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 P5CA0401133Pressure Valve · inoperativeDURING ENGINE START NR 3 ENGINE ROTATION WAS SLOW, LIGHT OFF NORMAL BUT WOULD NOT ACCELERATE PAST 30 PERCENT. REPLACED NR 3 ENGINE PRESSURE RELIEF VALVE, OPERATIONAL CHECK GOOD IAW MM 36-11-00.SDR MAC4801Selector Valve · leakingDURING TAXI, PNEUMATIC PRESSURE WENT TO 200 PSI RESULTING IN LOSS OF BRAKES AND STEERING. THE LANDING GEAR SELECTOR VALVE WAS DETERMINED TO HAVE CAUSED THE LOSS OF PNEUMATIC PRESSURE. THE VALVE WAS REPLACED AND THE A/C RETURNED TO SERVICE.SDR UIEA200400141Relief Valve · leakingRHI/MXP - NR 1 ENGINE WOULD NOT ATTAIN REQUIRED THRUST FOR T/OFF. WOULD ONLY ATTAIN 108.5 AGAINST THE STOP. ALL OTHER INDICATIONS NORMAL. NR 3 ENG WOULD NT ATTAIN REQUIRED THRUST FOR T/OFF. WOULD ONLY ATTAIN 110.0 AGAINST THE STOP. ALL OTHER INDICATIONS NSDR 04206500Pressure Valve · defectivePLANE RETURNED TO FIELD AFTER RECEIVING BLEED SOV CAS MESSAGE ON TAKEOFF, FOLLOWED BY LAV SMOKE CAS AT 1000 FT. BOTH INDICATIONS EXTINGUISHED WHILE RETURNING FOR LANDING. NO SMOKE WAS DETECTED. PASSENGERS DEPLANED AT THE GATE. LEFT MDPRSOV WAS REMOVED AND SDR LR7A2009040800001Duct · crackedDURING TAKE OFF, NR 1 ENGINE SHUT DOWN DUE TO NACELLE OVERHEAT INDICATION. REPLACED NR 1 ENGINE AFT UPPER "Y" DUCT IAW SMP581 CH 36-10 PG 205. LOG PAGE 21814 ITEM 1.SDR PCS2005F00000Ball Joint · looseDURING CLIMBOUT NR 3 ENGINE FIRE WARNING BELL AND LIGHT WHEN OFF. DISCHARGED LT FIRE EXTINGUISHER IAW EMERGENCY PROCEDURES AND ABNORMAL CHECK LIST. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED LT FIRE EXTINGUISHER IAW MM. IN ASDR COMA0460418Element · chafedFLIGHT 5215 RIGHT 14TH STAGE BLEED AIR DUCT WARNING DURING T/O. REPLACED THE 14TH STAGE BLEED LEAK SENSING ELEMENTS.SDR QXEA200400526Switch · failedPDX - FLIGHT 2318 - AFTER STARTING DESCENT, THE CREW RAN THE EMERGENCY CHECKLIST AFTER THE NR 2 BLEED HOT CAUTION LIGHT ILLUMINATED. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE NUMBER 2 NACELLE DUCT LEAK OVERTEMP SWITCH. OPERATIONAL CHECKS WERE GOOD SDR DLM88040649Oil System · leakingFIRST FLIGHT ATB SMOKE IN CABIN WITH LAV DETECTORS SOUNDING FLIGHT CXLD. MTC WORKING OPN'S 5088 AND 5089 SMOKE T/S AND DUCT BURN OUT.SDR UIEA200400122Valve · erraticNR 4 ENGINE SHUTDOWN DURING DECENT: NR 4 ENGINE SHUTDOWN RUMBLE AND EGT RISING. AFTER RISING RELIGHT IS STARTED SURGING. SHUTDOWN AGAIN. NR 4 HIGH STAGE VALVE DEACTIVATED, CLOSE AND PERFORMED ENGINE RUN UP, CHECK NORMAL, ENGINE RUN BY FLT CREW AND NR 4 ENGSDR USAABB04066Heat Exchanger · contaminatedCLT - FLT 1121 - CREW REPORTED AN OIL ODOR AND HAZE IN THE CABIN WHICH SET OFF THE 2L LAVATORY SMOKE DETECTOR. THE APU WAS INSPECTED AND NO LEAKS FOUND. THE PACKS WERE OPERATED AT HIGH TEMPERATURE FOR SEVERAL HOURS WITH NO ODOR NOTED. THE COMPLAINT WAS REPESDR MALA040495Pipe · damagedNR 4 ENG AIR BLEED SYSTEM, CLIMBING OUT OF MEM AROUND 14,000 FT, THE NR 4 PYLON OVERHEAT LIGHT ILLUMINATED. TURNED NR 4 BLEED AIR OFF AS PER QRH & THE LIGHT WENT OUT. RETURNED TO MEM LANDING WT 79,000 LBS. MAINTENANCE REPLACED PIPE, TEMP SENSOR AND GASKET.SDR P5CA0401117Valve · malfunctionedDMI NR 32768, NR 1 PYLON VALVE INOPERATIVE, ALSO HIGH PRESSURE BLEED VALVE ON ENGINE NR 1. REMOVAL AND REPLACEMENT. REMOVED AND REPLACED PYLON VALVE DUE TO NOT CLOSING COMPLETELY , OPS CHECK AND LEAK CHECKS GOOD IAW MM 36-11-04.SDR P5CA0401116Valve · malfunctionedON ENGINE START-UP NR 1 ENGINE PYLON VALVE WILL NOT OPEN DURING MANUAL ENGINE START. REPOSITIONED PYLON VALVE IN ORDER TO ACHIEVE ENGINE START, OPS CHECK GOOD IAW MM 36-11-04.SDR ASOA04481Control Unit · intermittentDURING DESCENT, THE CREW RECEIVED A 14 TH STAGE DUCT MESSAGE. THE QRH WAS COMPLIED WITH AND THE THRUST LEVER WAS REDUCED TO IDLE AT WHICH TIME THE MESSAGE EXTINGUISHED. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED SAFELY. MAINTENANCE REMOVED AND REPLACSDR 2004F00233Duct · separatedCOUPLING SEPARATED FROM END OF APU/GROUND START APU DUCT ASSY.SDR TSAA0436053Precooler · failedCLIMBING THROUGH 15,000 FT THE BLEED TRIP OFF LIGHT FOR THE NR 2 ENGINE ILLUMINATED. PERFORMED QRH CHECKLIST, RETURNED TO KWA. OVER-WEIGHT LANDING AT 131.2 K, LOW TO MEDIUM SINK RATE. VERIFIED NR 2 ENGINE BLEED TRIP ON THE GROUND. REMOVED AND REPLACED PRE-COOSDR TSAA0436052Precooler · failedETOPS FLIGHT 352, CLIMBING THROUGH 15,000 FT THE BLEED TRIP OFF LIGHT FOR THE NR 2 ENGINE ILLUMINATED. PERFORMED QRH CHECKLIST, RETURNED. OVER-WEIGHT LANDING AT 131.2 K, LOW TO MEDIUM SINK RATE. VERIFIED NR 2 ENGINE BLEED TRIP ON THE GROUND. REMOVED AND REPLASDR P5CA0401106Valve · failedNR 3 ENGINE FIRE WARNING CAME ON DURING CLIMB, A & B LOOPS READ 7 TO 10 UNITS, THAN STABILIZED TO 4 UNITS SCALE WHEN THROTTLE MOVED TO IDLE. FOUND NR 3 ENGINE HIGH-STAGE BLEED VALVE LEAK. REMOVED AND REPLACED NR 3 ENGINE HIGH STAGE BLEED VALVE AS PER MM 36-1SDR RAIA00406023Seal · deteriorated5747 - STL - BLEED 2 LEAK WARNING MESSAGE. MAINTENANCE REMOVED AND REPLACED COUPLING SEAL.SDR RAIA00406021Seal · deteriorated5766 - OKC - LEFT BLEED LEAK INDICATION. MAINTENANCE REMOVED AND REPLACED BLEED LINE COUPLING SEAL.SDR HNAA0400059Pipe · crackedAFTER TAKEOFF F/A REPORTED STRONG BURNING ODOR IN CABIN, THIS HAPPENED RIGHT AFTER BLEED WAS SELECTED. MX ISOLATED ENG BLEED LEAK AT FRONT SPAR BLEED PIPE. REMOVED AND REPLACED BLEED PIPE UNDER PANELS 261JT, NT LEAK CHECK GOOD. GROUND RAN A/C, NO SMELL NOTESDR GTIA040581Augment Valve · damagedMCO - FLT 940 - DURING THE USE OF ENGINE ANTI-ICE ON, PASSENGER COMPLAINED OF A BAKEOLITE OR OTHER SUBSTANCE, BURNING/OVER HEAT ODOR. REMOVED AND REPLACED LEFT AUG VALVE. (M)SDR RAIA00406017O-Ring · leaking3515 - PIT- DURING TAXI NR 2 LEAD LEAK INDICATION. MAINTENANCE REMOVED AND REPLACED DUCT O-RING IN DISTRIBUTION DUCT AFT AVIONICS BAY.SDR 2004FA0000570Shutoff Valve · leakingTHIS VALVE INSTALLED PREVIOUSLY TO COMPLY WITH REQURIEMENTS OF AD 2003-11-07. FOUND DURING INSPECTION THAT VALVE WILL NOT SHUT OFF OXYGEN FLOW WHEN TURNED TO CLOSED. REPLACED VALVE WITH NEW PN 27550-3, THIS CORRECTED PROBLEM.SDR AUS20040509Valve · faulty(AUS) LT BLEED AIR VALVE FAULTY.SDR ANCF200400012Shutoff Valve · failedDURING WING AND ENGINE ANTI-ICING USE CABIN CONTROL WITH AUTO 1 SELECTED, WITH 7.0 UNITS OF DIFFERENT TO LAND, 9500 OF ALTITUDE WITH STRONG PRESSURIZATION SURGE. THIS CONDITION WAS PRESENTED AT 35.000 FT WITH CABIN 2 SELECTED INDICATIONS WERE NORMAL. WAS REMOSDR P5CA0401102Relief Valve · leakingDURING A/C CLIMBOUT AT 23,000 FT, NR 4 ENGINE NACELLE TEMPERATURE WAS INDICATING 8 UNITS. ACCOMPLISHED PROCEDURE FOR ABNORMAL NACELLE TEMPERATURE RETURNED TO NORMAL. NACELLE TEMPERATURE FLUCTUATED WITH THROTTLE MOVEMENT. REMOVED AND REPLACED PRESSURE REGULASDR P5CA0401101Line · looseDURING CLIMBOUT NR 4 ENGINE FIRE LIGHT ILLUMINATION AND FIRE BELL SOUNDED. ENGINE SHUT DOWN, BOTTLES NOT FIRED. FOUND SENSE LINE OFF PRV. SECURED LINE & CHANGED UNION PER MM 36-11-19. OPERATIONAL CHECK OK.SDR UIEA200400108Precooler · cracked(D) CHECK, DURING MAINT INSP, DAMAGE WAS FOUND ON RT SIDE OF NR 3 PYLON STRUCTURE ASSY. CRACK DAMAGE WAS AT PRE-COOLER EXHAUST CUTOUT LOWER AFT CORNER AT NAC STA 248. INNER SKIN DOUBLER WAS TRIMMED, AT GRILL ATTACHED HOLE TO REMOVE CRACK DAMAGE. INNER SKIN SDR MALA040423Isolation Valve · malfunctionedNR 2 ENGINE AIR FAULT LIGHT CAME ON AFTER TAKEOFF. AIR RETURN TO MEM. MAINTENANCE REPLACED ISOLATION / PRESSURE REDUCING VALVE FOR NR 2 ENG IAW AVRO AMM 36-11-11. OPS AND LEAK CHECK GOOD. P/N ON 2985A000-003, P/N OFF 2985A000-002, S/N ON 923048-3, S/N OFF SDR RAIA00405022Duct · looseERI - BLEED AIR LEAK INDICATION NR 1 ENGINE. MAINTENANCE RE-SECURED BLEED AIR DUCT.SDR C1HA200474004Retainer · looseNR 3 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED AT 26.0. FOLLOWED COM PROCEDURE, LIGHT WENT OUT. PERFORMED DUCT INSPECTION AND LOOP INSPECTION DID 2 HIGH POWER ENGINE RUNS. OVERHEAT NOT DUPLICATED HOWEVER AIR LEAK WAS FOUND IN 8TH STAGE DUCT. NR 3 ENG 8TH STASDR AUS20040488Valve · faulty(AUS) RT ENGINE BLEED SYSTEM PRESSURE REDUCING VALVE (PRV) SUSPECT FAULTY. LIMITED INFORMATION PROVIDED.SDR AALA20040631Warning Light · illuminatedGRU - RIGHT PACK OFF LIGHT ILLUMINATED AND RIGHT ENGINE BLEED OFF LIGHT ILLUMINATED. ACCOMPLISHED BYTE CHECK. SYSTEM GROUND CHECKED NORMAL OPERATION.SDR RAIA00405013O-Ring · deterioratedSTL - BLEED LEAK NR 1 INDICATION. MAINTENANCE REMOVED AND REPLACED NR 1 BLEED LINE SEAL UNDER CARGO BAY FLOOR.SDR AUS20040481Manifold · cracked(AUS) LT BLEED AIR SPLITTER DUCT CRACKED AND LEAKING FROM THE MATING FLANGE RADIUS.SDR MALA040404Periseal · failedL ZONE HIGH TEMP ILLUMINATED DURING CRUISE. AIR RETURN. MAINTENANCE REPLACED PERI-SEALS (PN 706-3-200), ADJACENT TO PYLON O/H SWITCH IN LEADING EDGE. OPS AND LEAK CHECK GOOD IAW AMM CHPT 36.SDR DL757040443Clamp · failedTHE FOLLOWING IRREGULARITY WAS REPORTED BY FLIGHT CREW; RT ENG HI STAGE, RT ENG BLEED OFF, RT PACK OFF EICAS MSG, RT ENG FIRE LOOP 2 STATUS MSG, RT ENG OIL PRESS MISSING FROM LOWER EICAS DISPLAY. MTC FOUND RT ENG HIGH STAGE DUCT CLAMP FAILED AT COOLER, DAMAGISDR XNOA1186Duct · looseFIRE INDICATION ON NR 2 ENG. QRH COMPLETED, FIRE BOTTLE NOT DISCHARGED. OPS CHECK FIRE DETECTION SYSTEM IAW A300 MM REF 26-12-00, NO DEFECTS NOTED, OPS CHECKS GOOD. FOUND NR 2 ENGINE RECOUP DUCT RUPTURED. REMOVED AND REPLACED BOTH SECTIONS OF DUCT IAW A300SDR AWXA200400492Transducer · inoperativeON CLIMB OUT, EN ROUTE, RECEIVED ECAM MESSAGE (AIR ENG 2 BLEED ABNORMAL PRESSURE), BLEED VALVE INDICATED CLOSED WITH (0) PSI, TURNED BACK & LANDED WITHOUT FURTHER EVENT. MAINT R & R NR 2 ENG BLEED PRESSURE REGULATOR VALVE CONTROL SOLENOID (10HA2) IAW AMM, ANDSDR FBFQA1Bellows · crackedUPON INSPECTION AND PRESSURIZATION CHECKS THE WYE PIPE BELLOWS WAS FOUND TO BE CRACKED.SDR MASA200400235Shutoff Valve · inoperativeTHE CREW ABORTED T/O DUE TO AN WING OVERHEAT MESSAGE. MX IN THE PROCESS OF TROUBLESHOOTING. MX REPLACED 14TH STAGE SOV OPS CHECKED GOODSDR KBM2004F00048Pipe · chafedENGINE P2 AIR PIPE SUPPLYING AIR TO MODULE 5 BEARING HAS DEEP CHAFE. REMOVED AND REPLACED.SDR RAIA00404016Switch · inoperativeUNABLE TO CROSS START - CROSS BLEED VALVE WOULD NOT OPEN. MAINTENANCE REMOVED AND REPLACED NR 2 BLEED PUSH BUTTON SWITCH.SDR RAIA00404015O-Ring · leakingRT BLEED LEAK MESSAGE. MAINTENANCE REMOVED AND REPLACED O-RINGS IN THE NR 2 ENGINE BLEED LINE IN CARGO COMPARTMENT.SDR UIEA200400068Valve · inoperativeAZ9051 PVG/HKG NR 3 ENG BLEED OVERHEAT LIGHT CAME ON DURING TAKEOFF. FOLLOWED CHECKLIST IAW 3.36.5, NR 3 THRUST LEVER BACK TO IDLE LIGHT WILL EXTINGUISH. BUT LIGHT WILL COME BACK ON IF PUSH THRUST LEVER FORWARD MORE THAN 70 PERCENT N1. NR 3 THRUST LEVER USEDSDR 2004FA0000421Precooler · splitPILOTS NOTICED SLIGHT TEMP RISE IN RT ENGINE, AND AN UNUSUAL VIBRATION ALL ENGINE INDICATIONS IN NORMAL RANGES POSTFLIGHT WALK AROUND NOTICED A SPLIT IN THE PRESSURIZATION (BLEED AIR) PRE-COOLER IN THE RT PYLON. PAINT DISCOLORATION WAS NOTED NO DAMAGE TO ADJASDR GAIA04069OPClamp · looseNR 1 ENGINE STRUT OVERHEAT LIGHT CAME ON JUST AFTER TAKE-OFF. CREW RETURNED AIRCRAFT TO DEPARTURE AERODROME (FWA) WHERE AN UNEVENTFUL LANDING WAS MADE. DUPLICATED PROBLEM DURING GROUND ENGINE RUN. TIGHTENED SEVERAL CLAMPS ON BLEED LINES AND (B) NUT ON SENSESDR VNAA0404017Gasket · failedFLIGHT 2292 RETURNED TO GATE WITH ANTI ICE DUCT MESSAGE, BLEED LOOP FAIL. MAINTENANCE INSPECTED AND REPLACED THE GROUND AIR CONNECTION GASKET IN ACCORDANCE WITH THE BOMBARDIER MAINTENANCE MANUAL 36-17-01-400-801-A01. OPERATIONAL CHECKS WERE PERFORMED AND THE
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