JASC 3610
Service difficulty reports · 7,150
Reports filed under 3610 · Pneumatic Distribution System, newest first.
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 jasc_code = '3610' 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 jasc_code = '3610' 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 98ZZZX2238Heat Exchanger · rupturedTHE PART IN QUESTION IS A BLEED AIR HEAT EXCHANGER P/N 183680-3-2 USED ON A G-II AIRCRAFT. THE ORIGNAL PART WAS REPLACED DUE TO A RUPTURE OF THE LOW PRESSURE PASSAGE AFTER 18 YEARS AND 6,000 HOURS OF OPERATION. THE EXCHANGE UNIT IN QUESITON IS NOW RUPTURED WSDR USAASB98116Regulator · failedPIT - FLT 158 - AFTER TAKEOFF, AIRCRAFT WOULD NOT PRESSURIZE. RIGHT PACK SHOWED ZERO PSI. MANUAL AND AUTO SYSTEM DID NOT OPERATE. FLIGHT RETURNED TO FIELD AT PIT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND THE RIGHT ESDR AALA981003Fitting · looseDFW - FLT 568 - AFTER TAKEOFF DFW PASSING 9,000 FT TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED. RAN ABNORMAL PROCEDURE CHECKLIST, TAIL COMPARTMENT TEMPERATURE HIGH LIGHT FLICKERED A FEW MINUTES AND THAN EXTINGUISHED. A FEW MINUTES LATER, WHEN POWER ISDR 9809359752Air Ducts · failedDURING CLIMBOUT, THE TAIL COMPARTMENT OVERHEAT LIGHT ILLUMINATED. FLIGHT CREW FOLLOWED COM PROCEDURES, RETURNED TO BNA, AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE FOLLOWING LEFT SIDE COMPONENTS: THE 8TH AND 13TH STAGE AIR DUCTS, CROSSFEED VALVE, SDR S2YA98013Precooler · contaminatedFLT 1157 - MKE-MSN - SHORTLY AFTER TAKEOFF, THE FLIGHT CREW NOTICED A SLIGHT SMOKE HAZE IN THE COCKPIT. DECLARED AN EMERGENCY AND RETURNED TO MKE. AFTER MAKING AN UNEVENTFUL LANDING MAINTENANCE INSPECTED THE A/C. AFTER TESTING ALL SYSTEMS FOR PROPER OPERATISDR EISA98107Duct · looseDURING CLIMB-OUT, ENGINE NR 1 STRUT, OVERHEAT LIGHT ILLUMINATED. ACCOMPLISHED ABNORMAL CHECK LIST, AFTER CLOSING NR 1 BLEED VALVE, LEFT PACK PRESSURE WAS STILL 26 PSI. LIGHT EXTINGUISHED. GENERATED FROM PILOT REPORT. FOUND DUCT LEAKING NR 1 STRUT. TIGHTENSDR COMA9860106Clamp · corrodedA 24, 48 MONTH INSPECTION, BLEED AIR DUCT CLAMP CORRODED. REPLACED CLAMP.SDR USAABB98047Coupling · rupturedPHL - FLT 894 - APPROXIMATELY 40 MINUTES OUT OF PHL EN ROUTE TO FRA, CREW RECEIVED THE EICAS MESSAGE 'L ENG BLEED OFF' AND ASSOCIATED LIGHT. CREW ALSO RECEIVED THE EICAS MESSAGE 'L ENG OVHT' AND ASSOCIATED LIGHT. FLIGHT RETURNED TO PHL AND LANDED WITH NO FURSDR WTAA980076Air Regulator · leakingACV - RIGHT ENGINE DUCT LEAK LIGHT ILLUMINATED AFTER TAKEOFF. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. AIRCRAFT FERRIED TO FAT FOR REPAIRS. MAINTENANCE REPLACED RIGHT AIR REGULATOR. OPERATIONAL CHECK SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (M)SDR 99ZZZX1821Valve · misoverhauledRED, TI-TEMP RTV HAS BEEN APPLIED IN THE THROAT OF THE HOUSING AROUND THE BUTTERFLY SEAL SEAT. THIS BUTTERFLY SEAL IS DESIGNED TO FLOAT IN THE HOUSING, BUT IN THIS CASE, THE SEAL WAS PRESSED INTO THE BEAD OF SEALANT. SUBMITTER STATED THIS IS NOT AN ASSEMBLY SDR WRLA98083Duct · looseDURING T/O ROLL, NR 2 ENG EXPERIENCED HIGH EGT. FLT CREW ELECTED TO ABORT T/O. A/C RETURNED TO GATE W/O INCIDENT. HOWEVER, WHILE A/C WAS STANDING ON GATE 4 MAIN WHEEL ASSY'S LOST AIR PRESS DUE TO THERMAL PLUG RELEASE. MX PERSONNEL COOLED A/C BRAKES, AND RESDR 98FDEA00320Shutoff Valve · inoperativeREPEAT WRITE-UP FROM DISCREPANCY NR 01199454 ENGINE NR 3 STRUT OVERHEAT LIGHT ON. OVERHEAT LIGHT CAME ON PASSING FLIGHT LEVEL 250 AND APPROXIMATELY 20 MINUTES INTO FLIGHT. BOTH PACKS ON NR 1 BLEED OFF, NR 2 OPEN NR 3 OPEN CLIMB POWER WITHIN PARAMETERS. ADMISDR CA980602020Valve · failed(CAN) TAKEOFF ROLL ABORTED DUE TO NR 3 ENGINE THROTTLE ADVANCED WITH NO INCREASE IN POWER. THE PR VALVE WAS REPLACED BECAUSE THE SENSE LINE OF THE VALVE WAS WORN THROUGH. ENGINE RUN CARRIED OUT SERVICEABLE.SDR AALA980850Duct · looseMIA - FLT 2101 -DURING CLIMB AT ABOUT 20,000 FT LEFT ENGINE OVERHEAT WARNING APPEARED. RAN PROCEDURE AND WHEN RETARDING LEFT THROTTLE BELOW 70 PERCENT THE ENGINE OVERHEAT LIGHT EXTINGUISHED. CHECKED ALL PNEUMATIC DUCTS FOR CONDITION, ALL OK. CHECKED CLAMPS,SDR P5CA9800820Duct · crackedNR 2 PACK DUCT CRACKED AT DISCHARGE TEMP SENSOR BOSS. DUCT REMOVED FOR WELDING PER OHM 36-10-04 REV 66. DETAILS REF FORM 8130-3.SDR P5CA9800819Clamp · corrodedNR 3 TRIM AIR DUCT CLAMP AROUND COUPLING INBD OF PAC VALVE CORRODED. CLAMP REPLACED IAW MM 36-11-01.SDR USAABB98034Duct · rupturedCLT - FL 41 - AFTER TAKEOFF FROM CLT, CREW RECEIVED THE EICAS MESSAGES 'L ENG OVHT' AND 'CABIN ALTITUDE' AND THE 'OVERHEAT' LIGHT ILLUMINATED. THE CREW REDUCED POWER ON THE LEFT ENGINE AT WHICH TIME THE OVERHEAT LIGHT EXTINGUISHED. CABIN PRESSURIZATION COULDSDR CA980512021Duct Seal · missing(CAN) ON DEPARTURE, NR 2 ENG FIRE LIGHT ILLUMINATED. WHEN NR 2 ENGINE THRUST LEVER AT IDLE, ENGINE LIGHT WENT OUT. ENGINE WAS NOT SHUT DOWN. MAINTENANCE FOUND SEAL MISSING FROM HIGH PRESSURE DUCT FLANGE AT 7 O'CLOCK POSITION AND FLANGE AT 4 O' CLOCK POSITIOSDR CKSA98262Clamp · looseENG 3 FIRE DETECTION AT 7,000 FT WITH LIGHT ILLUMINATED AND RED T-HANDLE ILLUMINATED AND HYD BARRIER LIGHTS ON. TIGHTENED LOOSE DUCT CLAMP AT NR 3 ENGINE MIXING EJECTOR SYSTEM OPS AND LEAK CHECK GOOD WITHOUT FIRE LOOP LIGHT DETECTION IAW L1011 MM CH 36-11-08.SDR ABXA9800345Connector · failedLOUD AIR NOISE IN FWD COCKPIT AREA. HOT ODOR NOTICED IN COCKPIT. CREW EXPERIENCED BURNING EYES AND HEADACHE. NOISE WAS ELIMINATED BY TURNING OFF NR 3 CTC. REPLACED PNEUMATIC DUCT CONNECTOR, LEAK CHECKED GOOD.SDR AALA980750Valve · defectiveSFO - FLT 0037 - LT BLEED DUCT LEAK LIGHT ON TAKEOFF. LIGHT EXTINGUISHED AFTER ENGINE BLEED VALVE CLOSED. INSPECTED AND FOUND AFT GROUND AIR SUPPLY CHECK VALVE OPEN. REMOVED AND REPLACED GROUND AIR SUPPLY CHECK VALVE. LEAK CHECK GOOD. ACCOMPLISHED HIGH POWSDR ORJA9872Clamp · brokenRETURN TO GATE DUE TO TAIL COMPARTMENT TEMP HIGH LIGHT ILLUMINATED AFTER TAKEOFF. FOUND BROKEN CLAMP ON RT CROSSFEED VALVE. LEAK CHECK OK. REMOVED AND REPLACED CLAMP. LEAK CHECK GOOD. (M)SDR AALA980748Clamp · looseMCO - FLT 0626 - EN ROUTE FLL/LGA, TAIL COMPARTMENT HIGH TEMPERATURE LIGHT ILLUMINATED AND ACFT DIVERTED AND LANDED OVERWEIGHT MCO WITHOUT FURTHER INCIDENT. OVERWEIGHT INSPECTION ACCOMPLISHED WITH NO DAMAGE NOTED. TAIL COMPARTMENT DUCTING INSPECTED AND RIGHTSDR AALA980736Duct · rupturedDFW - FLT 1396 - AFTER TAKEOFF DFW DURING CLIMB-OUT THROUGH FL 230, TAIL COMPARTMENT HIGH TEMPERATURE LIGHT ILLUMINATED. ACCOMPLISHED ABNORMAL PROCEDURES AND AIRCRAFT RETURNED TO DFW LANDING WITHOUT INCIDENT. REPLACED RUPTURED DUCT ASSY. SYSTEM LEAK CHECKEDSDR HALA9800091Controller · failedFLT 25 - LOS - NR 1 MANIFOLD FAIL LIGHT ILLUMINATED DURING CLIMB. PERFORMED ABNORMAL PROCEDURE. SUPPLY SELECTOR AND PACK OFF. LIGHT DIDN'T GO OUT WITH SYSTEM UNPRESSURIZED AND PNEU TEMPERATURE BELOW 120 DEGREES. LEFT SYSTEM UNPRESSURIZED AND DEACTIVATED FASDR REXA98087Bleed Pipe · failedRIGHT ENGINE OVERTEMP AFTER TAKEOFF. REMOVED AND REPLACED HP BLEED PIPE AND CLAMP, AND PERFORMED BOROSCOPE INSPECTION OF HOT SECTION AND POWER TURBINE IAW WITH GE MM 72-00-00. NO DEFECTS NOTED. (M)SDR 98FDEA00235Valve · leakingON CLIMBOUT, ENGINE NR 3 STRUT OVERHEAT LIGHT CAME ON. COMPLETION OF RED TABS EXTINGUISHED LIGHT. OPERATED NR 3 ENGINE WITH NO FURTHER ILLUMINATION OF LIGHT. NR 3 BLEED AND NR 2 PACK TURNED OFF AND LEFT OFF PER RED TABS. REMOVED PYLON PANELS 5501-5502 FROMSDR 98FDEA00234Clamp · looseON CLIMBOUT PASSING APPROXIMATELY FLIGHT LEVEL 270, ENGINE NR 3 STRUT OVERHEAT LIGHT CAME ON. LIGHT WENT OUT WHEN NR 3 POWER LEVER PULLED TO IDLE. RESTORED POWER AND LIGHT DID NOT COME BACK ON. FOUND ONE CLAMP LEAKING AT CHECK VALVE GOING TO AIR CLEANER. RSDR HEEA0013756Valve · failedBLEED SOV INOPERATIVE.SDR 98FDEA00233Air Supply · brokenON CLIMBOUT, ENG NR 1 FIRE WARNING CAME ON. WARNING WENT OUT UPON ENG SHUTDOWN. RETURNED TO RAMP. FOUND TUBE-RS HP RECOUP AIR SUPPLY WAS BROKEN AND MANIFOLD-HPT ACTIVE CLEARANCE CONTROL WAS CRACKED. ALSO, CLAMP JAW WAS BROKEN. REPLACED ABOVE PARTS AND RANSDR 98FDEA00229Clamp · inoperativeON CLIMBOUT WITH AIRCRAFT CLEAN AND CLIMB POWER SET AT APPROXIMATELY 7,000 FEET THE ENGINE NR 3 STRUT OVERHEAT LIGHT ILLUMINATED. COMPLIED WITH RED TAB PROCEDURE AND LIGHT WENT OUT AND STAYED OUT FOR REMAINING 30 MINUTE OF FLIGHT. FOUND 6TH STAGE DUCT LEAKINSDR 98UAL900145Heat Exchanger · failedL BLEED PRSOV SHOWS CLOSED ON AIR SUPPLY MAIN T, BLEED LOSS WING L, BODY L, BLEED LEAK L STATUS MSG'S AND L PACK INOP. CREW HEARD POP JUST BEFORE MESSAGES APPEARED. RETURNED TO IAD AND LANDED OVERWEIGHT. *S/D* FOUND LT HEAT EXCHANGER TORN OPEN AT PRIMARY INSDR 98FDEA00228Duct · cracked98-0083 - ON CLIMB-OUT FROM ANC THROUGH FL 400 ENG 1 FIRE ALERT CAME ON. FOLLOWED EMERGENCY PROCEDURE AND RETURNED TO ANC. ALL ENGINE, HYDRAULIC, PNEUMATIC AND ELECTRICAL SYSTEMS NORMAL. SUSPECT BLEED AIR LEAK IN ENG NR 1. FOUND DUCT IN PYLON CHAFFED BY T/SDR P5CA9800748Isolation Valve · inoperativeLOW DUCT PRESS ON LEFT WING DURING START. ISOLATION VALVE DOES NOT CLOSE. REMOVE AND REPLACED ISOLATION VALVE. OPS CHECK GOOD IAW MM 36-11-07.SDR 9805439920Fitting · leakingTAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED AFTER TAKEOFF. FLIGHT WAS RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED LEAKING FITTING AT AUGMENTATION VALVE, OPERATIONAL CHECK NORMAL.SDR PLGA980330AControl Valve · failedBOS - FLT 4414 - CREW RECEIVED THE RIGHT DUCT OVERTEMP WARNING WHILE IN FLIGHT. CREW FOLLOWED PROCEDURES AND SHUT DOWN THE RIGHT BLEED AIR. WARNING LIGHT REMAINED ILLUMINATED. CREW STARTED RIGHT ENGINE SHUT DOWN PROCEDURES WHEN THE WARNING LIGHT EXTINGUISHESDR 9805469920Heat Exchanger · crackedTAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED AFTER TAKEOFF. FLIGHT WAS RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED CRACKED HEAT EXCHANGER, LEAK AND OPERATIONAL CHECK WAS NORMAL.SDR HEEA0013651Valve · failedVALVE FAILED. PIECES BROKEN INSIDE.SDR HEEA0013650Valve · failedVALVE HAS PIECES BROKEN INSIDE.SDR HEEA0013649Valve · failedVALVE INOPERATIVE, PIECES BROKEN ON INSIDE.SDR AALA980633Coupling · brokenBNA - FLT 0691 - DURING CLIMB-OUT AT 18,000 FEET, TAIL COMPARTMENT HIGH TEMPERATURE LIGHT ILLUMINATED. CREW FOLLOWED CHECK LIST AND TAIL COMPARTMENT HIGH TEMPERATURE LIGHT EXTINGUISHED. AIRCRAFT AIR INTERRRUPTED AND RETURNED TO BNA WITHOUT FURTHER INCIDENT. SDR COMA9810076O-Rings · wornLEFT HAND BLEED AIR DUCT LEAK WARNING AFTER TAKEOFF. REPLACED O-RING SEALS ON LEFT HAND BLEED AIR TUBING CONNECTIONS.SDR COMA9810077O-Rings · wornLEFT HAND BLEED AIR DUCT LEAK WARNING. REPLACED WORN O-RINGS AT LEFT WING BLEED AIR DUCT JOINT.SDR REXA98076Clamp · failedLEFT ENGINE LOST TORQUE AFTER TAKEOFF TEMP WENT TO 915 DEGREES. LEFT ENGINE SHUT DOWN AND RETURNED TO MEM. FOUND LEFT ENGINE HIGH PRESSURE BLEED PIPE CLAMP BOLT SHEARERD. REMOVED AND REPLACED CLAMP AND PERFORMED ENGINE. RUNS HELD AT 60, 70, 80, 90, 100 PERSDR SIMA980791Valve · inoperativeDFW - FLT 3620 - UPON ARRIVAL TO DFW, CREW SMELLED SMOKE AND CALLED FOR CFR. PAX AND CREW DEPLANED RAPIDLY. NO EMERGENCY EVACUATION ON THE TAXIWAY. NO FIRE DETECTED. CREW THEN BROUGHT A/C BACK TO GATE. NO FURTHER INCIDENTS REPORTED. A/C RETURNED TO SERVISDR 98FDEA00209Duct · failedDURING CLIMBOUT, THE NR 3 ENGINE STRUT OVERHEAT LIGHT ILLUM. BOTH NR 3 BLEED AND RIGHT PACK WERE ON AT THE TIME. AFTER RED TABS CALLED FOR CLOSING/OFF ON BOTH NR 3 BLEED AND RIGHT PACK, THE NR 3 STRUT LIGHT WENT OUT. ENGINE PARAMETERS OK. REMOVED AND REPLASDR IXXA9800029Regulator Valve · defectiveDURING CLIMBOUT, THE NUMBER ONE AND TWO ENGINE PNEUMATIC MANIFOLD OVER TEMPERATURE INDICATING LIGHTS ILLUMINATED, VERIFIED BY TEMPERATURE INDICATOR. THE FLIGHT ENGINEER SECURED THE NUMBER ONE AND TWO ENGINE BLEED SYSTEMS FOLLOWING COMPANY EMERGENCY PROCEDURESSDR CALA9800471Bleed Lines · looseCABIN PRESSURE WAS LOST WHILE EN ROUTE FROM IAH TO CZM. THE RIGHT PACK OUTPUT WENT TO ZERO. AN EMERGENCY DESCENT WAS PERFORMED AND THE O2 MASKS WERE DEPLOYED. THE AIRCRAFT LANDED AT CZM WITHOUT FURTHER EVENT. MAINTENANCE FOUND HIGH BLEED REGULATOR LINES LOSDR 98ZZZM441Duct · looseDURING CRUISE MASTER FIRE WARNING LIGHT CAME ON. VERIFIED NR 2 ENGINE AT FAULT. REDUCED POWER AND LIGHT WENT OUT. TESTED FIRE WARNING SYSTEM WHICH WAS SATISFACTORY. RESTORED POWER AND NO FURTHER INDICATION. GROUND INSPECTION REVEALED LOW PRESS PNEUMATIC DSDR SWIA971097Clamp · failedRIGHT 14TH STAGE BLEED AIR DUCT LEAK MSG OUT OF 18000 FT ON CLIMBOUT. SYNOPTIC PAGE SHOWED RED INSIDE OF VALVE. FOLLOWED QRH CLOSING 14TH STAGE VALVE, MSG WENT OUT. RETURNED TO SLC. SECURED AND SEALED RIGHT 14TH STAGE SHUT OFF VALVE THERMAL BLANKET. SECUR
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