Boeing 767-332
Service difficulty reports · 11,959
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 = '767332' 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 = '767332' 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 DL76P081666Valve · leakingINFLIGHT LEVEL 340, R HYD QTY EICAS MSG WARNING WITH ASSOCIATED LOSS TO 0.45 ON ARRIVAL AT GATE. RIGHT HYD QTY WENT TO 0.01.\D MODULE SHOWS NO FAULTS. REPLACED SELF RESETTING FUSE VALVE AT LEFT ANTI-SKID VALVE MODULE NR 5 LK CHECK OPS CK OK.SDR RYNA200800044Fan Blade · out of balanceDURING CLIMB AND LEVEL OFF AT F/L 370 RIGHT ENGINE VIBRATION REACHED 3.9 UNITS. THE AIRCRAFT DIVERTED TO ATLANTA FOR MAINTENANCE TO DELTA AIRLINES MAINTENANCE CENTER. ACCOMPLISHED BORESCOPE INSPECTION, FAN BLADE LUBRICATION, RIGGED VSV & VBV SYSTEM AND BALANSDR DL76G081652Valve · malfunctionedFLIGHT DECK TEMP CONTROL INOP IN AUTO AND MANUAL. FWD TO MCO PLACARD PER MEL 21-61-02A. VERIFIED FLT DECK TRIM AIR VALVE. DISCONNECTED AND STOWED CONNECTOR.SDR DL76G081647Pump · malfunctionedRTB - R FWD FUEL BOOST PUMP LOW PRESSURE LIGHT ON. FLT CREW PLACARD WAS ISSUED BUT A/C NEEDED FUEL ADDED DUE 120 RTE PER MEL.SDR DL76S081642Target · unserviceableAFTER TAKEOFF APPROX 200FT AGL, THE STICK SHAKER ACTIVATED. AIRSPEED WAS NML AND FLAPS 15DEG. DURING FLAP RETRACTION RECEIVED LEADING EDGE SLAT ASYM CAUTION MSG. PERFORMED QRH PROCEDURE. FOUND DAMAGED TARGET AT NR 10 SLAT INBD TRACK. REPLACED SAME. REPLASDR DL76P081624Actuator · malfunctionedRTB, DUE TO APU DOOR STATUS MESSAGE LOCKED DOOR OPEN PER MEL 49-15-01B. RECONNECTED APU INLET DOOR ACTUATOR CONNECTOR AND PUT ACFT IN NORMAL CONFIG. OPERATED APU START/STOP THRU SEVERAL CYCLES W/NO DEFECTS. APU OPS NML, MCO AND PLACARD REMOVED.SDR DL76G081622Pressure Switch · failedRT ENG WOULD NOT START. RTB, RT ENG PRESS SWITCH POPPING C/B REPLACED FUEL PRESSURE SWITCH PER M/M. OP CKS GOOD RAN ENG AT IDLE, NO FAULTS NOTED. ETOPS CATEGORY 'D': INABILITY TO CTRL ENG OR GET DESIRED PWR.SDR DL76L081615Coffeemaker · odorAT CRUISE F/A NOTICED ODOR IN MID GALLEY POSSIBLY ELECTRICAL, AFTER C/B PULLED FOR COFFEEMAKER, DISAPPEAR IN A FEW MINUTES. ALL AREA INSPECTED, COFFEEMAKER LIGHT AND ALL EQUIPMENTS CHECKED WITH NO FAULTS FOUND.SDR DL76G081614Pseu · no testON TAXI OUT WARN ELEX STATUS MESSAGE. STALL WARNING WILL NOT TEST. FOUND LT STALL WARNING TEST INTERMITTING BITE TEST ON WARNING ELEX MODULE A5 T/S PER M/M. REMOVED AND REPLACED PSEU PER AMM. TEST OK. WARN MSG CLEARED. STALL WARNING TEST OK.SDR DL76L081610Transmitter · inoperativeLT ENGINE OIL QTY INDICATION 0 QUARTS AFTER ENGINE START. AFTER SHORT TAXI QTY INDICATON RETURNED TO NORMAL. FWD TO MCO AND PLACARD T/S PER FIM FOUND OIL QTY TRANSMITTER INOP. REMOVED AND REPLACED OIL QTY TRANSMITTER AS PER AMM. PERFORMED OPS AND SYSTEM TSDR DL76G081580Blades · damagedRIGHT ENGINE BIRD INGESTION, ENGINE VIBS, DIVERTED TO DKR 3 FAN BLADES ARE DAMAGED BORO WAS GOOD. REPLACED FANBLADE SETS.SDR DL76L081565Connector · looseRTB - ON TAXI OUT RUDDER TRIM INOP. NO MEL RELIEF, MTC RESEATED CONNECTOR ON RUDDER TRIM MODULE SYSTEM. OPS CK OK.SDR HALA2008111700861Fire Detector · false activation"AFT CARGO DET 2" "FWD CARGO DET 2" STATUS PAGE. CHECKED COND AND SECURITY OF FWD AND AFT PIT NO DEFECTS NOTED. PERFORMED OPS CHECK OF FAULT DET SYSTEM, LIGHTS DID NOT RETURN REF AMM 26-16-00.SDR HALA2008111700856Fan Blade · distortedETOPS SIGNIFICANT SYSTEM, FOUND NR 1 ENGINE FAN BLADE 17 IS DISTORTED 1ST STAGE FAN. INSPECTED NR 1 ENGINE 1ST STAGE FAN BLADE 17. DISTORTION IS WITHIN LIMITS PER AMM 72-31-02-226-007-G00 SECTION U. RAN NR 1 ENGINE ALL PARAMETERS WITHIN TOLERANCE NO EXCESSISDR HALA2008111700855Fan Blade · distortedETOPS SIGNIFICANT SYSTEM, FOUND NR 1 ENGINE FAN BLADE 18 IS DISTORTED 1ST STAGE FAN. INSPECTED NR 1 ENGINE 1ST STAGE FAN BLADE 18. DISTORTION IS WITHIN LIMITS PER AMM 72-31-02-226-007-G00 SECTION U RAN ENGINE ALL PARAMETERS WITHIN TOLERANCE NO EXCESSIVE VIBESDR DL76G081563Pressure Switch · failedINTERMITTENT RIGHT ENGINE FUEL FILTER LIGHT. REMOVED AND REPLACED RT ENG FILTER PER M/M. INSPECTED NTF REMOVED AND REPLACED FUEL FILTER PRESSURE SW PER M/M RAN ENG MSG DID NOT RETURN.SDR HALA2008111600858Bypass Valve · failedETOPS SIGNIFICANT SYSTEM, APU HAD AUTO SHUTDOWN, FAULT LIGHT ILLUMINATED AND EICAS MSG APU FAULT DISPLAYED. TROUBLESHOT PER FIM 49-11-00 FIG 110. FOUND BAD OIL COOLER BYPASS VALVE. REMOVED AND REPLACED VALVE PER AMM 49-27-10, OPS AND LEAK CKS GOOD.SDR HALA2008111500857Seal · wornETOPS SIGNIFICANT SYSTEM, STATUS MESSAGE "APU OIL QTY" ON TAXI IN. APU RUNNING WHEN SHUT DOWN, MSG WENT AWAY. OIL QUANTITY LOW. RESERVICED OIL OPS CHECK GOOD NO LEAKS NOTED PER REF 49-11-00 FIG 116. FOUND OIL CAP RING WORN AND COCKED AND NOT SECURED PROPERSDR DL76L081591Stator · damagedDURING ACCOMPLISHMENT OF EA 51-470869-12 REV H MAINTENACE FOUND PMA STATOR HAD INTERNAL DAMAGE AND REPLACED THE STATOR, STATOR PN 2710540-1 WITH DEPT 335 AS PRIME SHOP. FAA HAS REQUESTED SDR AND QA FOLLOW-UP WITH VENDOR TO CONFIRM DAMAGE AND DETERMINE IT'S SOSDR HALA2008111100844Fan Blade · damagedUPON ARRIVAL FOUND NR 1 ENGINE HAD 2 1ST STAGE FAN BLADES WITH DAMAGE OUT OF LIMITS. ALSO 8-9 BLADES NEED TO BE BLENDED. REMOVED & REPLACED NR 1 ENGINE 1ST STAGE FAN BLADES PER AMM 72-31-02, OK FOR SERVICE.SDR DL76L081529Actuator · leakingCENTER HYDRAULIC SYSTEM WAS LOSING FLUID, ATB TO SVO. FOUND LCCA LEAKING.SDR DL76L081520Pitot Head · warning lightCAPTS PITOT HEAT LIGHT ILLUMINATED AFTER PUSHBACK. REMOVED AND REPLACED CAPTS PITOT PROBE.SDR HALA2008110900852Processor · inoperativeETOPS SIGNIFICANT SYSTEM, RT FUEL QUANTITY INDICATOR BLANK, TOTALIZER BLANK. NO EICAS MSG. ACCOMPLISHED FUEL QTY TEST IAW DELTA FIM 28-41-00 FIG 103. TEST OK PERFORMED FQIS BITE FAULTED B8, A8, C3, C6, 81, 82, 83 AND 88. REMOVED AND REPLACED FQIS PROCESSORSDR DL76L081505Starter · failedAFTER PUSH NR N2 RISE ON ENGINE START. REPLACED NR 1 ENG STARTER PER AMM 80-11-01. SERVICED OIL. CRANKED ENG AND LEAK CHECK PERFORMED OPS CK NORMAL. STARTER MFG 774860A4 S/N 960225.SDR DL76G081506Altimeter · malfunctionedATB - DUE TO ALTIMETER SPLITS.SDR DL76G081503Valve · warning lightAFTER SECOND ENGINE START NR 2 ENG, FWD EQUIPT VAL EICAS MSG WITH ASSOCIATED VALVE LIGHT ON EQUIPMENT COOLING PANEL. WENT TO STANDBY, NO HELP. RETURN TO GATE. VALVE LIGHT AND EICAS MSG WENT OUT WHEN NR 1 ENG SHUT DOWN. FWD TO MCO AND PLACARD PER MEL 21-58-0SDR DL76L081499A/C Pack · inoperativeL PACK TEMP EICAS MESSAGE WITH LEFT PACK INOP LIGHT RESET PER QRH WITH SAME RESULT. NO AUTO EVEN GENERATED. BITE PACK CONTROLLER NO FAULTS OPENED PACK BAY AND INSPECTED AREA FOR DUCT LEAKS WHILE OPERATING PACK. PACKS OPERATE NORMAL COULD NOT REPRODUCE PROBLSDR HALA2008110300841Oil System · lowETOPS SIGNIFICANT SYSTEM - "APU FAULT" EICAS, APU WILL NOT START AFTER LANDING. INSPECTED APU FOUND OIL CAP SECURE BUT OIL LEVEL LOW. SERVICED 3PT OIL. SECURED OIL CAP PER ETOPS 2 PROCEDURE & RAN APU. NO LEAKS NOTED. BITE CHECK PER 49-11-00/101 FIG 103 OKSDR DL76P081475Engine · defectiveFAILED EA 51-470869-12 REV B MGB OIL NOZZLES INSP. REPLACING NR 1 ENGINE. REPLACED NR 1 ENG PER TRANS 1T148AD.SDR DL76L081474Engine · defectiveFAILED EA 51-470869-12 REV B MGB OIL NOZZLES INSP. REPLACING NR 1 ENGINE.SDR DL76L081473Engine · defectiveFAILED EA 51-470869-12 REV B MGB OIL NOZZLES INSP. REPLACING NR 1 ENGINE.SDR DL76L081472Engine · defectiveENG FAILED EA 51-470869-12 REV B MGB OIL NOZZLES INSP. REPLACING NR 1 ENG. REPLACED NR 1 ENGINE PER TRANS 1T148.SDR DL76G081461Door · openRTB - APU DOOR LIGHT ILLUMINATED ON TAXI OUT. ACFT RELEASED AS PER MEL 49-15-01A APU INTAKE DOOR CLOSED.SDR DL76L081450Shutoff Valve · faultedLEFT ENG ANTI-ICE AFTER TAXI. FOUND HPSOV AT FAULT. FWD TO MEL.SDR DL76P081462Engine · failedOIL LOSS IN FLIGHT AND IFSD. REPLACED RT ENG PER TRANSMITTAL 1T149AD9.SDR HALA2008102500827Adc · faultyETOPS SIGNIFICANT SYSTEM - F/O ALTIMETER IN ERROR, IT READS 33850. CAPT ALTIMETER READS 34000. STBY ALT READS 34300, SELECTING ALTN AIR DATA CORRECTS FAULT. REPLACED RT ADC. OPS CHECK OK PER MM 34-12-01. PERFORMED MCDP TEST 30 TO RETAIN A/C LMP STATUS IN SDR DL76P081438Line · leakingAIRCRAFT ATB FOR NR 2 ENG LOSS OF OIL QTY AND OIL PRESSURE. CREW SHUT DOWN ENGINE PRIOR TO LANDING. T/S IN PROGRESS AIR/OIL COOLER OIL RETURN LINE FOUND CRACKED. REPLACED NR 2 ENGINE.SDR DL76G081436O-Ring · leakingON FLIGHT 30 ATB TO JFK DUE TO CTR SYS HYD QTY LOSING FLUID. FOUND NR 10 SPOILER PCA PLUS LEADING REF IPC FOR SPOILER P ITEM 425. REMOVED AND REPLACED DAMAGED O-RING PER AMM. OPS 2 LEAK CHK OK. ACFT RETURNED TO NML CONFIG ACFT OK FOR SERVICE. CTR HYDS SVCSDR DL76L081430Engine · malfunctionedAFTER LEVEL OFF AT FL 364 THE LEFT ENGINE SPOOLED BACK ON ITS OWN FOLLOWED BY NUMEROUS EEC AND ENGINE OUT MESSAGES. T/S PER FIM INSPECTION FUEL SAMPLES PLUS NR 1 ENG FUEL FILTER FOR CONTAMINATION. FILTER PLUS FUEL SAMPLE FOUND CLEAN C/W ENG FU SUCTION FEED OSDR DL76G081407Valve · intermittentDURING TAXI OUT OF BCN RT PACK VALVE WOULD NOT OPEN AFTER TURNED OFF FOR ENG START. RTB, SWAPPED PACK CONTROL CARDS NO HELP. RESEATED FCV CONNECTOR. NOW OPN NORMAL.SDR DL76L081625Engine · failedNR 2 ENGINE FAILED 25 CYCLE RE-INSPECT OF GEARBOX FOR BLAST CONTAMINANT. REPLACED NR 2 ENGINE.SDR DL76L081401Valve · malfunctionedRTB - DUE FWD CABIN TEMP CONTROL EICAS MSG. TEMP CONTROL FWD CABIN INOP LIGHT ILLUMINATED. NO MEL RELIEF BY FCP/C MTC CLOSED FWD TRIM VALVE AND RELEASED PER MEL 21-61-04A.SDR DL76L081394Nozzle · failedNR 1 ENG FAILED INSPECTION OF MAIN GEARBOX OIL NOZZLES PER EA-51470869-12. C/W EA 51-470869-12 FOUND CONTAMINATES IN BOTH NOZZLES. REQUIRES ENG CHG. REPLACED NR 1 ENG PER R/C TRANSMITTAL 23-.SDR HALA0800819Warning System · malfunctionedAFTER CLOSING MAIN CABIN DOOR, SLIDE LIGHT STARTED FLASHING. OPS CHECKED R1 DOOR SLIDE ARM/DISARM SYSTEM PER AMM 52-73-00, NO DEFECTS NOTED OK FOR SERVICE.SDR DL76L081376Light · intermittentFLICKERING LIGHT IN OVERHEAD NEAR MID GALLEY MISTAKEN FOR FIRE BY FA SHE GAVE HALON FE TO PAX WHO DISCHARGED SOME ON LIGHT.SDR DL76L081373Start Valve · failedLEFT ENGINE START VALVE FAILED TO OPEN. CONFIRMED START VLV INOP. PERF MANUAL START FWD TO MCO AND PLC PER MEL 80-00-02.SDR DL76L081372Apu · failedAPU FAILED AFTER PUSHBACK. RESTARTED APU. LOAD CKS GOOD PWR AND PNEUMATICS.SDR DL76L081368Warning Light · false activationAFTER LT ENG START AND APU SHUTDOWN LEFT GEN OFF LIGHT WITH LT ISOLATION BUSS TIE LIGHT. RAN ENG CYCLED POWER FOR LT ENG AND APU SEVERAL TIMES WITH LOAD ON GENERATORS. PERFORMED BITE AND BPCU HAD PILOT DUPLICATE POWER TRANSFER. WHEN PROBLEM OCCURRED NO FAULSDR DL76G081502Apu · unknownREPLACED APU DUE START HISTORY. APU REPLACED.SDR DL76L081365Start Valve · malfunctionedAFTER PUSHBACK LEFT ENGINE WILL NOT START. MANUALLY OPENED START VLV AND HAD ROTATION. REPLACED NR 1 ENGINE START VALVE PER AMM. STARTED NR 1 ENGINE, VALVE OPERATES NORMALLY.
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