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 CA990223021Check Valve · missing(CAN) BLEED AIR LINE REMOVED TO ALLOW REPLACEMENT OF AIR FILTER. IT WAS THEN NOTED THAT THE CHECK VALVE WAS NOT INTACT. THE EXHAUST COOLING DUCT WAS REMOVED TO FIND THE REMAINING PARTS OF VALVE.SDR CALA9900115Duct · brokenA FIRE WARNING INDICATION ON THE NR 3 ENGINE WAS RECEIVED AFTER TAKEOFF FROM BWI. CHECKLIST PROCEDURES WERE FOLLOWED, FUEL WAS DUMPED AND THE AIRCRAFT WAS RETURNED TO BWI WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NO EVIDENCE OF FIRE. THE NR 3 ENGISDR 99ZZZM209Duct · wornFLT 397 - HAD AN AIR TURN BACK TO TPA, ON CLIMB-OUT, ENGINE NR 2 FIRE INDICATION ILLUMINATED, RETARDED LEVER, LIGHT STAYED ILLUMINATED FOR A FEW SECONDS, DID INFLIGHT SHUTDOWN, RETURNED FOR LANDING. REPLACED NR 2 ENGINE 'Y' DUCTING FOR 13TH STAGE. (M)SDR 99ZZZM213Clamp · wornFLT 333 - EN ROUTE FROM TPA-DAY - NR 2 ENGINE FIRE WARNING ON MOMENTARILY. FOUND LEAKING DUCT CLAMP AT START VALVE UPPER CLAMP. REPLACED SAME. (M)SDR 99ZZZX823Duct · crackedAN INVESTIGATION WAS CONDUCTED TO DETERMINE THE CAUSE OF A VERY SUBSTANTIAL BLEED AIR LEAK IN THE TAIL COMPARTMENT. THE LEAK WAS TRACED TO A DRILLED HOLE IN THE OUTER WALL OF THE 45A63514-1 VENTURI. THE VENTURI WAS REMOVED AND INSPECTED INTERNALLY. THE INNERSDR 99FDEA00040Duct · rupturedNR 2 ENGINE FIRE HANDLE ILLUMINATED. FIRE LIGHT EXTINGUISHED WHEN NR 2 ENGINE RETARDED. REMOVED AND REPLACED NR 2 ENGINE CSD HIGH PRESSURE DUCT ASSY DUE TO HOLE IN DUCT PER M/M 36-00-1. RAN ENGINE AT IDLE, NO LEAKS, CK NORM.SDR UHLA99203Valve · brokenUHLA - FLT 220 - BUF-BDL - THE FLIGHT ATTENDANT NOTIFIED THE CREW OF SMOKE (IN THE CABIN SHORTLY AFTER TAKEOFF. THE CREW CLOSED THE BLEEDS AND RETURNED TO THE FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND NR 1 AIR SWITCHING VALVE BROKEN AND REPLACED AS REQSDR 99ZZZX925Muffler · looseMUFFLER/HEAT EXCHANGER END FLANGE SEPARATED FROM THE MUFFLER HOUSING CAUSING LARGE AMOUNTS OF EXHAUST TO ENTER THE CABIN. PART TT: 1,711.4 HOURS. MUFFLER MIGHT HAVE BEEN REPAIRED BY WELDING ON THE OUTSIDE OF BOTH THE FLANGES. SUBMITTER SUGGESTED NEW STYLE SDR 99FDEA00039Clamp · looseFIRE WARNING ON ENGINE NR 1. REMOVED PYLON ACCESS PANELS AND OPENED ENGINE COWL, CHECKED FIRE LOOP AND CONNECTIONS, TIGHTENED DUCT CLAMPS. OK FOR SERVICE.SDR AWXA9900037Duct · failedDIVERSION, PRECAUTIONARY LANDING MADE AT DSM. AIR WING LEAK, AIR APU BLEED LEAK, DETECTED BY ECAM. PRESSURIZATION WAS LOST FOR A SHORT TIME. MESSAGE CLEARED AND SYSTEM RESET, OPS NORMAL AFTER THAT. FOUND SEPARATED BLEED DUCT AT GROUND AIR START TO MANIFOLDSDR MALA976329Valve · failedBLEED FAULT ILLUMINATED AFTER TAKEOFF ON RIGHT ENGINE, COMPLETED QRH AND BLEED FAULT STILL ILLUMINATES. AIRCRAFT RETURNED TO DTW. MAINTENANCE REPLACED PRESSURE REGULATING VALVE AND BLEED PRESSURE SWITCH, OPS CHECK GOOD IAW SAAB AMM CHAPTER 74.SDR DHL9980534CBracket · brokenAT C-CHECK, LEFT WING L/E LOWER PANEL SUPPORT BRACKET FOR PNEU DUCT BROKEN. REMOVED AND INSTALLED FABRICATED BRACKET PER SRM 51-1-8. N/R 1416SDR 99ZZZX825Bleed Air Line · separated14TH STAGE BLEED AIR LINE CAME LOOSE ON NR 2 ENGINE. THIS HAPPENED IN-FLIGHT. PILOT POWERED BAD ENGINE AND LANDED UNEVENTULLY IN BTL. BLEED AIR DAMAGED COWL AND WIRE HARNESS. PARTS REPLACED AS NECESSARY. AIRCRAFT TEST FLOWN. CAUSE UNKNOWN. ACFT: 6,039SDR SCNA99015Clamp · looseDURING CLIMBOUT FROM SFO, THE ENGINE NUMBER ONE STRUT OVERHEAT LIGHT ILLUMINATED. FOUND ENGINE DUCT IN THE NUMBER ONE PYLON LEAKING JUST BEFORE THE PRECOOLER. TIGHTENED CLAMP AND RAN THE NUMBER ONE ENGINE TO LEAK CHECK. NUMBER ONE ENGINE LEAK CHECKED GOOD ISDR C2XA99CL009Valve · failedCLE - FLT 3161 - CREW REPORTED THAT THE RIGHT HAND BLEED AIR FAIL LIGHT ILLUMINATED IN-FLIGHT. AIRCRAFT RETURNED TO FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RIGHT HAND BLEED AIR SHUT OFF VALVE IAW B1900 MM 36-00-02, OPERATIONAL ANSDR EISA99015Pneumatic Line · fracturedNR 3 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED IN FLIGHT AFTER TAKEOFF. FOUND HOLE IN BRAIDED HIGH PRESSURE LINE IN THE ENGINE STRUT AREA. REMOVED AND REPLACED LINE IAW MM 36-12. LEAK AND OPS CHECK GOOD ON GROUND IAW 26-14 MM. (M)SDR EISA99007Pneumatic Line · puncturedNR 3 ENGINE STRUT OVERHEATS IN FLIGHT AFTER TAKEOFF. FOUND BRAIDED HP AIR LINE HOLE ENGINE STRUT. REMOVED AND REPLACED LINE IAW MM CHAPTER 36-12. LEAK AND OPS CHECK GOOD ON GROUND IAW MM 26-14. (M)SDR EISA99021Duct · crackedLOWER AFT BODY OVERHEAT LIGHT ILLUMINATED WHILE ENGINE ANTI-ICE WING ANTI-ICE WERE IN USE. CLOSING THE WING ANTI-ICE AND A CO-INCIDENTAL REDUCTION IN POWER DURING AN APPROACH EXTINGUISHED LIGHT. LOG PAGE 58944 MEL 30-2 PLACARD 980. REMOVED AND REPLACED CRACSDR C2XA99CL008Duct · chaffedCLE - FLT 4119 - CREW REPORTED THAT DURING CRUISE THEY RECEIVED A LEFT ENGINE BLEED LEAK LIGHT, THE AIRCRAFT RETURNED TO THE FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LEFT BLEED DUCT LOCATED IN FUSELAGE ABOVE THE LEFT WING IAW EMB-1SDR 99FDEA00014Clamp · loosedENGINE STRUT OVERHEAT LIGHT ILLUM. CK LIST TURN OFF AFFECT WING ANTI-ICE SWITCH CLOSED. ENG STRUT O/H LIGHT WENT OUT. CREW COMMENT, O/H LIGHT WENT OUT WITH ENG PWR DECREASED. FOUND LOOSE CLAMP AT 13TH STAGE CHECK VALVE. TIGHTENED CLAMP. NO O/H AT THIS TISDR AT9900018Clamp · brokenCLIMBING THROUGH 14,000 FEET MASTER WARNING LIGHT ILLUMINATED WITH TAIL COMPARTMENT TEMPERATURE HI-LIGHT ON, NORMAL PROCEDURES FOLLOWED. REPLACED BROKEN CLAMP AT LEFT HAND HEAT EXCHANGER PRIMARY AIR DUCTING PER MM 36-10.SDR C2XA99CL001Regulator · failedCLE - FLT 3063 - CREW REPORTED THAT WHILE CLIMBING THROUGH 10,000 FT THE RIGHT ENGINE DUCT LEAK LIGHT CAME ON, IT WOULD NOT GO OUT IN 3 MINUTES SO THE ENGINE WAS SHUT DOWN AND THEN THE LIGHT DID EXTINGUISH. AIRCRAFT RETURNED TO THE FIELD WITHOUT FURTHER INCIDSDR 99FDEA00005Valve · failedLOWER AFT BODY O/H LIGHT ILLUMINATED. FOLLOWED CK LIST PROCEDURE, CLOSED NR 1 BLEED VALVE AND LEFT PACK. RETARDED NR 1 THROTTLE TO CLIMB POWER. LIGHT REMAINED OUT AND TEST OK, INDICATIVE OF LEAK BETWEEN NR 1 BLEED VALVE AND LEFT PACK VALVE. REMOVED AND REPSDR DLM88990008Clamp · looseRT ENGINE NR 2 FAILED PASSING APPROX 5000 FT ON INITIAL CLIMBOUT. THIS APPEARED TO HAPPEN AFTER ENG ANTI-ICE WAS TURNED OFF. ENG RESTARTED NORMALLY AND RAN NORMAL. FOUND STARTER VALVE CLAMP UPSTREAM OF VALVE, OFF THE DUCT. REPLACED CLAMP, RAN ENGINE TO T/OSDR ASOA99001Clamp · looseFLT 4831 - CRP-DFW - WHILE LEVEL AT 6,000 FEET ON DESCENT INTO DFW, RIGHT ENGINE DUCT LEAK LIGHT ILLUMINATED, FOLLOWED BY AURAL WARNING. CREW C/W DUCT LEAK EMERGENCY CHECKLIST, AND WHEN AFTER 3 MINUTES LIGHT WAS STILL ILLUMINATED, SHUT DOWN THE RT ENGINE. CRSDR SWIA971349Valve · failedMIDDLE LEFT WING DEICE FAILS IN BOTH TIMER POSITIONS AND BOTH HEAVY AND LIGHT POSITIONS. RETURNED TO SLC. REMOVED AND REPLACED THE RIGHT BLEED AIR SHUT OFF VALVE IAW EMB 120 MM 36-10-00. RAN THE AIRCRAFT DEICE SYSTEM IN ALL CONFIGURATIONS, CHECKS GOOD. ALSSDR SWIA971348O Ring · failedLEFT ENGINE DUCT LEAK LIGHT ILLUMINATED SHORTLY AFTER TAKEOFF. COMPLIED WITH QRH AND RETURNED TO PSP AND CONTACTED MAINTENANCE. FOUND O-RINGS WORN ON COUPLER SLEEVE CAUSING LEFT ENGINE BLEED AIR DUCT TUBE ASSEMBLY TO LEAK AT LEADING EDGE AND AT WING TO FUSELSDR DHL98717004Valve · dirtySMOKE IN COCKPIT AFTER TAKEOFF. FOUND NR 1 ENGINE PRECOOLER CHECK VALVE STUCK OPEN. CLEANED VALVED AND RAN ENGINE, OPS CHECK GOOD.SDR DL72S982625Duct · brokenLOWER AFT BODY OVERHEAT LIGHT ON. REPLACED BLOWN DUCT UNDER APU IN KEEL BEAM.SDR DL72L982644Duct · failedON CLIMBOUT, NR 1 ENG STRUT OVERHEAT LIGHT ILLUMINATED. ALL CK LIST WERE RUN AND LIGHT DID NOT GO OUT. SHUT DOWN NR 1 ENG AND DUMP FUEL. RETURNED TO SEA. REPLACED LEAKING HP TAI DUCT, LEAK CK NORMAL.SDR ABXA9801189Duct · failedEN ROUTE FROM ONT TO ILN, AIRCRAFT EXPERIENCED RAPID DECOMPRESSION AT 33.000 FT. CABIN CLIMED TO 20,000 FT IN APPROX 2 MIN. EXECUTED EMERGENCY DESCENT. PRESSURE WAS REGAINED AT APPROX 10,000 FT. FOUND DUCT CLAMP LOOSE AND DUCT SEPARATED. RECONNECTED DUCT SDR USAABB98118Duct · leakingCLT - FL 795, AFTER TAKEOFF, CREW RECEIVED FIRE WARNING LIGHT AND FIRE WARNING BELL FOR LEFT ENGINE. CREW REDUCED POWER AND THE INDICATIONS EXTINGUISHED. FLIGHT RETURNED TO CLT AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE FOUND THE HP 6 DUCT ASSEMBLY LESDR CLCA9802Clamp · looseMIA/WI - FLT 085 - ABORTED TAKEOFF. ON TAKEOFF ROLL HAD NR 1 FIRE WARNING INDICATION. ABORTED TAKEOFF, PERFORMED CHECK LIST F/W LIGHT WENT OUT. UPON GROUND INSPECTION AT MIA, FOUND PDU SUPPLY DUCT CLAMP NOT INSTALLED PROPERLY WHICH ALLOWED 13TH STAGE HOT AISDR AWXA9800234Thermostat · malfunctionedBLEED 1 AND BLEED 2 FAULT. DPI ISSUED MEL 36-11-01. T/S FOUND TEMP THERMOSTAT CONTROL FAULTED. REMOVED AND REPLACED PER AMM CHAP 36-11. SYS OPS OK, NO FAULTS NOTED. ALSO, REMOVED AND REPLACED BMC NR 2 AS PREC PER MC AMM CHAP 36.SDR 99ZZZX114Shaft · shearedPUMP SEIZED, SHAFT SHEARED. SUBMITTER STATED CONTINUE TO HAVE SHORT LIFE WITH THESE PUMPS.SDR IXXA9800110Pneumatic Line · looseAFTER TAKEOFF FROM TOL, EN ROUTE TO FLL, THE NUMBER TWO ENGINE FIRE WARNING INTERMITTENTLY SOUND ACCOMPANIED BY AN INTERMITTENT MASTER FIRE WARNING LIGHT ILLUMINATING. THE FLIGHT CREW SECURED THE ENGINE FOLLOWING COMPANY PROCEDURES AND RETURNED TO TOL FOR AN SDR ORJA98308Controller · malfunctionedIN RNO - AFTER TAKEOFF, ROLL 6 FT PNEU SYSTEM FAULT REJECTED TAKEOFF RETURN TO GATE. RAN BIT TEST ON PNEU SYSTEM CONTROLLER, NO FAULTS NOTED SYSTEM FAULT CLEARED MESSAGE CLEARED. (M)SDR VNAA9811024Valve · failedDURING THE TAXI PRIOR TO TAKEOFF, A CROSS-BLEED FAIL WARNING MESSAGE ILLUMINATED. THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED AND REPLACED THE CROSS-BLEED VALVE, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 36-11-10. OPERATIONAL CHECKS WERE COSDR 99ZZZM81Duct · leakingFLT 711 - EWR - ENGINE FIRE INDICATION ONR NR 1 ENGINE DURING CLIMB-OUT. SHUT DOWN NR 1 ENGINE. REMOVED AND REPLACED FIRE BOTTLE AND SQUIB CARTRIDGE NR 1 ENGINE. RESEALED CLAMPS ON NR 1 ENGINE STARTER DUCT. (M)SDR COMA9860369Valve · stuckRIGHT ENGINE 10TH STAGE ISOLATION VALVE STUCK PARITALLY OPEN. REPLACED VALVE.SDR MALA976249Duct · failedNR 4 ENGINE FIRE WARNING ACTIVATED ON CLIMBOUT. NR 4 ENGINE SHUTDOWN AND RETURNED TO LEX. MAINTENANCE INSTALLED NEW DUCT BETWEEN 12 O'CLOCK POSITION. PERFORMED ENGINE RUNS AND VERIFIED NO FIRE WARNINGS.SDR MALA976240Valve · failedDURING FLIGHT, LEFT AIR VALVE ILLUMINATED WHEN SWITCH TURNED ON, NO TORQUE DROP OR ITT RISE NOTED. AIRCRAFT RETURNED TO DTW. MAINTENANCE REPLACED LEFT ENGINE START BLEED AIR VALVE. OPS CHECK FOR 15 MINUTES GOOD. ALL IAW GE MM.SDR MALA976239Valve · failedDURING FLIGHT, LEFT AIR VALVE LIGHT ILLUMINATED. CREW PERFORMED ALL APPROPRIATE CHECKS, STILL INOP. AIRCRAFT RETURNED TO DTW. MAINTENANCE REPLACED LEFT ENGINE AIR BLEED SHUT OFF VALVE. ALL IAW GE MM, OPS CHECK GOOD ON THE GROUND.SDR AU981493Precooler · cracked(AUS) NR 3 ENGINE AIR PRE-COOLER OUTER CASING CRACKED ON SEAM WELD. CRACK LENGTH 9.525 MM (0.375 INCH).SDR 98FDEA00703Cap · looseALL POWER LEVERS AT IDLE, NR 1 ENG FIRE LIGHT ON, REMAINED OUT WITH NR 1 AT IDLE. INSPECTED ALL PNEUMATIC PLUMBING AND DUCTING, AIR LEAKAGE ON SURROUNDING SURFACES, TIGHTENED AND RESAFTIED CAP. CHECKS SATISFACTORILY.SDR CA981130010Duct · leaking(CAN) DURING LANDING, LOUD BANG FROM LANDING GEAR AREA. RIGHT DUCT LEAK LIGHT AND MESSAGE ON SHORT FINAL. REPLACED PNEUMATIC DUCT DOWN STREAM OF RIGHT ISOLATION VALVE.SDR DHL98804003Pre Cooler · malfunctionedLEFT MANIFOLD TEMP RUNNING 250 DEGREE WITH NO ANTI-ICE ON, WITH ENG ANTI-ICE ON NR 1 MANIFOLD AIR OVER TEMP LIGHT ILLUMINATED. TEMP WENT TO 280 DEGREES. REPLACED NR 1 AND NR 2 ENGINE PRECOOLERS. GROUND OPS CHECK NORMAL.SDR DHL9872016DHeat Shield · crackedAT D CHECK, NR 1 ENGINE PRECOOLER FWD HEAT SHIELD CRACKED AND MISSING LOWER I/B CORNER. INSTALLED DOUBLER REPAIR AT FWD CORNER PER SRM 51-40-2, 6 BY 4, N/R 6777.SDR 99ZZZX440Manifold · crackedON CLIMB, NR 3 ENGINE FIRE DETECTION LIGHT REMAINED ILLUMINATED. ENGINE SHUT DOWN AFTER PERFORMING CHECK LIST ITEMS. AIRCRAFT RETURNED TO DEPARTURE AIRPORT AND LANDED WITHOUT INCIDENT. COMPANY MAINTENANCE DISCOVERED THE 13TH STAGE BLEED LINE SEPARATED AT 'TSDR AU981428Duct · cracked(AUS) APU BLEED AIR DUCT CRACKED CAUSING BLEED AIR TO ACTIVATE APU FIRE WARNING SYSTEM.
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