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 SWAA010645Regulator · inoperativeAIR TURNBACK. AFTER TAKEOFF, NR 1 ENG PNEUMATIC BLEED C/B TRIPPED. WOULD NOT RESET ON FIRST ATTEMPT AND BLEED AIR PRESS NOT STABLE. REMOVED AND REPLACED NR 1 PNEUMATIC HIGH STAGE REGULATOR PER MM.SDR DL757010358Clamp · failedSHORTLY AFTER TURNING ON WING A/I DUCT LEAK ILLUMINATED ALONG WITH RT ENG ANTI ICE. A/C DIVERTED INTO PHX. FOUND CLAMP DPN 366201022 HAD FAILED IN THE RT ENG/PYLON FWD SECTION, 16 SMALL RIVITS HAD FAILED ON THE CLAMP ALLOWING THE DUCT TO SEPARATE.SDR USAASB01057Regulator · failedORD - FLT 916 - ON CLIMB-OUT FROM ORD, EN ROUTE TO CLT, THE NR 2 ENGINE BLEED TRIP LIGHT ILLUMINATED. CAPTAIN TRIED TO RESET THE NR 2 ENGINE BLEED TRIP WITH NO HELP, AS LIGHT REMAINED ILLUMINATED. CABIN PRESSURE STARTED TO CLIMB WITH THE AIRCRAFT, SO THE CAPSDR SIMA0553O-Ring · wornORD - FLT 4137 - DURING CLIMB, CREW NOTED NR 1 BLEED LEAK, NO OTHER PROBLEMS WERE REPORTED. AIRCRAFT WAS RETURNED TO ORD. MAINTENANCE REPLACED O-RINGS AT THE UPPER BLEED DUCT LINE. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR 2001UALA00193Clamp · failedFORTY MINUTES AFTER TAKE-OFF, FLIGHT HAD MULTIPLE EICAS MESSAGES FOR THEIR RIGHT ENGINE NACELLE VENT VALVE. BLEED LOOP 2 WING R STATUS MSG, BLEED LEAK R, BLEED LOSS R AND PACK R. RESET THE BLEED BUT MESSAGES CAME BACK. RETURNED TO IAD AND LANDED OVERWEIGHT.SDR AALA20010330Clamp · brokenRDU - FLT 1389 - EN ROUTE RDU-ORD, DETECTED TAIL COMPARTMENT HIGH TEMPERATURE LIGHT ILLUMINATE. AIR INTERRUPTED, RETURNED RDU AND LANDED WITHOUT INCIDENT. REPLACED CLAMP AT RIGHT SIDE ACM. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)SDR AALA20010633Duct · rupturedDFW - FLT 946 - SHORTLY AFTER TAKEOFF, NR 3 AIR SYSTEM DIFFERENTIAL MESSAGE ILLUMINATED. NR 3 BLEED AIR PRESSURE OFF LIGHT ALSO ILLUMINATED. LANDED DFW WITHOUT FURTHER INCIDENT. REPLACED NR 3 INBOARD DUCT. LEAK CHECKS GOOD. SYSTEM GROUND CHECKED NORMAL OPSDR VNAA0102011Bleed Valve · failedAFTER CLIMB OUT, THE CREW RECEIVED A RIGHT HAND PACK OVERHEAT MESSAGE. THE CREW REFERENCED THE QUICK REFERENCE HANDBOOK THEN CONTACTED MAINTENANCE CONTROL WHO DIRECTED THEN TO RETURN TO PIT. MAINTENANCE INSPECTED AND REPLACED THE RIGHT HAND HIGH PRESSURE BLESDR AALA20010299Clamp · looseORD - FLT 430 - EN ROUTE ORD-DCA, DETECTED NR 1 BLEED FAULT LIGHT ILLUMINATE. RETURNED ORD AND LANDED WITHOUT FURTHER INCIDENT. RE-SECURED NR 1 TAIL DUCT CLAMP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)SDR C2XA01CL026O-Ring · leakingCLE FLIGHT 4293, THE CREW REPORTED A BLEED 1 LEAK MESSAGE AFTER TAKEOFF. THE NR 1 ENGINE WAS SHUTDOWN AND THE AIRCRAFT RETURNED TO CLEVELAND AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED AN O-RING ON THE NR 1 BLEED LINE IN THE CARGOSDR AALA20010634Duct · rupturedDFW - FLT 946 - SHORTLY AFTER TAKEOFF, NR 3 MANIFOLD FAIL LIGHT ILLUMINATED. LANDED DFW WITHOUT FURTHER INCIDENT. REPLACED NR 3 INBOARD DUCT PYLON. LEAK CHECKS GOOD. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)SDR 0100566729Clamp · failedDURING INITIAL CLIMB AT 300 FEET, THE NR 1 ENGINE FIRE WARNING ACTIVATED. THE NACELLE TEMPERATURE INDICATION WAS PEGGED IN THE WARNING RANGE AND THE POWER LEVER WAS STUCK IN MID RANGE. THE ENGINE WAS SHUT DOWN PER COM AND ONE FIRE BOTTLE WAS DISCHARGED. AFTSDR GLBA2001034Clamp · out of positionRETURN TO BLOCK - RIGHT BLEED AIR FAIL. REPOSITIONED CLAMP AND REPAIRED EVA TUBING, OPS CHECKED SYSTEM GOOD. RETURNED TO SERVICE.SDR 20010525SG001Duct · leakingCMH - FLT 5346 - CREW RETURNED TO FIELD DUE TO BAGGAGE SMOKE INDICATION FOLLOWED BY ENGINE TWO BLEED LEAK. MAINTENANCE REMOVED AND REPLACED THE NR 2 FUSELAGE THROUGH PYLON BLEED LINE AND THE CARGO DUCT ASSEMBLY. OPS CHECK WAS GOOD, FIRE BOTTLES WERE REPLACED SDR SIMA200104103Line · leakingCMH - FLT 5346 - CREW RETURNED TO FIELD DUE TO BAGGAGE SMOKE INDICATION FOLLOWED BY ENGINE TWO BLEED LEAK. MAINTENANCE REMOVED AND REPLACED THE NR 2 FUSELAGE THROUGH PYLON BLEED LINE AND THE CARGO DUCT ASSEMBLY. OPS CHECK WAS GOOD, FIRE BOTTLES WERE REPLACED SDR USAASB01045Regulator · failedPHL - FLT 1598 - EN ROUTE FROM IND TO PHL, AT FL370, THE LEFT ENGINE BLEED TRIP OFF LIGHT ILLUMINATED. CABIN RAPIDLY CLIMBED, SO THE CREW EXECUTED AN EMERGENCY DESCENT TO FL100. CREW WAS ABLE TO RESET THE PACK TO THE LOWER ALTITUDE AND IT OPERATED NORMALLY. SDR 2001UALA00080Clamp · failedNR 3 ENGINE OVERHEAT LIGHT CAME ON DURING CLIMB. RETURNED TO MIA. DECLARED AN AMBER ALERT AND LANDED OVERWEIGHT. *S/D* FOUND 2 CLAMPS LEAKING PNEUMATIC AIR FROM 6TH STAGE DUCTS. REPLACED BOTH CLAMPS. NO LEAKS FOUND.SDR MALA010176Periseal · leakingNR 2 LT ZONE HI TEMP LIGHT ILLUMINATED EN ROUTE. AIR TURNBACK TO DTW. UPON INSPECTION MAINTENANCE FOUND PERI-SEALS LEAKING AT LEADING EDGE ON NR 1 PYLON, REMOVED AND REPLACED PERI-SEALS IAW AVRO MM CHAP 30. P/N 460-200. PERFORMED GROUND RUNS AND ANTI-ICE SSDR SIMA200103503O-Ring · leakingORD - FLT 4047 - AFTER DEPARTURE FROM ORD RT/ENG BLEED LEAK LIGHT ILLUMINATED. CREW ELECTED TO RETURN TO ORD. REMOVED AND REPLACED O-RING AT RIGHT OVERWING BLEED IAW AMM. OPS CHECK GOOD. (M)SDR SWIA972331Shutoff Valve · failedLEFT 10TH SOV FAILED TO OPEN. RECEIVED STATUS MESSAGE L 10TH ARMED OPEN. RETURNED TO DEN. POWERED DOWN AIRCRAFT AND RE-POWERED. OPS CHECK GOOD.SDR USAASB01035Hose · failedYUL - FLT 0442 - EN ROUTE FROM PIT TO YUL, AT FL330, THE CABIN ALTITUDE WARNING HORN SOUNDED. CREW PERFORMED EMERGENCY PROCEDURES AND WHEN CABIN ALTITUDE CLIMED TO MORE THAN 10,000 FEET, THEY DECLARED AN EMERGENCY. CREW DESCENDED THE FLIGHTS TO FL100 AND WERSDR AU010091Duct · leaking(AUS) NR 1 BLEED AIR SYSTEM LEAKING.SDR DL72S010174Harness · burnedNR 2 ENGINE RT ISOLATION VALVE WIRING HARNESS BURNT IN TWO. REPAIRED WIRING. SYS OP CKS GOOD.SDR AU010095Duct · leaking(AUS) TAIL SECTION PNEUMATIC DUCT LEAK WARNING. INVESTIGATION COULD FIND NO LEAKS.SDR MALA010148Line · looseDURING CLIMBOUT OF DTW, LT AIR VALVE LIGHT ILLUMINATED. AIR TURNBACK TO DTW. MAINTENANCE FOUND LINE LOOSE ON LT AIR VALVE AND LOOSE C-CLAMP, TIGHTENED LINE AND CLAMPS AND OPS CHECK IAW SF340 MM CHAP 76. ALL CHECKS GOOD.SDR EISA20010003Clamp · wornNR 3 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED DURING FLIGHT. INSTALLED NEW CLAMPS ON DUCTS IN NR 3 STRUT. RAN UP TO POWER, NO LIGHT.SDR 2001UALA00059Regulator · failedRETURNED TO DEN DUE TO A PROBLEM WITH THE NR 1 BLEED AIR SYSTEM. *S/D* BLEED AIR VALVE WOULD NOT OPEN AFTER BLEEDS OFF TAKEOFF. REPLACED THE BLEED AIR REGULATOR.SDR AALA20010178Duct · leakingORD - FLT 682 - EN ROUTE SFO-ORD, ON FINAL APPROACH DETECTED A LOUD BANG AND LEFT SIDE PACK TURNED OFF. LEFT SIDE DUCT LIGHT ILLUMINATED. LANDED ORD WITHOUT FURTHER INCIDENT. REPLACED PNEUMATIC DUCTS AT WING AREA. ACCOMPLISHED LEAK CHECKS IAW THE MM. NO LSDR USAASB01014Regulator · failedBWI - FLT 1801 - EN ROUTE FROM BOS-ATL, THE CREW HAD TROUBLE MAINTAINING CABIN PRESSURIZATION. AT FL230, THE RIGHT BLEED PRESSURE WENT TO 30 PSI WHILE THE LEFT STAYED AT 0. CABIN ALTITUDE CLIMBED TO OVER 10,000 FEET AND SET OFF THE CABIN ALTITUDE WARNING HORSDR TSAA0136007Valve · defectiveFLT 210 - HNL-OGG - DURING TAKEOFF, NR 2 ENGINE BLEED LIGHT CAME ON. ABORTED TAKEOFF AND RETURNED TO GATE. REMOVED AND REPLACED THE NR 2 ENGINE PNEUMATIC SHUTOFF VALVE IAW MM 21-11-011-6. OPS AND LEAK CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)SDR AU010090Loop · faulty(AUS) WING LOOP A PNEUMATIC SYSTEM INOPERATIVE.SDR AWXA0001251Regulator · failedLAS-DIVERTED FLIGHT- EN ROUTE FROM PHX TO GEG THE RT AIR CONDITIONING PACK FAILED A FL350, RT BLEED DUCT PRESSURE WENT TO 0 AND THE FLIGHT DIVERTED TO LAS. MAINTENANCE TROUBLESHOOTING FOUND THE BLEED DID NOT RESPOND TO THE SWITCH WHEN TURNED ON. THE NR 2 ENGSDR C2XA01IA036Clamp · brokenIAH - FLIGHT 4211, THE CREW REPORTED THAT ON CLIMB THE CARGO BAY FILLED WITH SMOKE AND PRESSURIZATION WAS LOST. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE NUMBER ONE ENGINE PNEUMATIC DUCT CSDR C2XA01CL009Duct · crackedCLE - FLT 3641 - THE CREW REPORTED ON CLIMB-OUT, RECEIVED A NR 2 BLEED LEAK INDICATION. THE REPORTED A STRONG BURNING SMELL UNTIL THE BLEED WAS SHUT OFF. THE AIRCRAFT RETURNED TO CLEVELAND AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACESDR MALA010123Valve · failedAIR RETURN TO DTW WITH LT AIR VALVE LIGHT ON. MAINTENANCE REPLACED LT START BLEED VALVE P/N 5056T88P01, S/NB ON AEX10537, S/N OFF AEX10630. ALL CHECKS GOOD.SDR USAABB02007Duct · leakingCLT - FLT 1166 - ON DESCENT INTO CLT, CREW RECEIVED THE EICAS MESSAGE 'L ENGINE OVERHEAT' AND 'OVERHEAT' LIGHT. THE LIGHT EXTINGUISHED WHEN THE THROTTLE WAS RETARDED. FLIGHT CONTINUED TO CLT AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED LEAKING SDR USAABB02006Duct · leakingCLT - FLT 1166 - ON DESCENT INTO CLT, CREW RECEIVED THE EICAS MESSAGE 'L ENGINE OVERHEAT' AND THE 'OVERHEAT' LIGHT. THE LIGHT EXTINGUISHED WHEN THE THROTTLE WAS RETARDED. FLIGHT CONTINUED TO CLT AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED LEAKSDR DLM88010058Clamp · looseTAIL COMPARTMENT TEMP LIGHT CAME ON SHORTLY AFTER T/O. RAN CHECKLIST PER POM. LIGHT WENT OFF AFTER LEVEL OFF 3000 FT. LIGHT CAME BACK ON AFTER POWER INCREASED TO CLIMB. RETURNED TO MCO. RAN ENG AT T/O PWR. FOUND AUG VALVE LEAKING AT I/B CLAMP. REPLACED SDR SWAA010094Shutoff Valve · inoperativeAIR TURNBACK, NO BLEED AIR FROM NR 1 ENGINE AFTER T/O. REMOVED AND REPLACED PRSOV, LOW PRESSURE REGULATOR (P/N 3214552-5) AND PRSOV MUSCLE AIR LINE PER MM. OPS AND LEAK CHECK GOOD.SDR SWIA972262Warning Light · illuminatedRIGHT DUCT LEAK LIGHT ILLUMINATED PRIOR TO TAKEOFF. CLOSED RIGHT BLEED VALVE AND LIGHT REMAINED ILLUMINATED FOR MORE THAN 3 MINUTES. SHUT DOWN RIGHT ENGINE. LIGHT REMAINED ILLUMINATED FOR FOUR MINUTES, UNTIL POWER DOWN. ABORTED TAKEOFF. RAN RIGHT ENGINE ASDR DL72W010003Clamp · stretchedAT 60 KTS ON T/O ROLL, LEFT STRUT PNEUMATIC DUCT PRESSURE WENT TO 6 O'CLOCK POSITION. ON CLIMBOUT, NR 1 ENG STRUT OVERHEAT LIGHT ILLUMINATED. NR 1 ENGINE THROTTLE BROUGHT TO IDLE. LIGHT EXTINGUISHED. FOUND WORN DUCT CLAMP ON ENG BLEED SUPPLY DUCT. REPLACED SASDR 0004603260Service difficultyDURING DESCENT PASSING THROUGH 10,000 FEET AT IDLE POWER, THE NBR 2 ENGINE FLAMED OUT. ALL ENGINE PARAMETERS WERE IN THE GREEN THROUGHOUT FAILURE INCLUDING EGT. RELIGHT WAS SUCCESSFUL. FLIGHT CREW CONTINUED APPROACH AND EXPERIENCED NO FURTHER TROUBLE. MAINTSDR 20010126CW011Valve · failedAIRCRAFT EXPERIENCED LOSS OF BLEEDAIR INFLIGHT, AFTER LANDING, INVESTIGATION REVEALED UPON OPENING LEFT ENGINE COWLING HAD FOUND VALVE HAD FAILED, SENT TO ENGINEERING FOR INVESTIGATION.SDR 2000UALA00815Seal · leakingCREW REPORTED NR 2 ENGINE FIRE WARNING COMING ON WITH POWER ABOVE 85 PERCENT. REDUCED POWER AND LIGHT WENT OUT. ADVANCED POWER AND BELL AND LIGHT CAME ON AGAIN. RETURNED TO EWR. *S/D* 13TH STAGE SADDLE DUCT SEAL (RT) LEAKING. REPLACED SEAL. TESTED SYSTESDR 20010228SG001Duct · crackedSBP - FLT 3014 - THROUGH 5000 FT ON CLIMB, THE NR 2 OVERTEMP WITH RED LIGHT TQ INCREASED TO 120 PERCENT. PERFORMED DOWNLOAD FDAU. FOUND NO RECORD OF EXCEEDANCES OF GE MM LIMITS. PERFORMED BORESCOPE OF ENGINE. NO DEFECTS NOTED. PERFORMED ITT SYSTEM CHECK. SDR SIMA3612Duct · crackedSBP - FLT 3014 - THROUGH 5000 FT ON CLIMB, THE NR 2 OVERTEMP WITH RED LIGHT TQ INCREASED TO 120 PERCENT. PERFORMED DOWNLOAD FDAU. FOUND NO RECORD OF EXCEEDANCES OF GE MM LIMITS. PERFORMED BORESCOPE OF ENGINE. NO DEFECTS NOTED. PERFORMED ITT SYSTEM CHECK. SDR EISA20000229Regulator · failedUNABLE TO MAINTAIN CABIN ALTITUDE BELOW 10,000 FT AUTO OR MANUAL AIR TURNBACK TO AUS. REPLACED LEFT PRESSURE REGULATOR PER MM 36-12-51.SDR AWXA0001137Thermostat · intermittentPHX - AIR TURNBACK - ON CLIMB, NR 1 ENG. BLEED FAULT OCCURED; A RESET WAS PERFORMED PER MAINTENANCE CONTROL AND BLEED WORKED, RETURNED TO NORMAL; A/C RETURNED TO PHX DUE TO POSSIBLE REPEAT AND WEATHER CONDITIONS IN DCA. MAINTENANCE TROUBLESHOT AND REPLACED THESDR RRXA001095Duct · failedCLIMBING THRU 12,000 FEET NR 2 ENGINE FIRE WARNING SOUNDED. SECURED ENGINE PER EWW QRH. UPON INSPECTION OF ENGINE FOUND HIGH STAGE BLEED DUCT CRACKED AT FLEX COUPLING. REMOVED AND REPLACED HIGH STAGE BLEED DUCT IAW DC-8 M/M CH 36-11-61 AND FIRE WARNING CHECSDR 20010402CW002Manifold · malfunctionedON LT ENGINE START, RED INDICATOR BUTTON RETRACTED, GAGE DROPPED TO ZERO. PNEUMATIC PUMP SUPPLIED PRESSURE BUT ON PRESSURE WAS GETTING TO GYRO FLIGHT INSTRUMENTS, DOOR SEALS, GYRO PRESSURE REGULATOR OR PRESSURE GAGE. RIGHT ENGINE SHOWED NORMAL INDICATOR AND
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