# Boeing 767-3Y0 - Type: Aircraft model (FAA registry) - Registry code: 1385240 - Manufacturer (registry): BOEING - Model: 767-3Y0 - Aircraft type: Fixed wing multi engine - Category: Airplane - Engines: 2 ยท Turbo-fan - Seats: 190 - Weight class: 20,000 lb and over - Certification: Type certificated - Registered aircraft: 3 - Page: https://openairdocs.org/model/boeing-767-3y0 Model codes come from the FAA registry's reference file. ADs are matched to them by model name and maker. ## ADs that may apply (OpenAirDocs) Matched to this model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment. None matched. ## Registered aircraft (3) - [N1181A](https://openairdocs.org/aircraft/N1181A): [Msn 26206 LLC](https://openairdocs.org/faa-owner/MSN%2026206%20LLC), [Purchase, NY](https://openairdocs.org/faa-place/NY/Purchase), S/N 26206 - [N1619A](https://openairdocs.org/aircraft/N1619A): [Atlas Air Inc](https://openairdocs.org/faa-owner/ATLAS%20AIR%20INC), [Purchase, NY](https://openairdocs.org/faa-place/NY/Purchase), built 1994, S/N 26208 - [N642GT](https://openairdocs.org/aircraft/N642GT): [Wilmington Trust Co Trustee](https://openairdocs.org/faa-owner/WILMINGTON%20TRUST%20CO%20TRUSTEE), [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington), built 1983, S/N 26207 ## NTSB investigations None matched to aircraft with this model. ## FAA accident and incident reports None matched to aircraft with this model. ## Service difficulty reports (1,440, newest 50) As reported by operators and repair stations, by the model named in the report. - [SDR UIEA2026100800969](https://openairdocs.org/sdr/UIEA2026100800969), Oct 7, 2026: PSEU. FAULTED. ENTRY DOOR AND EMER DOOR DISCRETE LIGHTS ON OVERHEAD PANEL INOPERATIVE. REMOVED AND REPLACED PSEU IAW AMM 32-09-04-704-013. OPS CHKD GOOD. - [SDR UIEA2026100500945](https://openairdocs.org/sdr/UIEA2026100500945), Oct 5, 2026: PROXIMITY SENSOR. FALSE ACTIVATION. 40 MINS INTO FLIGHT @ FL340, RT LANDING GEAR DISCREET LIGHTS, AMBER REV LIGHT, AND ENTRY DOORS/EMER DOORS DISCREET LIGHTS ILLUMINATED. LANDING GEAR DISCREET LIG - [SDR UIEA2026100500950](https://openairdocs.org/sdr/UIEA2026100500950), Oct 4, 2026: BATTERY. INOPERATIVE. FLASHLIGHT NEXT TO LAV DEAD BATTERY, NOTICED POST FLIGHT. MX IN WORK WHILE IN AOGM FOR ATB, MULTIPLE ERRONEOUS LANDING GEAR, T/R AND DOOR INDICATIONS. AOGM ETR - [SDR UIEA2026100400943](https://openairdocs.org/sdr/UIEA2026100400943), Oct 4, 2026: PSEU. INOPERATIVE. APPROX 1 HR AFTER T/O DURING CRUISE @ FL360, LEFT LANDING GEAR DISCRETE LIGHT ILLUMINATED. INTERMITTENT - RT LANDING GEAR DISCRETE LIGHT ILLUMINATED. IN FLIGHT - [SDR UIEA2026100100935](https://openairdocs.org/sdr/UIEA2026100100935), Oct 1, 2026: DRIVE ASSY. FAULTED. ALT DISAGREE AT FL 230-270. FO AND CAPT ALTIMETER +/- 500; BELOW 10,000 NORMAL. AIRSPEED DISAGREE, CAPT & STANDBY AGREE +/-2 KNOTS. FO'S AIRSPEED +20 KTS. PITCH - [SDR UIEA2026082600801](https://openairdocs.org/sdr/UIEA2026082600801), Sep 11, 2026: SEAT TRACK. CORRODED. MAIN DECK, BS 1590 - 1600, LBL 11 SEAT TRACK CROWN CORRODED. CORROSION REMOVED IAW SRM 51-10-02, AND PROTECTED IAW SRM 51-20-01. MEASURED L: 0.9" X W: 0.7" X D: - [SDR UIEA2026082600802](https://openairdocs.org/sdr/UIEA2026082600802), Sep 11, 2026: SEAT TRACK. CORRODED. MAIN DECK, BS 1197+44, LBL 33 SEAT TRACK CROWN FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10-02, AND PROTECTED IAW SRM 51-20-01. MEASURED L: 5" X W: 0.7" X D - [SDR UIEA2026082600803](https://openairdocs.org/sdr/UIEA2026082600803), Sep 11, 2026: SKIN. DELAMINATED. LEFT WING T/E OTBD FLAP LOWER SKIN, BETWEEN FLAP FAIRINGS, FOUND DELAMINATED. PERFORMED COMPOSITE HOT BOND REPAIR IAW SRM 51-70-07, PAR 5 A(1). NO FURTHER DEFEC - [SDR UIEA2026082600804](https://openairdocs.org/sdr/UIEA2026082600804), Sep 11, 2026: SEAT TRACK. CORRODED. MAIN DECK, BS 1590, LBL 55 SEAT TRACK CROWN CORRODED. CORROSION REMOVED IAW SRM 51-10-02, AND PROTECTED IAW SRM 51-20-01. MEASURED L: 3" X W: 0.7" X D: 0.009". - [SDR UIEA2026082600806](https://openairdocs.org/sdr/UIEA2026082600806), Sep 11, 2026: SEAT TRACK. CORRODED. MAIN DECK, BS 1590 - 1600, LBL 33 SEAT TRACK CROWN CORRODED. CORROSION REMOVED IAW SRM 51-10-02, & PROTECTED IAW SRM 51-20-01. MEASURED L: 2.5" X W: 0.7" X D: 0 - [SDR UIEA2026082600807](https://openairdocs.org/sdr/UIEA2026082600807), Sep 11, 2026: SEAT TRACK. CORRODED. MAIN DECK, BS 1590 - 1600, RBL 33 SEAT TRACK CROWN CORRODED. CORROSION REMOVED IAW SRM 51-10-02, & PROTECTED IAW SRM 51-20-01. MEASURED L: 8" X W: 0.7" X D: 0.0 - [SDR UIEA2026082700811](https://openairdocs.org/sdr/UIEA2026082700811), Sep 11, 2026: SKIN. CRACKED. RIGHT WING NR 9 SLAT, INBD MAIN TRACK RIB SKIN AT FASTENER HOLE, CRACKED. SKIN REPAIRED IAW SRM 57-43-01-2R-2, REPAIR 2. NO FURTHER DEFECTS NOTED. - [SDR UIEA2026082700812](https://openairdocs.org/sdr/UIEA2026082700812), Sep 11, 2026: SKIN. CRACKED. RIGHT WING NR 10 SLAT, INBD MAIN TRACK RIB SKIN AT FASTENER HOLE, CRACKED. SKIN REPAIRED IAW SRM 57-43-01-2R-2, REPAIR 2. NO FURTHER DEFECTS NOTED. - [SDR UIEA2026082800816](https://openairdocs.org/sdr/UIEA2026082800816), Sep 11, 2026: SKIN. CRACKED. LEFT WING, NR 4 SLAT, INBD MAIN TRACK RIB SKIN AT FASTENER HOLE, CRACKED. SKIN REPAIRED IAW SRM 57-43-01-2R-2, REPAIR 2. NO FURTHER DEFECTS NOTED. - [SDR UIEA2026082800818](https://openairdocs.org/sdr/UIEA2026082800818), Sep 11, 2026: SKIN. CRACKED. RIGHT WING, NR 8 SLAT OTBD MAIN TRACK RIB SKIN FASTENER HOLE CRACKED. SKIN REPAIRED IAW SRM 57-43-01-2R-2, REPAIR 2. NO FURTHER DEFECTS NOTED. - [SDR UIEA2026082800819](https://openairdocs.org/sdr/UIEA2026082800819), Sep 11, 2026: SKIN. CRACKED. LEFT WING NR 4 SLAT OTBD MAIN TRACK RIB SKIN FASTENER HOLE CRACKED. NOSE SKIN REPAIRED IAW SRM 57-43-01-2R-2, REPAIR 2. NO FURTHER DEFECTS NOTED. - [SDR UIEA2026083100830](https://openairdocs.org/sdr/UIEA2026083100830), Sep 11, 2026: FRAME. CHAFED. NUMBER 1 ENG LT CORE COWL NR 2 FRAME MID AREA ANGLE FWD, CHAFED. FRAME REPAIRED IAW SRM 54-42-02-2R-2, REPAIR 2, & EA-1971A296, REV 0. NO FURTHER DEFECTS NOTED. - [SDR UIEA2026083100831](https://openairdocs.org/sdr/UIEA2026083100831), Sep 11, 2026: PAN. DAMAGED. WASTE SERVICE PAN FOUND TWO FASTENER HOLES WITHOUT BLANK OUT, AFTER DEACTIVATION. TWO RIVETS INSTALLED IAW DWG 146T3244, DL, & 146T3244, PL. NO FURTHER DEFECTS - [SDR UIEA2026083100832](https://openairdocs.org/sdr/UIEA2026083100832), Sep 11, 2026: FRAME. CRACKED. ONE CRACK FOUND ON BS 1809.5 BULKHEAD FWD OUTER FRAME BTWN STRS 6R-7R. RADIUS AREA APPROX 3/4 LENGTH. OUTER FRAME AREA REPAIRED IAW EO 6753A030, REV 16, PART 10 - [SDR UIEA2026083100833](https://openairdocs.org/sdr/UIEA2026083100833), Sep 11, 2026: FRAME. CRACKED. LEFT BS 1809.5 BULKHEAD OUTER CHORD HOLE, FOUND CRACK IN SKIN LAYER. CRACKED FASTENER HOLE, REPAIRED IAW RI-53-81-18478, REV A. NO FURTHER DEFECTS NOTED. - [SDR UIEA2026090100844](https://openairdocs.org/sdr/UIEA2026090100844), Sep 11, 2026: SEAT TRACK. CORRODED. M/D BS 522, LBL 88, SEAT TRACK FOUND CORRODED. THE SEAT TRACK WAS REPLACED IAW SRM 51-40-05. NO FURTHER DEFECTS NOTED. - [SDR UIEA2026090300847](https://openairdocs.org/sdr/UIEA2026090300847), Sep 11, 2026: SUPPORT RIB. CRACKED. LEFT WING, NR 3 SLAT, OTBD SUPPORT RIB FOUND CRACKED. RIB CRACK AREA REPAIRED IAW RI-57-42-18506, REV A. NO FURTHER DEFECTS NOTED. - [SDR UIEA2026090300848](https://openairdocs.org/sdr/UIEA2026090300848), Sep 11, 2026: BALL MAT. CRACKED. FWD CARGO BAY, BS 480 , MOT RT OTBD BALL MAT PANEL FWD MID SKIN AND SUPPORT FOUND DAMAGE. BALL MAT PANEL REPAIRED IAW RI-53-00-18499, REV A. NO FURTHER DEFECTS - [SDR UIEA2026090300849](https://openairdocs.org/sdr/UIEA2026090300849), Sep 11, 2026: SLAT TRACK. CRACKED. LEFT WING, NR 3 SLAT, OTBD MAIN TRACK RIB SKIN FASTENER HOLE CRACKED. SKIN REPAIRED IAW SRM 57-43-01-2R-2, REPAIR 2. NO FURTHER DEFECTS NOTED. - [SDR UIEA2026090400851](https://openairdocs.org/sdr/UIEA2026090400851), Sep 11, 2026: STRINGER. CRACKED. BS 434, STRINGER 22L FOUND ONE CRACK AT FASTENER HOLE ON VERTICAL FLANGE AREA AT 10 O'CLOCK, APPROX 3/16 LENGTH. STRINGER REPAIRED IAW IAI DOC CS-26207-005, VER - [SDR UIEA2026090800858](https://openairdocs.org/sdr/UIEA2026090800858), Sep 11, 2026: TRACK. DAMAGED. MEC ACCESS DOOR 119AL FOUND FWD ROLLER TRACK MISSING MATERIAL. THE NEW PART 1EA BOLT HOLE NOT ALIGNED. FASTENER HOLE REPAIRED, AND INSTALLED FREEZE PLUG IAW RI- - [SDR 21GA0260904001](https://openairdocs.org/sdr/21GA0260904001), Sep 4, 2026: NONE. PILOT ERROR. DURING CRUISE, THE FLIGHT CREW EXPERIENCED A SHUTDOWN OF THE LEFT ENGINE AND SUBSEQUENTLY DIVERTED THE AIRCRAFT TO PUNTA CANA (PUJ). THE AIRCRAFT LANDED SAFELY - [SDR UIEA2026060500452](https://openairdocs.org/sdr/UIEA2026060500452), Jun 5, 2026: SEAL. TORN. L1 DOOR ELT TAMPER PROOF SEAL TORN. REMOVED AND REPLACED PORTABLE ELT BY L1 DOOR IAW AMM 25-63-03. OPS CHECKS GOOD. - [SDR UIEA2026060400451](https://openairdocs.org/sdr/UIEA2026060400451), Jun 4, 2026: UNKNOWN. ODOR. FLIGHT CREW REPORTED OIL FUMES AND RUBBER SMELL DURING TAKE OFF. PERFORMED CHAPTER 5 INSPECTION IAW AMM 05-51-56-202-001. ALSO PERFORMED REMOVAL OF OIL CONTAMIN - [SDR UIEA2026052700365](https://openairdocs.org/sdr/UIEA2026052700365), May 24, 2026: SWITCH. FAULTED. AFTER TAKEOFF AROUND 3000FT AGL, GOT E/E ACCESS DOOR EICAS MESSAGE. R & R E/E ACCESS DOOR SWITCH PER AMM 52-71-00. OPS CHECK GOOD. DMI 253051 CLOSED

) - [SDR UIEA2026052400347](https://openairdocs.org/sdr/UIEA2026052400347), May 24, 2026: LINE. DISCONNECTED. SHORTLY AFTER TAKEOFF (AROUND 2000 AGL) GOT R ENG EEC MODE EICAS MSG. NO INDICATION OF EPR ON RIGHT ENGINE. FOUND THE PT2 LINE DISCONNECTED AT THE RIGHT ENGINE - [SDR UIEA2026032700108](https://openairdocs.org/sdr/UIEA2026032700108), May 12, 2026: SWITCH. SHORTED. DURING PREPARATION FOR ENG #2 COOLING BAROMETRIC SWITCH, OPS CHK FOUND DAMAGE TO A SCREW AT NACELLE ZONE VENT SOV. AFTER INVESTIGATING, WE FOUND THAT THIS SCREW - [SDR UIEA2026050500297](https://openairdocs.org/sdr/UIEA2026050500297), May 12, 2026: SIGN. BROKEN. DURING GVI OF MAIN DECK CARGO COMPARTMENT, FOUND SELF LUMINOUS EXIT SIGN, ATTACHED OVER THE ENTRY HATCH FOR THE MAIN CARGO, BROKEN. SELF ILLUMINATED EXIT SIGN R - [SDR UIEA2026050600298](https://openairdocs.org/sdr/UIEA2026050600298), May 12, 2026: SKIN. DAMAGED. DURING LIGHTNING STRIKE INSPECTION, FOUND 5EA BURN MARKS ON FUSELAGE SKIN AT STA.522-544. STRG 39L-39R. PERMANENT REPAIR HAS BEEN ACCOMPLISHED AS PER SRM 53-00- - [SDR UIEA2026050600300](https://openairdocs.org/sdr/UIEA2026050600300), May 12, 2026: SKIN. DAMAGED. DURING LIGHTNING STRIKE INSPECTION, FOUND 1EA BURN MARK ON FUSELAGE SKIN AT STA.654+44-654+66, BTWN. STRG 39L-39R. PERMANENT REPAIR HAS BEEN ACCOMPLISHED AS PER - [SDR UIEA2026050600301](https://openairdocs.org/sdr/UIEA2026050600301), May 12, 2026: SKIN. DAMAGED. DURING LIGHTNING STRIKE INSPECTION, FOUND 1EA BURN MARK ON FUSELAGE SKIN AT STA. 654+88-654+110. STRG 39L-39R. PERMANENT REPAIR HAS BEEN ACCOMPLISHED AS PER SRM - [SDR UIEA2026050600302](https://openairdocs.org/sdr/UIEA2026050600302), May 12, 2026: SKIN. DENTED. FOUND ONE DENT ON THE FUSELAGE SKIN RH SIDE BEHIND MLG WW ABOVE THE RAT HOUSING. GOUGE ON FUSELAGE SKIN STA 1153-1175 AT STR 29R IS OUT OF LIMITS IAW SRM 53-00- - [SDR UIEA2026050700305](https://openairdocs.org/sdr/UIEA2026050700305), May 12, 2026: SKIN. DAMAGED. DURING LIGHTNING STRIKE INSPECTION, FOUND 5EA BURN MARKS ON FUSELAGE SKIN AT STA. 522-544, BTWN STRG 39L-39R. REPAIR PARTS HAVE BEEN INSTALLED AS PER SRM 53-00- - [SDR UIEA2026050100286](https://openairdocs.org/sdr/UIEA2026050100286), May 1, 2026: OXYGEN BOX. INOPERATIVE. SUPERNUMERARY SEAT OXY MASK INOP ( SUPERNUMERARY OXYGEN SYSTEM, OXYGEN MASKS, ASSOCIATED SEAT NOT OCCUPIED, TRANSFER TO DMI 251838 PER MEL 35-11-03-02A CAT C DU - [SDR ABXR2026042900008](https://openairdocs.org/sdr/ABXR2026042900008), Apr 29, 2026: STRUCTURE. CRACKED. LEFT SIDE OF CHORD AT STA. 1809 TENSION FITTING FORWARD BOLT HOLE HAS CRACK - [SDR ABXR2026042900007](https://openairdocs.org/sdr/ABXR2026042900007), Apr 29, 2026: SKIN PANEL. DELAMINATED. LEFT HORIZONTAL INBD UPPER FIXED L/E IS DELAMINATED. - [SDR ABXR2026042900006](https://openairdocs.org/sdr/ABXR2026042900006), Apr 29, 2026: SKIN. CRACKED. FOUND CRACK ON UPPER FUSELAGE CROWN SKIN AT STA. 654+22, SR-1 SR-2 - [SDR ABXR2026042900005](https://openairdocs.org/sdr/ABXR2026042900005), Apr 29, 2026: ANGLE. CRACKED. VERTICAL ANGLE CRACKED AT STA. 1085 LBL 26. CLIP MONOCOQUE - [SDR UIEA2026032700109](https://openairdocs.org/sdr/UIEA2026032700109), Mar 26, 2026: BOTTLE. LOW PRESSURE. SUPERNUMERARY O2 BELOW LIMITS INOP. PLACARDS INSTALLED. SERVICED O2 TO 1710 PSI PER AMM 12-15-08. LEAK CHK GOOD. DMI 249872 CLOSED

) - [SDR 2026FA0000208](https://openairdocs.org/sdr/2026FA0000208), Mar 24, 2026: FEEDER CABLE. WRONG PART. DURING PREPARATION FOR NR 2 ENG COOLING BAROMETRIC SWITCH OPC FOUND DAMAGED SCREW AT NACELLE ZONE VENT SHUTOFF VALVE. AFTER INVESTIGATION FOUND THAT THIS SCREW - [SDR UIEA2026020700044](https://openairdocs.org/sdr/UIEA2026020700044), Feb 7, 2026: CONTROL PANEL. FAULTED. MCP ALTITUDE SELECTOR SELECTS ERRONEOUS ALTITUDES PLUS/MINUS 3000 FEET WHEN TURNING. REMOVED AND REPLACED MCP IAW AMM 22-11-02. PERFORMED MCDP GROUND TEST, 30-4 - [SDR UIEA2026020200028](https://openairdocs.org/sdr/UIEA2026020200028), Feb 1, 2026: ANTENNA. UNWANTED DEPLOY. ELT ANTENNA DEPLOYED STICKING STRAIGHT UP. REMOVED & REPLACED RT PORTABLE ELT IAW AMM 25-63-03. OPS CHK OK. - [SDR UIEA2026012900019](https://openairdocs.org/sdr/UIEA2026012900019), Jan 29, 2026: TAPE. DAMAGED. FIRST OBSERVER ELT TAPE IS DAMAGED(

RESECURED TAPE AS PER HONEYWELL CMM JOB TASK 25-60-10. NO FURTHER DEFECTS NOTED

) - [SDR UIEA2026012900020](https://openairdocs.org/sdr/UIEA2026012900020), Jan 28, 2026: FITTING. WRONG PART. LAVATORY PORTABLE O2 BOTTLE MASK HAS INCORRECT FITTING TO ATTACH TO O2 BOTTLE.(

REMOVED & REPLACED O2 MASK ASSY IAW AMM 35-31-00. OPS CHK OK.THIS CLEARS M - [SDR UIEA2026012000015](https://openairdocs.org/sdr/UIEA2026012000015), Jan 15, 2026: ELT. INOPERATIVE. ELT LOCATED RT AFT OF OBSERVERS SEAT INOP. REQ REPLACEMENT(

R/R ELT FROM RH AFT OF OBSERVERS SEAT IAW B767 AMM 25-26-03. NO DEFECTS NOTED

) All 1,440: https://openairdocs.org/model/boeing-767-3y0/reports.md --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.