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 96ZZZX835Diaphragm · rupturedDURING THE COURSE OF A 100-HOUR INSPECTION, FOUND BLEED AIR REGULATOR TO HAVE A BLOWN DIAPHRAGM. THIS IS THE REGULATOR LOCATED IN AFT BAGGAGE AREA THAT REDUCES THE BLEED AIR FROM THE ENGINE DOWN TO 18 PSI TO INFLATE THE DOOR SEAL AND DEICE BOOTS. SUBMITTER SSDR CA960320537Engine Duct · broken(CAN)DURING CLIMB AT 4,000 FT RIGHT ENGINE FIRE WARNING ILLUMINATED WITH BELL AND BOTH LOOP LIGHTS ON. ENGINE SHUT DOWN, FIRE CEASED AFTER AGENT 1 DISCHARGED. MAINTENANCE INVESTIGATION REVEALED ENGINE TO P YLON 13TH STAGE DUCT FAILURE AT CLAMP CONNECTION POINTSDR 96ZZZX1173Tube · crackedDURING INSPECTION OF SCAVENGE AIR SYSTEM, THE AIR TUBE WAS FOUND CRACKED ABOUT 4 INCHES ABOVE THE SOLENOID. IT APPEARS TO HAVE HAD WATER FROZEN AT THAT POINT AS THE TUBE IS EXPANDED ALONG THE CRACKED AREA AND RECENT TEMPERATURES HAVE BEEN SUB-ZERO.SDR TC8A96001Pneumatic Line · looseSBGR/SBGR - FLT 2405 - NR 1 ENGINE FIRE ALARM CAME 'ON' DURING CLIMB, SHORTLY AFTER TAKEOFF. TIGHTENED PNEUMATIC LINE AT AFT REVERSER SYSTEM. CHECK OPS OK IAW MM 78-02. (X)SDR CAL960058Clamp · wornGUM - FLT 0977 - NR 2 ENGINE A-FIRE LOOP LIGHT ILLUMINATED DURING CLIMB OUT OF GUM WITH B-LOOP ON PLACARD. THE B-LOOP HAD BEEN PLACARDED PREVIOUSLY FOR BEING INTERMITTENLY INOPERABLE. LATER, BOTH LOOP LIGHTS AND FIRE LIGHT WERE ON. ENGINE POWER REDUCED AND SDR 96FDEA00116Valve · damagedBOTH LT AND RT PURGE SHUTOFF VALVES PHYSICALLY DAMAGED, ENDS BLOWN OFF. REMOVED AND REPLACED VALVES, LT-12231, RT-C64198.SDR P5CA9600168Precooler Mount · crackedFOUND NR 3 PRECOOLER LOWER AFT MOUNT CRACKED. REPAIRED AS PER MM 36-10-02.SDR P5CA9600021Duct · crackedAFTER ENGINE START, WING LEADING EDGE OVERHEAT LIGHT ILLUMINATED. FLIGHT RETURNED TO BLOCKS. FOUND LEADING EDGE PNEUMATIC DUCT INBOARD OF NR 2 ENGINE CRACKED. REPLACED DUCT ASSEMBLY, INSPECTED AND LEAK CHECKED IAW MM 36-10-00.SDR 96ZZZX1079Tube · worn sleeveDURING ANNUAL INSPECTION, THE ENGINE AIR DISCHARGE TUBES (2 EACH) WERE FOUND WORN BEYOND LIMITS AT THE FORWARD SEAL RETAINING SLEEVE. REPLACED AIR TUBES.SDR 96ZZZX1078Tube · worn sleeveDURING ANNUAL INSPECTION, THE ENGINE AIR DISCHARGE TUBES (2 EACH) WERE FOUND WORN BEYOND LIMITS AT THE FORWARD SEAL RETAINING SLEEVE. REPLACED AIR TUBES.SDR HEEA966454Valve · inoperativeBLEED SOV SOLENOID INOPERATIVE.SDR 96ZZZX307Duct · crackedSTL - FLT 568 - AFTER TAKEOFF, NR 1 ENGINE FIREWARNING LIGHT ILLUMINATED. REMOVED AND REPLACED CRACKED 8TH STAGE DUCT. OPERATIONAL LEAK CHECK ACCOMPLISHED, NO LEAKS FOUND. OP-15 - 8-21-95 - STL.SDR MALA964809Switch · failedFLT 3127 - IN CRUISE FLIGHT, THE NR 1 AND NR 2 BLEED HOT LIGHTS CAME ON INTERMITTENTLY. THE AIRCRAFT RETURNED TO DTW. MAINTENANCE REPLACED THE LEFT PRESSURE SWITCH. SYSTEM OPERATED SATISFACTORILY. (X)SDR P5CA9600125Pneu Duct · crackedFOUND NR 3 ENGINE PNEUMATIC DUCT CRACKED. REPAIRED PER MM 36-10-02.SDR 96FDEA00016Duct · blownCLIMBING THROUGH 7,000 FT, RECEIVED ECAM AND FIRE HANDLE FIRE WARNING. WHEN THROTTLE MOVED TO IDLE ALL WARNINGS EXTINGUISHED, TESTED FIRE WARNING SYSTEM AND RETURNED TO EWR, ENG AT IDLE. OPENED UP NR 2 ENG AND FOUND HP RECOUP DUCT BLOWN, (P/N 9345M89-G01) RESDR P5CA9600124Tie Duct · brokenFOUND NR 4 ENGINE RIGHT HAND PNEUMATIC DUCT TIE LINK BROKEN. REMOVED AND REPLACED TIE LINK IAW 36-11-01.SDR P5CA9600103Duct Link · brokenNR 1 ENGINE PNEUMATIC DUCT LINK AT PYLON HORIZONTAL FIREWALL FOUND BROKEN ON LEFT SIDE. LINK ASSY REPLACED AND SECURED IAW MM 36-11-01.SDR HAL9601Augmentation Vlv · leakingINFORMATION FROM LOG PAGE 126945, 126946. HNL - FLT 534 - AFTER TAKEOFF, TAIL COMP. TEMP HI-LIGHT ON. PERFORMED ABNORMAL CHECK, LIGHT WENT OFF, RETURNED TO HNL. RAN ENGINES AT TAKEOFF POWER, FOUND LEFT AUGMENTATION VALVE LEAKING. NO LEAKS NOTED AT RIGHT AUSDR 96ZZZX302Duct Seal · failedMCI - FLT 469 - DURING CRUISE, NR 3 STRUT OVERHEAT LIGHT ILLUMINATED. REMOVED AND REPLACED NR 3 STRUT DUCT SEAL, MFG PN 10-61065-2. OPERATIONAL CHECK NORMAL. CHECK C-1 - 4-28-95 - MCI.SDR CAL951181Clamp · brokenFLT 1263 - CLE - THE NR 2 ENG FIRE WARN LIGHT ILLUMINATED DURING CLIMB-OUT OF CLE. THE FIRE LIGHT WENT OUT FOR ABOUT 1 MIN AFTER LEVELING OFF, AND CAME ON AGAIN FOR ABOUT 15 SEC. THE FIRE WARN WAS ACCOMPANIED BY NR 2 ENG OIL QTY LOSS AND THE CABIN WOULD NOT SDR 9521503215Clamp · looseDURING CLIMBOUT, RECEIVER 'AIR L WING LEAK' MESSAGE. FOLLOWED COCKPIT OPERATING MANUAL PROCEDURES AND DIVERTED TO MEM DUE TO ICING CONDITIONS AT ORIGINAL DESTINATION. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REINSTALLED CLAMP ON EXTERNAL AIR DUCT. OPSSDR DL76E954788Ducts · blownIR - ON DEPARTURE, LOUD BANG HEARD FOLLOWED BY BAD SMELL IN CABIN. PACK OFF LIGHT FOLLOWED BY NO AIR PRESSURE IN LT MANIFOLD. RETURNED FRA. FOUND ONE LT WING L/E SUPPLY DUCT AND ONE C/O SUPPLY DUCT. REPLACED BLOWN DUCTS, LEAK AND OPS CHECK NORMAL.SDR UIEA9602Stage 14 Duct · crackedLGW/LGW - FLT BA3571/20 - AIRCRAFT ABORTED TAKEOFF, APPROXIMATELY 140 KNOTS, GROSS WEIGHT 365,000 KGS DUE MASTER FIRE WARNING AND BELL SOUND. CREW EVACUATED AIRCRAFT PER FIRE CHIEF INSTRUCTIONS DUE TO BRAKE FIRE. AIRCRAFT INSPECTION REVEALED 8 BLOWN MAIN GEASDR 96ZZZX314Bracket · brokenKOAK/KLSC - FLT 518 - EN ROUTE KOAK, DIVERTED TO KLSC WITHOUT FURTHER INCIDENT. AT FL 370, AFTER LOUD NOISE, EXPERIENCED RAPID DEPRESSURIZATION. MAINTENANCE FOUND SLEEVE OFF OF SLIP JOINT ON SUPPLY DUCT IN RIGHT TUNNEL IN NLG WHEELWELL WITH DUCT SUPPORT BRACSDR 9520631158Pneu Manifold · failedDURING CLIMB, THE NR 2 PNEUMATIC MANIFOLD FAIL LIGHT ILLUMINATED INTERMITTENTLY. AIRCRAFT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. ITEM ENTERED IN MINIMUM EQUIPMENT LIST AND AIRCRAFT APPROVED FOR SERVICE.SDR CAL951148Duct · failedATL - FLT 1432 - THE NR 3 ENGINE FIRE LIGHT AND NR 3 START VALVE LIGHT BOTH ILLUMINATED INTERMITTENTLY IN-FLIGHT WITH A LOSS OF CABIN PRESSURE. ACFT RETURNED TO ATL WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NR 3 ENGINE'S 13TH STAGE PNEUMATIC DUCT BSDR 96ZZZX25Regulator · diaphragm blownDURING THE COURSE OF A 100-HOUR INSPECTION, FOUND THE BLEED AIR REGULATOR TO HAVE A BLOWN DIAPHRAGM. THIS IS THE REGULATOR LOCATED IN AFT BAGGAGE AREA THAT REDUCES THE BLEED AIR FROM THE ENGINE DOWN TO 18 PSI TO INFLATE THE DOOR SEAL AND DEICE BOOTS. HAVE FOSDR HEED95429Valve · defectiveBLEED SOV LEAKING. REPLACED UNITSDR 96ZZZX276Valve · defectiveRUDDER BOOST ENGAGED WHEN POWER WAS ADVANCED ABOVE 85 PERCENT. CHECKED SYSTEM, FOUND RIGHT FIREWALL SHUT-OFF VALVE OPERATED NORMALLY UNTIL APPLYING APPROXIMATELY 30 PSI SHOP AIR. THEN VALVE WOULD CLOSE, INDICATING ENGINE FAILURE.SDR HEED95414Valve · sticksVALVE STICKS OPEN . REPLACED UNITSDR 9519982285Flex Line · bbokenDURING CLIMB PASSING THROUGH 2000 MSL ON TAKEOFF, THE NR 3 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED. AIRCRAFT DIVERTED TO MEM AND LANDED WITHOUT INCIDENT. REPLACED BROKEN FLEX LINE. OPERATIONAL CHECK OK.SDR AALA952058Coupling · brokenSJU - FLT 0678 - AFTER TAKEOFF SJU DURING CLIMB-OUT, NR 2 ENGINE FIRE WARNING ILLUMINATED AND NR 2 ENGINE POWER LEVER BINDING NEAR TAKEOFF POWER SETTING. ACCOMPLISHED SHUT DOWN OF NR 2 ENGINE AND AIRCRAFT RETURNED SJU, LANDING WITHOUT INCIDENT. REPLACED NR 2SDR CAL951078Duct · rupturedFLT NR 1495 - BOS - THE NR 2 ENGINE SURGED ON TAKEOFF ROLL AT V1. THE TAKEOFF WAS CONTINUED AND ENGINE POWER WAS REDUCED TO KEEP EGT BELOW REDLINE. THE NR 2 ENGINE WOULD ONLY DEVELOP ABOUT 50 PERCENT POWER. THE AIRCRAFT WAS RETURNED TO BOS WHERE IT LANDED WSDR SWIA95687Clamp · failedLT 14TH STAGE DUCT WARNING, FOLLOWED BY LT JET PIPE OVERHEAT MESSAGE. REPLACED AFT CLAMP ON LT 14TH STAGE BLEED AIR SHUT-OFF VALVE. RAN LT 14TH STAGE BLEED AIR AND LEAK CHECK GOOD.SDR QXEA9500409Nr 2 Bleed Air · smokingGEG - NR 2 BLEED AIR GENERATING SMOKE IN CABIN. NR 2 BLEED AIR PLACED ON MEL 21-4.SDR 95ZZZX6826Air Pump · wornAIRCRAFT DEICE BOOTS INOP. FOUND AIR PUMP DRIVE GEAR LOOSE ON CLUTCH SHAFT. GEAR WAS WORN EXCESSIVELY AND CRACKED. THIS ITEM DIFFICULT TO INSPECT. SUBMITTER RECOMMENDS AD REQUIRING PERIODIC INSPECTION.SDR CAL951066Rubber Duct · blownGUM - FLT 0900 - THE SYSTEM NR 1 AND NR 2 MANIFOLD FAIL LIGHTS ILLUMINATED IN FLIGHT WITH NR 2 DISPLAYING THE LOWEST PRESSURE. THE AIRCRAFT WAS RETURNED TO GUM WHERE THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND A BLOWN RUBBER DUCT ON NR 2 PACK HEASDR CAL951049Duct · rupturedFLT NR 0382 - FLL - THE NR 3 ENGINE LIGHT ILLUMINATED AFTER TAKEOFF FROM FLL. ENGINE POWER WAS REDUCED AFTER LEVELING OFF AND THE ENGINE FIRE WARNING LIGHT EXTINGUISHED. FUEL WAS DUMPED AND THE AIRCRAFT WAS RETURNED TO FLL WHERE IT LANDED WITHOUT INCIDENT. SDR 95ZZZX6822Valve · dislodgedSHORTLY AFTER DEICE BOOTS WERE CYCLED AND AN I.F.R. LANDING APPROACH WAS ENTERED, ALL PRESSURE GYRO INSTRUMENTS FAILED AND SYSTEM PRESSURE WENT TO ZERO. BOTH RED INDICATOR BALLS REMAINED IN. FOUND LT CHECK VALVE IN MANIFOLD DEFECTIVE AND LT PUMP OUTPUT LOW. SDR 9518266628Duct · failedDURING ROTATION, THE NR 2 ENGINE FIRE WARNING ILLUMINATED, NACELLE TEMPERATURES PEGGED AND THE THRUST LEVER WOULD NOT REDUCE POWER. A FIRE BOTTLE WAS DISCHARGED, THE ENGINE WAS SHUTDOWN, AND ALL TEMPERATURES RETURNED TO NORMAL, 100,000 LBS OF FUEL WAS DUMPED SDR 95ZZZM713Clamp · distortedAT APPROX 6000 FEET, A LOW AIR PRESSURE WAS NOTED ON NR 3 BLEED SHORTLY THEREAFTER THE NR 3 FIRE WARNING LIGHT ILLUMINATED INTERMITTENTLY. THE NR 3 ENGINE WAS SHUT DOWN AND AIRCRAFT WAS LANDED AT CAE WITHOUT INCIDENT. FOUND 13TH STAGE BLEED DUCT SEPARATED FRSDR 1179596CKHose · deterioratedIN-FLIGHT MAIN DC CIRCUIT BREAKERS TRIPPED. CIRCUIT BREAKER PANEL WAS HOT TO TOUCH. BREAKERS WERE RESET AND A NORMAL LANDING MADE. INSPECTION OF ELECTRICAL SYSTEM AND CIRCUIT BREAKER PANEL REVEALED NO DEFECTS. A BLEED AIR HOSE UNDER THE PANEL WAS FOUND TO SDR SWIA95674Regulator Vlv · malfunctionedDUCT LEAKAGE LIGHT ILLUMINATED IN FLIGHT, PROCEEDED WITH ENGINE SHUTDOWN. FOUND GASKET NR 2 ENGINE BLOWN ON RT SIDE OF 18 PSI REGULATOR FOR DE-ICE SYSTEM. REPLACED 18 PSI REGULATOR VALVE. RAN RT ENGINE TO TAKEOFF POWER AND OPS CK GOOD.SDR 96ZZZX496Duct · blownEXPANSION JOINT RETAINING MESH HAS 'LET GO' AT EACH END ALLOWING THE EXPANSION BELLOWS TO KINK OUT OF ALIGNMENT. BELLOWS HAS RUPTURED. SUBMITTER STATED CAUSE UNKNOWN.SDR 95ZZZM661Poppet Valve · dirtyENGINE 1 DOES NOT MAKE TAKEOFF POWER. CLEANED NR 1 ENGINE POPPET VALVES SUCCESSFULLY GROUND RAN NR 1 ENGINE TO ACTIVE TAKEOFF POWER.SDR RAIA951031Pressure Switch · failedSTL - FLT 7180 - AIRFRAME AIRBLEED FAULT LIGHT ILLUMINATED IN FLIGHT. MAINTENANCE REMOVED AND REPLACED PRESSURE SWITCH, PERFORMED GROUND RUNS OPS CHECK GOOD. (M)SDR AALA951838Valve · defectiveMIA - FLT NR 0695, AFTER TAKEOFF MIA DURING CLIMB-OUT, NR 3 STRUT OVERHEAT LIGHT ILLUMINATED. ACCOMPLISHED QRH PROCEDURES AND AIRCRAFT RETURNED TO MIA, LANDING WITHOUT INCIDENT. REPLACED LEFT PNEUMATIC SHUTOFF VALVE. ALSO, REPLACED NR 3 STRUT OVERHEAT CONTRSDR 95ZZZX6192Joint · crackedINSPECTION REVEALED BLEED AIR JOINT WITH A CRACK APPROX 1 INCH BEYOND LIMITS. POSSIBLY CAUSED BY UNINTENTIONAL FORCE APPLIED TO AIR JOINT.SDR DLL10953993Clamp · wornPIREP, ABOUT 30 MINUTES AFTER T/O PRIOR TO TOP OF CLIMB, GOT A VALID J-AREA OVERHEAT. FOUND CLAMP LEAKING AT FUSELAGE ISOLATION VALVE IN HYD SV CTR. REPLACED CLAMP DAL (P/N 297201028) REF IPC 36-14-06 FIG 1 SHEET 2 ITEM 80. LEAK CHECK OK.SDR SWIA95634Press Valve · failedSHORTLY AFTER TAKEOFF, WE EXPERIENCED A DUCT LEAK WARNING. WE IMMEDIATELY LANDED AND SHUT THE ENGINE DOWN ON THE GROUND. REMOVED AND REPLACED PRESSURE VALUE, OPS RUN AND CKS GOOD.
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