Boeing 767-31B
Service difficulty reports · 617
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 = '76731B' 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 = '76731B' 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 UIEA2017090201591Radar · malfunctionedCAPTAIN`S RADAR DOESN'T PAINT ANYTHING WHEN ON LT OR RT SYSTEM , FIRST OFFICER`S RADAR WORKS. PERFORMED AN OPERATIONAL CHECK IAW AMM 34-43-00, NO FAULTS NOTED AT THIS TIME.SDR UIEA2017083101588Connector · damagedAPU DIED WHILE RUNNING. FOUND PUSHED PIN ON CONNECTOR D492 FOR APU ALTN CTRL CB. REPAIRED AND OP GOOD IAW AMM 49-41-01 AND 49-31-04.SDR UIEA2017082801560Engine · failedAPU FAULT, WOULD NOT START ON 2 ATTEMPTS. RPM WOULD NOT EXCEED 15 PERCENT.SDR UIEA2017082501548Fire Warning · false activationEICAS MESSAGE FOR FIRE OVERHEAT SYS JUST PRIOR TO LANDING. TROUBLESHOT IAW FIM 26-11 FT 804, NO DEFECTS NOTED.SDR UIEA2017082201523Warning Message · illuminatedMN CARGO LOOP 1 STATUS MESSAGE.SDR UIEA2017082201521Circuit Card · failedAPU FIRE LOOP 1 STATUS MESSAGE. PERFORMED TROUBLESHOOTING OF THE APU FIRE LOOP 1 IAW FIM 26-15-803. INSULATION RESISTANCE TEST PASSED. RESET AFOLTS CARD M685 SYSTEM FUNCTIONED NORMAL. REMOVED AND REPLACED THE APU FIRE DETECTION CIRCUIT CARD IAW AMM 26-10-0SDR UIEA2017082201520Apu · malfunctionedUNABLE TO START APU. OPS CHECK APU IAW FIM 49-11-988, APU OPS CHECKED NORMAL. NO DEFECTS NOTED. START EGT MAX 778, STABLE AT 343 EGT. KVA MAX ELEC AIR LOAD, EGT STABILIZED AT 450 DEGREES.SDR UIEA2017081501489Valve · malfunctionedRIGHT ENGINE SPAR VALVE OPERATIONAL CHECK UNSUCCESSFUL. RT ENGINE SPAR VALVE INDICATION INOPERATIVE. PERFORMED CONFIRMATION OF OPERATION IAW DDG 28-40-02.SDR UIEA2017081701497Smoke Detector · faultySTATUS MSG AFTER LANDING. MAIN CARGO LOOP 1. REMOVED SMOKE DETECTOR M12213 IAW AMM 26-14-01. OPS CHECK GOOD AND PLACARDS REMOVED.SDR UIEA2017081401471Starter · failedAPU COLD SOAK START FAILED ON THREE ATTEMPTS. REMOVED AND REPLACED THE STARTER , GROUND TESTED OK IAW AMM 49-41-01.SDR UIEA2017080901444Apu · malfunctionedAPU COLD SOAK START FAILED THREE ATTEMPTS AT FL 410 -49. CHECKED OIL QTY AND BITE CHECKED ECU AND OPS CHECKED ON GROUND IAW AMM 12-13-01, 49-01-05, AND 49-11-00.SDR UIEA2017072001245Rub Strip · damagedNR 1 ENGINE, LT CORE COWL EXTERIOR FWD SURFACE WEAR STRIP FOUND DAMAGED. WEAR STRIP REMOVED AND REPLACED AS PER SRM 51-40-02 REV 104.SDR UIEA2017070101081Bracket · wornNR 2 ENGINE LT CORE COWL ATTACH 5TH HAT FROM LOWER FOUND WORN. MOST AFT FRAME ATTACH WORN HAT (5TH FROM LOWER) REMOVED AND REPLACED AS PER SRM 51-40-02 REV 104.SDR UIEA2017070101082Rivet · shearedNR 2 ENGINE, RT CORE COWL INTERIOR AREA DATA SUPPORT PLATE ATACH RIVET FOUND SHEARED. THE RIVET WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.SDR UIEA2017073001380Window · crackedCOCKPIT, CAPTAIN SIDE WINDSHIELD FOUND CRACKED. THE WINDSHIELD WAS REMOVED AND REPLACED IAW AMM 56-11-01, REV 121.SDR UIEA2017072901375Indicator · looseFOUND APU CYCLE COUNTER INDICATOR LOOSE NEAR E6 IN THE AFT CARGO BAY. THE APU CYCLE COUNTER INDICATOR WAS REMOVED AND REPLACED IAW AMM 49-72 00, REV 121. CHECKED IAW AMM 49-72-00, REV 121.SDR UIEA2017072901376Attach Bracket · brokenFWD CARGO BAY, AIR COOLING FAN AT BS 390, LT CLEVIS ATTACHMENT FOUND BROKEN. THE ATTACH BRACKET WAS REMOVED AND REPLACED IAW AMM 20-11-00, REV 121.SDR UIEA2017072901377Transmitter · failedEICAS DISPLAY FOR LT PACK PRIMARY HX IN NO INDICATION. THE TEMP TRANSMITTER WAS REMOVED AND REPLACED IAW AMM 21-52-03, REV 121. OPS TESTED IAW AMM 21-52-03, REV 121.SDR UIEA2017073001378Controller · malfunctionedLEFT HPC BITE SWITCH FAULT DURING AIR SUPPLY MODULE BITE TEST. THE 1 ENGINE HPC WAS REMOVED AND REPLACED. AIR SUPPLY MODULE BITE TEST CARRIED OUT IAW AMM 36-11-08, REV 121. FOUND SATISFACTORY.SDR UIEA2017073001379Shutoff Valve · damagedNR 2 ENGINE PRSOV FOUND WITH BROKEN SENSE LINE. THESHUTOFF VALVE WAS REMOVED AND REPLACED IAW IAW AMM 36-11-09, REV 121.SDR UIEA2017072801342Sensor · corrodedRIGHT PACK COMPRESSOR OUTLET TEMP 2 SENSOR (TS5135) FOUND CORRODED. THE TEMP SENSOR WAS REMOVED AND REPLACED IAW AMM 21-56-06, REV 121. OPS TESTED IAW AMM 21-56-06, REV 121.SDR UIEA2017072301279Duct · crackedRIGHT AIR CON BAY WATER EXTRACTOR ASSY OTBD DUCT FOUND CRACKED. THE DUCT WAS REMOVED AND REPLACED IAW AMM 21-51-04, REV 121, AND INSTALLATION TEST AND LEAK CHECKED GOOD IAW AMM 21-51-04, REV 121.SDR UIEA2017072401297Pressure Switch · failedDC FUEL PUMP ON MESSAGE SHOWS ON EICAS DISPLAY. APU FUEL PRESSURE SWITCH REPLACED IAW AMM 28-25-03, REV 121, AND PRESSURE SWITCH OPERATION TESTED GOOD IAW AMM 28-25-03, REV 121.SDR UIEA2017072601313Frame · crackedA CRACK WAS FOUND APPROX. 0.7 INCHES IN LENGTH, DURING HFEC INSPECTION AT BS 903.5 RBL 89, BELOW WL 200 FRAME. REPAIRED IAW EN1146-17 REV, SB767-53A0209, FIG 24, REV 02.AND EO 6753A038, REV 8.SDR UIEA2017072801333Bonding Jumper · frayedLEFT AIR CONDITIONER BAY HEAT EXCHANGER PRIMARY AND SECONDARY LOWER BRACKET BONDING JUMPERS FOUND FRAYED. THE BONDING JUMPERS WERE REMOVED AND REPLACED IAW AMM 20-11-00, REV 121.SDR UIEA2017072801334Sleeve · leakingLEFT AIR CONDITIONER BAY AT ACM OUTLET DUCT SENSE LINE RUBBER SLEEVE FOUND LEAKING. REMOVED AND REPLACED THE SLEEVE IAW AMM 20-11-00, REV 121. LEAKED CHECKED IAW AMM 21-51-00 FOUND GOOD IAW REV 121.SDR UIEA2017072801335Clamp · damagedLEFT AIR CONDITIONER BAY FWD REHEATER SENSE LINE SUPPORT CLAMP RUBBER TORN. REMOVED AND REPLACED THE SUPPORT CLAMP IAW AMM 20-11-00, REV 121.SDR UIEA2017072801336Bonding Jumper · damagedLEFT AIR CONDITIONER BAY ACCESS DOOR 193NL FOUND THREE BONDING JUMPERS DAMAGED. THE BONDING JUMPERS WERE REMOVED AND REPLACED IAW AMM 20-10-21, REV 121, AND RESISTANCE CHECK PERFORMED IAW SWPM 20-20-00, REV 64.SDR UIEA2017072801337Clamp · damagedRIGHT AIR CONDITIONER BAY FWD REHEATER SENSE LINE SUPPORT CLAMP FOUND RUBBER TORN. REMOVED AND REPLACED THE SENSE LINE SUPPORT CLAMP IAW AMM 20-11-00, REV 121.SDR UIEA2017072801338Sleeve · leakingRIGHT AIR CONDITIONER BAY, AT ACM OUTLET DUCT SENSE LINE RUBBER SLEEVE FOUND LEAKING. REMOVED AND REPLACE SENSE LINE SLEEVE IAW AMM 20-11-00, REV 121. CARRIED OUT LEAK CHECK IAW AMM 21-51-00, FOUND GOOD IAW REV 121.SDR UIEA2017072801339Bonding Jumper · damagedRIGHT AIR CONDITIONING BAY ACCESS DOOR 194LR FOUND WITH TWO BONDING JUMPERS DAMAGED AND FRAYED. THE BONDING JUMPERS WERE REMOVED AND REPLACED IAW AMM 20-10-21, REV 121, AND BONDING RESISTENCE CHECK PERFORMED IAW SWPM 20-20-00, REV 64.SDR UIEA2017072801340Feeder Cable · damagedFOUND MAINTENANCE EICAS MESSAGES FOR THE NR 2 WINDOW HEAT. REPLACED THE NR 2 WINDOW HEAT WIRE CABLE IAW SWPM 20-10-11, REV 65, AND CARRIED OUT WINDOW OPERATIONAL TEST IAW AMM 56-11-02, REV 121.SDR UIEA2017072801341Bulb · corrodedRIGHT PACK COMPRESSOR INLET TEMP BULB FOUND CORRODED. THE INLET TEMP BULB WAS REMOVED AND REPLACED IAW AMM.SDR UIEA2017072201268Valve · failedEICAS SHOWS A FWD EQUIPMENT COOL VALVE MESSAGE AND P5 EQUIPMENT COOLING PANEL SHOWS VALUE LIGHT WHEN AIRCRAFT IN AIR MODE. FOUND GROUND EQUIPMENT COOLING EXHAUST VALUE INTERNAL POSITION CIRCUIT NO GOOD. EQUIPMENT COOLING OVERBOARD EXHAUST VALUE REMOVED & RESDR UIEA2017071901239Bonding Jumper · frayedLEFT ENGINE SPAR VALVE BONDING JUMPER FRAYED. THE BONDING JUMPER WAS REMOVED AND REPLACED IAW AMM 20-11-00, REV 121.SDR UIEA2017071901240Connector · crackedRIGHT WING REAR SPAR VALVE CONNECTOR (D1572) CRACKED. THE CONNECTOR WAS REMOVED AND REPLACED IAW SOPM 20-61-11, REV 64. OPS TEST PERFORMED IAW AMM 28-22-01, REV 121.SDR UIEA2017071901241Bonding Jumper · wornTWO BONDING WIRES AT THE APU AIR INLET FLAP ACTUATOR FOUND WORN. THE BONDING JUMPERS WERE REMOVED AND REPLACED IAW AMM 49-15-06, REV 121.SDR UIEA2017071901242Bonding Jumper · frayedAPU AIR INTAKE ACTUATOR FOUND WITH TWO BONDINGS FRAYED. THE BONDING JUMPERS WERE REMOVED AND REPLACED IAW AMM 49-15-06, REV 121.SDR UIEA2017072101252Duct · wornNR 2 ENGINE, RT CORE COWL PRECOOLER DUCT LIP FOUND WORN. REMOVED AND REPLACED IAW AMM 71-11-06, REV 121. LATCH CHECK CARRIED OUT IAW AMM 71-11-07, REV 121. FOUND SATISFACTORY.SDR UIEA2017072001246Support · corrodedROLLER TRAY SUPPORT AT BS 1197+44, RBL 8.5, FOUND CORRODED. THE CORROSION WAS REMOVED AND FOUND OUT OF LIMITS IAW SRM 53-00-07, DETAIL VIII, FIG 101, ALLOWABLE DAMAGE 1, REV 104. THE SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.SDR UIEA2017072101253Support · corrodedROLLER TRAY SUPPORT AT BS 1197, RBL 8.5 FOUND CORRODED. THE ROLLER TRAY SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.SDR UIEA2017072101254Duct · wornNR 2 ENGINE, RT CORE COWL PRECOOLER DUCT LIP FOUND WORN. REMOVED AND REPLACED IAW AMM 71-11-06, REV 121. LATCH CHECK CARRIED OUT IAW AMM 71-11-07, REV 121, FOUND SATISFACTORY.SDR UIEA2017072201264Frame · chafedBULK CARGO DOOR INTERNAL FRAME LOWER MID SECTION FOUND EDGE CHAFED. THE FRAME WAS REMOVED IAW SRM 51-40-02-0G-O, REV 104. FABRICATED A NEW FRAME IAW DWG 146T6322, REV A. THE NEW FRAME WAS INSTALLED IAW SRM 51-40-02, REV 104.SDR UIEA2017072201265Fastener · looseNR 2 ENGINE NOSE COWL UPPER AREA FOUND WITH SEVERAL FASTENERS LOOSE. THE FASTENERS WERE TIGHTEN IAW AMM 20-11-00, REV 121.SDR UIEA2017072201266Pan · corrodedAFT CARGO BAY 5L PDU PAN FOUND CORRODED. THE CORROSION WAS REMOVED AND FOUND WITHIN LIMITS IAW SRM 53-00-07, DETAIL 2, FIG 101, ALLOWABLE DAMAGED 1, REV 104.SDR UIEA2017070801131Bracket · wornNR 2 ENGINE, LT CORE COWL MOST FWD END BRACKET FOUND WORN. THE BRACKET WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.SDR UIEA2017070701120Bracket · wornNR 1 ENGINE, LT CORE COWL ATTACH BRACKET FOUND WORN. THE BRACKET WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.SDR UIEA2017070701121Bracket · wornNR 1 ENGINE, LT CORE COWL FAIRING MOST FWD END BRACKET FOUND WORN. THE BRACKET WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.SDR UIEA2017070701122Structure · scratchedNR 1 ENGINE, RT CORE COWL EXTERIOR SURFACE FOUND WITH A SCRATCH. THE SCRATCH WAS SMOOTHENED AND FOUND WITHIN LIMIT AS IAW SRM 54-45-01-1A-1, FIG 101, DETAIL 2, REV 104.SDR UIEA2017070701123Structure · scratchedNR 1 ENGINE, LT CORE COWL EXTERIOR SURFACE FOUND WITH SCRATCHED. THE SCRATCH WAS SMOOTHED AND FOUND WITHIN LIMIT IAW SRM 54-42-01-1A-1, FIG 101, DETAIL 3, REV 104.
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