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 IXXA2022090401None · gouged#1 ENG. I/B CORE COWL #2 RIB FROM AFT HAS GOUGE. 00-114 REF VT-SAA NR B000315Jul 27, 2022 · N227AZ · Boeing 767323 · Nacelle/Pylon StructureSDR IXXA2022090404Stiffener · worn#2 ENG INBD PYLON ACCESS PANEL AFT LANDING 434AL WORNJul 26, 2022 · N227AZ · Boeing 767323 · Nacelle/Pylon StructureSDR NACA2022072600001Skin Panel · dentedDURING WALKAROUND FOUND DENT ON RH SIDE OF FUS BETWEEN STA 1439-1461, STRINGERS BETWEEN S-24 AND S-25, LENGTH 22.750" WIDTH 2.250 AND DEPTH 0.234. REPAIR ACCOMPLISHED PER NAC EO 767-53-0026Jul 26, 2022 · N351CM · Boeing 767323 · Fuselage Main, StructureSDR IXXA20220903001None · chafed#2 ENG UPPER PYLON LANDIN FOR FAIRING 441AT HAS AREAS OF CHAFFING. 18-027Jul 25, 2022 · N227AZ · Boeing 767323 · Nacelle/Pylon StructureSDR IXXA20220802801Channel · cracked#2 AFT STRUT OUTBD J CHANNEL CRACKED AT 2 PLACES AT APPROX NAC 400.18-003 REF VT-SAA RN B000365 ATI-54-822-00-02Jul 25, 2022 · N227AZ · Boeing 767323 · Nacelle/Pylon StructureSDR IXXA2022090305None · crackedMEC ACCESS DOOR FWD EDGE IS DAMAGED IN 3 AREAS 49-012 REF VT-SAA NR B000056Jul 22, 2022 · N227AZ · Boeing 767323 · DoorsSDR NACA2022072200002Eicas · fault messageAFTER SHUTDOWN OF LEFT PACK, LEFT PACK OFF LIGHT AND EICAS MSG DOES NOT COME ON. FOUND CONNECTOR D-2770 LOOSE AND TIGHTENED SAME. PACK OPS NORMAL IAW AMM 21-51-00. ETOPS GROUND VERIFICATION COMPLETE.Jul 22, 2022 · N379CX · Boeing 767323 · Cabin Cooling SystemSDR IXXA20220725124Connector · detachedENROUTE, AUTOTHROTTLE DISCONNECTED ON CLIMBOUT AT 340. RT THROTTLE POPPED 1 DEGREE BACK. RT THROTTLE WOULD NOT RETARD BELOW 93.3, N1. THROTTLE WOULD MOVE BUT INDICATOR DIDN`T. RT ENG SHUTDOWN, EMERGENCY DECLARED. LANDED UNEVENTFUL. ACFT GROUNDED. RT ENG Jul 21, 2022 · N379AZ · Boeing 767323 · Engine Bleed Air System WiringSDR NACA2022072000002Engine · nickedCREW COMMENT #1 ENGINE BLADE #16 HAS A SMALL NICK APPROX 2" FROM BLADE TRIP. BLENDED SMALL NICK ON #1 ENGINE BLADE #16 APPROX 2" FROM TIP IAW B767 72-31-02, BLADE WITHIN SERVICEABLE LIMITSJul 20, 2022 · N351CM · Boeing 767323 · Engine (Turbine/Turboprop)SDR NACA2022072000001Eicas · fault messageL ENG PRV EICAS MESSAGE ON ENGINE START IN GATES @ MIA. REMOVED AND REPLACED LEFT ENGINE PRV IAW B767 AMM 36-11-18, AWAITING OPS CHECK AND LEAK CHECK SEE ITEM M-2 (GOOD). ETOPS GROUND VERIFICATION COMPLIED WITH.Jul 20, 2022 · N351CM · Boeing 767323 · Pneumatic Distribution SystemSDR IXXA20220804001Flap · crackedDENT ON LH IND FLAP 59.5 FROM INBD EDGE AND 44.5 FORM TRAILING EDGE. VT-SAA NR B000038Jul 19, 2022 · N227AZ · Boeing 767323 · Trailing Edge FlapsSDR NACA2022071100001Cowl Door · damagedRH ENGINE OB CORE COWL DUCT PRECOOLER EXIT DAMAGE. REMOVED AND REPLACED RH ENGINE OUTBOARD CORE COWL IAW AMM 71-11-06 PART INFO PENDING CHECK DOCUMENTATIONJul 11, 2022 · N351CM · Boeing 767323 · Engine Cowl FlapsSDR NACA2022071000002Blades · abnormalRH ENGINE #4 AND #6 BLADES WITH A NICK NEAR THE TIP. BLENDED RH ENGINE BLADE #6 BLADE WITHIN LIMITS IAW B767 AMM 72-31-02. DEFERRED DMI 72-31-02 ROUTINE SLIP TO MOC ACCOMPLISHMENT OF FPI WITHIN 50 FLIGHT HOURS, DUE TAT 107288@1447 7-10-22Jul 10, 2022 · N379CX · Boeing 767323 · Powerplant SystemSDR NACA2022071000001Apu · inoperativeAPU DOOR STATUS MESSAGE. PERFORMED MULTIPLE STARTS AND SHUTDOWNS, APUR OBSERVED TO OPERATE NORMAL PER FIM 49-11 FT 959, AND NO MESSAGES WERE OBSERVED, APU CHECKED NORMAL PER AMM 49-11-00Jul 10, 2022 · N351CM · Boeing 767323 · Fuselage Main, StructureSDR NACA2022070800001Eicas · fault messageR ENGINE HPSOV EICAS MESSAGE ON DESCENT. DEFERRED RIGHT ENGINE HPSOV PER MEL 36-11-02-02 CAT C @ 0730Z 8 JUL 22 MX PROCEDURES COMPLIED WITHJul 9, 2022 · N399CM · Boeing 767323 · Pneumatic Distribution SystemSDR NACA2022070900003Apu · fault messageAPU FAULT. ITEM PLACED ON MEL 49-11-01A CAT C 1503ZJul 9, 2022 · N321CM · Boeing 767323 · APU Cowling/ContainmentSDR NACA2022070900002Cowling · damagedACOUSTICAL LINER SEGMENT DAMAGED ON RIGHT HAND ENGINE @ 2 OCLOCK POSITION. DEFERRED ACOUSTICAL SEGMENT PER DMI 72-00 PER AMM 72-00-00 TABLE 645. CONTINUE IN SERVICE FOR 10 FLIGHT CYCLES @ 7/9/22 @ 0120Z.Jul 9, 2022 · N351CM · Boeing 767323 · Engine (Turbine/Turboprop)SDR NACA2022070900001Cowling · damagedACOUSTICAL LINER DAMAGED ON LH ENGINE AT 11 OCLOCK AND 8 OCLOCK POSITION. DEFERRED ACOUSTICAL SEGMENTS PER DMI 72-00 PER AMM 72-00-00 TABLE 645. CONTINUE IN SERVICE FOR 10 CYCLES ON 7/9/22 @ 0100ZJul 9, 2022 · N351CM · Boeing 767323 · Engine (Turbine/Turboprop)SDR IXXA2022082602Stiffener · elongated#2 AFT STRUT INTERIOR AT APPROX NAC 400 OUTBD STIFFENER HAS BOLTS WORN THROUGH.Jul 7, 2022 · N227AZ · Boeing 767323 · Nacelle/Pylon StructureSDR MK1Y202207060018Housing · corrodedL/H WING - MAIN FUEL TANK FUEL BOOST PUMP HOUSING REPAIRS - DURING MAINTENANCE INSPECTION AT IAI' CORROSIN WAS FOUND ON THE INNER FACE OF THE FUEL BOOST PUMP HOUSING ATTER REMOVING THE FWD FUEL BOOST PUMP SHUTOFF SLEEVEJul 6, 2022 · N203CM · Boeing 767323 · Fuel Boost PumpSDR MK1Y20220706017Repair · discoveredENG@ 2 - STRUT FAIRING - OUTBRD SIDE - NAC STA 304.5 - NAC STA 307.9 - - DURRING MAINTENANCE AT IAI - EXISTING UNDOCUMENTED REPAIR WAS FOUND ON STRUT OF ENGINE #2, OUTBRD SIDE FAIRUNG SKIN.Jul 6, 2022 · N203CM · Boeing 767323 · Nacelle/Pylon StructureSDR MK1Y20220706016Housing · corrodedL/H WING - MAIN FUEL TANK FUEL BOOST PUMP HOSING REPAIRS - DURING MAINTENANCE INSPECTION AT IAI, CORROSION WAS FOUND ON THE INNER FACE OF THE FUEL BOOST PUMP HOUSING AFTER REMOVING THE AFT FUEL BOOST PUMP SHUTOFF SLEEVE.Jul 6, 2022 · N203CM · Boeing 767323 · Fuel Boost PumpSDR NACA2022070600001None · noneSUPPLEMENTAL INFORMATION - PERFORMED BITE TEST OF ZONE TEMP CONTROLLER PER AMM 21-61-03 NO CURRENT OR PREVIOUS FAULT DISPLAYED. NO ASSOCIATED EICAS MESSAGES DISPLAYED. PERFORMED OPERATIONAL TEST OF ZONE TEMP CONTROL SYSTEM PER AMM 21-61-00 SYSTEMS OPERATION NOJul 6, 2022 · N321CM · Boeing 767323 · Cabin Temperature ControllerSDR NACA2022070600004None · noneDURING CRUISE ALTITUDE #2 ENG EGT SURGING BETWEEN 300 AND 800. ACCOMPLISHED FIM 77-21 FT 806. REMOVED AND REPLACED THERMOCOUPLE PROBE #2 IAW AMM 77-21-01, OPS CHECK NORMAL.Jul 6, 2022 · N379CX · Boeing 767323 · Cylinder Head Temperature (CHT) Indicating SystemSDR NACA2022070600003None · noneFLIGHT INTERRUPTION DUE TO APU DOOR STATUS MESSAGE DURING DEPARTURE @ 0410Z, 7/7/22. ITEM DEFERRED IAW MEL 49-15-01-01B CAT C, ETOPS PLACARD TURNED TO NO ETOPS, APU DOOR VISUALLY CHECKED CLOSED.Jul 6, 2022 · N351CM · Boeing 767323 · Airborne Auxiliary Power Unit (APU) SystemSDR NACA2022070600002None · unknownRIGHT ENGINE HPSOV MESSAGE. DEFERRED RIGHT ENG HPSOV PER MEL 36-11-02-02 CAT C @ 0049 7/7/22. REMOVED AND REPLACED RH BLEED AIR CIRCUIT ASSY PER AMM 36-11-12/401. OPS CHECK NORMAL NO FAULT NOTED AT THIS TIME. NO TIME INFO AVAILABLE IN TRAX.Jul 6, 2022 · N399CM · Boeing 767323 · Pneumatic SystemSDR MK1Y20220706015Skin Panel · crackedPROBLEM DESCRIPTION: PYLON #1, STRUT SIDE SKIN PANEL, PANEL 432AL, NAC 233,WL 143: FOUND EXTENDED CRACK BEYOND RIVET AT OUTER SKIN OF THE PYLON BY 1.8” IN LENGTH FROM THE CUTOUT OF PANEL 432AL.Jul 6, 2022 · N203CM · Boeing 767323 · Nacelle/Pylon, Plate/SkinSDR MK1Y20220706014Skin Panel · crackedPYLON # 2, OUTER SKIN PANEL 432AL, NAC 233, WL 143: FOUND EXTENDED CRACK BEYOND RIVET AT OUTER SKIN OF THE PYLON BY 2.5” IN LENGTH FROM THE CUTOUT OF PANEL 432AL.Jul 6, 2022 · N203CM · Boeing 767323 · Nacelle/Pylon, Plate/SkinSDR MK1Y20220706013Skin · out of limitsEXTERNAL FUSELAGE SKIN, STA 226 – STA 347, STR-28L – STR-29L: NRC M0143-EXTERNAL FUSELAGE SKIN BS 226.5 AND 2.2” BELOW STR 29L: SKIN THICKNESS: 0.080”. REMOVED FASTENER: JO-BOLT 0.185” DIA.OS-1 EXISTING REPAIR WASHER: DIAMETR: 0.580”, THICKNESS: 0.065”. NRC MJul 6, 2022 · N203CM · Boeing 767323 · Fuselage Main, Plate/SkinSDR MK1Y20220706012Repair · discoveredR/H HORIZONTAL STABILIZER – UPPER SKIN: DURING MAINTENANCE PRACTICES AT IAI IN TLV, AN EXISTING UNDOCUMENTED REPAIR WAS FOUND ON R/H HORIZONTAL STABILIZER UPPER SKIN. THE SKIN IS MADE FROM ALCLAD 7075-T6 1.100” IN THICK. THE REPAIR FOUND CONSISTS IN ONE DOUBLEJul 6, 2022 · N203CM · Boeing 767323 · Empennage StructureSDR MK1Y20220706011Repair · discoveredR/H MLG SHOCK STRUT DOOR:DURING MAINTENANCE INSPECTION AT IAI, EXISTING UNDOCUMENTED REPAIR WAS FOUND ON R/H MLG SHOCK STRUT DOORJul 6, 2022 · N203CM · Boeing 767323 · DoorsSDR MK1Y20220706010Repair · discoveredSTRUT # 2, INBD SIDE, SKIN 313T3310: DURING MAINTENANCE PRACTICES AT IAI IN TLV, AN EXISTING UNDOCUMENTED DOUBLER REPAIR WAS FOUND ON STRUT # 2 INBD SIDE, ON SKIN 313T3310. THE SKIN IS MADE FROM TWO BONDED SKINS OF ALCLAD 2024-T3 0.063” AND 0.040” IN THICKNESSJul 6, 2022 · N203CM · Boeing 767323 · Nacelle/Pylon StructureSDR MK1Y20220706009Skin · damagedDURING MAINTENANCE INSPECTION LIGHTNING STRIKES WERE DISCOVERED ON THE EXTERNAL FUSELAGE SKIN BETWEEN STA 212 AND STA 303, STR-29L – STR-30L. THE LIGHTNING STRIKES WERE BLENDED OUT. THE BLEND OUT AREA IS LOCATED COMMON TO THE EXISTING FASTENERS. AFTER INSPECTIJul 6, 2022 · N203CM · Boeing 767323 · Fuselage Main, Plate/SkinSDR MK1Y20220706008Skin Panel · corrodedCENTER WING SECTION, UPPER CHORD AREA, STA 955, RBL 11.00: DURING CONVERSION WORK AT IAI, A CORROSION WAS FOUND AT DATUM LOCATION ON SKIN PANEL NO.1 OF CENTER WING, PRESSURE DECK WEB, AND UPPER CHORD OF REAR SPAR OF CENTER WING. THE SKIN AND WEB WERE BLENDED AJul 6, 2022 · N203CM · Boeing 767323 · Fuselage Structure (General)SDR MK1Y20220706007Repair · discovered: ENGINE #1, STRUT FAIRING, INBD SIDE, NAC STA 304.1 – NAC STA 311.1: DURING MAINTENANCE INSPECTION AT IAI, THE EXISTING UNDOCUMENTED REPAIR WAS FOUND ON THE STRUT FAIRING AT DATUM LOCATION.Jul 6, 2022 · N203CM · Boeing 767323 · Nacelle/Pylon StructureSDR MK1Y20220706006Skin · damagedDURING MAINTENANCE INSPECTION LIGHTNING STRIKES WERE DISCOVERED ON THE EXTERNAL FUSELAGE SKIN BETWEEN STA 368 AND STA 412, STR-28L – STR-30L. THE LIGHTNING STRIKES WERE BLENDED OUT. THE BLEND OUT ARE LOCATED COMMON TO THE EXISTING FASTENERS. AFTJul 6, 2022 · N203CM · Boeing 767323 · Fuselage Structure (General)SDR MK1Y20220706005Skin · scratched: EXTERNAL FUSELAGE SKIN, STA 1487, STR-22L – STR-23L: DURING MAINTENANCE INSPECTION AT IAI, SCRATCHES WERE FOUND AT DATUM LOCATION. THE DAMAGE WAS BLENDED OUT AND FOUND WITHIN LIMITS, HOWEVER, THE BLEND OUT IS AMONG THE FASTENERS THAT PROHIBITED PER SRM 53-0Jul 6, 2022 · N203CM · Boeing 767323 · Fuselage Main, Plate/SkinSDR MK1Y20220706004Repair · discoveredENGINE #2, STRUT ACCESS PANEL 446BR, NAC STA 249 – NAC STA 253: DURING MAINTENANCE INSPECTION AT IAI, EXISTING UNDOCUMENTED REPAIR WAS FOUND ON ENGINE #2, STRUT, ACCESS PANEL NO. 446BR.Jul 6, 2022 · N203CM · Boeing 767323 · Nacelle/Pylon StructureSDR MK1Y20220706003Stub Frame · crackedTHE CRACK FOUND IN THE TRANSITION RADIUS OF THE RIGHT FUSELAGE FRAME STUB BEAM LOCATED STA 883.5 AND RBL 89. THE CRACK WAS FOUND DURING A REPETITIVE HFEC SURFACE INSPECTION IAW BOEING SERVICE BULLETIN 767-53A0209, AS MANDATED BY AIRWORTHINESS DIRECTIVE 2012-22Jul 6, 2022 · N203CM · Boeing 767323 · Fuselage Main, FrameSDR MK1Y20220706002Stub Frame · crackedTHE CRACK FOUND IN THE TRANSITION RADIUS OF THE LEFT FUSELAGE FRAME STUB BEAM LOCATED STA 859.5 AND LBL 89. THE CRACK WAS FOUND DURING A REPETITIVE HFEC SURFACE INSPECTION IAW BOEING SERVICE BULLETIN 767-53A0209, AS MANDATED BY AIRWORTHINESS DIRECTIVE 2012-22-Jul 6, 2022 · N203CM · Boeing 767323 · Fuselage Main, FrameSDR MK1Y20220706001Skin Panel · corrodedCENTER WING, UPPER SKIN, PANEL NO. 1, STA 955, LBL 74.00: DURING MAINTENANCE INSPECTION AT IAI, CORROSION WAS FOUND AT DATUM LOCATION. THE DAMAGE WAS BLENDED OUT AND FOUND WITHIN LIMITS, HOWEVER, THE BLEND OUT IS AMONG THE FASTENERS THAT PROHIBITED PER SRM 53-Jul 6, 2022 · N203CM · Boeing 767323 · Wing, Plate/SkinSDR NACA2022070400002Apu · fault messageAPU AUTO SHUT DOWN, ECU BITE "GEN FILTER" - ACCOMPLISHED FIM 49-11 FAULT TREE 969. REMOVED AND REPLACED GENERATOR SCAVENGE FILTER AND GENERATOR SCAVENGE ELEMENT PER AMM 49-27-03, LEAK AND OPS CHECK FOUND GOOD.Jul 4, 2022 · N379CX · Boeing 767323 · APU Cowling/ContainmentSDR NACA2022070400001Eicas · fault messageRIGHT ENGINE HPSOV EICAS MESSAGE ON DESCENT, ALSO ON STATUS PAGE. DEFERRED RIGHT ENGINE HPSOV REF MEL 36-11-02-02 CAT C, RH HPSOV SECURED TO CLOSED POSITION AT 0730Z ON 7/4/2022, INSTALLED PLACARD. ACCOMPLISHED BITE CHECK PER AMM 36-11-07, NO FAULT NOTED AT THJul 4, 2022 · N399CM · Boeing 767323 · Pneumatic Distribution SystemSDR NACA2022070200001None · noneR ENGINE HPSOV STATUS MESSAGE IN FLIGHT. COMPLETED BITE CHECK IAW AMM 36-23-00, NO FAULT FOUND AIRCRAFT REMAINS ETOPS 180Jul 2, 2022 · N399CM · Boeing 767323 · Pneumatic Distribution SystemSDR NACA2022062500002None · noneENGINE ANTI-ICE LEFT AND RIGHT VALVE LIGHT SWITCH DISAGREEMENT. PERFORMED ENGINE ANTI-ICE TEST, FOUND NORMAL.Jun 25, 2022 · N379CX · Boeing 767323 · Ice/Rain Protection SystemSDR NACA2022062500001None · noneR ENGINE HPSOV EICAS MSG BRIEFLY DISPLAYED AT TOP OF DESCENT. MSG DISAPPEARED AFTER 2 MINUTES. ACCOMPLISHED BITE CHECK PER AMM 36-11-7, NO FAULT FOUND. AIRCRAFT REMAINS ETOPS 180.Jun 25, 2022 · N399CM · Boeing 767323 · Pneumatic SystemSDR IXXA20220626119Window · inoperativePRIOR TO DEPARTURE, L2 WINDOW CRANK BINDING TOWARD CLOSE. L2 WINDOW ADJUSTED IAW B767 AMM 56-11-02. OPERATIONAL CHECK GOOD.Jun 23, 2022 · N443AZ · Boeing 767323 · Flight Compartment WindowsSDR NACA2022062000002None · noneSTATUS MSG RIGHT ENGINE FIRE LOOP 2. DEFERRED PER MEL 26-11-01-01 CAT C ON 6/20/2022 @0610Z. ETOPS VERIFICATION CWJun 20, 2022 · N351CM · Boeing 767323 · Smoke DetectionSDR NACA2022062000001None · noneAPU BLEED SURGE DUCT HAS A HOLE. REMOVED AND REPLACED BLEED DUCT SECTION PN# 3884292-2 WITH HOLE IAW AMM 49-53-01. NO PARTS INFO IN TRAX. OPS CHECK GOOD LEAK CHECK GOOD.Jun 20, 2022 · N321CM · Boeing 767323 · Airborne Auxiliary Power Unit (APU) SystemSDR NACA2022061900001None · noneFOUND RH ENGINE PRV FORWARD CLAMPS HAVE PNEUMATIC LEAK. RH ENG PRV E-SEALS REMOVED AND REPLACED IAW AMM 36-11-18, LEAK CHECK GOOD.Jun 19, 2022 · N399CM · Boeing 767323 · Pneumatic System
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