Boeing 767-323
Service difficulty reports · 8,542
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 = '767323' 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 = '767323' 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 IXXA20250713030Computer · faultedAIR TURN BACK INITIATED DUE TO MULITPLE ENGINE INDICATION FLUCTUATIONS FOR EXHAUST GAS TEMPERATURE, OIL PRESSURE, OIL TEMPERATURE AND OIL QUANTITY. STATUS MESSAGE EICAS DISAGREE ON THE GROUND AFTER LANDING. NO EMERGENCY DELCARED. SYSTEM DEFERRED 64215, MEL CATSDR IXXA20250809009Repair · unknownUNIDENTIFIED REPAIR ON THE NO. 1 PYLON, INBOARD, SIDE STRUT SKINSDR IXXA20250809006Skin · not reportedNUMBER 2 PYLON, INBOARD SIDE, STRUT SKIN REPAIR HAS INSUFFICIENT TECH DATA.SDR IXXA20250710001Skin · crackedR1 DOOR CUTOUT AFT LOWER CORNER IS CRACKED AT 2 HOLES LOCATIONS BOTH ARE THRU SKIN,THE LOWER HOLE IS THROUGH THRU BEAR STRAPSDR IXXA20250809010Limiter · gouged#1 ENGINE, INBD T/R, FWD DEFLECTION LIMITER IS GOUGEDSDR IXXA20250809011Skin · corrodedLEFT WING, UPPER SURFACE SKIN IS CORRODED APPROX 7" OUTBD OF THE FUSELAGE STA 960SDR IXXA20250809005Skin Panel · gougedNUMBER 2 PYLON AT HYDRAULIC ACCESS BAY, OUTBOARD INTERNAL PANEL STRUCTURE HAS 2EA GOUGES.SDR CNMA2025090002Skin · dentedDENT NR 12 LT FUSELAGE STATION 368 +8 INCHES, STRINGER 17L +4 INCHES. DURING SCHEDULED MAINTENANCE, TWO DENT DAMAGES WERE FOUND COMMON TO THE LOWER FUSELAGE SKIN BETWEEN STA 368 - STA 390 AND STGR 17L - STGR 19L..SDR CNMA2025100001Spar · damagedDURING C-CHECK AT YHM, THE RH HORIZONTAL STABILIZER AUXILIARY SPAR WEB NEAR OUTBOARD CLOSURE RIB AT HSBL 357.442 WAS FOUND TO HAVE TOOLING MARKS, AFTER BLENDING OUT OF THE DAMAGED AREAS, TWO CRACKS OF 0.300" AND 0.250" LONG WERE FOUND.SDR IXXA20025061301Skin · crackedCRACK IN FUSELAGE SKIN BS 1629.5 TO 1645.0 AT FUSELAGE STRINGER 14R ABOVE WATER LINE 241, B767SDR IXXA20250610001Stringer · corrodedCORROSION ON STR 34R BETWEEN FSTA 452 AND FSTA458 IN LOWER LOBE OF FLCSDR IXXA20250606002Tray · crackedFLC PDU 2R HAS A CRACKED MOUNTING TRAYSDR IXX2025F00011Structure · corrodedSTA 1197+132, UPPER CHORD CORRODED UNDER NUTPLATES IN MULTIPLE AREASSDR IXXA2025060205Structure · corrodedSTA 1219 RBL 30 UPPER CHORD CORRODEDSDR IXXA2025060204Shear Tie · corrodedSTA 1219 S38L-S37L SHEAR TIE CORRODEDSDR IXXA2025060203Angle · corrodedSTA 1395 S39L STRINGER FRAME CLIP CORRODEDSDR IXXA2025060202Angle · crackedSTA 1087 RBL 35 ANGLE CRACKEDSDR IXXA2025060201Angle · crackedSTA 1087 LBL 35 ANGLE ON FRAME CRACKEDSDR IXXA2025060101Skin · crackedR1 DOOR HAS 2EA CRACKS IN 2 LWR HOLES AT AFT CORNER OF DOOR CUTOUTSDR NACA20250717003Floorbeam · damagedAFTER REMOVAL OF BALLMAT FOUND AFT CARGO DOOR FLOOR FRAME UPPERFLANGE EXFOLIATED/ BLOWN OUT STA 1380 RBL 14. ACCOMPLISHED EA NO. 767-5360-73-B0524 REV IR ON AFT CARGO FLOOR FRAME UPPER FLANGE STA 1395 RBL 5 AND RBL 25.SDR IXXA20250509021Engine · faultedENROUTE FROM KBWI TO KSBD, CREW REPORTED LT ENG FILTER EICAS MESSAGE. CREW ELECTED A LT ENG SHUTDOWN FOLLOWED BY A DIVERSION WITH AN EMERGENCY DECLARATION TO KDEN. LANDING WAS WITHOUT INCIDENT & NO ADDITIONAL PRECAUTIONARY ACTIONS TAKEN. ON ARRIVAL, ACFT WAS GSDR NACA20250717002Skin · damagedLH INBD AFT FLAP HAS 2 DENTS ON LOWERSURFACE JUST BEHIND AND OTBD OF #5 TIRE. EVALUATED L/H I/B AFT FLAP AT LOWER SURFACE AT 2EA DENTS, FOUND DENTSTO BE NEAR EACH OTHER APPROX. .50", MINIMUM IS 3" TO OTHER DENT, AREASIS NOT WITHING ALLOWABLE LIMITS, DENTS ARESDR IXXA20250502001Skin · dentedEXTERIOR FUSELAGE SHIN HAS SEVERAL OUTWARDLY PROTUDING DENTS BETWEEN STA 654+44 - STA 654+68, AT STRINGERS S-R1 THOUGH S-4L. 8110-3 ISSUED.SDR IXXA20250430006Floor Support · gougedAPPROX 8" AFT OF AFT ENTRY DOOR L2 FLOOR STRUCTURE HAS GOUGESDR IXXA20250430005Skin · chafed#1 PYLON UNDER PANEL 431AT SKIN HAS CHAFFING MARK AT NAC STA 155 APPROX AS MARKEDSDR IXXA20250430004Skin · wornL WING WINGLET L/E PANEL HAS 1 FASTENER HOLE THAT IS OVER SIZEDSDR IXXA20250430003Stringer · gougedR WING INTERNAL STRINGER L10 HAS 1 FASTENER HOLE AT APPROX WS 850 RIB 26 WITH GOUGE DAMAGE AT FASTENER HOLESDR IXXA20250430002Stiffener · dentedMAIN CABIN LONGITUDINAL STIFFER ABOVE CANTED BULKHEAD AT APPROX STA 1021 HAS 3 EACH DENTS AT APPROX RBL30SDR IXXA20250430001Stiffener · dentedMAIN CABIN LONGITUDINAL STIFFENER ABOVE CANTED BULKHEAD AT APPROX BS 1043+14 RBL 23 HAS DENT/GOUGE ON TOP AREASDR NACA2025071701Skin · corrodedLH FUSELAG E SKIN HAS NUMEROUS AREAS OF CORROSION AT LAP SEAM STA 883 TO STA 965, ACCOMPLISHED EA 767-53-50-73 - B0479 REV.IR AT L/H FUSELAGE SKIN LAP SEAM STA 883 TO STA 965 S-17LSDR CNMA202504280002Regulator · leakingAT 10,000 MSL, CREW O2 QTY DROPPED TO 70 PSISDR NACA2025042200003Seat Track · crackedMOST OUTBOARD L/H SEAT TRACK STA 1060 TO STA 1070 FOUND TO BE CRACKED AT 2EA AREAS OF VERTICAL FLANGE RADIUS. ACCOMPLISHED NAC 767 E.O. 767-53-0076 REV. IR PERMANENT REPAIR OF SEAT TRACK LOCATED BETWEEN L/H STA 925 TO STA 1100, LBL 88.5.SDR IXXA20250421002Floor Panel · delaminatedFLOOR PANEL AT L2 DOORWAY STA 1461-1582 LBL 60-80 HAS PUNCTURE. HAECO WO 32011 NR 35279SDR IXXA20250417001Former · crackedR/H WING L/E AREA NOSE FORMER ANGLE IS CRACKED AT APPROX LES490. REF HAECO WO 320011 NR 34425SDR IXXA20250429003Frame · gouged#2 ENG I/B CORE COWL HAS GOUGE ON 4TH FRAME FROM FWDSDR IXXA20250429002Frame · gouged#2 ENG I/B CORE COWL HAS GOUGE ON 2ND FRAME FROM FWDSDR IXXA20250429001Frame · gouged#2 ENG I/B CORE COWL HAS GOUGE ON 3RD FRAME FROM FWDSDR IXXA20240421003Attach Bracket · crackedRIGHT UPPER WING TO BODY PANEL 196DR PANEL LANDING ATTACH BRACKET IS CRACKED. REF HAECO WO 320011 NON ROUTINE 35368SDR PCSA20250416001Turbine · damagedLEFT ENGINE FAILURE DURING FLIGHT. AFTER INSPECTION FOUND HOT SECTION DAMAGE.SDR NACA2025041400001Probe · faultedR ENG EEC STATUS MESSAGE. PERFORMED FIM 71-01 FT 803 PMU BITE PROCEDURE SHOWED 2.9 BLEED VALVE THERMOCOUPLE PROBE CH-B OPENED. REMOVED AND REPLACED CH-B PROBE IAW AMM 75-32-06SDR IXXA20250427001Former · crackedRH WING NOSE FORMER IS BROKEN AT OSS 429. REF HAECO WO 320011 NR 35357SDR IXXA20250422001Former · crackedRIGHT WING LEADING EDGE NOSE FORMER IS BROKEN AT OSS 456. HAECO WO 320011 AND NR 35356SDR IXXA20250410002Bracket · cracked5 SLAT O/B L/E PANEL NOSE FORMER BRACKET CRACKED AND FASTENER PULLING THROUGHSDR IXXA20250408002Splice · gougedFWD CARGO COMPT, FLOOR BEAM SPLICE HAS SMALL GOUGES STA 654+110, LBL 32, WL 196SDR IXXA202504080101Splice · gougedFWD CARGO COMPT, FLOOR BEAM SPLICE HAS SMALL GOUGES, STA 654+88, RBL 11 WL 196SDR IXXA2025040803Support Web · corrodedCORROSION ON UPPER BILGE PANEL ALC 1335 RBL16SDR IXXA2025040802Skin Panel · corrodedLEFT HORIZ STAB UPPER SKIN PANEL LE STA 250-305 INTERNAL SKIN DISBONDEDSDR IXXA2025040801Skin Panel · delaminatedLEFT HORIZ STAB UPPER SKIN PANEL DISBONDED LE STA 250.SDR IXXA20250410001Access Panel · corrodedRIGHT WING LOWER ACCESS PANEL 632AB IS WORN AND CORRODEDSDR IXXA2025040703Bracket · corrodedFLC ROLLER TRAY STAND-OFF BRACKET CORRODED STA 478, LBL44
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