Boeing 767-223

Service difficulty reports · 2,039

Newest first. General aviation reporting is voluntary.

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 = '767223'
  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 ABXA20150930186Skin · corrodedFOUND CORROSION AT APPROX WS 110 RT WING TE FLANGE. REMOVED CORROSION AT UPPER RT WING TE WBL110, PN 112T3101-6 IAW REA B657-61760-MR. SDR INFO, CORRODED LEVEL 2, PN 112T3101-6, SN NSN, PART NAME SKIN, FROM WS110. ACFT WAS GNDED.Sep 30, 2015 · N315AA · Boeing 767223 · Wing, Plate/SkinSDR ABXA20150930159Structure · corrodedLEFT WING ACCESS PANEL 552AB HAS CORROSION ON AFT INBD FLANGE UPPER SIDE. GAINED ACCESS & REMOVED LOWER TE CHORD AT WS 157 - 228. INSTALLED NEW CHORD PN 654T0391-35 & REINSTALLED PANELS IAW DWG 113T1400 & SRM CH51-40-02-PAR 7. CORRODED, PART NAME CHORD, PN Sep 30, 2015 · N312AA · Boeing 767223 · Wing Miscellaneous StructureSDR ABXA20150929168Longeron · corrodedLEFT WW FS APPROX 980 OVERWING LONGERON TOP SIDE HAS CORRODED FASTENERS & POSSIBLY AROUND BASE OF FASTENERS. REMOVED CORROSION, ORIGINAL MATERIAL .080, REMOVED .003, REMAINING .077 IAW REA B653-61756-MR, RFTS NR E-46344 REV DATE ER 9 23 15. SDR INFO CORRODEDSep 29, 2015 · N315AA · Boeing 767223 · Fuselage Main, Longeron/StringerSDR ABXA20150928187Failsafe · crackedFOUND CRACK AT LOWER OF 3 FASTENER HOLES INSPECTED. CRACK PLAINLY VISIBLE. REPAIRED AREA IAW DOCUMENT 470080RD06 & EA 53500014-003. SDR, CRACKED, LENGTH : 1.7 INCHES, PN 14T9524-22, PART NAME FAIL SAFE, SN NSN, FS & BS LOCATION SM 955, STRINGER & WS LOCATIOSep 28, 2015 · N315AA · Boeing 767223 · Fuselage Main, FrameSDR ABXA20150924157Stringer · corrodedCORROSION WHERE STRINGER 35L MEETS FUSELAGE SKIN AT FS 412, FOUND CORROSION ON STRINGER 35L, STATION 412, OUT OF LIMITS. FABRICATED STRINGER IAW SRM 53-00-03 FIG 201 REPAIR 2. CORRODED, PN 144T3001, PART NAME STRINGER, SN NSN, FS & BS LOCATION 412, STRINGER Sep 24, 2015 · N312AA · Boeing 767223 · Fuselage Main, Longeron/StringerSDR ABXA20150923158Skin · crackedFORWARD LOWER CORNER OF R1 DOOR HAS AN EXTERNAL HFEC CRACK INDICATION, APPROX 3/8" LONG. INSTALLED REPAIR TO FWD LOWER CORNER OF R1 DOOR CUT OUT IAW SRM 53-10-01. PN 141T3330, PART NAME SKIN, CRACKED 3/8", EXACT FS LOCATION ON ACFT 287. ACFT WAS GROUNDED.Sep 23, 2015 · N312AA · Boeing 767223 · Passenger/Crew DoorsSDR ABXA20150924191Angle · corrodedUPON CURSORY INSPECTION FOUND CORROSION WITHIN AREA UNDER FWD HEAT SHIELD PANEL AT LOWER AFT PYLON AREA, JUST ABOVE AFT EDGE OF EXHAUST NOZZLE, APPROX NAC STATION 350. R & R CORRODED ANGLE INSIDE OF FWD HEAT SHIELD PANEL AREA IAW SRM 51-40-02. SDR INFO, CORRSep 21, 2015 · N315AA · Boeing 767223 · Nacelle/Pylon Miscellaneous StructureSDR ABXA20150918171Spar · corrodedCORROSION UNDER NUTPLATE ON UPPER CHORD OF WING REAR SPAR TO TE BEAM AT WING STATION 434, OTBD SIDE AS SEEN THRU PANEL 561AB. R & R UPPER CHORD OF WING REAR SPAR IAW SRM BCSF 51-40-02 PARA 7 D. SDR INFO CORRODED LEVEL 2, PN 113T1510-33, SN NSN, PART NAME CHOSep 18, 2015 · N315AA · Boeing 767223 · Wing SparSDR ABXA20150914185Support Fitting · corrodedFLAP SUPPORT NR 1, TENSION BOLT HOLE NR 1 HAS A DEFECT INDICATION, REFERENCE JC EA5750006-001. REAMED HOLE TO .672, NO FURTHER DEFECTS NOTED, REFERENCE REA B657-61708-MR REV A. SDR INFO CORRODED LEVEL 2, PN 113T1345-43, PART NAME, FLAP SUPPORT FITTING NR 1, Sep 14, 2015 · N315AA · Boeing 767223 · Wing, Control Surface Attach FittingsSDR ABXA20150914184Support Fitting · corrodedFLAP SUPPORT NR 2, TENSION BOLT HOLE NR 3 HAS A DEFECT INDICATION, REFERENCE JC A57500018-001. REAMED FASTENER HOLE TO .8285, NO DEFECTS NOTED REFERENCE REA B657-61708-MR REV A. SDR INFO CORRODED LEVEL 2, PN 113T1345-48, PART NAME, FLAP SUPPORT FITTING NR 2,Sep 14, 2015 · N315AA · Boeing 767223 · Wing, Control Surface Attach FittingsSDR ABXA20150914183Support Fitting · corrodedFLAP SUPPORT NR 2, TENSION BOLT HOLE NR 2 HAS A DEFECT INDICATION, REFERENCE JC A57500018-001. REAMED HOLE TO .829, NO DEFECTS NOTED REFERENCE REA B657-61708-MR REV A. SDR INFO CORRODED LEVEL 2, PN 113T1345-48, PART NAME, FLAP SUPPORT FITTING NR 2, WS LOCATISep 14, 2015 · N315AA · Boeing 767223 · Wing, Control Surface Attach FittingsSDR ABXA20150914182Support Fitting · corrodedFLAP SUPPORT NR 2, TENSION BOLT HOLE NR 1 HAS DEFECT INDICATION, REFERENCE JC EA57500018-001. REAMED FASTENER HOLE TO .8285, NO FURTHER DEFECTS, REFERENCE REA B657-61708-MR REV A. SDR INFO CORRODED LEVEL 2, PN 113T1345-48, PART NAME, FLAP SUPPORT FITTING NR Sep 14, 2015 · N315AA · Boeing 767223 · Wing, Control Surface Attach FittingsSDR ABXA20150914181Support Fitting · corrodedFLAP SUPPORT NR 7, TENSION BOLT HOLE NR 4 HAS DEFECT INDICATION, REFERENCE JC EA57500019-001. REAMED FASTENER HOLE TO .7985, NO DEFECTS NOTED IAW REA B657-61708-MR REV A. SDR INFO, CORRODED LEVEL 2, PN 113T1345-47, PART NAME FLAP SUPPORT FITTING NR 7, WS LOCSep 14, 2015 · N315AA · Boeing 767223 · Wing, Control Surface Attach FittingsSDR ABXA20150914180Support Fitting · corrodedFLAP SUPPORT NR 7 TENSION BOLT HOLE NR 2 HAS A DEFECT INDICATION, REFERENCE JC EA57500019-001. REAMED FASTENER HOLE TO .7985, NO DEFECTS NOTED IAW REA B657-61708-MR REV A. SDR INFO CORRODED LEVEL 2, PN 113T1345-47, PART NAME FLAP SUPPORT FITTING NR 7, WS LOCSep 14, 2015 · N315AA · Boeing 767223 · Wing, Control Surface Attach FittingsSDR ABXA20150914179Support Fitting · corrodedFLAP SUPPORT NR 7 TENSION BOLT HOLE 1 HAS A DEFECT INDICATION, REFERENCE JC EA57500019-001. REAMED FASTENER HOLE TO .7985, NO DEFECTS NOTED IAW REA B657-61708-MR REV A. SDR INFO, CORRODED LEVEL 2, PN 113T1345-47, PART NAME FLAP SUPPORT FITTING 7, WS LOCATIOSep 14, 2015 · N315AA · Boeing 767223 · Wing, Attach FittingsSDR ABXA20150914178Support Fitting · corrodedFLAP SUPPORT 8 TENSION BOLT HOLE 4 HAS DEFECT INDICATION. REFERENCE JC EA57500017-001. REAMED FASTENER HOLE TO .875, NO DEFECTS NOTED IAW REA B657-61708-MR REV A. SDR INFO, CORRODED LEVEL 2, PN 113T1345-44, PART NAME FLAP SUPPORT FITTING 8, WS LOCATION 798 Sep 14, 2015 · N315AA · Boeing 767223 · Wing, Attach FittingsSDR ABXA20150914177Support Fitting · corrodedNUMBER 8 FLAP SUPPORT TENSION BOLT HOLE 3 HAS A DEFECT INDICATION. REFERENCE JC EA57500017-001. REAMED FASTENER HOLE TO .672, NO DEFECTS NOTED IAW REA B657-61078-MR REV A. SDR INFO, CORRODED LEVEL 2, PN 113T1345-44, PART NAME FLAP SUPPORT FITTING 8, WS LOCASep 14, 2015 · N315AA · Boeing 767223 · Wing, Attach FittingsSDR ABXA20150914176Support Fitting · corrodedNUMBER 8 FLAP SUPPORT TENSION BOLT HOLE NR 1, HAS DEFECT INDICATION. REFERENCE JC EA57500017-001. REAMED FASTENER HOLE TO .672, NO DEFECTS NOTED IAW REA B657-61708-MR REV A. SDR INFO CORRODED LEVEL 2, PN 113T1345-44, PART NAME, FLAP SUPPORT FITTING NR 8, WSSep 14, 2015 · N315AA · Boeing 767223 · Wing, Control Surface Attach FittingsSDR ABXA20150910172Beam · crackedNUMBER 2 STRUT INSIDE PANEL 447BR, LOWER BEAM IS CHAFED & CRACKED AT THIRD HOLE FROM THE FWD END. R & R LOWER BEAM INSIDE NR 2 PYLON PANEL 447BR IAW SRM 54-51-71 & DWG 313T2380. SDR INFO, PN 313T2380-29, PART NAME, BEAM, SN NSN, CRACKED .5 INCHES, EXACT FS &Sep 10, 2015 · N315AA · Boeing 767223 · Nacelle/Pylon, Main FrameSDR ABXA201509010155Floorbeam · corrodedAFT LOWER CARGO FLOORBEAM, UPPER CHORD STATION 1153 WAS CORRODED BEYOND LIMITS & WAS REPLACED IAW DWG 146T1204. PN 146T1204-7, SN NSN, PART NAME UPPER CHORD, CORRODED LEVEL 2, EXACT FS & BS LOCATION ON ACFT STATION 1153, EXACT STRINGER & WS LOCATION ON ACFT LSep 10, 2015 · N312AA · Boeing 767223 · Fuselage Main, Floor BeamSDR ABXA20150908152Attach Fitting · corrodedREAR SPAR TO WING TE PANEL ATTACH BEAM, LOWER CHORD CORRODED ABOVE WIRE BUNDLE RACE WAY AT WS 250, INBD & OTBD SIDES AS SEEN IN RT WW. FOUND ATTACH BEAM CORRODED BEYOND LIMITS. REPAIRED ATTACH BEAM IAW SRM 51-70-12 FIG 1 DETAIL III. CORRODED L2, PN 113T1621Sep 8, 2015 · N312AA · Boeing 767223 · Wing, Attach FittingsSDR ABXA20150828156Support Angle · corrodedAFT LOWER CARGO ON UNDER SIDE, CORRODED STATION 1219, LBL 24 - 34. R & R SUPPORT ANGLE 451T2409-2 IAW DWG 451T2402. CORRODED LEVEL 2, PN 451T2409-2, PART NAME SUPPORT ANGLE, SN N/A, FS & BS LOCATION STATION 1219, STRINGER & WS LOCATION LBL 24 TO LBL 34. ACFAug 28, 2015 · N312AA · Boeing 767223 · Fuselage Miscellaneous StructureSDR ABXA20150828153Attach Fitting · corrodedREAR SPAR TO TE, UPPER PANEL ATTACH BEAM, UPPER CHORD CORRODED AROUND NUTPLATES AT WS 290 AS SEEN IN RT WW. FOUND ATTACH BEAM TO BE CORRODED OUT OF LIMITS IAW SRM 51-10-00. R & R ATTACH BEAM IAW SRM 51-40-2 & 51-40-5. CORRODED LEVEL 2, PN 113T1622-125, PARTAug 28, 2015 · N312AA · Boeing 767223 · Wing, Attach FittingsSDR ABXA20150816151Skin · crackedAPU DOOR 316AL EXTERIOR SKIN, LOWER EDGE BENT IN SEVERAL PLACES. FWD CORNER HAD 2 CRACKS .2 INCHES DEEP, OUT OF LIMITS IAW SRM 52-40-01 FIG 101 DETAIL III. ROUTED OUT 2 CRACKS AT EDGE OF PANEL WITHIN LIMITS IAW SRM 52-40-01 FIG 101 DETAIL III. STOP DRILLED Aug 16, 2015 · N312AA · Boeing 767223 · Auxiliary Power Unit (APU) DoorsSDR IXXA20141113033Unknown · unserviceableNUMBER 5 EMER DESCENT DEVICE EXTENDED & UNSERVICEABLE. R & R NR 5 EMER DESCENT DEVICE IAW AMM 25-61-03.Nov 10, 2014 · N761CX · Boeing 767223 · Emergency EquipmentSDR IXXA20141113032Unknown · unserviceableNUMBER 4 EMER DESCENT DEVICE EXTENDED & UNSERVICEABLE. R & R NR 4 EMER DESCENT DEVICE IAW AMM 25-61-03.Nov 10, 2014 · N761CX · Boeing 767223 · Emergency EquipmentSDR IXXA20150115016Skin · corrodedLEFT HORIZONTAL STAB CORROSION ON TOP SURFACE AT REAR SPAR 16, 108 INCHES FROM FUSELAGE, RS STATION 24 - 26.15 & 127.25 - 129.5 ABOVE REAR SPA. REPAIRED IAW REPAIR EO 47120REA08. INBOUND BLEND ACCOMPLISHED IAW EO 47120REA08.Oct 13, 2014 · N761CX · Boeing 767223 · Horizontal Stabilizer, Plate/SkinSDR IXXA20150115012Rib · corrodedPANEL 652HB REAR SPAR TO TE RIB UPPER & LOWER CHORDS CORRODED AROUND NUTPLATES. R & R LOWER CHORD IAW SRM 51-40-02.Oct 10, 2014 · N761CX · Boeing 767223 · Wing, Rib/BulkheadSDR IXXA20150115011Rib · corrodedPANEL 661AB REAR SPAR TO TE ATTACH RIB UPPER CHORD CORRODED AROUND NUTPLATE WS 435. R & R TE UPPER RIB CHORD IAW SRM 51-40-02 & REA 47120REA04.Oct 10, 2014 · N761CX · Boeing 767223 · Wing, Rib/BulkheadSDR IXXA20150115009Attach Fitting · corrodedUPPER TE PANEL ATTACH CHORD CORRODED AROUND NUTPLATE AS SEEN THRU PANEL 652CB OPENING. R & R TE CHORD IAW SRM 51-40-02.Oct 10, 2014 · N761CX · Boeing 767223 · Wing Miscellaneous StructureSDR IXXA20150115004Beam · corrodedREAR SPAR TO TE PANEL ATTACH BEAM AT WS 285 UPPER CHORD CORRODED AROUND NUTPLATES. UPPER PANEL ATTACH CHORD WAS FABRICATED REA 47120REA03 & REPLACED IAW SRM 51-40-02.Oct 10, 2014 · N761CX · Boeing 767223 · Wing Miscellaneous StructureSDR IXXA20150115017Intercostal · corrodedHINGED PANEL 651XB HAS CORROSION AROUND NUTPLATE. REMOVED CORROSION BEYOND LIMITS. NEW INTERCOSTAL FABRICATED. INSTALLED TO PANEL 651XB IAW SRM 51-40-02.Oct 9, 2014 · N761CX · Boeing 767223 · Wing Miscellaneous StructureSDR IXXA20150115008Attach Fitting · corrodedPANEL 652CB AFT ATTACH CHORD SPLIT ON EDGE. R & R AFT ATTACH CHORD AT PANEL 652GB IAW SRM 51-40-2.Oct 8, 2014 · N761CX · Boeing 767223 · Wing Miscellaneous StructureSDR IXXA20150115015Attach Fitting · corrodedTRAILING EDGE PANEL 652EB ATTACH FITTING CORRODED AROUND NUTPLATE. R & R TE PANEL 652EB ATTACH FITTING IAW SRM 51-40-02.Oct 6, 2014 · N761CX · Boeing 767223 · Wing Miscellaneous StructureSDR IXXA20150115006Attach Fitting · corrodedAFT UPPER WING PANEL ATTACH CHANNEL CORRODED AROUND NUTPLATES AS SEEN THRU PANEL 651TB. R & R WING PANEL ATTACH CHANNEL IAW SRM 51-40-02 & REA 47120REA02.Oct 6, 2014 · N761CX · Boeing 767223 · Wing Miscellaneous StructureSDR IXXA20150115005Attach Fitting · corrodedHINGED PANEL 651TB REAR SPAR TO TE OTBD ATTACH CHANNEL SPLIT ON EDGE. R & R ATTACH CHANNEL FOR HINGED PANEL 651TB REAR SPAR TO TE OTBD IAW SRM 51-40-02.Oct 6, 2014 · N761CX · Boeing 767223 · Wing Miscellaneous StructureSDR IXXA20150115014Bulkhead · corrodedNOSE WHEEL BULKHEAD FWD FACE WL 170, RBL 25 CHORD CRACKED. REMOVED DAMAGE SECTION OF CHORD & REPAIRED AREA IAW SRM 51-70-12.Sep 30, 2014 · N761CX · Boeing 767223 · Fuselage Main, BulkheadSDR IXXA20150115013Bulkhead · corrodedNOSE WHEEL BULKHEAD FWD FACE WL 170, LBL 25 CHORD CRACKED. REMOVED DAMAGE SECTION OF CHORD & REPAIRED AREA IAW SRM 51-70-12.Sep 30, 2014 · N761CX · Boeing 767223 · Fuselage Main, BulkheadSDR IXXA20150115007Channel · corrodedLOWER PANEL DIAGONAL ATTACH CHANNEL INBD OF H BLOCK AT WS 289 SPLIT ON EDGE. R & R IAW SRM 51-40-02.Sep 30, 2014 · N761CX · Boeing 767223 · Wing Miscellaneous StructureSDR IXXA20150115010Structure · corrodedPANEL 661AB REAR SPAR TO TE ATTACH RIB LOWER CHORD SPLIT ON EDGE WS 435. LOWER CHORD R & R IAW SRM 51-40-02.Sep 24, 2014 · N761CX · Boeing 767223 · Wing Miscellaneous StructureSDR ABXA20140915293Inverter · damagedCREW REPORTED EICAS MESSAGE STBY INVERTER DISPLAYED, SMOKE IN THE CABIN & A STRONG ELEC BURNING ODOR. THE FLIGHT WAS DIVERTED TO NEAREST SUITABLE AIRPORT. THE STATIC INVERTER WAS REPLACED IAW AMM. 767 FAULT ISOLATION MANUAL PROCEDURES 24-33-807 808 WERE ACCSep 15, 2014 · N315AA · Boeing 767223 · DC Rectifier/ConverterSDR ABXA20140910291Engine · bird ingestionON ROTATION, BIRD STRIKE TO THE LT ENG. CREW HEARD LOUD NOISE & FELT AIRFRAME VIBRATION. LT ENG VIBRATION INDICATED OVER 4.5 & LT THRUST LEVER BEGAN REDUCING TO IDLE. LT ENG WAS SHUTDOWN & CREW PERFORMED AIR TURN BACK. PERFORMED BIRD STRIKE INSPECTION. RESep 10, 2014 · N315AA · Boeing 767223 · Turbine Engine Compressor SectionSDR IXXA201405140080Cable · defectiveNUMBER 2 DESCENT DEVICE CABLE IS EXTENDED, NEEDS REPLACED. IAW MM 25-61-03 R & R NR 2 EMERGENCY DESCENT DEVICE, NO DEFECTS NOTED.May 10, 2014 · N761CX · Boeing 767223 · Emergency EquipmentSDR IXXA2014041100060Battery Pack · dischargedAT SERVICE CHECK RT SIDE EMERGENCY EXIT LIGHT INOPERABLE. R & R EMERGENCY BATTERY PACK AT M736. OPERATIONAL CHECK SATISFACTORY IAW MM SUPP 33-51-00.Apr 9, 2014 · N761CX · Boeing 767223 · Emergency LightingSDR AALA20140206001Sensor · inoperativeDFW INFLIGHT LAX-JFK CREW REPORTED FWD CARGO COMPARTMENT DOOR LIGHT ILLUMINATED DURING CRUISE. EMERGENCY DECLARED FLIGHT DIVERTED DFW LANDED WITHOUT INCIDENT. PLACARDED FWD CARGO DOOR INDICATION INOPERATIVE IAW MEL 52-8. AUTHORIZATION 2-198DC-C. FWD CARGO Feb 6, 2014 · N328AA · Boeing 767223 · Door Warning SystemSDR AALA20140203001Cover · missingFIRST CLASS RT EMERGENCY EXIT SIGN COVER MISSING. REPLACED FIRST CLASS RT EMERGENCY EXIT SIGN COVER. OPERATIONS CHECKED NORMAL.Feb 3, 2014 · N319AA · Boeing 767223 · Emergency LightingSDR AALA20140129001Light · inoperativeSEAT MOUNTED EMERGENCY LIGHTS AT 19HJ INOPERATIVE. REPLACED LAMP FOR SEAT MOUNTED EMERGENCY LIGHTS 19HJ. OPERATIONS CHECKED NORMAL.Jan 28, 2014 · N339AA · Boeing 767223 · Emergency LightingSDR IXXA201401300040Power Supply · inoperativeLEFT FWD CABIN ENTRY DOOR EMERGENCY EXIT LIGHT INOPERATIVE. EMERGENCY LIGHT POWER SUPPLY M735 AT FAULT, ACFT WAS GNDED.Jan 27, 2014 · N761CX · Boeing 767223 · Emergency LightingSDR CA140116001Static Inverter · overheated(CAN) WHILE TOWING ACFT INTO THE HANGAR, A BURNING ODOR WAS DETECTED, THE SOURCE WAS DETERMINED TO BE COMING FROM THE AVIONICS COMPARTMENT. FURTHER INVESTIGATION IDENTIFIED THE STATIC INVERTER AS THE SOURCE OF THE PROBLEM. THE STATIC INVERTER EXHIBITED SIGNSJan 10, 2014 · Boeing 767223 · DC Power Distribution SystemSDR CA140106003Module · failed(CAN) UPON TOUCHDOWN, C SYSTEM HYD QTY AND PRESSURE WAS LOST. MAINTENANCE FOUND THE FILTER BOWL TO BE SEPARATED FROM THE MAIN HYD MODULE ASSY. THE MODULE ASSY WAS REPLACED WITH A SERVICEABLE UNIT AND THE ACFT WAS RETURNED TO SERVICE.Jan 4, 2014 · Boeing 767223 · Hydraulic System, Main
Back to Boeing 767-223