Boeing 767-200

Service difficulty reports · 568

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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 = '767200'
  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 TAMF20070036SSkin · corrodedDURING INSPECTION OF (C2) CHECK WAS FOUND A CORROSION ON PRESSURE SKIN STA 582 BETWEEN STRINGER 34-35 RT. DAMAGED AREA WAS REPAIRED IAW EWO 767-53-058 AND SERVICE REQUEST 1-526668594. THIS REPAIR CONSTITUTES A MAJOR REPAIR, FORM 8100-9 WAS ISSUED APPROVING THAug 26, 2007 · N768QT · Boeing 767200 · Fuselage Main, Plate/SkinSDR TAMF20070035SSill · corrodedDURING INSPECTION OF (C2) CHECK WAS FOUND A CORROSION ON CARGO DOOR SURROUND STRUCTURE, MAIN SILL, OUTER CHORD STA 569.65 RT. DAMAGED AREA WAS REPAIRED IAW EWO 767-53-056 AND SERVICE REQUEST 1-527218048. THIS REPAIR CONSTITUTES A MAJOR REPAIR, FORM 8100-9 WAAug 26, 2007 · N768QT · Boeing 767200 · Fuselage Miscellaneous StructureSDR TAMF20070034SSill · corrodedDURING INSPECTION OF (C2) CHECK WAS FOUND A CORROSION ON CARGO DOOR SURROUND STRUCTURE, MAIN SILL, OUTER CHORD STA 632 RT. DAMAGED AREA WAS REPAIRED IAW EWO 767-53-059 AND SERVICE REQUEST 1-533874348. THIS REPAIR CONSTITUTES A MAJOR REPAIR, FORM 8100-9 WAS ISAug 26, 2007 · N768QT · Boeing 767200 · Fuselage Miscellaneous StructureSDR TAMF20070017SBeam · crackedDURING C-CHECKS INSPECTION WAS FOUND A CRACK ON FIXED LEADING EDGE NOSE BEAM WEB STA OSS 644.58-694.55 - RT. DAMAGED AREA WAS REPAIRED IAW EWO 767-57-025 AND SRM 57-41-13 REPAIR 1-2. THIS REPAIR CONSTITUTES A MAJOR REPAIR.Aug 26, 2007 · N768QT · Boeing 767200 · Wing Main, Frame StructureSDR TAMF20070032SSkin · chafedDURING INSPECTION OF (C) CHECK WAS FOUND A WEAR ON RUB STRIPS SKIN STA 1725.50 STRINGER 22 - RT/LT. DAMAGED AREA WAS REPAIRED IAW EWO 767-53-054 AND MFG SERVICE REQUEST 1-524791119. THIS REPAIR CONSTITUTES A MAJOR REPAIR. FORM 8100-9 WAS ISSUED APPROVING THAug 25, 2007 · N768QT · Boeing 767200 · Fuselage Main, Plate/SkinSDR TAMF20070031SSkin · wrinkledDURING (C) CHECKS INSPECTION WAS FOUND AN EXISTING REPAIR WRINKLED ON LEADING EDGE SLAT NR 2 UPPER SKIN. DAMAGED AREA WAS REPAIRED IAW EWO 767-57-029 AND MFG SERVICE REQUEST 1-527377149. THIS REPAIR CONSTITUTES A MAJOR REPAIR. FORM 8100-9 WAS ISSUED APPROVINGAug 25, 2007 · N768QT · Boeing 767200 · Leading Edge DevicesSDR TAMF20070029SSill · corrodedFWD CARGO COMPARTMENT LOWER MAIN SILL, THE UPPER EXTERIOR EXTRUDED SECTION HAS CORROSION AT STA 610. REMOVED AND REPLACED MAIN SILL IN FWD CARGO COMPARTMENT UPPER EXTERIOR EXTRUDED SECTION STA 610 IAW SRM 51-40-02 PAGE 2-3 AND SRM 51-40-02 PAGE 4-7.Aug 25, 2007 · N768QT · Boeing 767200 · Fuselage Miscellaneous StructureSDR TAMF20070028SSkin · dentedDURING INSPECTION OF (C2) CHECK WERE FOUND SEVERAL DENTS ON FUSELAGE SKIN STA 1417-1436 STRINGER 33 -36-LT. DAMAGED AREAS WERE REPAIRED IAW EWO 767-53-055 AND SERVICE REQUEST 1-527218048. THIS REPAIR CONSTITUTES A MAJOR REPAIR. FORM 8100-9 WAS ISSUED APPROVAug 25, 2007 · N768QT · Boeing 767200 · Fuselage Main, Plate/SkinSDR TAMF20070023SCowling · damagedDURING C CHECK INSPECTION WAS FOUND CORE COWL P/N: 224-2301-513 S/N: 0130 WITH ELONGATED HOLE AT FRAME STA NAC 294 - CF6-80C2. DAMAGED AREA WAS REPAIRED IAW CV07-1781-01 AND EWO 767-54-020. THIS REPAIR CONSTITUTES A MAJOR REPAIR.Aug 25, 2007 · N768QT · Boeing 767200 · Nacelle/Pylon, Main FrameSDR TAMF20070020SRib · chafedDURING C-CHECK INSPECTION WAS FOUND A WEAR OUT OF LIMITS ON IB AILERON RT - OB CLOSURE RIB WEB.DAMAGED AREA WAS REPAIRED IAW EWO 767 57-026 AND SERVICE REQUEST 1-525478883. THIS REPAIR CONSTITUTES A MAJOR REPAIR. FAA FORM 8100-9 WAS ISSUED APPROVING THIS REPAIAug 25, 2007 · N768QT · Boeing 767200 · AileronsSDR TAMF20070019SSkin · dentedDURING INSPECTION OF (C2) CHECK WAS FOUND A DENT A/Y=40 ON LAP SKIN STA 1536 STR 36 - LT. DAMAGED AREA WAS REPAIRED IAW EWO 767-53-049 AND SRM 53-00-01 REPAIR 12. THIS REPAIR CONSTITUTES A MAJOR REPAIR.Aug 25, 2007 · N768QT · Boeing 767200 · Fuselage Main, Plate/SkinSDR TAMF20070018SSkin · dentedDURING INSPECTION OF (C2) CHECK WAS FOUND A DENT A/Y=20 ON FUSELAGE SKIN AT STA 1506, STR 31-32 -LT. DAMAGED AREA WAS REPAIRED IAW EWO 767-53-048 AND SRM 53-00-01 REPAIR 6. THIS REPAIR CONSTITUTES A MAJOR REPAIR.Aug 25, 2007 · N768QT · Boeing 767200 · Fuselage Main, Plate/SkinSDR TAMF20070015SSkin · dentedDURING INSPECTION OF (C2) CHECK WAS FOUND A DENT OVER REPAIR DOUBLER AT SKIN STA 676-698 STRINGER 37-38 - RT. THE DOUBLER NEEDS TO BE REPLACE. DAMAGED AREA WAS REPAIRED IAW EWO 767 53-047 AND SRM 53-00-01 REPAIR 14. THIS REPAIR CONSTITUTES A MAJOR REPAIR.Aug 25, 2007 · N768QT · Boeing 767200 · Fuselage Main, Plate/SkinSDR TAMF20070030SFairing · corrodedDURING C CHECK INSPECTION WAS FOUND A CORROSION ON HORIZONTAL STABILIZER TIP LT NOSE IB - LT.DAMAGED AREA WAS REPAIRED IAW EWO 767-57-030 AND MFG SERVICE REQUEST 1-524791300. THIS REPAIR CONSTITUTES A MAJOR REPAIR. FORM 8100-9 WAS ISSUED APPROVING THIS REPAIRAug 24, 2007 · N768QT · Boeing 767200 · Horizontal Stabilizer StructureSDR TAMF20070022SSkin · dentedDURING INSPECTION OF C2 CHECK WAS FOUND A DENT ON LAP SKIN STA 212.5, STR 30-RT. DENT ON LIMITS IAW EWO 767-53-051 AND MFG SERVICE REQUEST 1-526586182. FAA FORM 8100-9 WAS ISSUED APPROVING THIS REPAIR.Aug 22, 2007 · N768QT · Boeing 767200 · Fuselage Main, Plate/SkinSDR TAMF20070021SSkin · dentedDURING INSPECTION OF (C2) CHECK WAS FOUND A DENT ON LAP SKIN STA 1339 STR 17 - LT. DAMAGE ON LIMITS IAW EWO 767-53-05 AND BOEING SERVICE REQUEST 1-526586182. FAA FORM 8100-9 WAS ISSUED APPROVING THIS REPAIR.Aug 22, 2007 · N768QT · Boeing 767200 · Fuselage Main, Plate/SkinSDR TAMF20070016SSkin · corrodedDURING INSPECTION OF (C2) CHECK WAS FOUND CORROSION OVER REPAIR DOUBLER AT SKIN STA 456, STR 31-32 -RT. THE DOUBLER NEEDS TO BE REPLACED. DAMAGED AREA WAS REPAIRED IAW EWO 767-53-046 AND SRM 53-00-01 REPAIR 14.THIS REPAIR CONSTITUTES A MAJOR REPAIR.Aug 22, 2007 · N768QT · Boeing 767200 · Fuselage Main, Plate/SkinSDR ABXA070266Actuator · failedDURING MAINTENANCE, REF JOB CARD 12-003-C1, STABILIZER TRIM BALL NUT UPPER SEAL APPEARED TO HAVE FAILED - STEP (23) (B) NOTE 2 (BEAVER UNIT). REMOVED AND REPLACED TRIM BALL SCREW ACTUATOR IAW B767 MM 27-41-10.Aug 11, 2007 · N752AX · Boeing 767200 · Stabilizer ActuatorSDR TAMF20070011SSkin · damagedDURING C CHECK INSPECTION (MFG TASK CARD 06-084-01-2) WAS FOUND WEAR ON STRUT SKIN STA 148.50. THE MINIMUM THICKNESS IS 0.047 INCH. CF6-80C2 ENGINE NR 2. DAMAGED AREA WAS REPAIRED IAW EWO 767 54-017 AND MFG SERVICE REQUEST 1-512263744. THIS REPAIR CONSTITUTESAug 9, 2007 · N767QT · Boeing 767200 · Nacelle/Pylon, Plate/SkinSDR TAMF20070014SFairing · crackedDURING C-CHECK INSPECTION WAS FOUND NR 2 NACELLE STRUT NR 446CL ACCESS PANEL DELAMINATED AND CRACKED. ACCESS PANEL WAS FABRICATED AND INSTALLED IAW MFG SERVICE REQUEST 1-50853397 AND DRAWING 015T0563-8.Aug 7, 2007 · N767QT · Boeing 767200 · Nacelle/Pylon, Main FrameSDR TAMF20070013SStructure · corrodedDURING C-CHECK INSPECTION (MFG TASK CARD 53-456-00) WAS FOUND A CORROSION ON FWD CARGO COMPARTMENT CARGO DOOR UPPER SURFACE, INNER CHORD AT MAIN SILL LARGE CARGO DOOR, BETWEEN STA 544-566. DAMAGED AREA WAS BLENDED OUT AND CORROSION REMOVED IAW SRM 51-10-02 PAAug 5, 2007 · N767QT · Boeing 767200 · Cargo/Baggage DoorsSDR TAMF20070010SSkin · damagedDURING C CHECK INSPECTION (MFG TASK CARD 06-091-01-2) WAS FOUND CORE COWL P/N:224-2301-517, S/N: 0115 WITH ELONGATED HOLE AT FRAME STA NAC 294, ENGINE NR 2.DAMAGED AREA WAS REPAIRED IAW EWO 767 54-016 AND AUTHORIZATION CV07-1674-01.Aug 5, 2007 · N767QT · Boeing 767200 · Nacelle/Pylon, Plate/SkinSDR TAMF20070009SSpar · corrodedRT WING FRONT SPAR UPPER FWD CHORD AT STA OSS 456.98 HAS CORROSION. REMOVED CORROSION FROM UPPER FWD CHORD AT RT WING FRONT SPAR, STA OSS 456.98 IAW SRM 51-10-02 PAGE 12-13. THICKNESS FOUND, MAX: 0.078 INCH, MIN: 0.055 INCH. NO CRACKS FOUND. BLENDING LIMITS OAug 5, 2007 · N767QT · Boeing 767200 · Wing SparSDR TAMF20070008SFrame · damagedDURING INSPECTION OF C-CHECK (MFG TASK CARD 06-091-01-2) WAS FOUND CORE COWL P/N: 224-2301-541 S/N: 0217 WITH ELONGATED HOLE AT FRAME STA NAC 294 - CF6-80C2 ENGINE NR 2. DAMAGED AREA WILL BE REPAIRED IAW CV07-1678-01 AND EWO 767-54-015.Aug 5, 2007 · N767QT · Boeing 767200 · Nacelle/Pylon, Frame/Spar/RibSDR TAMF20070006SSpar · crackedDURING C-CHECK INSPECTION (MFG TASK CARD 06-099-01-1) WAS FOUND A CRACK ON LOWER CHORD AT FRONT SPAR STA ISS 256-261 RT. DAMAGED AREA WAS REPAIRED IAW MFG SERVICE REQUEST 1-499965004 AND EWO 767-57-021. THIS REPAIR CONSTITUTES A MAJOR REPAIR. FAA FORM 8100-9 Aug 5, 2007 · N767QT · Boeing 767200 · Leading Edge DevicesSDR TAMF20070007SWeb · wornDURING (C) CHECK INSPECTION (TASK CARD 57-592-00) WAS FOUND WORN OUT OF LIMITS ON IB AILERON LT - OB CLOSURE RIB WEB. DAMAGE WAS REPAIRED IAW BOEING SERVICE REQUEST 1-500301558 AND EWO 767-57-024. ALSO, FAIL-SAFE FITTING PN 113T6145-11 WAS FABRICATED AND INSTAug 4, 2007 · N767QT · Boeing 767200 · AileronsSDR TAMF20070004SSpar · corrodedDURING C-CHECK INSPECTION (TASK CARD 06-099-01-2) WAS FOUND A CRACK ON LOWER CHORD AT FRONT SPAR STA ISS 256-261 RT. DAMAGED AREA WAS REPAIRED IAW MFG SERVICE REQUEST 1-495025865 AND EWO 767-57-020. THIS REPAIR CONSTITUTES A MAJOR REPAIR. FAA FORM 8100-9 WAS Aug 4, 2007 · N767QT · Boeing 767200 · Leading Edge DevicesSDR TAMF20070012SSkin · damagedDURING C CHECK INSPECTION (MFG TASK CARD 57-666-00) WAS FOUND A LIGHTNING STRIKE ON WING UPPER SKIN STA 1018.2 RT. DAMAGED AREA WAS REPAIRED IAW MFG SERVICE REQUEST 1-490432776 AND EWO 767 57-023. THIS REPAIR CONSTITUTES A MAJOR REPAIR. FAA FORM 8100-9 WAS ISAug 2, 2007 · N767QT · Boeing 767200 · Wing, Plate/SkinSDR TAMF20070003SSkin · corrodedDURING C-CHECK INSPECTION (TASK CARD 57-500-00) WAS FOUND A CORROSION ON SLAT NR 2 LOWER SKIN STA OSS 953.48 LT. DAMAGED AREA WAS REPAIRED IAW MFG SERVICE REQUEST 1-495025537 AND EWO 767-57-022. THIS REPAIR CONSTITUTES A MAJOR REPAIR. FAA FORM 8100-9 WAS ISSUAug 2, 2007 · N767QT · Boeing 767200 · Leading Edge DevicesSDR TAMF20070005SBeam · corrodedDURING C-CHECK INSPECTION (TASK CARD 53-426-00) WAS FOUND CORROSION ON NLG W/W BULKHEAD, STA 287, CENTER BEAM PN 141T2939. CORRODED AREA WAS REMOVED IAW SRM 51-10-02 PAG 12-13 AND IT WAS FOUND OUT OF LIMITS (MAX 0.190 IN, MIN 0.160 IN) IAW SRM 53-10-14 FIGUREAug 1, 2007 · N767QT · Boeing 767200 · Fuselage Main, StructureSDR ABXA070242Indicator · burnedSTA: JFK, MAINTENANCE SMELLED ELECTRICAL SMOKE IN COCKPIT. CO-PILOT EADI BLANK. INSPECTED AND FOUND F/O'S EADI DAMAGED. REMOVED AND REPLACED F/O'S EADI IAW B767 AMM 34-22-34. OPS CHECKED GOOD.Jul 13, 2007 · N798AX · Boeing 767200 · Attitude Gyro and Indicating SystemSDR ABXA070246Skin · crackedL1 DOOR CUTOUT, LOWER AFT CORNER CRACKED. REPAIRED AREA IAW REA B653-56023-MR.Jul 8, 2007 · N799AX · Boeing 767200 · Fuselage Main, Plate/SkinSDR ABXA070248Pin · defectiveRIGHT OUTER PIVET PIN OF HORIZONTAL STABILIZER SHOWS INDICATION OF LINEAR DEFECT ON INNER SURFACE. REMOVED AND REPLACED RIGHT OUTER PIVOT PIN ON JOB CARD 7302001 IAW B767 SRM.Jul 6, 2007 · N799AX · Boeing 767200 · Horizontal Stabilizer StructureSDR ABXA070247Skin · crackedR1 DOOR LOWER AFT CUTOUT CORNER WAS CRACKED. REPAIRED AREA IAW B767 SRM.Jul 4, 2007 · N799AX · Boeing 767200 · Fuselage Main, Plate/SkinSDR ABXA070236Wire · detachedR1 EMERGENCY EXIT LIGHT DID NOT ILLUMINATE WHEN EMERGENCY TEST SWITCH WAS DEPRESSED. FOUND WIRES TO EXIT LIGHT NOT ATTACHED. CHECKED AND ATTACHED WIRES, OPS CHECKED GOOD IAW BOEING MM.Jun 29, 2007 · N797AX · Boeing 767200 · Light System WiringSDR ABXA070235Wire · out of positionEMERGENCY 02 TEST LIGHT WOULD NOT PRESS TO TEST (INOPERATIVE) SUPERNUMERARY AREA. REPOSITIONED WIRING AT DEPRESS LIGHT L9003 IAW WDM 33-24-11. OPS CHECKED GOOD IAW BOEING MM.Jun 29, 2007 · N797AX · Boeing 767200 · Light System WiringSDR ABXA070216Skin · debondedLEFT ELEVATOR OUTBOARD HAD INTERPLY DISBOND AT EACH ACTUATOR FITTING AREA ON LOWER LEADING EDGE. REPLACED LEFT ELEVATOR ON NON ROUTINE 0395 IAW BOEING SRM.Jun 1, 2007 · N797AX · Boeing 767200 · Elevator, Plate/SkinSDR ABXA070215Rib · corrodedCORROSION WS 564, RIGHT WING LEADING EDGE PANEL SUPPORT/RIB. REPLACED STRUT RIB IAW B767 SRM 51-40-02.May 25, 2007 · N797AX · Boeing 767200 · Wing, Rib/BulkheadSDR ABXA070214Rib · corrodedCORROSION WS 720, RIGHT WING LEADING EDGE LOWER PANEL SUPPORT/RIB. REPLACED STRUT RIB IAW B767 SRM 51-40-02.May 25, 2007 · N797AX · Boeing 767200 · Wing, Rib/BulkheadSDR ABXA070213Pin · corrodedRIGHT HORIZONTAL STABILIZER PIVOT PIN HAD CORRODED PITTING IN THREADS. REPLACED PIVOT PIN IAW JOB CARD 7302001.May 24, 2007 · N797AX · Boeing 767200 · Horizontal Stabilizer, Attach FittingsSDR ABXA070212Doubler · crackedL1 DOOR CUTOUT LOWER CORNER INTERNAL DOUBLER AFT CORNER HAD CRACK INDICATION. TWO CRACKS, ONE .275 INCH AND ONE .210 INCH. REPAIRED AREA IAW REA B653-55867-MR.May 24, 2007 · N797AX · Boeing 767200 · Fuselage Miscellaneous StructureSDR ABXA070211Pin · crackedLEFT OUTER HORIZONTAL STABILIZER PIVOT PIN CRACKED. REPLACED PIVET PIN AND OUTBOARD PIVOT SPACER IAW B767 JOB CARD 7302001.May 24, 2007 · N797AX · Boeing 767200 · Horizontal Stabilizer, Attach FittingsSDR ABXA070210Stiffener · crackedCRACKED STIFFENER COCKPIT FLOORBEAM STA 266.5 APPROXIMATELY LEFT BUTT LINE 10.50. REMOVED, FABRICATED AND INSTALLED STIFFENER ON FLOORBEAM STA 266.5, LEFT BUTT LINE 10.50 IAW BOEING SRM.May 23, 2007 · N797AX · Boeing 767200 · Fuselage Miscellaneous StructureSDR ABXA070209Cylinder · crackedRIGHT MAIN LANDING GEAR HAD A LARGE CRACK AT CASTING ON UPPER CENTER AFT END. REPLACED RIGHT MAIN LANDING GEAR ON JOB CARD 32-045-01-2 IAW BOEING SRM.May 23, 2007 · N797AX · Boeing 767200 · Main Landing Gear Strut/Axle/TruckSDR ABXA070208Structure · crackedR1 DOOR CUTOUT HAD DEFECT EXTENDING FROM RIVET AND LOWER AFT CORNER. REPAIRED AREA IAW REA B653-55851-MR.May 22, 2007 · N797AX · Boeing 767200 · Fuselage Miscellaneous StructureSDR TAMF20070002OConnector · damagedR ENG OIL TEMP HIGH DURING TAKEOFF ROLL. ENGINE WAS SHUTDOWN AND T/O REJECTED. FRM 7902XB02. FIM 31-41-00 WAS PERFORMED AND R ENG OIL TEMP CONNECTOR, D11062 PIN NR 3 WAS FOUND LOOSE. PIN WAS REPLACED IAW WDM 79-34-11 WITH SATISFACTORY RESULT, NO EICAS MESSAGEMay 17, 2007 · N770QT · Boeing 767200 · Engine Oil System WiringSDR TAMF20070002SWeb · crackedDURING INSPECTION CHECK WAS FOUND A CRACK AT AFT WING FAIRING WEB STA 1080 BL 62-70-LT. DAMAGED AREA WAS REPAIRED IAW EWO 767 53-035 AND MFG SERVICE REQUEST 1-311853573. THIS REPAIR CONSTITUTES A MAJOR REPAIR. FAA FORM 8100-9 WAS ISSUED APPROVING THIS REPAIR.Apr 6, 2007 · N769QT · Boeing 767200 · Aerodynamic FairingsSDR TAMF20070001SFairing · crackedDURING INSPECTION, FOUND A CRACK AT AFT WING FAIRING WEB STA 1080, BL 62-70, LT. DAMAGED AREA WAS REPAIRED IAW MFG SERVICE REQUEST 1-303353670 AND EWO 767-53-031. THIS REPAIR CONSTITUTES A MAJOR REPAIR. FAA FORM 8100-9 WAS ISSUED APPROVING THIS REPAIR.Mar 21, 2007 · N767QT · Boeing 767200 · Aerodynamic FairingsSDR ABXA070048Control Unit · malfunctionedAS CREW WAS ON FINAL AT ILN, GOING THROUGH 27K, NR 2 ENGINE HAD AN UNCOMMANDED SHUTDOWN. CREW RESTARTED ENGINE WITHOUT ANY FURTHER ISSUES. NO EMERGENCY DECLARED. NO EN ROUTE DELAY. REMOVED AND REPLACED NR 2 ENGINE MAIN ENGINE CONTROL IAW B767 AMM 73-21-01-Feb 15, 2007 · N752AX · Boeing 767200 · Fuel Control/Turbine EnginesSDR TAMF20070001OGearbox · leakingDURING CLIMB ON FLIGHT # 861 (MDE-SCL) LT ENGINE OIL QTY DECREASED TO ZERO AND OIL PRESS DECREASED FROM 64 TO 15 PSI. ENGINE WAS REDUCED TO IDLE AND OIL PRESS REMAINED IN 15 PSI. AIRCRAFT WAS RETURNED TO MDE AND LANDED IN NORMAL CONDITION. DURING MAINTENANCE Jan 14, 2007 · N768QT · Boeing 767200 · Turbine Engine Reduction Gear
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