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 RAIA0009003Seal · failed6179-JFK- LEFT DUCT FAIL CAPTION ILLUMINATED DURING TAXI. MAINTENANCE INSPECTED AND REPLACED LEFT DUCT GAMMAH SEALS.SDR ASOA00097Boot · looseFLT 4887 - DURING CLIMB-OUT ON FLIGHT FROM OKC TO DFW, CREW RECEIVED RIGHT DUCT LEAK LIGHT. CREW FOLLWED CHECKLIST. CREW DECLARED AN EMERGENCY AND RETURNED TO OKC. MAINTENANCE INSPECTED RIGHT PACK AREA AND FOUND HEAT EXCHANGER BOOT LOOSE. MAINTENANCE RESECSDR RAIA0008021Seal · failed7316-STL- RIGHT BLEED LEAK FAULT ILLUMINATED ON TAXI. MAINTENANCE INSPECTED AND DEFERRED PER MEL. MAINTENANCE REPLACED RIGHT LEADING EDGE BLEED DUCT SEALS.SDR AALA20001428Valve · defectiveDFW - FLT 1632 - SECONDS AFTER TAKEOFF, TAIL COMPARTMENT TEMP HIGH LIGHT ILLUMINATED. LIGHT REMAINED ON FOR FIVE MINUTES. RETURNED AND LANDED DFW WITHOUT INCIDENT. REPLACED LEFT AUGMENTATION VALVE. SYSTEM GROUND CHECK NORMAL OPERATION. (M)SDR ASOA00100Duct · brokenFLT 4341 - DURING FLT FROM CRW TO ATL, A LOUD POOP SOUND CAME FROM THE LEFT ENGINE AREA FOLLOWED BY A SMOKE SMELL IN THE COCKPIT AND A DUCT LEAK AURAL WARNING AND LIGHT ON THE LEFT SIDE. CAPTAIN PULLED THE POER LEVER TO IDLE ON THE LEFT ENGINE TO REDUCE BLEEDSDR SIMA2396Seal · leakingMIA - FLT 5215 - CREW ABORTED TAKEOFF DUE TO BLEED LEAK INDICATION. MAINTENANCE RELACED THE BLEED DUCT SEALS IN THE RIGHT WING LEADING EDGE. NO DEFECTS NOTED ON GROUND ENGINE RUN. AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR AALA20001427Clamp · looseDFW - DURING FLIGHT, TAIL COMPARTMENT TEMP HIGH LIGHT ILLUMINATED. RETURNED AND LANDED DFW WITHOUT INCIDENT. TIGHTENED LEFT AUGMENTATION VALVE CLAMP. SYSTEM GROUND CHECK NORMAL OPERATION. (M)SDR GAIA00507Shutoff Valve · stuckFLT 6831 - PHX-MHR - DURING CLIMB-OUT FROM PHX, LEFT ENGINE BLEED TRIP OCCURRED, IT WAS RESET IAW ABNORMAL PROCEDURES CHECK LIST AND DID NOT RECUR. SOON THEREAFTER LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED. ABNORMAL PROCEDURES WAS ACCOMPLISHED AND LIGHT EXTISDR RAIA0008013Seal · failed6315-BOS- BLEED 1 LEAK EICAS MESSAGES ILLUMINATED DURING TAXI. MAINTENANCE INSPECTED AND REPLACED BLEED DUCT SEALS ON LEFT SIDE AFT OF LEFT WING CONNECTION.SDR CA000907026Pipe · ruptured(CAN) CREW REPORTED FLOOR HEAT AND WINDOW DEFOG SYSTEMS INEFFECTIVE/LOW FLOW. TROUBLESHOOTING REVEALED HOT AIR PIPE RUPTURED AT BEND ABOVE L/H WHEEL WELL UNDER L/H WING ROOT FAIRING. HOT AIR PIPE REPLACED AND AREA INSPECTED FOR HEAT DAMAGE NONE FOUND. AIRCRAFTSDR RAIA0008009Seal · failed7364-STL- RIGHT DUCT FAIL ILLUMINATED SHORTLY AFTER FLOW IS TURNED ON. MAINTENANCE INSPECTED AND REPLACED RT BLEED AIR DUCT SEALS.SDR EISA20000130Duct · rupturedLOWER AFT BODY OVERHEAT LIGHT ILLUMINATED AFTER NR 2 ENGINE BLEED OPENED AFTER TAKEOFF, APPROX 1500 AGL. WENT THROUGH AOM ABNORMAL PROCEDURE, OVERHEAT LIGHT EXTINGUISHED APPROX 1-2 MINUTES AFTER NR 2 ENGINE REDUCED TO IDLE. OVER NEXT 15 MINUTES, SLOWLY INCRESDR EISA20000129Shutoff Valve · inoperativeLOWER AFT BODY OVERHEAT LIGHT ILLUMINATED IN FLIGHT, COMPLETED PROCEDURES PER AOM. THE LIGHT EXTINGUISHED WHEN THE NR 1 BLEED WAS CLOSED. REPLACED SHUT OFF VALVE PER M/M 36-12. OPS CHECK NORMAL.SDR EISA20000128Clamp · looseNR 3 ENGINE STRUT OVERHEAT LIGHT CAME ON AFTER 10 MINUTES OF FLIGHT ON CLIMBOUT. PULLED NR 3 THROTTLE BACK AND LIGHT WENT OUT. WENT THROUGH PROCEDURES AND LIGHT DID NOT COME ON. CHECKED STRUT AREA FOR LEAKS, REPLACED 1 CLAMP ON 13TH STAGE DUCT PER M/M 36-00SDR EISA20000127Clamp · looseON CLIMBOUT, ENGINE NR 3 STRUT OVERHEAT LIGHT ILLUMINATED, WENT OUT WHEN THROTTLE RETARDED REPEAT. REMOVED AND REPLACED WITH NEW CLAMP ON BLEED VALVE PER M/M 36-00, OPS CHECK AND LEAKS CHECK NORMAL.SDR EISA20000126Clamp · looseNR 3 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED ON CLIMB WITH CLIMBING EPR, RETARD THROTTLE LIGHT GOES OUT. REPOSITIONED 13TH STAGE DUCT CLAMP, ENGINE OPS CHECK GOOD M/M 36-20. NO DEFECTS NOTED.SDR RAIA0008011Relay · failed7260-STL- LEFT ENGINE BLEED LEAK INDICATION DURING TAXI. MAINTENANCE INSPECTED AND DEFERRED PER MEL. MAINTENANCE REPLACED RELAY 43HA.SDR DL72S001559Duct · rupturedENG NR 1 STRUT OVERHEAT LIGHT ILLUMINATED IN CLIMB PASSING FL 250. COMPLETED WITH POM PROCEDURES, LIGHT REMAINED EXTINGUISH WITH THROTTLE AT IDLE. NR 1 BLEED SWITCH HAS NO EFFECT. DIVERTED TO DFW. FOUND HI STAGE PNEUMATIC -Y- DUCT IN PYLON RUPTURED. RSDR DLL14001555Duct · damagedON CLIMBOUT OF DFW, NR 1 ENG NACELLE OVERHEAT LIGHT CAME ON FWD PANEL WITH A AND B LIGHTS ON F/E PANEL. FOLLOWED ABNORMAL PROCEDURE, GOT LIGHT OUT AND CONTINUED OPERATION. SHORTLY THEREAFTER STILL IN CLIMB B NACELLE LIGHT CAME ON AGAIN. HAD TO OPERATE AT RESDR AALA20001330Clamp · brokenDFW - FLT 1959 - TAIL COMPARTMENT HIGH LIGHT CAME ON APPROXIMATELY 1 MINUTE AFTER TAKEOFF. RETURNED AND LANDED DFW WITHOUT INCIDENT. REPLACED CLAMP ON HEAT EXCHANGER. SYSTEM GROUND CHECK NORMAL OPERATION. (M)SDR 0003086623Valve · failedDURING CLIMB, THE NR 3 EPR DROPPED AND EGT ROSE FOLLOWED BY AN ENGINE FIRE WARNING. DISCHARGED ONE FIRE BOTTLE AND AIRCRAFT RETURNED TO SFO AND LANDED WITHOUT INCIDENT. REPLACED THE HIGH STAGE VALVE, HIGH STAGE CONTROL, AND PRESSURE RELIEF VALVE. OPERATIONASDR 0002866623Valve · failedDURING CLIMB, THE NR 3 EPR DROPPED AND EGT ROSE FOLLOWED BY AN ENGINE FIRE WARNING. DISCHARGED ONE FIRE BOTTLE AND AIRCRAFT RETURNED TO SFO AND LANDED WITHOUT INCIDENT. REPLACED THE HIGH STAGE VALVE, HIGH STAGE CONTROL, AND PRESSURE RELIEF VALVE. OPERATIONASDR 20001214SH002Guide · separatedADHESIVE USED TO INSTALL THE KALREZ PACKING IN THE GUIDE ASSY FAILED TO PROVIDE GOOD ADHESION ALLOWING THE PACKING TO SEPARATE AWAY FROM THE ECCOBOND 104 ADHESIVE CAUSING THE OVERPRESSURE SWITCHER NOT TO OPERATE WITHIN LIMITS. POSSIBLE CAUSE, POOR ADHESION BESDR AALA20001325Valve · leakingORD - FLT 1626 - TAIL COMPARTMENT TEMP HIGHT LIGHT CAME ON DURING CLIMBING. THE LIGHT WENT OUT AFTER ABOUT 5 MINUTES. RETURNED AND LANDED ORD WITHOUT INCIDENT. REPLACED RIGHT SIDE PNEUMATIC SYSTEM AUGMENTATION VALVE. SYSTEM GROUND CHECKED, NORMAL OPERATIONSDR VNAA0008008Sensor · failedAFTER DEPARTURE THE CREW WAS GETTING A LEFT HAND BLEED VALVE FAIL MESSAGE. AFTER A MAINTENANCE CALL AND DIFFERENT PROCEDURES, MAINTENANCE CONTROL ADVISED THE CREW TO RETURN TO PIT. MAINTENANCE INSPECTED AND REPLACED THE LEFT HAND HIGH PRESSURE TEMPERATURE SESDR 00FDEA00539Clamp · looseNR 1 ENGINE STRUT OVERHEAT LIGHT ILLUM AFT T/O. FOUND V-BAND CLAMP LOOSE AND LEAKING. TIGHTENED CLAMP PER MM 36-00-001-2. LEAK CHECK GOOD. SECURED ACCESS PANELS.SDR 2000UALA00533Duct · failedFROM OBSERVER ON GROUND, DURING INITIAL CLIMBOUT, WHITE SMOKE OBSERVED COMING FROM THE NR 2 ENGINE AND METALLIC OBJECT DEPARTED AIRCRAFT FROM THE AREA OF NR 2 ENGINE. HAD NR 2 ENGINE FIRE WARNING FOR ABOUT 10 SECONDS. ENGINE SHUT DOWN. DUMPING FUEL IN PREPASDR SWIA971915Clamp · looseRIGHT 14TH DUCT MESSAGE AFTER TAKEOFF. RETURNED TO SLC. FOUND LOOSE CLAMP ON 14TH STAGE BLEED VALVE. TIGHTENED CLAMPS AND RAN RIGHT ENGINE. OPS CHECK 14TH BLEED SYSTEM, NO LEAKS AND NO MESSAGES.SDR AALA20001267Valve · leakingDFW - FLT 1357 - TAIL COMPARTMENT HIGH TEMP LIGHT CAME ON DURING CLIMB-OUT. WENT OUT WHEN PACKS PUT TO MP BLEED OFF. THEN CAME BACK ON IN APPROXIMATELY 30 SECONDS. WENT OUT AFTER LEFT ENGINE BROUGHT TO IDLE BUT CAME BACK ON IN LESS THAN 1 MINUTE. BOTH ENGISDR CA000824032Line · worn(CAN) BLEED AIR LINE LOCATED AT THE FRONT OF THE FIREWALL FOUND TO BE WORN, BY STARTER GENERATOR COOLING DUCT. LINE WAS REPLACED. BOTH OTHER COMPANY 208S WERE INSPECTED, ONE WAS FOUND TO HAVE CONTACT IN THE SAME AREA. DUCT WAS SECURED AWAY FROM THE BLEED AIR SDR COMA0060621Line · crackedRIGHT HAND JET PIPE OVERHEAT WARNING. REPLACED A CRACKED SECTION OF THE 14TH STAGE BLEED AIR SUPPLY LINE IN ENGINE PYLON.SDR RAIA0007026Seal · failed6235-JFK- APU BLEED LEAK ONE EICAS MESSAGE ILLUMINATED ON GROUND. MAINTENANCE INSPECTED AND DEFERRED APU PER MEL. MAINTENANCE REPLACED APU BLEED AIR DUCT SEALS.SDR DLM88001353Duct · crackedON CLIMBOUT THUR 1200 FT, TAIL COMPARTMENT TEMP HI LIGHT CAME ON EVEN WITH BOTH A/C SUPPLY SWITCHES IN HP BLEED OFF. LIGHT ILLUMINATES WHEN CLIMB THRUST APPLIED. FOUND A/C WATER SEPARATOR TO CHECK VALVE DUCT CRACKED. REMOVED DUCT WELDED CRACK PER ERA 377908SDR GAIA00391Clamp · looseFLT 1759 - IAH-MEM - DURING CRUISE, THE NR 3 STRUT OVERHEAT LIGHT ILLUMINATED. THE CREW COMPLIED WITH THE APPROPRIATE CHECKLISTS, AND LIGHT WENT OUT WHEN NR 3 ENGINE WAS RETURNED TO THE IDLE POSITION. THE AIRCRAFT CONTINUED TO MEM AND LANDED WITHOUT ANY FURTSDR GAIA00390B-Nut · looseFLT 1760 - FWA-IAH - DURING CRUISE, THE NR 3 STRUT OVERHEAT LIGHT ILLUMINATED. THE CREW COMPLIED WITH THE APPROPRIATE CHECKLISTS, AND CONTINUED TO IAH AND LANDED WITHOUT ANY FURTHER DIFFICULTIES. FOUND B-NUT LOOSE ON 13TH STAGE MODULATION VALVE. RESECURED LSDR 00FDEA00451Clamp · leakingLWR AFT BODY OVERHEAT LIGHT IN FLT. PERFORMED PROC ON 2-7-14 TO STEP 14, LIGHT WENT OUT. FOUND CLAMP ON PURGE AIRLINE TO AIR CLEANER IN LEFT AFT AIRSTAIRS LEAKING. TIGHTENED CLAMP PER STANDARD MAINT PRACTICES. RAN APU PER JET RUN HDBK, NO LEAKS NOTED.SDR GAIA00387Clamp · unsecureFLT 1804 - ELP-FWA - THE LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED, AND SPLIT IN DUCT PRESSUR WAS INDICATED. THE FLIGHT CONTINUED TO FWA AND LANDED SAFELY WITHOUT ANY FURTHER DIFFICULTIES. CHECKED FOR DUCT LEAKS AND NO DEFECTS WERE NOTED. FOUND THE OVERHEATSDR RAIA0007015Switch · failed7320-STL- RIGHT BLEED OVERTEMP DURING TAXI. MAINTENANCE INSPECTED AND DEFERRED RIGHT BLEED PER MEL. MAINTENANCE REPLACED RIGHT BLEED OVERTEMP SWITCH.SDR DLL10001293Duct · leakingDURING CLIMB HAD SMOKE IN COCKPIT AND CABIN. FOUND LEFT COMPENSATOR DUCT LEAKING BENEATH C1 B/B. REPLACED DUCT.SDR AALA20001121Line · looseFLT 464 - PLS-MIA - EN ROUTE, NR 3 STRUT OVERHEAT LIGHT ILLUMINATED DURING CLIMB-OUT. LIGHT EXTINGUISHED WHEN THROTTLE WAS RETARDED PER EMERGENCY PROCEDURES CHECKLIST. RETURNED PLS AND LANDED WITHOUT FURTHER INCIDENT. TIGHTEN FLEXIBLE LINE AT 36-10-009, ACCSDR ASOA00080Controller · inoperativeFLT 4101 - CREW RECEIVED A RIGHT ENGINE 14TH STAGE BLEED WARNING. CAPTAIN STARTED RETURNING TO ATL, WARNING WENT AWAY. MESSAGE THEN CAME BACK ON. CAPTAIN HAD TO SHUT ENGINE DOWN PER THE POH AND DIVERTED AIRCRAFT TO HSV. AIRCRAFT LANDED SAFELY. MAINTENANCESDR CA000731022Cooler · cracked(CAN) AIRCRAFT ARRIVED WITH SMALL OIL LEAK ON RT LOWER ENGINE NACELLE. PRECOOLER HAD CRACKED ALLOWING HOT P3 AIR TO BLOW ONTO OIL COOLER. OIL COOLER FINS MELTED ALLOWING OIL LEAK. OIL COOLER P/N 114-389000-5.THIS IS SECOND INSTANCE FOR THIS DEFECT FOR OUR FLEESDR UPS00633145Shutoff Valve · fluctuatesPILOTS REPORT, LT ENGINE DUCT PRESSURE FLUCTUATION. T/S PER FIM TO LT ENGINE HIGH-STAGE VALVE. REPLACED LEFT ENGINE HPSOV PER AHM 36-11-07 PAGE 401-109 ALL TEST NORMALSDR 20001012AP002Seal · wornFLT 286 - OGG-ITO - FLIGHT CREW EXPERIENCED A LEFT WING BODY OVERHEAT LIGHT ON. LIGHT WENT OUT AFTER LEFT BLEED SWITCH WAS TURNED OFF AND ISOLATION VALVE CLOSED. CREW RETURNED TO OGG AFTER CONFERRING WITH DISPATCH THAT THER WAS NO MAINTENANCE SUPPORT AVAILABSDR TSAA0026160Clamp · wornFLT - 286 - OGG-ITO - FLIGHT CREW EXPERIENCED A LEFT WING-BODY OVERHEAT LIGHT ON. LIGHT WETN OUT AFTER LEFT BLEED SWITCH WAS TURNED OFF AND ISOLATION VALVE CLOSED. CREW RETURNED TO OGG AFTER CONFERRING WITH DISPATCH THAT THERE WAS NO MAINTENANCE SUPPORT AVAISDR DLM11001207Controller · failedAT CRUISE ENG-WING-TAIL ANTI ICE SELECTED ON. AFTER APPROX 1 MIN AVIONICS OVRD AND FLOW LT CAME ON AND CABIN PRESSURE WENT FULL CLOSED NR 1 & 3 BLEEDS SHUT OFF. SHUT OFF ANTI ICE AND NR 2 BLEED LOST. AFTER 30 SEC ALL BLEEDS CAME BACK ON WITH AVIONICS OVRDSDR SCNA00063Duct · looseAFTER A HEAVY MAINTENANCE CHECK, DURING THE ACCEPTANCE FLIGHT, THE LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED DURING CLIMB. THE AIRCRAFT COULD NOT MAINTAIN THE CABIN WITH ONE PACK. THE MAX AIRCRAFT ALTITUDE 19,000 FT AND THE MAX CABIN ALTITUDE 7,000 FT. REMOSDR CA000731023Cooler · cracked(CAN) PILOTS REPORT RT ENGINE RUNNING HOTTER THAN LT. RT PRECOOLER HAD CRACK IN IT, P3 AIR STRIKING OIL COOLER CAUSED LEAK. SMALL AMOUNT OF OIL COMING FROM OIL COOLER, P/N 114-3890005. THIS IS ONE OF TWO INSTANCES OF PRECOOLER BURNING INTO OIL COOLER THIS MONTSDR 00FDEA00383Duct · damagedNR 1 ENGINE STRUT OVERHEAT CAME ON IN FLT (WITH ENG ANTI-ICE SELECTED). EXTINGUISH WHEN THROTTLES PULL BACK TO IDLE. *S/D* REMOVED AND REPLACED DUCT AS PER MM 36-11-051-4. NO LEAKS AND NO OVHT LIGHT. OK FOR SERVICE.SDR DLM88001130Duct · dislodgedAPU FIRE WARNING OFF/AGENT, BOTTLES DISCHARGED. REPLACING FIRE BOTTLES, FOUND APU SURGE VALVE DUCT CLAMP AND BOOT BLOWN OFF. HOT SURGE AIR CAUSED FIRE INDICATION. REPLACED BOOT AND LEAK CHECKED. REPLACED FIRE BOTTLES. A/C RETURNED TO SERVICE.
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