Boeing 767-323
Service difficulty reports · 8,544
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 IXXA20240726001Skin · crackedR1 DOOR CUTOUT, AFT LOWER CORNER, ROTO SCAN SHOWS INDICATION AT SECOND HOLE FROM BOTTOMSDR IXXA20240816003Seal Depressor · crackedMCD CUTOUT FWD LOWER SEAL DEPRESSOR ATTACH FITTING IS CRACKEDSDR IXXA202407250004Nut Plate · corrodedCENTER SHEAR WEB PANEL NUTPLATE STRIP CORRODED TOP AND BOTTOM STA 1153SDR IXXA20240725003Floor Panel · corrodedCORROSION ON THE UPPER SURFACE OF THE SUBFLOOR, FROM STA.276 TO 340, LBL85, UNDER THE COMPSITE FLOOR PANEL LOCATED JUST INSIDE OF THE L1 DOORSDR IXXA20240725002Bracket · corrodedCORROSION ON THE BRACKET UNDER THE FWD END OF THE RIGHT BULK CARGO SLOPING SIDEWALL PANEL SUPPORT, LOCATED ON THE FWD SIDE OF FRAME 1417, RBL48.SDR IXXA20240725001Support · corrodedALC PDU 8R I/B SUPPORT BEAM EXFOLIATED AROUND FWD & AFT MOUNT BOLT NUT PLATESSDR IXXA2024020605Skin · delaminatedLW OUTBD FLAP UPPER SURFACE AREA OF DELAMINATION.SDR IXXA202400724003Skin · chafedSEVERAL CHAFFE MARKS IN THE UPPER SURFACE OF THE PANEL, ON TOP OF THE RIGHT PYLON, WHERE THE FWD FAIRING 441AT (DOGHOUSE PANEL)SDR IXXA20240724001Skin · chafed#1 PYLON FWD NACELLE STRUT FAIRING UPPER SKIN IS CHAFED IN 4EA SPOTS LOCATED JUST AFT OF THE INLET AT THE 12:00 POSITIONSDR NACA2024071800001Igniter · inoperativeON STARTING RIGHT ENGINE, NO IGNITION WITH IGNITER SET TO ONE. REMOVED AND REPLACED RH ENG SYS NR 1 IGNITER PLUG IAW AMM 74-21-02 OPS CHECK GOOD.SDR IXXA20240721052Battery · inoperativeDURING SERVICE CHECK, LINE MAINTENANCE REPORTED AISLE STAND EMERGENCY FLASH LIGHT BATTERY INOPERATIVE. FLASHLIGHT BATTERY REMOVED AND REPLACED PER BOEING 767 AIRCRAFT MAINTENANCE MANUAL 25-64-80. OPERATIONAL CHECK GOOD.SDR IXXA20240721051Outflow Valve · faultedAT FL340, CREW REPORTED LOSS OF CABIN PRESSURE, EICAS MSG AND AURAL WARNINGS-MASTER CAUTION-ILLUMINATED. CREW COMPLIED WITH ATI QUICK REFERENCE HANDBOOK PROCEDURES, AND ELECTED AIR RETURN TO DEPARTURE STATION KRFD WITH AN EMERGENCY DECLARATION DUE TO OVERWEISDR IXXA20240816002Retainer · gougedCOCKPIT CAPTAIN L2 WINDOW OPENING LOWER SEAL RETAINER STRUCTURE TAB IS GOUGEDSDR IXXA202407152049Carriage · crackedFOLLOWING ROUTINE MAINTENANCE, FIRST OFFICER'S OPENABLE WINDOW SLIDING TRACK BRACKET CRACKED IN TWO PLACES. REMOVED AND REPLACED FIRST OFFICER'S #2 OPENABLE WINDOW SLIDING TRACK BRACKET IN ACCORDANCE WITH AIRCRAFT MAINTENANCE MANUAL 56-11-04. OPERATIONAL CHECKSDR IXXA202400712002Frame · corrodedALC HAS SURFACE CORROSION AT STA. 1197+66 RBL-8.SDR IXXA20240712001Support · corrodedCORROSION ON THE UPPER AND LOWER SURFACES OF THE LOWER PANEL SUPPORT COMMON TO THE LEFT BULK CARGO SLOPING SIDEWALLSDR IXXA202407110002Door Sill · corrodedCORROSION ON THE LOWER SURFACE OF THE LOWER SILL, AT THE BULK CARGO DOOR FUSELAGE CUTOUT, UNDER THE AFT I/B NUTPLATE, AS VIEWED INSIDE OF THE FWD LIGHTENING, AT STA.1426.SDR IXXA20240711001Floor Support · corrodedCORROSION UNDER 8 NUTPLATES, ON THE LOWER SURFACES OF THE 4 GREEN PANEL SUPPORT CHANNEL REPAIRS, FOR THE BULK CARGO FLOOR SUPPORTS, FROM STA.1415 TO STA.1422, AT LBL23, LBL16, LBL9, AND RBL9.SDR IXXA20240816001Sidewall Panel · damagedMAIN CABIN SIDEWALL #L4 IS DAMAGED. REFER TO HAECO WO 320007 NON ROUTINE 38783SDR IXXA2024071003Support Angle · corrodedALC FLOORBOARD SUPPORT ANGLE CORRODED1263 I/B OF PDU 7LSDR IXXA20240710001Angle · corrodedUNDERSIDE OF FLC FLOOR SUPPORT LONGITUDINAL ANGLE IS CORRODED AROUND FWD ATTACH HI-LOK, LOCATED AT LFS 654+121, LBL 21SDR NACA2024070800003Panel · corrodedDAMAGE (CORROSION) FOUND ALONG WS 825.2 JUST FORWARD OF PANEL 661B. EXTERNAL/GENERAL VISUAL RIGHT WING TRAILING EDGE. ACCOMPLISHED NAC EO 767-57-0029 DATED 7/11/2024 REV 1RSDR IXXA20240708002Skin · chafed#1 PYLON FWD NACELLE STRUT FAIRING UPPER SKIN IS CHAFFED IN 4EA SPOTS LOCATED JUST AFT OF THE INLET AT THE 12:00 POSITIONSDR NACA2024070400001Egt Indication · illuminatedAPU FAULT DURING TAXI IN, HIGH EGT THEN SHUTDOWN. DEFERRED PER MEL 49-11-01A. PERFORMED DETAIL VISUAL INSPECTION OF EGT THERMOCOUPLES, NO DEFECTS NOTED. INSPECTED MAGNETIC CHIP DETECTORS IAW AMM 49-27-04. NO FAULTS FOUND.SDR IXXA20240816010Rib · crackedRIGHT WINGLET AFT ATTACH FRAME IS CRACKED INTERNAL JUST AFT OF UPPER AFT MOUNT BOLT. REF HAECO WO 320007 NON ROUTINE 38717SDR IXXA202408010004Retainer · gouged#2 ENG RH TR SEAL RETAINER FOUND GOUGED, CAUSE UNDETERMINED. ACCOMPLISHED BLENDOUT REPAIR MEASURING 0.750"W X 1.75"L X 0.018" DEEPSDR IXXA202408010003Mount Fitting · gouged#2 ENG RH TR FWD DEFLECTION LIMITER GOUGED, CAUSE UNDETERMINEDBLEAND OUT MEASURES 1.6"L X 0.096" DEPTHSDR IXXA2024070201Support · corrodedL1 DOOR SCUFF PLATE SUPPORT CORRODED.SDR IXXA202408010002Mount Fitting · gouged#1 ENGINE O/B T/R LOWER FWD DEFLECTION LIMITER FITTING WAS FOUND GOUGEDSDR IXXA2024080403Beam · chafed#1 PYLON AFT FAIRING ASSY, INBD LATCH BEAM CHAFED EDGE DAMAGE DUE TO CONTACT WITH BROKEN HOLD OPEN RODSDR NACA2024063000001Anti-Ice Valve · failedR ENGINE ANTI-ICE VALVE LIGHT ON WITH THE SWITCH OFF. REMOVED AND REPLACED RIGHT ENG ANTI-ICE VALVE IAW MM 30-21-03 OPS CHECK NORMAL.SDR IXXA20240701046Transmitter · faultedENROUTE, CENTER HYD QTY EICAS & LIGHT ILLUM IN CRUISE. STATUS PAGE SHOWED 0 QTY & MAGENTA RF WITH 3000 PSI. DIVERTED, EMER DECLARED. LANDED WITHOUT INCIDENT. ACFT GROUNDED. CENTER HYD IND DEFERRED IAW MEL 29-33-02-01. HYD IND INOP. ACFT RELEASED TO SERVISDR IXXA2024080601Rib · gougedLEADING EDGE RIB AT OSS 494 ON LEFT WING IS GOUGED ON INBOARD SIDE, BLENDED OUT AREA MEASURE 2" X 1"SDR IXXA2024080404Keel · corrodedCORROSION FOUND ON RBL 9.50 KEEL CHORD UPPER SURFDACE , APPROXIMATELY AT BS 786SDR IXXA2024080402Longeron · chafed#1 PYLON PANEL 431AT INNER FWD STRUCTURAL CHANNELS (PN 313T2100-86 AND 313T2100-82) ARE CHAFED ON THE FWD ENDSSDR IXXA2024080401Fairing · damagedR/H STAB FAIRING #314CRX FOUND TO HAVE 2EA PUNCTURES IN INNER SKINSDR IXXA20240801001Support Beam · chafedR/H AFT MLG SUPPORT BEAM FWD EDGE OF THE LOWER FREE FLANGE HAS CHAFING DAMAGE DUE TO CONTACT WITH LOWER BULB SEAL ATTACH ANGLE APPROX 30" OTBD OF THE INBD END OF BEAMSDR IXXA2024073102Skin · crackedCRACK FOUND IN FORWARD ENTRY DOOR AFT LOWER CORNER FUSELAGE SKIN EXTENDING FROM FASTENER IN 10 O'CLOCK POSITIONSDR IXXA202407310001Skin · crackedCRACK FOUND IN SKIN OF FORWARD SERVICE DOOR AFT LOWER CORNER EXTENDING OUT FROM FASTENER IN 2 O'CLOCK AND 8 O'CLOCK POSITIONSDR IXXA2024080303Panel · erodedL.WING L/E PANEL 511CB ERRODED ON THE ERROSION STRIP EDGESDR IXXA2024080300003Panel · crackedL.WING L/E PANEL 511BB CRACKED AT FASTENER HOLE ON AFT SURFACE AND DELAMINATION ON FWD EDGESDR NACA2024062300002Outflow Valve · openON INITIAL CLIMBOUT FWD EQUIP OVHT EICAS, EQPT COOLING EICAS FWD EQUIP VAL EICAS, AC WASNT PRESSURIZING. DURING WALKAROUND FOUND OVBD EQUIP EXH VALVE OPEN, CLOSED VLV PER MEL PROCEDURES. ACCOMPLISHED CABIN PRESSURE LEAK TEST GOOD. ALL EQUIP EICAS MESSAGES OPS SDR NACA2024062300001Warning Message · illuminatedFWD EQUIP OVHT EICAS MESSAGE CAME ON AT START OF TO ROLL. PERFORMED FIM 21-58 TREE 912, MESSAGE OFF EICAS OPS PER MEL 21-58-07-02-01SDR NACA2024062100002Valve · faultedEICAS MSG FWD EQUIP OVHT VAL. DURING GROUND OPERATIONS AND HAVING MCD OPEN, AMBIENT TEMPERATURE ROSE ABOVE 29.6C CAUSING OVHT MESSAGE. WITH BOTH PACKS RUNNING AND MCD CLOSED OVERHEAT MESSAGE EXTINGUISHED.SDR NACA2024061900001Valve · failedLEFT ENG SPAR VALVE ASSOCIATED EICAS L FUEL SPAR VAL EICAS MESSAGES ILLUMINATED WHEN ADDING THRUST FOR TAKEOFF. THRUST LEVERS WERE BROUGHT TO IDLE. REMOVED AND REPLACED LH ENG SPAR SHUTOFF VALVE IAW AMM 767 28-22-11.SDR NACA2024061800001Valve · intermittentFWD EQUIP EXH VALVE INTERMITTENT. CAME ON DURING ENG START THEN WENT OUT PRIOR TO TAXI/TAKEOFF. ACCOMPLISHED FIM 21-58-00 IAI SUPP FIG 105, FOUND OPEN GROUND AT PIN 4 K1005 AND V 12 VALVE. REPAIRED WIRE IAW SWPM 20-30-12, OPS TEST NORMAL.SDR IXXA20240619041Warning System · activatedON CLIMB OUT CREW REPORTED, MAIN CARGO DOOR LIGHT ILLUMINATED AT FL280. PRESSURIZATION OK. CREW ELECTED AIR TURN BACK TO KLAL WITH AN EMERGENCY DECLARATION. LANDING WAS WITHOUT INCIDENT AND NO ADDITIONAL PRECAUTIONARY ACTIONS NOTED. POST FLIGHT LINE MAINTENANSDR NACA2024061600002Idg · failedR GEN DRIVE EICAS MSG. R GEN OFF EICAS MSG. REMOVED AND REPLACED RH GEN DRIVE IAW MM 24-11-01 OPS CHECK NORMAL, NO LEAKS NOTED.SDR NACA2024061600001Valve · faultedMI@0620Z @KMIA DUE TO FWD EQUIP VAL VALVE EICAS MSG. REMOVED AND REPLACED V12 EXHAUST OVERBOARD VALVE IAW B767 AMM 21-58-05 OPS TEST NORMALSDR IXXA20240617040Warning Light · illuminatedON CLIMB OUT CREW REPORTED, MAIN CARGO DOOR LIGHT ILLUMINATED AT FL280. PRESSURIZATION OK. CREW ELECTED AIR TURN BACK TO KLAL WITH AN EMERGENCY DECLARATION. LANDING WAS WITHOUT INCIDENT AND NO ADDITIONAL PRECAUTIONARY ACTIONS NOTED. FAULT TRANSFERRED TO DEFERR
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