Boeing 767-338

Service difficulty reports · 1,328

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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 = '767338'
  ORDER BY difficulty_date DESC"

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SDR 2013F00116Sleeve · damaged(VHOGN) VISUAL INSPECTION OF THE FUEL TANK BOOST PUMP WIRING IAW SB 767-28A0053, REV 03. DURING THE INSPECTION OF LT MAIN BOOST PUMP WIRING OUTER SLEEVING FOUND SPLIT, AT AREAS WHERE SLEEVING WAS PUSHED FLAT ON FOLD LINES OF SLEEVING WAS NO LONGER ROUND. May 14, 2013 · Boeing 767338 · Fuel System WiringSDR ABXA20130416428Control Panel · faultyFLIGHT MANAGEMENT COMPUTER SYSTEMS "CDU" FIRST OFFICER, DISPLAY BLANK. SELECTING ALT FMC DID NOT CORRECT FAULT. FIRST OFFICERS FMCS CDU CIRCUIT BREAKER POPPED AND ELECTRIC BURNING SMELL ALSO NOTED. REMOVED AND REPLACED FLIGHT MANAGEMENT PANEL PER AMM 34-61-0Apr 16, 2013 · N362CM · Boeing 767338 · Flight Management Computing Hardware SystemSDR ABXA20130416425Pin · misinstalledLOSS OF NR 2 BRAKE ROD PIN ALLOWED BRAKE ROD TO ROTATE INTO A POSITION THAT PREVENTED LEFT MAIN LANDING GEAR FULL RETRACTION INTO WHEEL WELL. ON LANDING, BRAKE ROTATED WITH WHEEL ASSEMBLY CAUSING FIELD REPAIRABLE DAMAGE TO LEFT MAIN LANDING GEAR. BRAKE ROD PApr 16, 2013 · N362CM · Boeing 767338 · Landing Gear Brake SystemSDR 2012F00268Sleeve · crackedDURING VISUAL INSPECTION OF THE FUEL BOOST PUMP WIRING IAW SB 767-28A0053, REV 3. .5 LONG SPLITS WERE FOUND IN THE OUTER TEFLON SLEEVING OF THE LT AFT BOOST PUMP. THERE WAS NO DAMAGE ON THE INNER SLEEVE SO THE OUTER SLEEVE WAS REPLACED.Dec 11, 2012 · Boeing 767338 · Fuel System WiringSDR IXXA20121115023Thrust Reverser · crackedNR 2 ENGINE OTBD THRUST REVERSER HAS A .5" CRACK AT THE OPENING ACTUATOR BOTTOM END BRACKET. R & R THE NR 2 ENGINE OTBD THRUST REVERSER IAW AMM 78-31-01. ADJUSTED LATCH RING IAW AMM 78-31-02. OPS CHECK GOOD IAW AMM 78-31-00.Nov 15, 2012 · N316CM · Boeing 767338 · Engine Thrust ReverserSDR ABXR2012101900063Skin · crackedDENT ON EXISTING REPAIR AT STATION 618-635, STRINGERS S-26R AND S-30R. REPAIR REMOVED, CRACKS DISCOVERED IN 3 LOCATIONS ON THE SKIN. CUT OUT DAMAGE AND REPAIRED IAW EA B653-60359-MR, REV IR.Oct 19, 2012 · N363CM · Boeing 767338 · Fuselage Main, Plate/SkinSDR IXXA2012110100002Support · brokenRT MLG MAIN DOOR ACTUATOR AFT SUPPORT LINK LOWER END BROKEN AT ATTACH POINT. REPLACED RT MLG DOOR ACTUATOR AFT SUPPORT LINK IAW AMM 32-32-12 3F(1-3,6).Oct 2, 2012 · N316CM · Boeing 767338 · Fuselage Miscellaneous StructureSDR IXXA20120920024Fitting · crackedNR 2 PYLON FAN COWL SUPPORT BEAM FITTING ASSY CRACKED AT OTBD ATTACHING LUG. R & R SUPPORT BEAM FITTING ASSY FOR FAN COWL IAW DWG 311T2210 AND SRM 51-40-02.Sep 20, 2012 · N316CM · Boeing 767338 · Nacelle/Pylon, Main FrameSDR IXXA2012110100022Skin · dentedNR 7 SLAT L/E SKIN DENTED (6.0" X 2.0" X 0.75") AND CRACKED (0.5" IN LENGTH) ON INBD END. INBD RIB DAMAGE 0.5" CRACK. PERFORMED TRIMOUT AT THE CRACKED AREA IAW SRM 57-43-01, FIG 201. COMPLIED WITH HFEC INSP OF TRIMOUT AREA IAW NDT MANUAL 51-00-19. REPAIRED NSep 20, 2012 · N316CM · Boeing 767338 · Leading Edge DevicesSDR IXXA2012110100021Angle · crackedLOWER ANGLE CRACKED THRU LOCK FASTENER HOLE ON UPPER RIB STRUT AFT OF NR 9 SLAT AT L/E STA 531 ADJACENT TO FRONT SPAR. STOP DRILLED CRACK IAW SRM 57-41-09. REPAIR 4 ITEM 2 AND PERFORMED HFEC INSPECTION IAW NDT MANUAL 51-00-19, PART 6. NO DEFECTS NOTED. INSTSep 20, 2012 · N316CM · Boeing 767338 · Leading Edge DevicesSDR IXXA201211010001Angle · crackedLOWER ANGLE CRACKED THRU LOCK FASTENER HOLE ON UPPER RIB STRUT AFT OF NR 8 SLAT AT L/E STA 512 ADJACENT TO FRONT SPAR. STOP DRILLED CRACK IAW SRM 57-41-09. REPAIR 4 ITEM 2 AND PERFORMED HFEC INSPECTION IAW NDT MANUAL 51-00-19, PART 6. NO DEFECTS NOTED. INSSep 20, 2012 · N316CM · Boeing 767338 · Leading Edge DevicesSDR IXXA2012110100020Skin · corrodedCORROSION WAS FOUND AT FIVE LOCATIONS ON THE LOWER LT WING SKIN AT LOCATIONS 872, 889, 896, 951 AND 957 AT FASTENER LOCATIONS. FASTENERS WERE REMOVED AND CORROSION BLENDED IAW SRM 51-10-02. FASTENERS WERE REPLACED IAW SRM 51-40-02.Sep 19, 2012 · N316CM · Boeing 767338 · Wing, Plate/SkinSDR QLMY2012F00205Wire · damagedDURING HEAVY MX, A VISUAL INSPECTION OF THE FUEL TANK BOOST PUMP WIRING IAW SB 767-28A0053, REV 03. DURING THE INSPECTION A .5 INCH LONG SPLIT WAS FOUND IN THE OUTER TEFLON SLEEVE ABOUT 16 INCHES FROM THE REAR OF RT AFT FUEL BOOST PUMP CONNECTOR D1540. THSep 12, 2012 · Boeing 767338 · Fuel System WiringSDR ABXA20120909273Smoke Detector · defectiveNR 5A CARGO SMOKE DETECTOR LIGHT IS AMBER. REMOVED AND REPLACED NR 5A SMOKE DETECTOR IAW MM 26-14-01. OPS CHECK GOOD. OPS CHECK GOOD PER AMM 26-14-01, ACFT WAS GROUNDED.Sep 9, 2012 · N362CM · Boeing 767338 · Smoke DetectionSDR ABXR2012030100052Skin · misrepairedSTA 1417, STRINGER 30, LT TO 31, LT NEEDS EVALUATED FOR COMPLIANCE TO SRM. UPON REPAIR REMOVAL A DENT WAS DISCOVERED EXCEEDING SRM LIMITS. REA B652-59863-MR REV IR DATED 5/21/12 PROVIDED INSTRUCTION TO REMOVE THE DENT AND REPAIR IAW SRM 52-30-01, FIG 201.Jun 1, 2012 · N317CM · Boeing 767338 · Cargo/Baggage DoorsSDR ABXR201206010051Door · misrepairedEXTERNAL DOUBLER EXISTING REPAIR AT STA 1439 TO 1461, STR 25 LT TO 27 LT NEEDS EVALUATED. R & R DOUBLER AND REPAIRED DAMAGE IAW REA B652-59860-MR, AND SRM 52-30-01 FIG 201.Jun 1, 2012 · N317CM · Boeing 767338 · Cargo/Baggage DoorsSDR IXXA20120518011OTransfer Sys · malfunctionedRT MAIN TANK TRANSFERRED FUEL INTO CENTER TANK AT A RATE OF 200 KILOGRAMS PER MINUTE. RETURNED TO STATION. DEFUEL/REFUEL VALVES CHECKED GOOD. R & R RT DEFUELING VALVE IAW AMM 28-26-01/401. R & R CENTER RT DISCHARGE CK VALVE IAW AMM 28-22-05/401. R & R RIGMay 17, 2012 · N319CM · Boeing 767338 · Fuel Transfer ValveSDR ABXR2012033100041Skin · crackedFUSELAGE SKIN CRACKED AT STA 1726. REPAIRED IAW SRM.Mar 31, 2012 · N363CM · Boeing 767338 · Fuselage Main, Plate/SkinSDR ABXR2012033100040Failsafe · corrodedFAILSAFE AREA CORRODED AT BS 955 S23-26L. REPAIRED IAW AMES REA 46938REA05.Mar 31, 2012 · N363CM · Boeing 767338 · Fuselage Main, StructureSDR ABXR2012033100039Skin · corrodedRIGHT WING UPPER SURFACE CORRODED IN SEVERAL SPOTS BETWEEN WS 350 AND WS 1021. REPAIRED IAW SRM AND REA 46938REA13.Mar 31, 2012 · N363CM · Boeing 767338 · Wing, Plate/SkinSDR ABXR2012033100038Skin · corrodedLEFT WING LOWER SURFACE CORRODED IN SEVERAL SPOTS BETWEEN WS 375 AND WS 992. REPAIRED IAW SRM AND AMES REA 46938REA10.Mar 31, 2012 · N363CM · Boeing 767338 · Wing, Plate/SkinSDR ABXR2012033100037Skin · corrodedLEFT WING UPPER SURFACE CORRODED IN SEVERAL SPOTS BETWEEN WS 344 AND WS 916. REPAIRED IAW SRM AND REA'S 46938REA09, 46938REA12, AND 46938REA24.Mar 31, 2012 · N363CM · Boeing 767338 · Wing, Plate/SkinSDR ABXR2012033100036Skin · damagedRT WING LOWER SURFACE HAS DAMAGE TO SEVERAL FASTENER HOLES BETWEEN WS 375 AND WS 1067. REPAIRED IAW SRM AND REA'S 46938REA11, 46938REA20, AND 46938REA26.Mar 31, 2012 · N363CM · Boeing 767338 · Wing, Plate/SkinSDR ABXR2012033100035Skin · corrodedRIGHT WING LOWER SURFACE CORRODED IN SEVERAL SPOTS BETWEEN WS 375 AND WS 1067. REPAIRED IAW SRM AND REA'S 46938REA11 AND 46938REA16.Mar 31, 2012 · N363CM · Boeing 767338 · Wing, Plate/SkinSDR ABXR2012033100034Fitting · damagedBS 1809 RT LOWER CHORD TENSION FITTING HAS HOLE DAMAGE. R & R TENSION FITTING IAW REA 46938REA22.Mar 31, 2012 · N363CM · Boeing 767338 · Fuselage Main, Attach FittingsSDR ABXR2012033100033Fitting · crackedRIGHT BS 1809 FWD SPLICE FITTING HAS CRACK INDICATION. R & R SPLICE FITTING IAW REA 46938REA28.Mar 31, 2012 · N363CM · Boeing 767338 · Fuselage Main, Attach FittingsSDR ABXR2012033100032Fitting · corrodedLEFT KICK FITTING CORRODED. R & R KICK FITTING IAW REA 46938REA21.Mar 31, 2012 · N363CM · Boeing 767338 · Wing, Fuselage Attach FittingsSDR ABXR2012033100031Housing · debondedRIGHT OVERWING FILL HOUSING DID NOT BOND CHECK PROPERLY. REPAIRED IAW AMES REA 46938REA15.Mar 31, 2012 · N363CM · Boeing 767338 · Wing Main, Frame StructureSDR ABXR2012033100029Skin · chafedFUSELAGE SKIN DAMAGED AT STA 1809, S12R. REPAIRED IAW SRM.Mar 31, 2012 · N363CM · Boeing 767338 · Fuselage Main, Plate/SkinSDR ABXR2012033100030Skin · corrodedFUSELAGE SKIN EXPOSED BY LT FAILSAFE STRAP CORRODED. REPAIRED IAW SRM AND REA 46938REA06.Mar 31, 2012 · N363CM · Boeing 767338 · Fuselage Main, Plate/SkinSDR ABXR2012033100028Structure · crackedBS 1809 RT/FWD UPPER CHORD CRACKED AT LWR/FWD FASTENER HOLE. R & R CHORD IAW AMES REA 46938REA19.Mar 31, 2012 · N363CM · Boeing 767338 · Fuselage Miscellaneous StructureSDR IXXA20120321008OWire · burnedDURING INSPECTION, FOUND BURNED WIRES AT BS 680 FORWARD CARGO COMPARTMENT POWER DRIVE UNIT WIRE HARNESS IN POSITION 13L. REPAIRED WIRES IAW IAW WDM 25-53-14 SHT 5, 25-53-12 SHT 1 AND SWPM 20-60-11, 20-00-11 AND 20-30-12. OPS TEST NORMAL IAW AMM 25-53-00/501.Mar 20, 2012 · N319CM · Boeing 767338 · Electrical Power System WiringSDR ABXR2012022000027Wire · arcedDURING INSPECTION FOUND WIRE W9021-015-16 SHOWING SIGNS OF ARCING. R & R AFFECTED WIRE IAW SWPM.Feb 20, 2012 · N362CM · Boeing 767338 · Electrical Power System WiringSDR IXXA20120203002OSwitch · out of adjustDURING FL310, MAIN CARGO DOOR LIGHT ILLUMINATED. THE CREW RETURNED TO DEPARTURE WITHOUT INCIDENT. FOUND SWITCH S9022 OUT OF TOLERANCE. ADJUSTED SWITCH IAW AMM 52-71-09. DOOR LIGHTS AND SWITCHES OP CHECKED GOOD. DEPRESSURIZED ACFT. PREFORMED OPS CHECKED ANFeb 3, 2012 · N319CM · Boeing 767338 · Door Warning SystemSDR IXXA110080OSelector Switch · defectiveRIGHT ENGINE ANTI ICE SWITCH SMOKED AND HAD BURNING ODOR WHEN PLACED TO ON POSITION. MX R & R SWITCH ASSY IAW MM 33-13-00/201 AND WDM 30-21-11. SWITCH OPS CHECK GOOD. VERIFIED, ACFT RELEASED TO ETOPS 180.Dec 7, 2011 · N319CM · Boeing 767338 · Air Intake Anti/De-Ice SystemSDR IXXA20111019117Switch · out of adjustDURING CRUISE, THE MAIN CARGO DOOR LIGHT ILLUMINATED. THE CREW RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MX PERFORMED FIM PROCEDURES 52-71-00, FIG 106 BLOCKS 1, 2, 11, AND 22. ADJUSTED AFT DOOR LOCK SWITCH IAW AMM 52-71-09/201. DOOR WARNING SYS CHECKEDOct 19, 2011 · N319CM · Boeing 767338 · Door Warning SystemSDR IXXA110070OWarning Light · illuminatedDURING CRUISE, THE MAIN CARGO DOOR LIGHT ILLUMINATED. THE CREW RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. OPENOct 19, 2011 · N319CM · Boeing 767338 · Door Warning SystemSDR IXXA110067OSwitch · out of adjustDURING CLIMB OUT, FAULT CODE 52-34-XB-00, MAIN CARGO DOOR LIGHT ILLUMINATED. THE CREW RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MX TROUBLESHOT MAIN CARGO DOOR SYS AND FOUND LOCK BAR SWITCH OUT OF ADJUSTMENT. THEY ADJUSTED LOCK BAR SWITCH IAW IAI MM SUPOct 7, 2011 · N319CM · Boeing 767338 · Cargo/Baggage DoorsSDR IXXA1100660Warning Light · false activationDURING CLIMB OUT, FAULT CODE 52-34-XB-00, MAIN CARGO DOOR LIGHT ILLUMINATED. THE CREW RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MX PERFORMED CARGO DOOR OPS CHECK IAW IAI 52-32-00. PRESSURIZED ACFT TO 4.5 IAW MM 05-51-22. INDICATIONS WERE NORMAL. INSPECOct 7, 2011 · N319CM · Boeing 767338 · Door Warning SystemSDR IXXA110064OShutoff Valve · defectiveDURING DESCENT, SHORTLY AFTER FLAPS 1 SELECTED; EICAS MESSAGES DISPLAYED, C HYD PRIME 1, REV BRAKE VALVE, HYD QTY AND RESERVE BRAKE & STEERING SWITCH VALVE. CREW ACCOMPLISHED CHECKLIST PROCEDURES, AN ADVISORY IN CHECK LIST PROCEDURES WARNED OF POSSIBLE LOSSep 24, 2011 · N319CM · Boeing 767338 · Hydraulic System, MainSDR IXXA110053SStructure · crackedDURING PRE DEPARTURE CHECK FOUND LT INBD T/E FLAP CRACKED. FABRICATED AND INSTALLED REPAIR IAW SRM 57-33-01, FIG 201. ACFT RETURNED TO SERVICE.Aug 10, 2011 · N316CM · Boeing 767338 · Trailing Edge FlapsSDR AU510002189Idg · failedRT ENGINE INTEGRATED DRIVE GENERATOR (IDG) FAILED. INVESTIGATION CONTINUING.Dec 12, 2005 · Boeing 767338 · AC Generator-AlternatorSDR AU510002162Valve · faultyRT ENGINE PRESSURE REDUCING VALVE (PRV) SUSPECT FAULTY.Dec 12, 2005 · Boeing 767338 · Pneumatic Distribution SystemSDR AU510002128Oil System · lowAPU OIL QUANTITY LOW. INVESTIGATION CONTINUING.Dec 12, 2005 · Boeing 767338 · APU Oil SystemSDR AU510002115Fitting · shearedLT INBOARD TRAILING EDGE FLAP OUTBOARD HINGE FITTING OUTBOARD LUG SHEARED. FOUND DURING INSPECTION IAW AD/B767/188 (EI 767-57-073).Dec 12, 2005 · Boeing 767338 · Trailing Edge FlapsSDR AU510002113Hose · leakingRT MAIN LANDING GEAR RETRACTION CYLINDER DOWN LINE HOSE LEAKING. LOSS OF HYDRAULIC FLUID.Dec 12, 2005 · Boeing 767338 · Landing Gear Retraction/Extension SystemSDR AU510002048Adc · failedAIR DATA COMPUTER (ADC) FAILED.Dec 12, 2005 · Boeing 767338 · Air Data ComputerSDR AU510002037Rotor · disintegratedMAIN LANDING GEAR NR 6 BRAKE ROTOR DISINTEGRATED.Dec 12, 2005 · Boeing 767338 · BrakeSDR AU510001910Pressure Valve · faulty(AUS) RT ENGINE BLEED AIR SYSTEM PRESSURE REGULATING VALVE (PRV) FAILED. INVESTIGATION FOUND EXCESSIVE BUTTERFLY SHAFT PLAY DUE TO WORN CARBON SHAFT BUSHINGS. (CASA NR 510001910)Dec 12, 2005 · Boeing 767338 · Pneumatic Distribution SystemSDR AU510001904Clutch · faulty(AUS) NR 1 ENGINE AUTO THROTTLE CLUTCH PACK FAULTY. INVESTIGATION FOUND THE TORQUE LIMITER FAILED TO JUMP TO THE NEXT POSITION AT THE FORCE OF 49 POUNDS TO 60 POUNDS FOR BOTH CLUTCHES. (CASA NR 510001904)Dec 12, 2005 · Boeing 767338 · Power Lever
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