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 RAIA00307193Seal · blown5641-STL- LEFT DUCT FAIL INDICATION. MAINTENANCE REMOVED AND REPLACED THE LEFT DUCT GAMMA SEAL.SDR 2003FA0000765Pump · wornINSTRUMENT AIR SYSTEM INDICATED LOW OUTPUT ON GAUGE. UPON FURTHER INVESTIGATION OF PNUEMATIC SYSTEM FOUND INSTRUMENT AIR PUMP VANES WHERE WORN. PROBABLE CAUSE IS A COMBINATION OF ENGINE HEAT AND CARBON VANE HARDNESS.SDR 2003FA0000767Pump · inoperativeFLIGHT CREW REPORTED THAT GYRO WOULD NOT ERECT AT LOW RPM. DISCOVERED LOW INSTRUMENT AIR PRESSURE. REPLACED AIR PUMP AND SYSTEM OPS CHECKED NORMAL. NO RECOMMENDATION AT THIS TIME.SDR DL777030635Controller · malfunctionedENROUTE, BLEED OFF LT ENG EICAS MSG ILLUMINATED, REPLACED THE LEFT HIGH PRESSURE FAN AIR CONTROLLER AND THE LEFT MANIFOLD DUAL TEMP SENSOR (M36004). RAN THE ENGINE AT HIGH POWER ALL CHECKS WERE NORMAL. ETOPS CATEGORY 'B': DIVERSION OR TURNBACK.SDR MWEA030273Flex Line · crackedAT 35,000 FEET RED MASTER WARNING LIGHT ILLUMINATED ALONG WITH THE RED CABIN ANNUCIATOR, MASK DROPPED -- REPLACED COALESER BAG AND CLEANED BOTH WATER OUTLET SCEENS, ALSO PERFORMED A CABIN PRESSURIZATION CONTROL ADJUST, REMOVED AND REPLACED WATER SEPERATOR TESDR P8UF200300001Duct · leakingMANIFOLD FAIL LIGHT ON NR 2. SMOKE DETECT CABIN CARGO NR 8, 9, 10 LIGHT ON. SMOKE DETECT AFT CARGO NR 1, 2, 3 AND HEAT DET AND AFT CARGO FIRE LIGHT ON. PRESENCE OF SMOKE IN ALL CARGO MAIN UPPER & COCKPIT.SDR 2003FA0000720Pump · failedINSTRUMENT AIR PRESSURE BELOW LIMITS AT LOWER RPM. GYRO WARNING LIGHT ON AT 1100 RPM. LOW VOLUME FROM AIR PUMP.SDR RAIA00307185O-Ring · damaged5304-STL- NR 1 BLEED LEAK WARNING INDICATION. MAINTENANCE REMOVED AND REPLACED BLEED LINE O-RING AT LEFT SIDE BAGGAGE COMPARTMENT.SDR QXEA200300778Shutoff Valve · failedBOI- ON FLIGHT 2524 "SMOKE AFT LAVATORY" EICAS WARNING OCCURRED WITH SMOKE DETECTOR ALARM ACTIVATION IN LAVATORY. WARNING DISAPPEARED FOLLOWING PULLING CIRCUIT BREAKERS AS PER CHECKLIST. AIRCRAFT LANDED WITHOUT INCIDENT. REMOVED AND REPLACED NO.2 HOT AIR SHUTOSDR RAIA00306178Line · cracked5722-STL- AFTER TAKEOFF WHEN CHANGING FROM T/O TO CLIMB ON POWER PANEL THE RIGHT ENGINE ITT WENT INTO THE RED. MAINTENANCE REMOVED AND REPLACED CRACKED BLEED LINE FROM RT BLEED SYS.SDR WRLA200314Heat Exchanger · leakingNR 2 PNEUMATIC MANIFOLD FAILURE LIGHT ILLUMINATED WITH TWO PACKS OFF AND TWO PNEUMATIC SYSTEMS OFF. AGAIN EXECUTE VOL II 01-10-09 EMERGENCY PROCEDURE. FOUND EXCESSIVE HOT AIR LEAKAGE FROM NR 1 AND NR 2 HEAT EXCHANGERS TO BOTH ACM'S CONNECT SLEEVES AND FROM BSDR 2003FA0000719Pump · failedAIR PUMP FAILED TO PROVIDE AIR PRESSURE. RECOMMEND DIFFERENT VANES OR BETTER MATERIAL.SDR 2003FA0000727Pump · inoperativePUMP OUTPUT DECREASED AS ENGINE WARMED UP UNTIL IT BECAME UNACCEPTABLE AT LOWER RPM. AT 1000 RPM PRESSURE DROPPED BELOW 3 INCHES ON INDICATOR. TESTED AIR SYSTEM FOR LEAKS AND FOUND NONE. CHECKED REGULATOR AND MANIFOLD VALVE, REPLACED BOTH THE SYSTEM STILL FSDR RU3A03011Sense Line · damagedEN ROUTE AT FL200 RIGHT BLEED AIR FAIL ANNUNCIATOR LIGHT ILLUMINATED. EXECUTED EMERGENCY ROCEDUES AND LANDED AT NEAREST AIRPORT. FBO MAINTENANCE TROUBLESHOT SYSTEM AND FOUND HOLE IN RIGHT BLEED AIR SENSING LINE. SPLICE LINE AND OPS CHECK GOOD. (M)SDR 2003FA0000742Pump · wornAVIONICS PERSONNEL FOUND INSTRUMENT AIR PRESSURE LOW ON GROUND RUN UP. ON FURTHER INVESTIGATION FOUND VANES WORN ON PUMP. RECOMMEND PUTTING DIFFERENT TYPE OF VANES IN PUMP TO LAST LONGER.SDR 2003UALA00473Seal · defectiveRETURN TO FIELD DUE TO ECAM RIGHT WING LEAK. WITH NR 1 BLEED SYSTEM ALREADY DEFERRED INOPERATIVE, AIRCRAFT EXPERIENCED LOSS OF BLEED SYSTEM NR 2 DUE TO RIGHT WING AIR LEAK. REPLACED SEALS AND COUPLING AT RIGHT PACK HEAT EXCHANGER. SUBSEQUENT MAINTENANCE INCSDR 2003FA0000730Shaft · shearedDURING FLIGHT, THE INSTRUMENT VACUUM SYSTEM FAILED. THE AIRCRAFT RETURNED TO MAINTENANCE AND AN INSPECTION OF THE SYSTEM REVEALED THAT THE ROTOR SHAFT HAD SHEARED. PROBABLE CAUSE MAY BE THE ENGINE MOUNTS USED ARE TOO SOFT AND ALLOW THE ENGINE TO VIBRATE TOO SDR 2003FA0000753Pump · failedDURING GROUND RUN, ENGINE DRIVEN DRY AIR PUMP FAILED TO PUT OUT PROPER PRESSURE AT IDLE RPM. RAN AIRCRAFT UP AND AIR PRESSURE STILL LOW AT HIGHER RPM. PROBABLE CAUSE IS HEAT AND VANES WEARING ON THIS DRY AIR PUMP.SDR 2003FA0000752Pump · wornDURING GROUND RUN, ENGINE DRIVEN DRY AIR PUMP FAILED TO PUT OUT PROPER PRESSURE AT IDLE RPM. RAN AIRCRAFT UP AND AIR PRESSURE STILL LOW AT HIGHER RPM.SDR CA030610006Regulator · failed(CAN) PNEUMATIC REGULATOR FAILURE IN CRUISE FLIGHT OCCURRED. PILOTS HAD TWO BLEED AIR FAIL LIGHTS, LEFT AND RIGHT, AND ALSO NOTED LOSS OF SUCTION AND PNEUMATIC PRESSURES CONFORMING LIGHT INDICATION. PILOTS RETURNED TO BASE. UPON INSPECTION THE REGULATOR FOUND SDR P5CA0300884Clamp · looseBOTH A&B NR 2 NACELLE TEMP SPIKING RETARDED THROTTLE NACELLE INDICATIONS NORMAL. ON LEAK CK FOUND FAILED DUCT CLAMP BETWEEN HEAT EXCHANGER & ENG DUCT. INSTALLED NEW CLAMP AND ON LEAK CHECK NIL LEAKS NOTED. THREADS STRIPPED ON HOLDING BOLT FOR CLAMP.SDR SIMA200314703Clamp · looseCLE - FLT 4383 - DURING APPROACH, THE CREW RECEIVED A BLEED ONE LEAK WARNIGN IN ICING CONDITIONS. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT WAS LANDED SAFELY IN CLE WITH NO FURTHER INCIDENTS REPORTED. MAINTENANCE INSPECTED ALL BLEED LINES AND RESECURED LOOSSDR 2003F00383Clamp · looseON CLIMB-OUT FROM MIA, PASSING THROUGH F/ 29 LOWER AFT BODY OVERHEAT LIGHT CAME ON. FOLLOWED AOM AND ISOLATION PROCEDURES. RETURNED TO MIA FOR MAINTENANCE ACTION. T/S PER MM 26-14-0. FOUND LOOSE CLAMP IN AFT CARGO COMPARTMENT SIDEWALL FORWARD CORNER. SECUSDR 2003F00490Precooler · delaminatedAT C-CHECK, FOUND NR 1 ENGINE INTAKE PRECOOLER, ON BOTH SIDES OF THRUST REVERSER C-DUCT DELAMINATED. REPAIRED PRECOOLER IAW SRM 54-02-00. (M)SDR MALA030266Hose · leakingDURING CLIMBOUT ON FLIGHT NR 3105, RIGHT BLEED AIR LEAK LIGHT ON THE OVERHEAT A/C PANEL ILLUMINATED. QRH- LIGHT EXTINGUISHED AFTER BLEEDS WERE CLOSED. MAINTENANCE TRANSFERRED TO 409 NR 181703. REPLACED RT SIDE BLEED AIR FUSELAGE HOSE P/N 9303688-100 IAW AMMSDR SWAA031036Duct · looseDUAL AIR TURNBACK, NR 2 ENG OVERHEAT LIGHT ILLUMINATED WITH THROTTLE LEVER ADVANCEMENT. FOUND NR 2 ENG 9TH STG PNEUMATIC BLEED AIR DUCT MANIFOLD LOOSE. TIGHTENED DUCT MANIFOLD BOLTS PER MM.SDR 2003FA0000496Pump · wornDURING GROUND RUN UP OUTPUT OF ENGINE DRIVEN DRY AIR PUMP FAILED TO PUT OUT PROPER PRESSURE AT IDLE RPM. RAN AIRCRAFT UP AND AIR PRESSURE STILL LOW AT HIGHER RPM. TESTED SYSTEM AND FOUND ENGINE DRIVEN AIR PUMP NO WORKING PROPERLY. BELIEVE DRY AIR PUMP VANESSDR 2003FA0000495Pump · wornDURING GROUND RUN UP OUTPUT OF ENGINE DRIVEN DRY AIR PUMP FAILED TO PUT OUT PROPER PRESSURE AT IDLE RPM. RAN AIRCRAFT UP AND AIR PRESSURE STILL LOW AT HIGHT RPM. TESTED SYSTEM AND FOUND ENGINE DRIVEN AIR PUMP NO WORKING PROPERLY. BELIEVE DRY AIR PUMP VANES SDR 2003FA0000494Pump · wornDURING GROUND RUN UP OUTPUT OF ENGINE DRIVEN DRY AIR PUMP FAILED TO PUT OUT PROPER PRESSURE AT IDLE RPM. RAN AIRCRAFT UP AND AIR PRESSURE STILL LOW AT HIGHTER RPM TESTED SYSTEM AND FOUND ENGINE DRIVEN AIR PUMP NOT WORKING PROPERLY. BELIEVE DRY AIR PUMP VANESSDR 2003FA0000493Pump · wornDURING GROUND RUN UP OUTPUT OF ENGINE DRIVEN DRY AIR PUMP FAILED TO PUT OUT PROPER PRESSURE AT IDLE RPM. RAN AIRCRAFT UP AND AIR PRESSURE STILL LOW AT HIGHER RPM. TESTED SYSTEM AND FOUND ENGINE DRIVEN AIR PUMP NOT WORKING PROPERLY. BELIEVE DRY AIR PUMP VANESDR 2003FA0000491Pump · brokenDURING FLIGHT AIRCREW REPORTED NO AIR PRESSURE. MAINTENANCE INVESTIGATED AND FOUND DRIVE SHAFT ON AIR PUMP HAD SHEARED. PROBABLE CAUSE IS VANES HAD SHEAR AND JAMMED SHAFT CAUSE IT TO SHEAR. NO RECOMMENDATIONS.SDR USAASB03060Control Valve · failedAT FL330, NR 2 ENGINE BLEED TRIPPED. LT PACK WOULD NOT HOLD CABIN AT FL330. CREW INITIATED RAPID DESCENT TO FL180 WHERE CABIN PRESSURE STABILIZED. NR 2 ENGINE BLEED RESET WHILE PASSING THROUGH FL250. FLIGHT CONTINUED AND LANDED WITHOUT FURTHER INCIDENT AT SDR DL733030417Heat Exchanger · crackedRIGHT WING BODY OVERHEAT LIGHT CAME ON DURING CLIMB RAN PROCEDURE BUT LEFT PACK WOULD NOT HOLD CABIN ALTITUDE CABIN UNDER CONTROL AT 18000 MAX CABIN ALT 9500. FOUND FIBERGLASS PLENUM AT HEAT EXCHANGER BLOWN OUT ON LOWER SEAM ALSO FOUND BOTH HEAT EXCHANGERS CSDR 03FDEA00674Hose · leakingAPPROX 5 MIN AFTER TAKEOFF PASSING THROUGH 1000 FT, ENG. 3 STRUT LT ILLUMINATED. LT EXTINGUISHED ON ITS OWN BEFORE ANY QRH ITEMS WERE ACCOMPLISHED. FOLLOWED QRH TESTED SYSTEM-GOOD AND MONITORED. PARAMETERS: A/C WEIGHT 180.0 TAT +12 EPR 1.90,1.95,1.90 NSDR USAASA03037Controller · malfunctionedEN ROUTE PIT-DEN, WHILE IN CRUISE FLIGHT, AT FL350, ECAM MESSAGE 'L WING LEAK' CAME ON, FOLLOWED BY A LOS OF CABIN PRESSURE. A RAPID DESCENT WAS MADE. THE FLIGHT DIVERTED TO ORD AND LANDED WITHOUT FURTHER INCIDENT. AIRCRAFT WAS FERRIED TO PIT FOR MAINTENANCSDR 03FDEA00671Tube · crackedNR 1 ENGINE PRECOOLER CRACKED AT COOLING TUBE INSTALLED PRECOOLER IAW W/C 64S0202 WO 22877 AT MAE.SDR AUS20030453Valve · faulty(AUS) STRUT OVERHEAT WARNING. HIGH STAGE VALVES AND PYLON VALVES REPLACED. LIMITED INFORMATION PROVIDED.SDR P5CA0300873Duct · leakingPILOT REPORTED BY PHONE PATCH THAT LT WING HAD A BLEED AIR LEAK. FOUND BLOWN DUCTS ON INSPECTION. REPLACED DUCTS AND REPAIRED WING TO BODY FAIRING PNL. (191KL)SDR 2003F00253Duct · leakingON TAKEOFF FROM CAE, AFTER GEAR RETRACTION NR 1 ENGINE STRUT OVERHEAT LIGHT CAME ON. ACCOMPLISHED ABNORMAL CHECKLIST PROCEDURES AND ENGINE SHUTDOWN PROCEDURES. DECLARED AN EMERGENCY WITH ATC AND AIRCRAFT CLEARED TO SAV FOR LANDING. LANDED AT SAV WITHOUT INCSDR AWXA200300359Shutoff Valve · inoperativeMCI - ABORTED TAKEOFF - FLT 702 - PREPARING FOR TAKEOFF AT MCI EN ROUTE FOR PHX LT BLEED PRESSURE INDICATED ZERO, TAXIED OFF RUNWAY AND RETURNED TO GATE. MAINTENANCE ISSUED MEL 36-5, COND 2, NR 1 ENG BLEED AIR SHUTOFF VALVE INOP. WHEN AIRCRAFT RETURNED TO PHSDR RAIA00304104Seal · deterioratedMLI- ENGINE NR 2 BLEED LEAK WARNING. MAINTENANCE REMOVED AND REPLACED GAMA DUCT O-RING, OPS CHECK OK.SDR COMA0370010Gasket · misinstalledFLIGHT 5814 LT BLEED AIR DUCT WARNING. REPLACED IMPROPERLY INSTALLED GASKET ON EXTERNAL AIR CONNECTOR.SDR MEX2003123Clamp · looseDURING TRANSIT, HIGH TEMPERATURE LIGHT OF TAIL COMPARTMENT COME ON WITH LEFT AIR CONDITIONING SYSTEM ON. LEFT AIR CONDITIONING SYSTEM WAS DEFERRED IAW MEL, CATEGORY C. AT BJX, PNEUMATIC LEAK WAS FOUND DUE TO LOSE CLAMP. CLAMP WAS REPOSITIONED AND TORQUED IASDR AUS20030403Clamp · corroded(AUS) NR 1 ENGINE SHUT DOWN FOLLOWING LT WING OVERHEAT WARNING.INVESTIGATION FOUND THE CLAMP ATTACHED TO THE PNEUMATIC FLOWCONTROL VALVE DOWNSTREAM FROM THE NO1 ENGINE BLEED PORT CORRODEDAND RUPTURED CAUSING EXCESSIVE AIR LEAKS.SDR CHQU4603Clamp · leakingLAV SMOKE WARNING (AURAL, VISUAL, EICAS) ON CLIMB OUT OF IND. RETURNED TO IND. EMERGENCY DECLARED AND MADE UNEVENTFUL LANDING. FIRE DEPT MET WITH AIRCRAFT. NO EVIDENCE OF SMOKE. UPON INSPECTION FOUND 2 CLAMPS LEAKING IN PYLON BY PRECOOLER. REMOVED AND RESDR CHQA000248Thermostat · out of adjustBLEED 1 OVER TEMP WARNING DURING CLIMBOUT OF IND. WE HAD JUST EXITED ICING CONDITIONS. FOLLOWED QRH AND WARNING WENT AWAY. TURNED BLEED BACK ON AND WARNING CAME BACK ON. DECLARED INFLIGHT EMERGENCY AND MADE UNEVENTFUL LANDING AT IND. PERFORMED ADJUSTMENT ASDR CHQA000247Clamp · leakingLAV SMOKE WARNING (AURAL, VISUAL, EICAS) ON CLIMB OUT. ALSO HAD NR 1 BLEED LEAK WARNING. EMERGENCY WAS DECLARED AND LANDED WITHOUT INCIDENT. FIRE DEPT MET WITH AIRCRAFT. NO SMOKE WAS NOTED. UPON INVESTIGATION, FOUND 2 CLAMPS LEAKING IN NR 1 PYLON BY PRECOSDR GLBA2003043Tube · disconnectedLEFT BLEED AIR FAIL ANNUC ILLUM. RECONNECTED EVA TUBING ON LEFT WING.SDR UIEA200300015Clamp · looseNR 1 ENGINE FIRE WARNING LIGHT ILLUMINATED & FIRE BELL ACTIVATED DURING CLIMB THROUGH 3000 FT. NR 1 ENGINE NACELLE TEMP INDICATES 'F' FOR BOTH 'A' AND 'B' LOOPS. ENG FIRE CHECKLIST ACCOMPLISHED. 80,000 KGS OF FUEL DUMPED. AFTER PULLING FIRE HANDLE LIGHT WSDR 2003FA0000342Shaft · damagedDURING FLIGHT AIR PRESSURE INDICATED ZERO OUTPUT. MAINTENANCE TECH FOUND BROKEN SHAFT ON DRY AIR PUMP. PROBABLE CAUSE: VIBRATION FROM ENGINE. C/A: MFG TO INVESTIGATE PUTTING STIFFER LORD MOUNTS ON ENGINE FRAME TO REDUCE ENGINE VIBRATION TO OTHER COMPONENTS
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