JASC 7500
Service difficulty reports · 1,369
Reports filed under 7500 · Engine Bleed Air 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 = '7500' 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 = '7500' 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 RAIA201803270001Clamp · looseNR 1 BLEED LEAK DURING FLIGHT. BLEED LEAK CHECKED. FOUND MULTIPLE LEAKS IN PYLON. LOOSENED AND TIGHTENED ALL CLAMPS. LEAK TESTED GOOD.SDR SOKF20180326003Actuator · damagedDURING TAKE OFF, THE TAKE OFF WAS REJECTED DUE TO ECAM WARNING MESSAGE NR 2 ENGINE COMPRESSOR VANE. PERFORMED TSM 75-30-00-810-853-A, REMOVED AND REPLACED THE VSV ACTUATOR IAW AMM 75-32-41. PERFORMED IDLE LEAK CHECK AMM 71-06-00-710-012-A IDLE LEAK CHECK OK SDR 2018F00031Clamp · brokenAFTER TAKEOFF, LEFT ENGINE FIRE AND OVERHEAT WARNING ILLUMINATED ON THE ECAM, INSPECTED AND FOUND A BROKEN CLAMP ON THE ENGINE BLEED DUCT, CLOSE TO OVER PRESSURE VALVE.SDR VNAA2018030111101Warning Message · false activationTHE CREW RECEIVED A BLEED DUCT WARNING MESSAGE DURING FLIGHT AND DIVERTED AND DECLARED AN EMERGENCY. MAINTENANCE PERFORMED OPS TEST OF BLEED-AIR DETECTION AND WARNING SYSTEM NO DEFECTS NOTED. PERFORMED LEAK TEST OF BLEED-AIR DISTRIBUTION NO DEFECTS NOTED.SDR E07A201912020002Precooler · crackedCRACKED LH ENGINE PRECOOLER INLET DIVERTER WELDS FOUND DURING INSPECTION. REPLACED WITH OVERHAULED UNIT.SDR E07A201912020001Precooler · crackedCRACKED RH ENGINE PRECOOLER INLET DIVERTER WELDS FOUND DURING INSPECTION. REPLACED WITH OVERHAULED UNIT.SDR DXTA201802160598Duct · blownALL RIGHT SIDE COLD MESSAGES ILLUMINATED. CHECKLIST ACCOMPLISHED. MESSAGES EXTINGUISHED AFTER CROSS FLOW SELECTED. LATER, ENGINE CONTROL FAULT LT AND WINDSHIELD HEAT INOPERATIVE ILLUMINATED SIMULTANEOUSLY. BOTH CHECKLISTS WERE ACCOMPLISHED. WARNINGS STASDR R61A201801140056Module · failedBLEED 2 LEAK. DECLARED EMERGENCY, RETURNED TO FIELD, LANDED WITHOUT INCIDENT. SWAPPED SPDA 2 MODULES SLOTS 18 AND 25 FOR T/S. CLEARED NVM. BLEED SYSTEM OPS CHECK GOOD.SDR RAIA201712300001Seal · leakingNR 2 BLEED LEAK IN FLIGHT. PERFORMED A NR 2 BLEED LEAK INSPECTION, FOUND A SUBSTANTIAL LEAK ON JUNCTION NR 28. REMOVED AND REPLACED THE BLEED SEALS ON THE NR 28, NO LEAKS FOUND. OPS CHECKED GOOD. THE FOLLOWING WAS CLEARED IN CONJUNCTION WITH PREVIOUS DISCRSDR SIMA20171212001Shutoff Valve · failedL ENG BLEED CAUTION-C/A-REMOVED AND REPLACED LH PRSOV IAW CRJ AMM TASK 36-12-01. OPS CHECK GOODSDR ASAA2017103122373Link · wornWHILE ACCOMPLISHING AN ENGINE INLET INSPECTION, NR 1 ENGINE, FOUND 1ST AND 2ND DUCT ATTACH LINKS WORN ABOVE THE HIGH STAGE VALVE. ACFT GROUNDED. REPLACED INTERSECTION MANIFOLD DUCT ASSY AND BOTH ATTACH LINKS, IAW AMM 36-11-01. LEAK CHECKED GOOD.SDR CALA2017091103127Valve · faultyNR 2 ENGINE EGT OVER RED LINE. EMERGENCY DECLARED. ACCOMPLISHED BOROSCOPE INSPECTION OF THE NR 2 ENGINE HPT AND LPT STAGES 1 THRU 3 BLADES, NO DEFECTS NOTED IAW AMM 72-00-00-200-807-F00, AND 72-00-00-200-808-F00. REMOVED AND CLEANED ALL T49.5 THERMOCOUPLESSDR E07A2017083100001Intercooler · blew outDURING CRUISE, CREW NOTICED HIGH ITT ON THE LT ENGINE AND THEN RECEIVED CAS WARNING OF DUCT OVERTEMP. DIVERTED AND LANDED WITHOUT INCIDENT. FOUND THE LT BLEED AIR DUCT INTERCOOLER HAD A HOLE IN IT.SDR AALA201708239048Solenoid Valve · failedDESCENDING AT 11,000 FEET, THE ENGINE SPOOLED FROM FLIGHT IDLE, AIRCRAFT YAWED, AND THE NR 2 ENGINE SHUTDOWN. CAPTAIN AND FIRST OFFICER COMPLETED ECAM. DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE REPORTED ENGINE NR 2 FAILED BLEED VALVE TESSDR AALA201708239047Solenoid Valve · failedDESCENDING AT 11,000 FEET, THE ENGINE SPOOLED FROM FLIGHT IDLE, AIRCRAFT YAWED, AND THE NR 2 ENGINE SHUT DOWN. CAPTAIN AND FIRST OFFICER COMPLETED ECAM. DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE REPORTED THE NR 2 ENGINE FAILED A BLEEDSDR AALA201708239046Solenoid Valve · failedDESCENDING AT 11,000 FEET, ENGINE SPOOLED FROM FLIGHT IDLE, AIRCRAFT YAWED, AND THE NR 2 ENGINE SHUTDOWN. CAPTAIN AND FIRST OFFICER COMPLETED ECAM. DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE REPORTED THE NR 2 ENGINE FAILED A BLEED VALVSDR AALA201707219003Hose · chafedDURING TAKE OFF AT MAX POWER, ENGINE POWER WAS EQUAL. AT 200 FT AGL RT MOTOR ROLLED BACK TO 60% N1. ANY CLIMB MODE CREATED A 30% N1 SPLIT. VISUAL APPROACH AND VISUAL DOWNWIND WITH AUTOTHROTTLE OFF, COULD KEEP THE THRUST SYMMETRICAL. IMMEDIATELY AFTER TAKEOFSDR YRJR201707180001Clamp · brokenAFTER TAKE OFF, A FIRE WARNING ON THE NR 1 ENGINE ILLUMINATED. AIRCRAFT RETURNED TO AIRPORT. EXAMINATION REVEALED TWO HIGH PRESSURE BLEED AIR CLAMPS HAD FAILED. THIS ALLOWED BLEED AIR TO SET OFF THE FIRE WARNING.SDR HALA2017062200162Bleed Air Sys · inoperativeNR 2 ENGINE BLEED AIR INOPERATIVE. REMOVED AND REPLACED PRSOV IAW AMM 36-11-09. REMOVED AND REPLACED FAN AIR VALVE IAW AMM 36-11-16. OPS CHECKED GOOD. OK FOR SERVICE.SDR CALA2017061601830Clamp · looseAT FL390, THE RT ENGINE OVERHEAT EICAS INDICATOR ILLUMINATED. EMERGENCY DECLARED. FOUND THE NR 2 ENGINE UPPER FIRE COMBUSTION & TURBINE CASE SENSOR MID CLAMP LOOSE IAW FIM TASK 26-11-00-815-803. SECURED THE CLAMP IAW EIPC 26-11-01 ITEM 430. WRENCH CHECKED SDR CALA2017061601829Solenoid · faultyENGINE SPEED PARAMETERS EXCEEDED FOR LEFT ENGINE DURING TAKEOFF ROLL. PERFORMED BORO INSPECTION OF THE NR 1 ENGINE IP COMPRESSOR IAW MM 72-00-00-206-147-R02, AND IP TURBINE INSPECTION IAW 72-00-00-206-173-R02. NO DEFECTS NOTED. REMOVED AND REPLACED LEFT AND RSDR UIEA2017061100995Bleed Air Sys · oscillatesLEFT BLEED PRESSURE OSCILLATES DURING CLIMB THRU 10000 FT, 15-50 PSI RANGE. STOPS AT 10000 FT BUT REMAINS LOUDER THAN RIGHT BLEED. NO BLEED SPLIT AT 410. PACK OPS NORMAL. NO EICAS STATUS. COMPLIED WITH FIM 36-10-01, FAULT TREE 803. INSPECTED BOX AND FOUNDSDR HDNA2017030515Line · meltedPLASTIC TUBING "SENSE" LINE FOR BLEED AIR INDICATING ANNUNCIATION MELTED DUE TO IMPROPER ROUTING CAUSING THE BLEED AIR FAIL CAUTION TO ILLUMINATE.SDR 2017FA0000039Duct · brokenTHE AIRCRAFT DEPARTED. APPROXIMATELY 2-3 MINUTES AFTER TAKEOFF THE ENGINE NR 2 FIRE LIGHT ILLUMINATED. THE CREW IMPLEMENTED THE PROPER PHASE ONE PROCEDURE. CLEARED FOR THE VISUAL APPROACH, AND TO LAND ON RUNWAY 6. AFTER LANDING THEY CLEARED THE RUNWAY AND SDR CALA2016122701175Sensor · faultyLT ENGINE BLEED OVERHEAT, FOLLOWED BY LT PACK OFF AND LT BLEED OFF, FOLLOWED CHECK LIST. EMERGENCY DECLARED. REPLACED THE NR 1 ENGINE FAN AIR TEMP SENSOR IAW AMM 36-11-17. RAN HIGH POWER RUN AND PERFORMED AMM 36-00-3 NO LEAKS NOTED NO FAULTS NOTED IN THE SDR J7SA20161215001Seal · failedAIR TURNBACK DUE TO "R BLEED LEAK" CAS MESSAGE. RAN EMERGENCY CHECKLIST AND TURNED BACK TO AIRFIELD. LANDED WITHOUT INCIDENT. REPLACED BOTH SEALS AND BOTH V BAND CLAMPS ON RT INTERMEDIATE VALVE. LEAK AND OPS CHECKED GOOD.SDR AALA201612069016Actuator · failedDURING TAKEOFF ROLL WITH FLEX THRUST SET AT APROXIMATELY 60--70 KNOTS, A ECAM ENG 1 COMPRESSOR VANE FAULT OCCURRED AND THE TAKEOFF WAS ABORTED. MAINTENANCE REPLACED THE NR 1 ENGINE VSV ACTUATOR AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECKED IAW 26T400750SDR SIMA20161103001Clamp · unsecureDURING CLIMB, CREW RECEIVED NR 1ENGINE BLEED LEAK MESSAGE. CREW COMPLIED WITH AOM VOL 1 PROCEDURES, DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE WITHOUT INCIDENT. PERFORMED LEAK CHECK BLEED 1 SYSTEM JOINT NO LEAKS FOUND. DURING INSPECTION FOUND BLEED 1 SDR O2GA2016102650301Seal · leakingAFTER TAKEOFF THE LEFT ENGINE ITT INCREASED TO 723 DEGREES. TAPE TURNED RED. AFTER SELECTING CLIMB POWER ITT DECREASED BELOW 720 DEGREES. ENGINE ITT EXCEEDANCE WAS WITHIN ENGINE PERFORMANCE LIMITS PER THE EMM. DURING ENGINE RUNS SEVERAL BLEED AIR MANIFOLD COSDR W6JA20160802008Control Unit · faultedTHE CREW NOTED A RED LEFT "BLEED AIR LEAK" EICAS MESSAGE FOR AN ENGINE BLEED AIR LEAK. MESSAGE ILLUMINATED AT FLIGHT 350. CREW FOLLOWED THE QRH PROCEDURES TO SHUT THE ENGINE DOWN DUE TO THE "BLEED AIR LEAK" MESSAGE WOULD NOT EXTINGUISH. CREW DID DECLARE AN EMSDR AALA201607119001Actuator · warning messageDURING TAKEOFF, FLIGHT CREW REPORTED THAT AN ECAM MESSAGE FOR A NR 2 ENGINE COMPRESSOR VANE FAULT OCCURRED AND THE TAKEOFF WAS ABORTED AROUND 80 KNOTS.THE AIRCRAFT RETURNED TO THE GATE WITH NO FURTHER INCIDENT. AIRCRAFT WAS GROUNDED. MAINTENANCE ACCOMPLISHED SDR UHLA201606140326Clamp · looseBLEED 1 LEAK AFTER TAKEOFF. AFTER RUNNING QRH, MESSAGE WENT AWAY. ON AFTER LANDING WHILE USING THE APU BLEED, BLEED 1 LEAK MESSAGE RETURNED. DECLARED EMERGENCY, RETURNED TO FIELD, LANDED WITHOUT INCIDENT. FOUND LOOSE CLAMPS ON TEMP CONTROL UCU. REPAIR AS SDR E07A201606010001Valve · stickingBLEED 2 DUCT OVERTEMP. VALVE STICKS.SDR 9SUA2016032301Clamp · detachedON INITIAL DESCENT, THE FLIGHT CREW NOTICED A VIBRATION ON THE AIRPLANE WITH NO INDICATION PROBLEMS. THEY CONTINUED TO DESCEND AND THROUGH FL200, HAD A RT ENGINE FIRE ANNUNCIATION. THEY REDUCED POWER, AND THE ANNUNCIATOR EXTINGUISHED. THEY PROCEEDED WITH THE SDR RAIA201602020004Pressure Switch · inoperativeBLEED 2 CLOSED EICAS MSG. R & R NR 1 HIGH STAGE PRESSURE SWITCH. OPS CHECK GOOD.SDR 29GA2016012700001Clamp · bentLEFT ENGINE FAILURE AND AUTO COARSENED WHILE CLIMBING THROUGH 400 FT ON TAKEOFF, LEFT ENGINE OVERTEMP LIGHT ILLUMINATED. REPLACED HP BLEED LINE CLAMP IAW AMM 36-11-00 PERFORMED BORESCOPE INSPECTION OF HOT SECTION AND POWER TURBINE MODULE IAW MM 72-00-00 AS RESDR 2016F00045Tube · chafedAFTER TAKEOFF AT 3000 FT AGL, LT BLEED FAIL, LIGHT ILLUMINATED. LT BLEED SWITCH WAS SELECTED "OFF" AND RTB WITH OUT INCIDENT. OVERHEAT DETECTION TUBING UNDER CO-PILOTS FLOOR WAS FOUND CHAFED AND PREVIOUSLY REPAIRED, TUBING WAS REPLACED WITH NEW. LT FIREWALLSDR TIMA2016F00020Bleed Air Sys · smokeENROUTE, THE LT BLEED FAIL WARNING ILLUMINATED. WHILE FINISHING THE CHECKLIST FOR THE FAILURE SMOKE ENTERED THE CABIN OF THE AIRCRAFT. ELECTED TO CONDUCT A LANDING. UPON LANDING, THE SMOKE DISSIPATED FROM THE CABIN OF THE AIRCRAFT.SDR HALA2015112000239Transducer · malfunctionedNR 2 ENGINE HP VALVE NOT OPENED IAW TSM 36-00-00-820-961-A, AMM 36-11-15-400-804-A. R & R NR 2 ENGINE BLEED PRESSURE TRANSDUCER. OPS CHECK GOOD, OPS CHECK GOOD. NO FAULTS NOTED.SDR ASAA2015110613675Bleed Air Sys · malfunctionedON CLIMB NOTICED BLEED DUCT SPLIT PASSING FL280, L18, R41, N1, 100.5 LEVEL FL370, L20, R40, N1 89.5. ACFT GROUNDED. ON DEFERRAL.SDR CA151102007Bleed Air Sys · inoperative(CAN) THE FLIGHT CREW REPORTED A FUME EVENT DURING THE FLIGHT. MAINTENANCE IS INVESTIGATING. LT BLEED SYS INOPERATIVE. ENGINEERING DEFERAL ISSUED TO COVER INTERNAL OIL LEAK. OIL CONSUMPTION IS BEING MONITORED DAILY. STILL NO FIX, AS OF NOV 19 2015.SDR CA151015004Switch · malfunctioned(CAN) LOST PRESSURIZATION AT ALTITUDE. CREW DECENDED AND LANDED WITHOUT INCIDENT. THEY CYCLED THE BLEED AIR AIR SOURCE SWITCH AND PRESSURIZATION CAME BACK. EICAS MESSAGES AIR SOURCE OFF, WHITE AND AIR CONDITIONING FAULT, CYAN.SDR CA150909001Venturi · cracked(CAN) DURING ENGINE OIL SERVICING, MAINTENANCE NOTICE THAT THE VENTURI ADAPTER FOR THE P3 BLEED AIR ON THE RT ENGINE WAS SPLIT OPEN. THE AFT INSULATION BLANKET WAS ALSO DAMAGED BY HEAT.SDR AALA20150803010Tube · brokenAIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT OVERWEIGHT. DURING CLIMB, THE TAIL COMPARTMENT TEMP HIGH LIGHT ILLUMINATED. R & R TUBE ASSEMBLY FROM TURBINE NOZZLE VLV TO EJECTOR INLET, BROKEN OFF, IAW AMM 21-20-06. R & R LT & RT TAIL COMPARTMENT HISDR CA150520002Duct · ruptured(CAN) DURING WALK AROUND, MAINTENANCE HEARD AN UNUSUAL NOISE COMING FROM NR NR 1 ENGINE. SOUND OF BLEED LEAK, RUSHING AIR. AFTER OPENING THE THRUST REVERSER COWLS, THE TECH FOUND A RUPTURED DUCT ON THE THRUST REVERSER PRESSURE REGULATING AND SHUTOFF VALVE, PSDR 29GA2015042100001Clamp · looseRIGHT BLEED AIR LEAK LIGHT ILLUMINATED, EMERGENCY DECLARED. LANDED, 1 ENGINE INOPERATIVE. FOUND ORANGE BLEED DUCT ELBOW RT SIDE ABOVE WING ROOT CLAMP LOOSE, RESECURED AS NECESSARY AND PERFORMED ENGINE RUN, OPS CHECK WAS GOOD.SDR DXTA2015041606006Seal · failedCLIMBING THROUGH 9000 FEET BOTH MWS SYS LIGHTS STARTED FLASHING FOLLOWED BY REAR BAY OVERHEAT LIGHT. REDUCED POWER & CLIMBED WHICH EXTINGUISHED REAR BAY OVERHEAT LIGHT. BOTH MAIN AIR VALVES WERE OPEN, ENG ANTI-ICE WAS OFF. NO SMOKE IN CABIN. DECLARED EMER SDR JGVR20150407001Gasket · blownDURING ENGINE REMOVAL FOR MPI, FOUND THE NR 1 ENGINE HP BLEED AIR DUCT ASSEMBLY 90 DEGREE CONNECTION, PN SBJ10531-505, WITH A BLOWN GASKET, PN BA7684. SB 150-71-154 "POWERPLANT-ENGINE HIGH PRESSURE (HP) AIR DUCT ASSEMBLY SBJ10532-507. MISMATCH TO ADDRESS THISDR 2015FA0000113Pressure Valve · defective(XC-UJM) ENGINE HIGH PRESSURE SHUTOFF VALVE, HPSOV, WILL NOT PASS FUNCTIONAL TEST AS OUTLINED IN AMM 36-11-07.SDR 2015FA0000111Pressure Valve · defective( XC-UJM) ENGINE HIGH PRESSURE SHUTOFF VALVE, HPSOV, WILL NOT PASS FUNCTIONAL TEST AS OUTLINED IN AMM 36-11-07.
Back to JASC 7500