Boeing 767-3Y0
Service difficulty reports · 1,440
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 = '7673Y0' 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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR UIEA2026100800969Pseu · faultedENTRY 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 UIEA2026100500945Proximity Sensor · false activation40 MINS INTO FLIGHT @ FL340, RT LANDING GEAR DISCREET LIGHTS, AMBER REV LIGHT, AND ENTRY DOORS/EMER DOORS DISCREET LIGHTS ILLUMINATED. LANDING GEAR DISCREET LIGHTS EXTINGUISHED 10 MINS AFTER. LDG GEAR MONITOR STATUS MSG. REPLACED S-242 AND S-564 PROXIMITY SENSSDR UIEA2026100500950Battery · inoperativeFLASHLIGHT 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 07OCT26. REMOVED AND REPLACED FLASHLIGHT & BATTERY NEXT TO LAV. OPS CHECK GOOD IAW AMM 20-11-00, 2SDR UIEA2026100400943Pseu · inoperativeAPPROX 1 HR AFTER T/O DURING CRUISE @ FL360, LEFT LANDING GEAR DISCRETE LIGHT ILLUMINATED. INTERMITTENT - RT LANDING GEAR DISCRETE LIGHT ILLUMINATED. IN FLIGHT DURING CRUISE, INTERMITTENT RT AMBER REV; NO ASSOCIATED EICAS MESSAGE.(<P>ANC MX PERFORMED FIM 32-09SDR UIEA2026100100935Drive Assy · faultedALT 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 OFSDR UIEA2026082600801Seat Track · corrodedMAIN 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 1SDR UIEA2026082600802Seat Track · corrodedMAIN 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 10SDR UIEA2026082600803Skin · delaminatedLEFT 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 UIEA2026082600804Seat Track · corrodedMAIN 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, DETASDR UIEA2026082600806Seat Track · corrodedMAIN 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 101SDR UIEA2026082600807Seat Track · corrodedMAIN 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, FIGSDR UIEA2026082700811Skin · crackedRIGHT 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 UIEA2026082700812Skin · crackedRIGHT 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 UIEA2026082800816Skin · crackedLEFT 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 UIEA2026082800818Skin · crackedRIGHT 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 UIEA2026082800819Skin · crackedLEFT 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 UIEA2026083100830Frame · chafedNUMBER 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 UIEA2026083100831Pan · damagedWASTE 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 UIEA2026083100832Frame · crackedONE 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 UIEA2026083100833Frame · crackedLEFT 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 UIEA2026090100844Seat Track · corrodedM/D BS 522, LBL 88, SEAT TRACK FOUND CORRODED. THE SEAT TRACK WAS REPLACED IAW SRM 51-40-05. NO FURTHER DEFECTS NOTED.SDR UIEA2026090300847Support Rib · crackedLEFT 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 UIEA2026090300848Ball Mat · crackedFWD 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 UIEA2026090300849Slat Track · crackedLEFT 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 UIEA2026090400851Stringer · crackedBS 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 UIEA2026090800858Track · damagedMEC 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 21GA0260904001None · pilot errorDURING 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 FUSDR UIEA2026060500452Seal · tornL1 DOOR ELT TAMPER PROOF SEAL TORN. REMOVED AND REPLACED PORTABLE ELT BY L1 DOOR IAW AMM 25-63-03. OPS CHECKS GOOD.SDR UIEA2026060400451Unknown · odorFLIGHT 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 CONTASDR UIEA2026052700365Switch · faultedAFTER 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</P>)SDR UIEA2026052400347Line · disconnectedSHORTLY 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 GSDR UIEA2026032700108Switch · shortedDURING 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 SCRSDR UIEA2026050500297Sign · brokenDURING 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 UIEA2026050600298Skin · damagedDURING 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 UIEA2026050600300Skin · damagedDURING 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 UIEA2026050600301Skin · damagedDURING 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 UIEA2026050600302Skin · dentedFOUND 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 UIEA2026050700305Skin · damagedDURING 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 UIEA2026050100286Oxygen Box · inoperativeSUPERNUMERARY 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 ABXR2026042900008Structure · crackedLEFT SIDE OF CHORD AT STA. 1809 TENSION FITTING FORWARD BOLT HOLE HAS CRACKSDR ABXR2026042900007Skin Panel · delaminatedLEFT HORIZONTAL INBD UPPER FIXED L/E IS DELAMINATED.SDR ABXR2026042900006Skin · crackedFOUND CRACK ON UPPER FUSELAGE CROWN SKIN AT STA. 654+22, SR-1 SR-2SDR ABXR2026042900005Angle · crackedVERTICAL ANGLE CRACKED AT STA. 1085 LBL 26. CLIP MONOCOQUESDR UIEA2026032700109Bottle · low pressureSUPERNUMERARY O2 BELOW LIMITS INOP. PLACARDS INSTALLED. SERVICED O2 TO 1710 PSI PER AMM 12-15-08. LEAK CHK GOOD. DMI 249872 CLOSED</P>)SDR 2026FA0000208Feeder Cable · wrong partDURING 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 SCREWSDR UIEA2026020700044Control Panel · faultedMCP 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 UIEA2026020200028Antenna · unwanted deployELT ANTENNA DEPLOYED STICKING STRAIGHT UP. REMOVED & REPLACED RT PORTABLE ELT IAW AMM 25-63-03. OPS CHK OK.SDR UIEA2026012900019Tape · damagedFIRST OBSERVER ELT TAPE IS DAMAGED(<P>RESECURED TAPE AS PER HONEYWELL CMM JOB TASK 25-60-10. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026012900020Fitting · wrong partLAVATORY PORTABLE O2 BOTTLE MASK HAS INCORRECT FITTING TO ATTACH TO O2 BOTTLE.(<P>REMOVED & REPLACED O2 MASK ASSY IAW AMM 35-31-00. OPS CHK OK.THIS CLEARS MDDR 246793. </P>)SDR UIEA2026012000015Elt · inoperativeELT LOCATED RT AFT OF OBSERVERS SEAT INOP. REQ REPLACEMENT(<P>R/R ELT FROM RH AFT OF OBSERVERS SEAT IAW B767 AMM 25-26-03. NO DEFECTS NOTED</P>)
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