RHE REPAIRS ARE DEFINED FOR THE AIRPLANES IDENTIJan 2, 2022 · N396AN · Boeing 767323 · Fuselage Structure (General)SDR MK1Y202201024None · noneTHE ENGINEERING ORDER PROVIDES DETAILED INSTRUCTIONS FOR THE REPAIR OF THE FUSELAGE MAIN FRAME INNER CHORD TRANSITION RADII LOCATED ON THE LEFT SIDE OF B767-300 AIRCRAFT THAT HAVE TYPE III OVER WING EXIT DOOR. RHE REPAIRS ARE DEFINED FOR THE AIRPLANES IDENTIFJan 2, 2022 · N396AN · Boeing 767323 · Fuselage Structure (General)SDR MK1Y202201023None · noneDENT DAMAGE AND AN EXISTING BLEND-OUT WAS FOUND ON THE LOWER WING SKIN PANEL (P/N 112T4702-1) COMMON TO THE OUTBOARD STRINGER L-9.5 (P/N 767-3421-7) BETWEEN WS 990.2 AND WS 1006. AN EXISTING FREEZEPLUG AND THE OUTBOARD STRINGER L-9.5 HAD BEEN INSTALLED PER SERJan 2, 2022 · N396AN · Boeing 767323 · Wing StructureSDR MK1Y202201022None · nonePROBLEM DESCRIPTION: ENGINE #2, THRUST REVERSER TRANSLATING COWL, INNER SKIN, P/N CF6-F23G019, S/N R647-129: DURING MAINTENANCE INSPECTION AT IAI A CRACKED DENT WAS FOUND IN THE INNER SKIN OF INBD THRUST REVERSE IN CLOSE PROXIMITY TO AN EXISTING REPAIR OF ENJan 2, 2022 · N396AN · Boeing 767323 · Engine Thrust ReverserSDR MK1Y202201021None · noneR/H WING, UNDERSIDE, MAIN FUEL TANK, FUEL BOOST PUMP HOUSING, WS 226.3 – WS 255.4, P/N 50060050: DURING MAINTENANCE INSPECTION AT IAI, CORROSION WAS FOUND ON THE INNER FACE OF THE BOOST PUMP HOUSING AFTER REMOVING THE AFT FUEL BOOST PUMP SHUTOFF SLEEVE.Jan 2, 2022 · N396AN · Boeing 767323 · Fuel Boost PumpSDR MK1Y202201020None · noneL/H WING, UNDERSIDE, MAIN FUEL TANK, FUEL BOOST PUMP HOUSING, WS 226.3 – WS 255.4, P/N 50060050: DURING MAINTENANCE INSPECTION AT IAI, CORROSION WAS FOUND ON THE INNER FACE OF THE BOOST PUMP HOUSING AFTER REMOVING THE AFT FUEL BOOST PUMP SHUTOFF SLEEVE.Jan 2, 2022 · N396AN · Boeing 767323 · Fuel Boost PumpSDR MK1Y202201019None · nonePROBLEM DESCRIPTION: SLAT NO. 4, OSS 579.05: SHOP FOUND A DENT ADJACENT TO A BULGE IN UPPER LE SKIN OF SLAT NO. 4. THE DAMAGED AREA LOCATED ON A RIB AND STIFFENER. SLAT: P/N 114T4104-203G; S/N 000010.Jan 2, 2022 · N396AN · Boeing 767323 · Wing StructureSDR MK1Y202201018None · noneFUSELAGE SKIN (SEC 45), STA 999 AND STA 1043, STR-2L AND STR-2R: DURING CONVERSION PROCESS, AIRCRAFT MAINTENANCE WAS REQUIRED TO DEACTIVATE AND REMOVE THE HIGH GAIN SATCOM SYSTEM PER CUSTOMER REQUEST THAT WAS INSTALLED BY THE PREVIOUS OPERATOR. THE LARGE EXTERJan 2, 2022 · N396AN · Boeing 767323 · Fuselage Structure (General)SDR MK1Y202201017None · nonePROBLEM DESCRIPTION: SLAT NO 5 AT OSS 389.71: SHOP FOUND DENT AMONG FASTENERS AT THE EDGE OF SLAT LE SKIN ATTACHMENT COMMON TO A RIB. THE REPORTED DAMAGE WAS FOUND SMOOTH WITHOUT SHARP EDGES OR LOOSE FASTENERS.Jan 2, 2022 · N396AN · Boeing 767323 · Wing StructureSDR MK1Y202201016None · noneHORIZONTAL STABILIZER, CENTER SECTION, UPPER SKIN, REAR SPAR – AT RBL10.33 STR U3 TO REAR SPAR: DURING MAINTENANCE INSPECTION AT IAI, CORROSION WERE FOUND.THE CORROSION WAS REMOVED AS PER SRM 51-20-01.THE SKIN REMAINING MATERIAL THICKNESS WAS ACCOMPLISHED. THEJan 2, 2022 · N396AN · Boeing 767323 · Empennage StructureSDR MK1Y202201015None · noneHORIZONTAL STABILIZER, CENTER SECTION, UPPER SKIN, REAR SPAR – AT LBL10.83 STR U3 TO U2 AND LBL 11.83 STR U2 TO U1: DURING MAINTENANCE INSPECTION AT IAI, CORROSION WERE FOUND.THE CORROSION WAS REMOVED AS PER SRM 51-20-01.THE SKIN REMAINING MATERIAL THICKNESS WJan 2, 2022 · N396AN · Boeing 767323 · Empennage StructureSDR MK1Y202201014None · noneHORIZONTAL STABILIZER, CENTER SECTION, UPPER SKIN, REAR SPAR – AT RBL10.33 STR U1 TO REAR SPAR: DURING MAINTENANCE INSPECTION AT IAI, CORROSION WERE FOUND.THE CORROSION WAS REMOVED AS PER SRM 51-20-01.THE SKIN REMAINING MATERIAL THICKNESS WAS ACCOMPLISHED. THEJan 2, 2022 · N369AN · Boeing 767323 · Empennage StructureSDR MK1Y202201013None · nonePROBLEM DESCRIPTION: #2 ENGINE OUTBOARD THRUST REVERSER DAGMAR FAIRING DAMAGE, ASSY IDENT: 683L136613, MODEL NO. TR-CF6-F23G019, S/N R647-129: DURING MAINTENANCE INSPECTION AT IAI, MAINTENANCE DISCOVERED ELONGATED HOLES SUNK RIVETS AND GOUGES ACROSS THE FASTJan 2, 2022 · N396AN · Boeing 767323 · Engine Thrust ReverserSDR MK1Y202201012None · noneENGINE #1 OUTBD CORE COWL HAT FRAME NAC STA 303.75, LOWER AREA: DURING THE MAINTENANCE INSPECTION AT IAI, CRACK WAS FOUND AT DATUM LOCATION WITH 1.5 INCH LENGTH.Jan 2, 2022 · N396AN · Boeing 767323 · Powerplant SystemSDR MK1Y202201011Tear Strap · corrodedTEAR STRAP, INNER SKIN, STA 544, S-1R AND S-4R, DOOR SURROUND ZONE: SHOP DISCOVERED DEEP CORROSION ON TEAR STRAP EDGE COMMON TO S-2R (LAP SPLICE). THE DAMAGED AREA IS LOCATED IN CONVERSION INSTALLATION ZONE.Jan 2, 2022 · N396AN · Boeing 767323 · Fuselage Main, Plate/SkinSDR MK1Y202201010None · nonePROBLEM DESCRIPTION: R/H WING LOWER SKIN SURFACE BETWEEN WS.994.7 AND WS.1001.7: SHOP FOUND TOOL MARK AMONG FASTENERS, PAINT STRIPPED AND PERFORMED NDT THICKNESS INSPECTION WAS PERFORMED .Jan 2, 2022 · N396AN · Boeing 767323 · Wing StructureSDR MK1Y202201009None · noneWORN CORE COWL ALUMINUM HAT FRAME – ENGINE# 1, R/H CORE COWL, HAT FRAME, NAC STA 303.75, UPPER AREA DURING THE MAINTENANCE INSPECTION AT IAI, MAINTENANCE DISCOVERED ON #1 ENGINE, R/H CORE COWL HAT CHANNEL FRAME NAC STA 303.75 UPPER SECTION WITH WORN, DAMAJan 2, 2022 · N396AN · Boeing 767323 · Powerplant SystemSDR MK1Y202201008None · none. DURING A/C SURVEY AT TLV, MAINTENANCE DISCOVERED EXISTING BLENDOUT AT THE EDGE OF AN EXISTING FLUSH REPAIR CUTOUT LOCATED ON THE FUSELAGE SKIN AT STA 616 BETWEEN S38L AND S39L. THE EXISTING FLUSH REPAIR WAS FOUND TO BE INSTALLED BY THE PRIOR OPERATOR, AMERIJan 2, 2022 · N396AN · Boeing 767323 · Fuselage Structure (General)SDR MK1Y202201007None · noneENGINE # 2, LH CORE COWL, HAT FRAME, NAC STA 303.75, MID LOWER AREA: DURING MAINTENANCE INSOECTION AT IAI, MAINTENANCE DISCOVERED ON #2 ENGINE, LH CORE COWL HAT CHANNEL FRAME NAC STA 303.75 MID LOWER SECTION WITH CRACK AND GOUGE. PLEASE REFER TO FIGURE 2 FOR TJan 2, 2022 · N396AN · Boeing 767323 · Engine Cowling SystemSDR MK1Y202201006None · noneNLG SUPPORT STRUCTURE, AFT VERTICAL STIFFENERS, UPPER EDGES, STA 287, L/RBL 13.10 DURING THE MAINTENANCE INSPECTION AT IAI, TWO CRACKS WERE FOUND AT DATUM LOCATIONS WITH 0.6 INCH LENGTH EACH ONE. THERE IS NO APPLICABLE DAMAGE EXISTING. VERTICAL STIFFENERS PIJan 2, 2022 · N396AN · Boeing 767323 · Fuselage Structure (General)SDR MK1Y202201005None · noneEXTERNAL FUSELAGE SKIN, STA 1487, STR-21L & STA 1460, STR-29L-STR-30L: DURING THE MAINTENANCE INSPECTION AT IAI, SCRATCHES WERE FOUND AND BLENDED OUT PER SRM 51-10-02. THE BLEND OUTS EXCEED\ THE SRM 51-00-01, AD1, DETAIL II, THE FASTENERS ARE INSIDE THE AFFEJan 2, 2022 · N396AN · Boeing 767323 · Fuselage Structure (General)SDR MK1Y202201004None · noneEXTERNAL FUSELAGE SKIN, STA 308, STR-33L: DURING THE MAINTENANCE INSPECTION AT IAI, A SCRATCH WAS FOUND AND BLENDED OUT PER SRM 51-10-02. THE BLEND OUT EXCEEDS THE SRM 51-00-01, AD1, DETAIL II, THE FASTENERS ARE INSIDE THE AFFECTED AREA.Jan 2, 2022 · N396AN · Boeing 767323 · Fuselage Structure (General)SDR MK1Y202201003None · noneEXTERNAL FUSELAGE SKIN, STA 588, STR-33R: DURING THE MAINTENANCE INSPECTION AT IAI, A SCRATCH WAS FOUND AND BLENDED OUT PER SRM 51-10-02. THE BLEND OUT EXCEEDS THE SRM 51-00-01, AD1, DETAIL II, THE FASTENERS ARE INSIDE THE AFFECTED AREA.Jan 2, 2022 · N396AN · Boeing 767323 · Fuselage Structure (General)SDR MK1Y202201002None · noneFAN COWL SUPPORT BEAM LINK, #2 PYLON, P/N 31112522-1 DURING THE MAINTENANCE INSPECTION AT IAI, THE BORES IN THE #2 PYLON FAN COWL SUPPORT BEAM LINK PIN 311T2522-1 WERE FOUND TO BE WORN. THE BORE DIAMETERS WERE FOUND TO BE Ø.8770". THE NOMINAL DIAMETER OF THEJan 2, 2022 · N396AN · Boeing 767323 · Nacelle/Pylon StructureSDR MK1Y202201001None · nonePROBLEM DESCRIPTION: DURING THE MAINTENANCE INSPECTION FOUND SCRATCHES ON EXTERNAL FUSELAGE SKIN AMONG FASTENERS AREA. - SHOP CLEANED DAMAGED AREA IAW SRM 51-10-02. SHOP REMOVEDJan 2, 2022 · N396AN · Boeing 767323 · Fuselage Structure (General)SDR NACA2021123100001Not Reported · not reportedAPU SHUTDOWN AFTER PARKING SDQ. ACCOMPLISHED FIM 49-11 FAULT TREE 958, RESET ECU AND APU OPS CHECK NORMAL PER AMM 49-11-00Dec 31, 2021 · N351CM · Boeing 767323 · APU Cowling/ContainmentSDR NACA2021122900001Not Reported · not reportedAPU FAULT ON START IN MIA. ACCOMPLISHED FIM 49-11 FAULT TREE 958, NO FAULTS NOTED. RESET ECU APU OPS CHECK NORMAL AT THIS TIME PER AMM 49-11-00Dec 29, 2021 · N379CX · Boeing 767323 · APU Cowling/ContainmentSDR IXXA20220102001Proximity Switch · intermittentDURING DAILY SERVICE CHECK, LINE MAINTENANCE IDENTIFIED EMERGENCY DOOR DISCRETE LIGHT FLICKERING. SYSTEM DEFERRED-MEL CAT C. REMOVED AND REPLACED PROX SWITCH ELECTRONIC UNIT IAW AMM 32-09-04. OPERATIONAL CHECK SATISFATORY. FAULT NOT DUPLICATED. DEFERRAL 27916Dec 29, 2021 · N251AZ · Boeing 767323 · Emergency LightingSDR NACA2021122800001Unknown · unknownRIGHT ENGINE FAN VIBE PEAKS AT 3.3 ON CLIMBOUT. PERFORMED VISUAL INSPECTION RIGHT ENGINE INLET FAN BLADE AND EXHAUST IAW B767 AMM 72-00-00, FOUND TO BE WITHIN LIMITS. FAN BLADE LUBE SCHEDULED.Dec 28, 2021 · N379CX · Boeing 767323 · Engine Vibration AnalyzerSDR NACA2021122500001None · noneSUPPLEMENTAL INFORMATION. ALL ASSOCIATED WIRING FOR LH EEC WDM 73-21-11 AND 73-21-13 WERE WRUNG OUT AND INSPECTED IAW 20-10-39. A SHAKEDOWN OF THE ASSOCIATED WIRING WAS ACCOMPLISHED IAW 20-80-24. EXTREME MOISTURE AND DIRT WERE FOUND IN BOTH J1 AND J2 CONNECTORDec 25, 2021 · N321CM · Boeing 767323 · Engine Fuel Indicating SystemSDR NACA2021122400003None · noneRIGHT ENGINE FAN BLADE #19 HAS A SMALL DENT 2 INCH APPROX FROM TIP. BLENDED RIGHT ENGINE FAN BLADE 19 @ 2" APPROX FROM TIP AND FOUND WITHIN LIMITS IAW B767 AMM 72-31-02. DENT WAS 2 MM X .25 MM. NDT ACCOMPLISHED WITH NO FAULTS FOUND.Dec 24, 2021 · N351CM · Boeing 767323 · Turbine Engine Air Inlet SectionSDR NACA2021122400002None · noneRIGHT ENGINE FAN BLADE #18 HAS A SMALL DENT 6 IN APPROX FROM TIP. BLENDED RIGHT ENGINE FAN BLADE 18 AND FOUND WITHIN LIMITS IAW B767 AMM 72-31-02. DENT WAS 2 MM X 0.5 MM. NDT INSPECTION ACCOMPLISHED, NO FAULTS NOTED.Dec 24, 2021 · N351CM · Boeing 767323 · Turbine Engine Air Inlet SectionSDR NACA2021122400001None · noneLEFT ENGINE ANTI-ICE EICAS MESSAGE. ACTUAL EICAS MSG L ENG TAI VALVE. PERFORMED FIM 30-21 FAULT TREE 805, MSG CLEARED. OPS CHECK GOOD, NO FAULT FOUND. AC REMAINS ETOPS 180Dec 24, 2021 · N321CM · Boeing 767323 · Air Intake Anti/De-Ice SystemSDR NACA2021122300001None · noneLEFT ENGINE # 28 BLADE HAS BLEND. INSPECTED AND FOUND # 28 BLADE WITHIN LIMITS IAW B767 AMM 72-00-000Dec 23, 2021 · N379CX · Boeing 767323 · Turbine Engine Air Inlet SectionSDR NACA2021122100001None · noneAPU FAILED FIRST TWO START ATTEMPTS IN SMJP. PERFORMED FIM 49-11 FT 958, RESET ECU APU OPS CHECK NORMAL IAW AMM 49-11-00Dec 21, 2021 · N379CX · Boeing 767323 · APU Cowling/ContainmentSDR 2021FA0000415Pressure Switch · disconnectedDURING INSPECTION OF THE CARGO FIRE BOTTLE IT WAS IDENTIFIED THE PRESURE SENSING SWITCHES WERE NOT INSTALLED AS PER AMM INSTRUCTION. THE PRESSURE SENSING SWITCHES WERE FOUND DISCONNECTED FROM THEIR CORRECT INSTALLED POSIITONS.Dec 21, 2021 · N342AN · Boeing 767323 · Fire Bottle, FixedSDR 2021FA0000414None · noneDURING A FWD ENTRY DOOR CLOSING OPERATION TASK, THE VIEWING WINDOW/PRISM WAS IDENTIFIED NOT INSTALLED CORRECTLY PER AMM. THE VIEWING WINDOW/PRISM WAS DISLODGED FROM ITS CORRECT INSTALLED POSITION AND THE RETAINING HARDWARE IDENTIFIED AS NOT WITHIN AMM REQUIREDDec 21, 2021 · N342AN · Boeing 767323 · DoorsSDR NACA2021122000001None · noneLH AC PACK CONNECTOR ASSY SEALS WORN. REMOVED AND REPLACED LH AC PACK CONNECTOR ASSY SEAL IAW AMM 36-11-01, NO LEAKS NOTED.Dec 20, 2021 · N351CM · Boeing 767323 · Pneumatic Distribution SystemSDR NACA2021121900002None · noneAPU FAULT AFTER LANDING. PERFORMED FIM 49-11 F/T 958. RESET APU ECU, APU OPS CHECK NORMAL IAW AMM 49-11-00Dec 19, 2021 · N379CX · Boeing 767323 · APU Cowling/ContainmentSDR NACA2021121900001None · noneLEFT ENGINE PRV EICAS STATUS MESSAGE ILLUMINATED IN FLIGHT. PERFORMED EICAS MSG ERASE PROCEDURE PER AMM 31-41-00. L ENG PRV STATUS MESSAGE CLEARED. PERFORMED AIR SUPPLY STATUS BITE PER AMM 36-23-00, FOUND L PRV WIRE FAULT. REPLACED K/46 AIR/GROUND RELAY. AIR BDec 19, 2021 · N399CM · Boeing 767323 · Pneumatic Distribution SystemSDR NACA2021121800002None · none3 APU START ATTEMPTS IN KMIA EACH ENDED IN APU FAULT STATUS MESSAGE. PERFORMED FIM 49-11 RESET ECU MESSAGES AND PERFORMED APU OPS CHECK IAW AMM 49-11-00. APU CHECKED NORMAL.Dec 18, 2021 · N379CX · Boeing 767323 · APU Cowling/Containment
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