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"

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SDR ABXA2014022830Angle · crackedSTATION 266 BACK SIDE OF FLOOR BEAM VERTICAL STRAP CRACKED LT SIDE FWD ACCESSORY. REMOVED DAMAGED ANGLE INSTALLED NEW ANGLE PN 141T5198 IAW 51-40-02. SDR PN 141T5198, SN NSN, PART NAME ANGLE BRACKET, CRACKED 1/2 INCHES. FUSELAGE STATION & BODY STATION LOCAFeb 28, 2014 · N798AX · Boeing 767200 · Fuselage Main, Floor BeamSDR 2012F00080Valve · openDURING CRUISE, WITH EQUIPMENT COOLING SWITCH IN STANBY, EICAS MESSAGE " FWD EQPT OVHT" DISPLAYED AND OVERHEAT LIGHT ILLUMINATING. IAW AMM TASK CARD 21-58-29-004-001 R & R DIFFERENTIAL PRESSURE SWITCH. R & R EQUIPMENT COOLING INDICATION CONTROL IAW AMM 21-58-May 5, 2012 · N768QT · Boeing 767200 · Cabin Cooling SystemSDR XV6A2012021600001Battery Pack · inoperativeRIGHT OVERWING EMERGENCY EXIT SIGN INOPERATIVE. REPLACED EMERGENCY BATTERY PACK FOR THIS POSITION IAW B737 AMM 33-51-07. NOTE: TIMES BELOW ARE NOT CORRECT DUE TO PART IS NOT TIME CONTROLLED.Feb 16, 2012 · N766VA · Boeing 767200 · Emergency LightingSDR FOTR201112172268Structure · damagedLT WING L/E SLAT NR 3 INBD LOWER CORNER IS DAMAGED. REPAIRED ON FAS W/O 8233, NR 2268.Dec 17, 2011 · N767AN · Boeing 767200 · Leading Edge DevicesSDR ABXR2011122200054Angle · corrodedLARGE AREA OF CORROSION BENEATH R2 DOOR THRESHOLD DRAIN CHANNEL. REPLACED ANGLE IAW SRM 51-40-02.Apr 21, 2011 · N734AG · Boeing 767200 · Fuselage Miscellaneous StructureSDR ABXR2011122200053Stringer · crackedSTRINGER 33RT HAS APPROX 2" CRACK AT BS 1081 IN AFT LOWER CARGO. REPAIRED STRINGER 33RT AT STA 1081 IAW SRM 53-00-03.Apr 18, 2011 · N734AG · Boeing 767200 · Fuselage Main, Longeron/StringerSDR ABXR2011122200052Mount · corrodedNR 2 ENGINE AFT MOUNT CORRODED. INSTALLED NEW MOUNT IAW AMM 71-21-02.Apr 16, 2011 · N734AG · Boeing 767200 · Engine Mount SectionSDR MU1Z2011020200002Angle · crackedDURING HFEC INSPECTION CLOSE OUT ANGLE OF THE RT PYLON WAS FOUND CRACKED.Feb 22, 2011 · N421AV · Boeing 767200 · Nacelle/Pylon Miscellaneous StructureSDR ANCF2010100900068Engine · leakingRIGHT PACK INOP LIGHT ILLUMINATED EICAS MESSAGE RT PACK TEMP DISPLAYED. LIGHT DID NOT EXTINGUISH WHEN STBY SELECTED. RESET PUSHED, LIGHT EXTINGUISHED THEN RE-ILLUMINATED. LIGHT SMOKE COMING FROM THE GASPERS IN BOTH CABIN SECTIONS. LIGHT SMOKE STOPS FLOWING Oct 9, 2010 · N421AV · Boeing 767200 · Turbine Engine Oil SystemSDR TAMF20100045SFrame · damagedDURING SC4 CHECKS, INSP FOUND FUSELAGE FRAME WEB STA 1395, RBL 14.5, STR 37R-38R DAMAGE ALONG HOLES AND BEND ON SKIN, REPAIR ACCOMPLISHED IAW EWO 767-53-103R0, SR 1-1631817691.Jul 15, 2010 · N767QT · Boeing 767200 · Fuselage Main, FrameSDR ABXA201003220008Warning System · malfunctionedDURING INITIAL CLIMB AT ABOUT 2000FT AGL THE MAIN CARGO DOOR INDICATIONS WENT OFF, LIGHT & SIREN. DEFERRED MAIN CARGO DOOR INDICATION IAW B767 CODE 11 MEL 52-71-1-2. RE-INSPECT DI, VERIFY CLOSE/LATCH PLACARD INSTALLED - CLEAR - INSPECTED HOOK AND LATCH SWITCMar 21, 2010 · N792AX · Boeing 767200 · Door Warning SystemSDR ABXA201003260020Skin · crackedLEFT OUTBOARD FLAP AFT SKIN IS CRACKED AT INBOARD END CAP. REPAIRED DAMAGED AREA IAW 767 SRM 51-70-03.Dec 14, 2009 · N752AX · Boeing 767200 · Trailing Edge FlapsSDR ABXA201003260019Support Beam · crackedNR 1 ENGINE PYLON SUPPORT BEAM IS CRACKED AND HAS LOOSE / MISSING NUT PLATES CON TO PANEL 437ERX. REPAIRED SUPPORT BEAM IAW REA B654-58641-MR.Dec 9, 2009 · N752AX · Boeing 767200 · Nacelle/Pylon Miscellaneous StructureSDR ABXA200907280037Spring · out of positionCLOSING SWITCH GUARD ON EMERGENCY LIGHT SWITCH TURNS EMERGENCY LIGHTS OFF. FOUND GUARD SWITCH COVER TOGGLE SPRING OFF OF EMERGENCY LIGHT TOGGLE SWITCH. RE-ATTACHED SPRING & FUNCTION CHECKED GOOD.Jul 28, 2009 · N792AX · Boeing 767200 · Emergency LightingSDR 2009FA0000487Duct · brokenAFTER A BANG HEARD DURING CL, FWD EQPT OVHT DISPLAYED AND OVHT LGT ILLUM AFTER SELECTOR WAS POSITIONED TO STBY, LGT REILLUM FOLLOWING 5MIN DELAY AFTER SELECTOR WAS POSITIONED TO OVRD. EICAS MSG FWD EQPT COOLING DISPLAYED AND NO COOLING LGT ILLUM. WX FAIL AND HJun 2, 2009 · N767QT · Boeing 767200 · Air Distribution SystemSDR TAMF20090028ODuct · brokenAFTER A BANG HEARD DURING CLIMB, FWD EQPT OVHT DISPLAYED AND OVHT LGT ILLUM AFTER SELECTOR WAS POSITIONED TO STBY, LGT REILLUM FOLLOWING 5MIN DELAY AFTER SELECTOR WAS POSITIONED TO OVRD. EICAS MSG FWD EQPT COOLING DISPLAYED AND NO COOLING LGT ILLUM. WX FAIL ANJun 2, 2009 · N767QT · Boeing 767200 · Air Distribution SystemSDR ANCF2009051500043Module · faultyAFTER LIFT OFF FIRE AURAL WARNING SOUND CONTINUOSLY WITHOUT ANY INDICATION UNTIL ON GROUND, C/B H35 WAS PULLED IAW FIM 31-51-00 FIG 103 BLOCKS 1 TO 6 AND 50 AND IAW AMM 31-51-04 PAGE 401. THE BELL CHIME AURAL WARNING MODULE (M1000) WAS REPLACED, PERFORMED OPMay 15, 2009 · N421AV · Boeing 767200 · Fire DetectionSDR ABXA080153Control Panel · defectiveAFTER TAKEOFF FROM STA JFK, RIGHT ENGINE OVERHEAT LIGHT AND EICAS MESSAGE. PERFORMED NON NORMAL - SECURED RIGHT ENGINE. LIGHT DID NOT GO OUT AFTER THRUST LEVER RETARDED. AN EMERGENCY WAS DECLARED AND AN AIR TURNBACK TO JFK WAS PERFORMED. TROUBLESHOT PER FIMay 17, 2008 · N799AX · Boeing 767200 · Overheat DetectionSDR TAMF20080022OCircuit Card · burnedAFTER TAKEOFF WHEN LANDING GEAR LEVER WAS MOVED TO UP A SMOKE FUME APPEARED IN THE COCKPIT (P3-1) WITH NO VISUAL EVIDENCE OF FIRE. AC RETURNED TO DEPARTURE. AFTER MAINT, INSP ON PANEL LIGHT DOOR MODULE KIT (P3-1) 2 DIODES FOUND BURN. NO ADDITIONAL DAMAGES WEMay 1, 2008 · N767QT · Boeing 767200 · Landing Gear System WiringSDR TAMF20080016SSill · corrodedDURING C2 CHECK WAS FOUND CORROSION ON AFT CARGO DOOR SURROUND STRUCTURE MAIN SILL - INNER CHORD - RT. CORROSION WAS REMOVED IAW SRM 51-10-02 PAGE 12-13. THICKNESS OUT OF LIMITS. TEMPORARY REPAIR WAS PERFORMED IAW EWO 767 53-076 PART I AND MFG SERVICE REQUESTMar 17, 2008 · N770QT · Boeing 767200 · Fuselage Miscellaneous StructureSDR TAMF20080021SSkin · corrodedDURING (C2) CHECK WAS FOUND SKIN PN 146T3240 WITH CORROSION. STA 1417, STRINGER 36 RT. DAMAGED AREA WAS REPAIRED IAW EWO 767-53-075 AND SR 1-79124788. FAA FORM 8100-9 WAS ISSUED APPROVING THIS REPAIR.Mar 16, 2008 · N770QT · Boeing 767200 · Fuselage Main, Plate/SkinSDR TAMF20080015SSill · corrodedDURING C2 CHECK WAS FOUND CORROSION ON LOWER SILL OF LARGE CARGO DOOR CUTOUT BETWEEN STA 500-522. DAMAGED AREA WAS REPAIRED IAW EWO 767 53-074 AND MFG SERVICE REQUEST 1-791518899. THIS REPAIR CONSTITUTES A MAJOR REPAIR. FAA FORM 8100-9 WAS ISSUED APPROVING THIMar 16, 2008 · N770QT · Boeing 767200 · Fuselage Miscellaneous StructureSDR TAMF20080019SRib · corrodedCORROSION ON LT WING OB L/E RIB LOWER OUTER CHORD AT STA 441.60. CORRECTIVE ACTION: RIB WAS FABRICATED AND INSTALLED IAW MFG AUTHORIZATION PO214240, DRAWING 114T2200 AND SRM 51-40-02 PG 1-7.Mar 15, 2008 · N770QT · Boeing 767200 · Wing, Rib/BulkheadSDR ABXA080131Strap · crackedSTRAP ON UPPER CAP OF FRONT SPAR WAS CRACKED LES 485. REMOVED AND REPLACED UPPER SPAR CAP STRAP SECTIONS IAW B767 SRM.Mar 14, 2008 · N752AX · Boeing 767200 · Wing SparSDR ABXA080130Keelbeam · corrodedLOWER RIGHT KEEL BEAM APPROXIMATELY STA 970 CORRODED. BLENDED CORROSION ON LOWER RIGHT KEEL BEAM STA 970 IAW B767 SRM.Mar 14, 2008 · N752AX · Boeing 767200 · Fuselage Main, KeelSDR ABXA080129Keelbeam · corrodedLOWER RIGHT KEEL BEAM CORD APPROXIMATELY STA 1030 - CORRODED. BLENDED CORROSION ON LOWER RIGHT KEEL BEAM STA 1030 IAW B767 SRM.Mar 14, 2008 · N752AX · Boeing 767200 · Fuselage Main, KeelSDR TAMF20080014SSpar · corrodedDURING C2 CHECK INSPECTION WAS FOUND CORROSION ON THE CENTER WING REAR SPAR WEB NEAR RBBL 75 AT THE REAR SPAR BULKHEAD FITTINGS. DAMAGED AREA WAS BLENDED TO A MINIMUM WEB THICKNESS OF 0.288 INCHES AND NDT (EDDY CURRENT) INSPECTION DID NOT REVEAL ANY REMAINING Mar 14, 2008 · N770QT · Boeing 767200 · Wing SparSDR ABXA080137Skin · crackedL1 DOOR CUTOUT LOWER AFT CORNER INTERIOR DOUBLER HAD 2 EACH .25 INCH CRACKS AT THE FASTENER HOLE AND THE EXTERIOR SKIN HAD A .125 INCH CRACK AT SAME HOLE. REPAIRED L1 DOOR CUTOUT LOWER AFT CORNER IAW REA B653-57165-MR.Mar 13, 2008 · N752AX · Boeing 767200 · Fuselage Main, Plate/SkinSDR ABXA080128Skin · crackedCRACK IN SKIN APPROXIMATELY 1.375" LONG AT FASTENER FS 1654 AT STRINGER 6 LEFT. REPAIRED AREA IAW B767 SRM 53-80-01.Mar 13, 2008 · N752AX · Boeing 767200 · Fuselage Main, Plate/SkinSDR ABXA080127Skin · crackedL1 DOOR CUTOUT LOWER AFT CORNER INTERIOR DOUBLER HAD 2 EACH .25 INCH CRACKS AT THE FASTENER HOLE AND THE EXTERIOR SKIN HAD A .125 INCH CRACK AT THE SAME HOLE. REPAIRED L1 DOOR CUTOUT LOWER AFT CORNER IAW REA B653-57165-MR.Mar 13, 2008 · N752AX · Boeing 767200 · Fuselage Main, Plate/SkinSDR ABXA080126Door Frame · crackedR1 DOOR CUTOUT LOWER AFT CORNER INTERIOR DOUBLER HAD A .125 INCH CRACK AT THE FASTENER HOLE. REPLACED R1 DOOR CUTOUT LOWER AFT CORNER IAW REA 13653-57164-MA.Mar 13, 2008 · N752AX · Boeing 767200 · Fuselage Main, StructureSDR TAMF20080020SFitting · crackedDURING C CHECK INSPECTION WAS FOUND A CRACK ON CF6-80C2, THRUST REVERSER FITTING P/N 3114M90-001 AT 2 O’CLOCK. DAMAGED AREA WAS REPAIRED IAW EWO 767 54-036 AND TAC-080316. THIS REPAIR IS CLASSIFIED AS TEMPORARY REPAIR AND THE AFFECTED FITTING MUST BE CHANGED AMar 13, 2008 · N770QT · Boeing 767200 · Engine Thrust ReverserSDR TAMF20080013SDoor · corrodedDURING C2 CHECK INSPECTION WAS FOUND CORROSION ON MAIN FUEL TANK ACCESS DOORS 541LB AND 541GB PN: 112N6101-3. DAMAGED AREA WAS BLENDED TO A MINIMUM DOOR THICKNESS OF 0.120 INCHES (541LB) AND 0.106” INCHES (541GB). NDT (EDDY CURRENT) INSPECTION WAS PERFORMED AMar 13, 2008 · N770QT · Boeing 767200 · Fluid Service DoorsSDR TAMF20080012SSplice · crackedDURING C2 CHECK INSPECTION WAS FOUND A CRACK ON SPLICE PLATE FRONT SPAR LOWER CHORD STA ISS 256.15 261.26 - RT. DAMAGED AREA WAS REPAIRED IAW EWO 767 57-041 AND MFG SERVICE REQUEST 1-789000676. THIS REPAIR CONSTITUTES A MAJOR REPAIR. FAA FORM 8100-9 WAS ISSUMar 13, 2008 · N770QT · Boeing 767200 · Wing SparSDR TAMF20080011OCdu · malfunctionedPILOT REPORT, DURING TAXIING RIGHT CDU WENT BLANK ALONG WITH ELECTRICAL SMOKE. INITIALLY ITEM WAS TRANSFERRED TO DMI 09052 MEL 34-61-1-1 CAT C, AND MAP 34-61-1-1 WAS PERFORMED. RIGHT CDU WAS REMOVED AND REPLACED IAW AMM 34-61-02 PG 201-206.Mar 7, 2008 · N769QT · Boeing 767200 · Central DisplaySDR TAMF20080010SSlat · damagedDURING CHECK INSPECTION WAS FOUND A BIRD STRIKE ON SLAT 12. DAMAGED AREA WAS REPAIRED IAW EWO 767-57-037 AND IAAC TAC-080225 REPAIR ORDER. FAA FORM 8110-3 WAS ISSUED APPROVING THIS REPAIR.Mar 1, 2008 · N769QT · Boeing 767200 · Leading Edge DevicesSDR TAMF20080001SAccess Door · corrodedDURING INSPECTION CHECK, FOUND LT WING 541AB MAIN FUEL TANK ACCESS DOOR OUTER SKIN WITH A SCRATCH AND CORROSION. DAMAGED AREA WAS REPAIRED IAW EWO 767-57-038 AND BOEING SERVICE REQUEST 1-771920168. THIS REPAIR IS CLASSIFIED AS MAJOR REPAIR. FAA FORM 8100-9 Mar 1, 2008 · N769QT · Boeing 767200 · Wing, Plate/SkinSDR TAMF20080003SSkin · nickedDURING C CHECK INSPECTION, FOUND SKIN CORROSION AND NICK ON STA 478.6 STRINGER 31RT. DAMAGED AREA WAS REPAIRED IAW EWO 767-53-071 AND BOEING SERVICE REQUEST 1-775312353. FAA FORM 8100-9 WAS ISSUED APPROVING THIS REPAIR.Feb 29, 2008 · N769QT · Boeing 767200 · Fuselage Main, Plate/SkinSDR TAMF20080008SFitting · crackedDURING C CHECK INSPECTION, FOUND THRUST REVERSER FITTING POS 4 O'CLOCK CRACKED. DAMAGED AREA WAS REPAIRED IAW EWO 767-54-032 AND IAAC TAC-080227. FAA FORM 8110-3 WAS ISSUED APPROVING THIS REPAIR.Feb 27, 2008 · N769QT · Boeing 767200 · Engine Thrust ReverserSDR TAMF20080004SSplice Plate · crackedDURING C CHECK INSPECTION WAS FOUND A CRACK ON LEFT WING LEADING EDGE LOWER SPLICE PLATE - ISS 257-. DAMAGED AREA WAS REPAIRED IAW EWO 767-57-035 AND BOEING SERVICE REQUEST 1-773976194. FAA FORM 8100-9 WAS ISSUED APPROVING THIS REPAIR.Feb 26, 2008 · N769QT · Boeing 767200 · Wing Miscellaneous StructureSDR TAMF20080009SFrame · crackedDURING C CHECK INSPECTION, FOUND CRACK DAMAGE AT FRAME P/N 491B1330014-003 AT 5 O’CLOCK POSITION OF THRUST REVERSER P/N 681L272G07 (RT). DAMAGED AREA WAS REPAIRED IAW EWO 767-54-031 AND IAAC TAC-080226. FAA FORM 8110-3 WAS ISSUED APPROVING THIS REPAIR. THISFeb 26, 2008 · N769QT · Boeing 767200 · Engine Thrust ReverserSDR TAMF20080006SWeb · chafedDURING C CHECK INSPECTION, FOUND CLOSURE RIB WEB WITH CHAFING OUT OF LIMITS AT LT WING INBOARD AILERON. DAMAGED AREA WAS REPAIRED IAW EWO 767-57-033 AND BOEING SERVICE REQUEST 1-773827820. FAA FORM 8100-9 WAS ISSUED APPROVING THIS REPAIR.Feb 25, 2008 · N769QT · Boeing 767200 · AileronsSDR TAMF20080002SRib · chafedDURING INSPECTION CHECK, FOUND A WEAR OUT OF LIMITS ON INBOARD AILERON RT OUTBOARD CLOSURE RIB WEB. DAMAGED AREA WAS REPAIRED IAW EWO 767-57-034 AND BOEING SERVICE REQUEST 1-773827820. FAA FORM 8100-9 WAS ISSUED APPROVING THIS REPAIR.Feb 25, 2008 · N769QT · Boeing 767200 · AileronsSDR TAMF20080007SSkin · chafedDURING C CHECK INSPECTION, FOUND SKIN WEAR ON RUB STRIPS, STA 1725.5 STRINGER 22RH. DAMAGED AREA WAS REPAIRED IAW EWO 767-53-070 AND BOEING SERVICE REQUEST 1-773844480. FAA FORM 8100-9 WAS ISSUED APPROVING THIS REPAIR.Feb 18, 2008 · N769QT · Boeing 767200 · Fuselage Main, Plate/SkinSDR ABXA070427Connector · looseLOST THE LEFT ENGINE AT CRUISE. DID ENGINE SECURE CHECKLIST, NO OTHER ABNORMALITIES. CREW ACCOMPLISHED ENGINE INFLIGHT START. THE ENGINE STARTED FINE, LANDED AT MSP. INSPECTED ENGINE INLET AND EXHAUST, NO DEFECTS. SUMPED MAIN FUEL FILTER, NO DEBRIS NOTED.Dec 24, 2007 · N799AX · Boeing 767200 · Engine Fuel System WiringSDR TAMF20070038SSkin · damagedDURING TRANSIT CHECK THE AIRPLANE WAS HIT AT FUSELAGE WITH A STAIRWAY. SECTION 43, STA 347, STRINGER 31 RT. DAMAGED AREA WAS REPAIRED IAW SRM 53-00-01 REPAIR 1 AND EWO 767-53-061. THIS REPAIR IS CLASSIFIED AS TEMPORARY REPAIR. PERMANENT REPAIR WAS PERFORMED Nov 30, 2007 · N770QT · Boeing 767200 · Fuselage Main, Plate/SkinSDR TAMF20070033SSkin · dentedDURING INSPECTION OF (C2) CHECK WAS FOUND A DENT A/Y=25 ON SKIN STA 1307-1329 STR 32-33 - LT. DAMAGED AREA WAS REPAIRED IAW EWO 767-53-052 AND SRM 53-00-01 REPAIR 6. THIS REPAIR CONSTITUTES A MAJOR REPAIR.Aug 29, 2007 · N768QT · Boeing 767200 · Fuselage Main, Plate/SkinSDR TAMF20070024SSpar · damagedDURING C CHECK INSPECTION (TASK CARD 57-650-00) WAS FOUND LOOSE MATERIAL ON SPLICE PLATE AT FRONT SPAR STA ISS 864.92 873.13 RT. DAMAGED AREA WAS REPAIRED IAW EWO 767-57-028 AND SERVICE REQUEST 1-527347746. THIS REPAIR CONSTITUTES A MAJOR REPAIR. FAA FORM 81Aug 28, 2007 · N768QT · Boeing 767200 · Wing SparSDR TAMF20070037SStrap · corrodedDURING INSPECTION OF (C2) CHECK WAS FOUND A CORROSION ON CARGO DOOR SURROUND STRUCTURE, SAFE FAIL STRAP P/N 146T8048-3. REMOVED, FABRICATED AND INSTALLED A NEW FAIL SAFE STRAP P/N 146T8048-3 IAW EWO 767-53-057 AND SERVICE REQUEST 1-557292575. THIS REPAIR CONAug 27, 2007 · N768QT · Boeing 767200 · Fuselage Miscellaneous StructureSDR TAMF20070025SSpar · damagedDURING C CHECK INSPECTION (TASK CARD 06-102-01-1) WAS FOUND A LOOSE MATERIAL ON SPLICE PLATE AT FRONT SPAR STA ISS 1009 - 1017 LT. DAMAGED AREA WAS REPAIRED IAW EWO 767-57-027 AND SERVICE REQUEST 1-526643882. THIS REPAIR IS CONSIDERED A MAJOR REPAIR. FORM 810Aug 27, 2007 · N768QT · Boeing 767200 · Wing Spar
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