ANC MX PERFORMED FIM 32-09 - [SDR UIEA2026100100935](https://openairdocs.org/sdr/UIEA2026100100935.md): Drive Assy · faulted · Oct 1, 2026 · N642GT · Boeing 7673Y0 · Weather Radar System > 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 & POWER CROSS CHK CAPT'S ASI, BELOW 10,000 NORMAL. WXR SYS LT & RT FAILED AFTER APPROX 3 MINS OF - [SDR UIEA2026082600801](https://openairdocs.org/sdr/UIEA2026082600801.md): Seat Track · corroded · Sep 11, 2026 · N642GT · Boeing 7673Y0 · Fuselage, Seat/Cargo Attach Fittings > 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: 0.016". WITHIN SRM 53-00-52 ALLOWABLE DAMAGE 1, FIG 101, & SRM 53-00-52, ALLOWABLE DAMAGE 1, FIG 1 - [SDR UIEA2026082600802](https://openairdocs.org/sdr/UIEA2026082600802.md): Seat Track · corroded · Sep 11, 2026 · N642GT · Boeing 7673Y0 · Fuselage, Seat/Cargo Attach Fittings > 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 0.010". WITHIN SRM 53-00-52 ALLOWABLE DAMAGE 1, FIG 101, & SRM 53-00-52, ALLOWABLE DAMAGE 1, FIG 10 - [SDR UIEA2026082600803](https://openairdocs.org/sdr/UIEA2026082600803.md): Skin · delaminated · Sep 11, 2026 · N642GT · Boeing 7673Y0 · Wing, Control Surfaces > 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 DEFECTS NOTED. - [SDR UIEA2026082600804](https://openairdocs.org/sdr/UIEA2026082600804.md): Seat Track · corroded · Sep 11, 2026 · N642GT · Boeing 7673Y0 · Fuselage, Seat/Cargo Attach Fittings > 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". WITHIN SRM 53-00-52 ALLOWABLE DAMAGE 1, FIG 101, & SRM 53-00-52, ALLOWABLE DAMAGE 1, FIG 101, DETA - [SDR UIEA2026082600806](https://openairdocs.org/sdr/UIEA2026082600806.md): Seat Track · corroded · Sep 11, 2026 · N642GT · Boeing 7673Y0 · Fuselage, Seat/Cargo Attach Fittings > 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: 0.029". WITHIN SRM 53-00-52, DAMAGE 1 FIG 101, LIMITS, AND SRM 53-00-52, ALLOWABLE DAMAGE 1, FIG 101 - [SDR UIEA2026082600807](https://openairdocs.org/sdr/UIEA2026082600807.md): Seat Track · corroded · Sep 11, 2026 · N642GT · Boeing 7673Y0 · Fuselage, Seat/Cargo Attach Fittings > 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: 0.015". IAW SRM 53-00-52, ALLOWABLE DAMAGE, FIG 101 LIMITS, & SRM 53-00-52, ALLOWABLE DAMAGE 1, FIG - [SDR UIEA2026082700811](https://openairdocs.org/sdr/UIEA2026082700811.md): Skin · cracked · Sep 11, 2026 · N642GT · Boeing 7673Y0 · Leading Edge Devices > 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.md): Skin · cracked · Sep 11, 2026 · N642GT · Boeing 7673Y0 · Leading Edge Devices > 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.md): Skin · cracked · Sep 11, 2026 · N642GT · Boeing 7673Y0 · Leading Edge Devices > 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.md): Skin · cracked · Sep 11, 2026 · N642GT · Boeing 7673Y0 · Leading Edge Devices > 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.md): Skin · cracked · Sep 11, 2026 · N642GT · Boeing 7673Y0 · Leading Edge Devices > 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.md): Frame · chafed · Sep 11, 2026 · N642GT · Boeing 7673Y0 · Nacelle/Pylon, Frame/Spar/Rib > 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.md): Pan · damaged · Sep 11, 2026 · N642GT · Boeing 7673Y0 · Fuselage Main, Structure > WASTE SERVICE PAN FOUND TWO FASTENER HOLES WITHOUT BLANK OUT, AFTER DEACTIVATION. TWO RIVETS INSTALLED IAW DWG 146T3244, DL, & 146T3244, PL. NO FURTHER DEFECTS NOTED. - [SDR UIEA2026083100832](https://openairdocs.org/sdr/UIEA2026083100832.md): Frame · cracked · Sep 11, 2026 · N642GT · Boeing 7673Y0 · Fuselage Main, Frame > 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, AND RI-53-80-18470, REV A. NO FURTHER DEFECTS NOTED. - [SDR UIEA2026083100833](https://openairdocs.org/sdr/UIEA2026083100833.md): Frame · cracked · Sep 11, 2026 · N642GT · Boeing 7673Y0 · Fuselage Main, Frame > 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.md): Seat Track · corroded · Sep 11, 2026 · N642GT · Boeing 7673Y0 · Fuselage, Seat/Cargo Attach Fittings > 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.md): Support Rib · cracked · Sep 11, 2026 · N642GT · Boeing 7673Y0 · Leading Edge Devices > 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.md): Ball Mat · cracked · Sep 11, 2026 · N642GT · Boeing 7673Y0 · Fuselage Floor Panel > 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 NOTED. - [SDR UIEA2026090300849](https://openairdocs.org/sdr/UIEA2026090300849.md): Slat Track · cracked · Sep 11, 2026 · N642GT · Boeing 7673Y0 · Leading Edge Devices > 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.md): Stringer · cracked · Sep 11, 2026 · N642GT · Boeing 7673Y0 · Fuselage Main, Longeron/Stringer > 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, VERSION IR. NO FURTHER DEFECTS NOTED. - [SDR UIEA2026090800858](https://openairdocs.org/sdr/UIEA2026090800858.md): Track · damaged · Sep 11, 2026 · N642GT · Boeing 7673Y0 · Electrical/Electronic Compartment Doors > 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-52-40-18516, REV A. NO FURTHER DEFECTS NOTED. - [SDR 21GA0260904001](https://openairdocs.org/sdr/21GA0260904001.md): None · pilot error · Sep 4, 2026 · N1181A · Boeing 7673Y0 · Standard Practices/Structures > 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 IN PUJ AT APPROXIMATELY 1256Z. PRELIMINARY INFORMATION RECEIVED FROM THE CREW INDICATES THAT THE FU - [SDR UIEA2026060500452](https://openairdocs.org/sdr/UIEA2026060500452.md): Seal · torn · Jun 5, 2026 · N642GT · Boeing 7673Y0 · Emergency Locator Beacon > 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.md): Unknown · odor · Jun 4, 2026 · N642GT · Boeing 7673Y0 · Air Distribution System > 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 CONTAMINATION FROM AIR CONDITIONING AND PNEUMATIC SYSTEM IAW AMM 21-00-21-102-030, NO EVIDENCE OF OIL CONTA - [SDR UIEA2026052700365](https://openairdocs.org/sdr/UIEA2026052700365.md): Switch · faulted · May 24, 2026 · N1619A · Boeing 7673Y0 · Door Warning System > 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.md): Line · disconnected · May 24, 2026 · N1619A · Boeing 7673Y0 · Fuel Controlling System > 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 EEC. RECONNECTED PT2 PER AMM 77-11-00/001. PERFORMED ENGINE RUN IAW AMM 71-00-00. ALL OPS CHECKED G - [SDR UIEA2026032700108](https://openairdocs.org/sdr/UIEA2026032700108.md): Switch · shorted · May 12, 2026 · N1619A · Boeing 7673Y0 · Engine Cooling System > 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 WAS TOUCHING THE FEEDER CABLES. TWO CABLES GOT DAMAGED AND PRODUCED ARCING TO THE VALVE HOUSING SCR - [SDR UIEA2026050500297](https://openairdocs.org/sdr/UIEA2026050500297.md): Sign · broken · May 12, 2026 · N1619A · Boeing 7673Y0 · Emergency Lighting > 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 REPLACED IAW AMM 33-51-02 REV.147 NO FURTHER DEFECTS NOTED. - [SDR UIEA2026050600298](https://openairdocs.org/sdr/UIEA2026050600298.md): Skin · damaged · May 12, 2026 · N1619A · Boeing 7673Y0 · Fuselage Main, Plate/Skin > 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 53-00-01-2R-1, REPAIR 1. REV. 131. - [SDR UIEA2026050600300](https://openairdocs.org/sdr/UIEA2026050600300.md): Skin · damaged · May 12, 2026 · N1619A · Boeing 7673Y0 · Fuselage Main, Plate/Skin > 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 SRM 53-00-01-2R-1, REPAIR 1. REV. 131. - [SDR UIEA2026050600301](https://openairdocs.org/sdr/UIEA2026050600301.md): Skin · damaged · May 12, 2026 · N1619A · Boeing 7673Y0 · Fuselage Main, Plate/Skin > 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 53-00-01-2R-1, REPAIR 1. REV. 131. - [SDR UIEA2026050600302](https://openairdocs.org/sdr/UIEA2026050600302.md): Skin · dented · May 12, 2026 · N1619A · Boeing 7673Y0 · Fuselage Main, Plate/Skin > 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 53-00-01-1A-1. ALLOWABLE DAMAGE 1 REV 131. PERFORMED SKIN REPAIR IAW SRM 53-00-01-2R-1 REPAIR 1 REV 131. - [SDR UIEA2026050700305](https://openairdocs.org/sdr/UIEA2026050700305.md): Skin · damaged · May 12, 2026 · N1619A · Boeing 7673Y0 · Fuselage Main, Plate/Skin > 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 53-00-01-2R-1, REPAIR 1. REV. 131. - [SDR UIEA2026050100286](https://openairdocs.org/sdr/UIEA2026050100286.md): Oxygen Box · inoperative · May 1, 2026 · N642GT · Boeing 7673Y0 · Crew Oxygen System > 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 DUE DATE 11MAY26. R & R RH OTBD O2 MASK STOWAGE BOX IAW AMM 35-11-51. OPS & LK CHK GOOD. - [SDR ABXR2026042900008](https://openairdocs.org/sdr/ABXR2026042900008.md): Structure · cracked · Apr 29, 2026 · N1181A · Boeing 7673Y0 · Horizontal Stabilizer Miscellaneous Structure > LEFT SIDE OF CHORD AT STA. 1809 TENSION FITTING FORWARD BOLT HOLE HAS CRACK - [SDR ABXR2026042900007](https://openairdocs.org/sdr/ABXR2026042900007.md): Skin Panel · delaminated · Apr 29, 2026 · N1181A · Boeing 7673Y0 · Horizontal Stabilizer Miscellaneous Structure > LEFT HORIZONTAL INBD UPPER FIXED L/E IS DELAMINATED. - [SDR ABXR2026042900006](https://openairdocs.org/sdr/ABXR2026042900006.md): Skin · cracked · Apr 29, 2026 · N1181A · Boeing 7673Y0 · Fuselage Main, Plate/Skin > FOUND CRACK ON UPPER FUSELAGE CROWN SKIN AT STA. 654+22, SR-1 SR-2 - [SDR ABXR2026042900005](https://openairdocs.org/sdr/ABXR2026042900005.md): Angle · cracked · Apr 29, 2026 · N1181A · Boeing 7673Y0 · Horizontal Stabilizer Miscellaneous Structure > VERTICAL ANGLE CRACKED AT STA. 1085 LBL 26. CLIP MONOCOQUE - [SDR UIEA2026032700109](https://openairdocs.org/sdr/UIEA2026032700109.md): Bottle · low pressure · Mar 26, 2026 · N642GT · Boeing 7673Y0 · Crew Oxygen System > 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.md): Feeder Cable · wrong part · Mar 24, 2026 · N1619A · Boeing 7673Y0 · Electrical Power System Wiring > 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 WAS TOUCHING THE FEEDER CABLES. TWO CABLE GOT DAMAGED AND PRODUCED ARCING TO THE VALVE HOUSING SCREW - [SDR UIEA2026020700044](https://openairdocs.org/sdr/UIEA2026020700044.md): Control Panel · faulted · Feb 7, 2026 · N642GT · Boeing 7673Y0 · Autopilot System > 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, 30-40 TEST PASS, NO FAULTS NOTED. - [SDR UIEA2026020200028](https://openairdocs.org/sdr/UIEA2026020200028.md): Antenna · unwanted deploy · Feb 1, 2026 · N642GT · Boeing 7673Y0 · Emergency Locator Beacon > 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.md): Tape · damaged · Jan 29, 2026 · N642GT · Boeing 7673Y0 · Emergency Locator Beacon > 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.md): Fitting · wrong part · Jan 28, 2026 · N642GT · Boeing 7673Y0 · Portable Oxygen System > 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 MDDR 246793.
) Next page: https://openairdocs.org/model/boeing-767-3y0/reports.md?page=2 ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 = '7673Y0' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/model/boeing-767-3y0/reports --- 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.