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 C2XA98CL055Valve · failedORF - FLT 3347 - CREW REPORTED THE LEFT ENGINE DUCT LEAK LIGHT ILLUMINATED IN FLIGHT AND REMAINED ILLUMINATED AFTER THE CHECKLIST WAS ACCOMPLISHED. THE LEFT ENGINE WAS SECURED AND THE AIRCRAFT RETURNED TO THE FIELD WITHOUT FURTHER INCIDENT. THE AIRCRAFT WAS SDR 98UAL900354Switch · failedNR 2 BLEED OVERHEAT LIGHT ILLUMINATED. RETURNED TO ORD. *S/D* REPLACED AIR DUCT OVER TEMPERATURE SWITCH.SDR 98FDEA00473Duct · failedCLIMBING THRU 10,000 FT GOT NR 1 ENG NACELLE TEMP ADVISORY, TEMP AT 95 CELSIUS. CLOSED BLEED, NO HELP. OPENED NR 1 BLEED AND RETARDED THROTTLE AND TEMP DECREASED. RESUMED CLIMB POWER AND TEMP AGAIN INCREASED TO 110C. FOUND HPT RECOUP DUCT BLOWN. REMOVED SDR TWRA9839Clamp · looseNR 1 ENGINE FIRE WARNING MOMENTARILY INDICATED ON CLIMB-OUT FROM TLV, RETARDED THRUST LEVER TO IDLE BEFORE ANY ACTION TAKEN. LIGHT/HORN EXTINGUISHED, OTHER INDICATIONS NORMAL. 'A' LOOP DROPPED TO NORMAL. 'B' LOOP CONTINUED TO RUN ABOVE 'A' LOOP. FOUND PNEUSDR 98FDEA00458Duct · broken98-0180 STA-MEM: SHORTLY AFTER T/O THE ENG 1 STRUT OVERHEAT LIGHT CAME ON. COMPLETE THE RED TAB PROCEDURES PAGES 2-7-10 AND 2-7-11 AND THE LIGHT EXTINGUISHED AFTER RETARD THE NR 1 THRUST LEVER NR 1 THRUST WAS SLOWLY RESTORED AND THE LIGHT REMAIN EXTINGUISH WSDR 98FDEA00457Duct · rupturedSTA-OAK: ON CLIMB 250 KTS/10000. ADVANCED THROTTLE FOR CLIMB AND NR 2 ENG FIRE WARNING ILLUMINATED B-LOOP WAS CHECKED AND TURNED OFF. LEVELED OFF THEN STARTED TO CLIMB AGAIN. FIRE WARNING ILLUMINATED AGAIN THEN GOT HOT AIR SUPPLY OVERHEAT. RETURNED TO OAKSDR VJ9800223Clamp · looseNR 1 ENGINE A-LOOP INDICATION INTERMITTENT DURING FLIGHT. REPLACED 13TH STAGE PNEUMATIC CLAMP AND REPOSITIONED. SUBSEQUENTLY, CHECKED SYSTEM, RECONNECTED CONNECTORS P1-824 AND P1-825 TO R5-27 AND R5-29 RESPECTIVELY. SYSTEM CHECKED GOOD IAW MM 26-10.SDR TWRA9837Clamp · looseFLT 92 - SJU-MIA - ON CLIMB, NR 1 ENGINE FIRE SWITCH ILLUMINATED AND FIRE BELLSOUNDED. ENGINE SHUT DOWN. WHEN START LEVER WAS CUT OFF THE FIRE SWITCH LIGHT STOPPED ILLUMINATION. NACELLE TEMP DROPPED. FIRE BOTTLE WAS NOT DISCHARGED. AIR TURN BACK TO SJU. SDR SCNA98072Modulating Valve · failedTHE NUMBER ONE ENGINE STRUT OVERHEAT LIGHT ILLUMINATED. LIGHT EXTINGUISHED FOLLOWING COM PROCEDURES AND AIRCRAFT DIVERTED TO ATL. THE NUMBER ONE ENGINE PYLON INSPECTED FOR LEAKS WITH NONE FOUND. BLEED VALVE AT 13TH STAGE FOUND CLOSED. REMOVED AND REPLACED SDR WRLA98088Line · looseDURING TAXI FOR DEPARTURE, FLIGHT CREW RECEIVED NR 1 ENGINE BLEED 'INOP ALERT'. FLIGHT CREW ELECTED TO RETURN TO GATE. AIRCRAFT RETURNED TO GATE WITHOUT FURTHER INCIDENT. NOTED ON LOG PAGE 100802. MAINTENANCE FOUND PNEUMATIC LINE LOOSE ON NR 1 ENGINE PNUEMSDR 98UAL900318Duct · leakingLOWER AFT BODY OVERHEAT WARNING WITH AN ELECTRICAL ODOR IN CABIN AND COCKPIT. ALSO, NR 2 ENGINE OIL TEMP REDLINE, CABIN EXCESSIVE TEMP. INFLIGHT SHUT DOWN OF NR 2 ENGINE. TEMP AND ELECTRICAL ODOR SUBSIDED. DIVERTED TO AKO. *S/D* FOUND LEAKING FLEX TUBE TSDR SWIA971215Valve · malfunctionedAFTER DEPARTURE WITH APU ASSIST TAKEOFF WHEN SWITCHING TO ENGINE BLEED, DUCT LEAK ILLUMINATED. LIGHT EXTINGUISHED AT 3 MINUTES. RETURNED TO SLC. REMOVED AND REPLACED LEFT SIDE PRESSURE VALVE WITH SERVICEABLE UNIT, IAW MM 30-10-06. OPS CHECKS GOOD.SDR MALA976161Bleed Pipe · crackedLEFT BLEED AIR LEAK DETECT ANNUNICATOR CAME ON, RESET VALVES PER QRH, NO CHANGE. AIRCRAFT RETURNED TO DTW. MAINTENANCE REPLACED CRACKED BLEED PIPE AT POSITION 18 ON LEFT SIDE. ALL CHECKS GOOD.SDR 9809806641Pneumatic Syst · failedDURING CLIMB, THE NR 2 ENGINE FIRE WARNING SOUNDED. SHUT DOWN THE ENGINE AND DISCHARGED THE FIRE BOTTLE. AIRCRAFT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REPLACED THE NR 2 ENGINE STARTER, CONSTANT SPEED DRIVE, STARTER SHUTOFF VALVE, HIGH STAGE VALVE, ASDR EISA98173Line · failedAFTER DEPARTURE FROM LAX, PASSING 4500 FT, NR 1 STRUT OVERHEAT LIGHT ILLUMINATED, PERFORMED CHECKLIST LIGHT EXTINGUISHED. FOUND LEAKING SENSE LINE AT 13TH STAGE MODULATION VALVE. REPLACED LINE, OPS CHECK GOOD PER MM 36-10-00, 36-12-00, NO OTHER LEAKS NOTED. SDR EISA98172Clamp · failedON CLIMB-OUT OF PDX AT APPROXIMATELY 4500 FT, NR 1 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED, AOM ABNORMAL ACCOMPLISHED. OVERHEAT LIGHT EXTINGUISHED AS SOON AS THROTTLE RETARDED. LIGHT REMAINED OFF REST OF FLIGHT, EVEN AFTER NR 1 THROTTLE RETURNED TO NORMAL. RSDR EISA98171Clamp · looseAFTER TAKEOFF FROM LAX WHILE CLIMBING THROUGH 5000 FEET, NR 1 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED, AOM ABNORMAL ACCOMPLISHED. OVERHEAT LIGHT EXTINGUISHED AS SOON AS THROTTLE RETARDED. LIGHT REMAINED OFF REST OF FLIGHT, EVEN AFTER NR 1 THROTTLE RETURNED TSDR EISA98170Clamp · looseAFTER TAKEOFF FROM MCI WHILE CLIMBING THROUGH 3200 FT, NR 1 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED. AOM ABNORMAL ACCOMPLISHED. OVERHEAT LIGHT EXTINGUISHED AS SOON AS THROTTLE RETARDED. LIGHT REMAINED OFF REST OF FLT, EVEN AFTER NR 1 THROTTLE RETURNED TO NOSDR 98FDEA00427Bleed Line · loose98-0165 STA-FLL: LWR AFT BODY OVERHEAT LIGHT ILLUM PASSING FLT LEVEL 20. THE LIGHT EXTINGUISHED 3 MIN AFTER CLOSING NR 1 ENG BLEED AND THE LEFT PACK AS DIRECTED IN CHECKLIST. THE INITIAL CONFIGURATION WHEN THE LIGHT ILLUM WAS BOTH PACKS ON NR 1 AND RIGHT NRSDR EISA98149Clamp · looseDFW - DURING CLIMB-OUT, NR 1 STRUT OVERHEAT LIGHT ILLUMINATED, REDUCED POWER, CLOSED NR 1 ENGINE BLEED PER ABNORMAL CHECKLIST, LIGHT EXTINGUISHED. TIGHTENED CLAMP TO DUCT. START LEAK TEST, OK FOR SERVICE IAW MM 26-14. (M)SDR USAASB98163Shut Off Valve · failedPIT - FLT 296 - CREW ADVISED VIA ACARS WERE ENCOUNTERING PROBLEMS WITH THE DUCT PRESSURES. AT CLIMB POWER, THE LEFT DUCT PRESSURE READS 80 PSI WHILE THE RIGHT READS 38 PSI. THE DECISIION WAS MADE TO DIVERT TO PIT. NO EMERGENCY WAS DECLARED AND THE FLIGHT LASDR 98FDEA00422Pack Valve · leakingCLIMBING THRU 17,000 LOWER AFT BODY HEAT LIGHT CAME ON. COMPLIED WITH PROCEDURES. LIGHT WENT OUT AFTER SECURING NR 1 BLEED. LEAK BETWEEN PACK AND BLEED VALVE ON NUMBER 1 ACCORDING TO PROCEDURE. RAN ENGINE DUPLICATING BLEED CONFIGURATION. CHECKED DUCTING CSDR CA980707028Hpsov · failed(CAN) TAKEOFF ABORTED AT 70 KNOTS DUE MASTER CAUTION SOUNDED AND EICAS MESSAGE R-HPSOV AND R-BLEED LT. A/C OPERATED PER MEL WITH R-HPSOV AND T/R LOCKED OUT. REPLACED HPSOV. A/C SERVICEABLE.SDR CKSA98353Clamp · looseAFTER TAKEOFF, NR 3 ENGINE FIRE DET LOOP B ILLUMINATED, SWITCHED TO A LOOP AND FULL FIRE WARNING EXPERIENCED. WHEN PULLING THROTTLE BACK ALL INDICATIONS EXTINGUISHED. FHB EMERGENCY PROCEDURES C/W, ENGINE SHUTDOWN. FOUND NR 3 ENGINE HIGH PRESSURE VALVE CLAMPSDR 98UAL900307Bleed Air · malfunctionedON CLIMB-OUT, BLEED AIR PROBLEMS DEVELOPED. RETURNED TO IAD.SDR VNAA9806013Valve · failedA CROSSBLEED WARNING MESSAGE OCCURED DURING THE TAXI FOR TAKEOFF. THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED AND REPLACED THE CROSSBLEED VALVE, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 36-11-10. OPERATION CHECKS WERE COMPLETED, AND THE AISDR COMA9860162Clamps · crackedAT 24 MONTH INSPECTION TASK 002-53-170-321, UNDER FLOOR BLEED AIR DUCT LAMPS (2) ARE CRACKED. REMOVED AND REPLACED CLAMPS.SDR 98UAL900272Duct · failedA BANG AND RUSHING SOUND OF AIR REPORTED COMING FROM AREA OF DOOR 4 CROSS AISLE. RETURNED TO GATE.SDR TWRA9836Clamp · looseAT START OF DESCENT TO SJU FROM FL 37,000 FEET, THRUST LEVER AT IDLE, LEFT WING OVERHEAT LIGHT CAME ON. ABNORMAL PROCEDURES FOR WING OVERHEAT COMPLETED, LIGHT WENT OUT AFTER 8 MINUTES. THRUST LEVER AT IDLE, SYSTEM NORMAL AND LIGHT NEVER CAME BACK ON. FOUND SDR DL73E981270Duct · crackedWITH APU BLEED OPEN POWERING RIGHT PACK LEFT WING BODY OVERHEAT LIGHT ILLUMINATED APU BLEED PLACED OFF AFTER DELAY LIGHT WENT OUT LATER F/A NOTICED BURNING SMELL IN MID CABIN AREA. FOUND APU BLEED LINE CRACKED JUST AFT OF APU BLEED VALVE. REPLACED BLEED DUCTSDR SI3R98010Housing · fracturedUPON RECEIPT OF UNIT, THE FOLLOWING CONDITIONS WERE NOTED AT INCOMING INSPECTION. FOR DESCRIPTION, (REF: CMM 36-12-06 PG 602). VALVE CAP WORN, ANTI-ROTATION TEETH BROKEN OFF, CHECK VALVE STOP WORN OFF. GUIDE TUBE FRACTURED INTO 2 PIECES. POPPET SHAFT TEETSDR GAIA9862AClamp · failedMKE - AFTER DEPARTING JUST PRIOR TO FLAP RETRACTION, THE NR 1 FIRE WARNING CAME ON. FIREWARNING LIGHT WENT OUT AFTER NR 1 THROTTLE WAS RETARDED. AIRCRAFT RETURNED TO MKE AND MADE UNEVENTFUL LANDING. FOUND 8TH STAGE BLEED VALVE, AFT CLAMP UNSECURED. SECUREDSDR RRXA98235Clamp · failedDURING CRUISE, RT MAN IND 22PSI WITH LT MAN TEMP NORM, NEXT NR 3 ENG EGT WENT OFF SCALE LOW, NEXT CAPTS STICK SHAKER WENT OFF, NEXT RT MAN TEMP WENT OFF SCALE HIGH WITH NO OVHT LITES COMING ON. ISOLATED S/O BLEED VALVES TEMP BEGAN TO DROP. NEXT NR 4 ALT LOW SDR COMA9860140Duct · failedLEFT HAND 14TH STAGE BLEED AIR DUCT FAIL WARNING. COULD NOT DUPLICATE DISCREPANCY. FUNCTIONAL CHECK OF SYSTEM FOUND NO DEFECTS.SDR AALA981159Clamp · failedMIA - FLT 1153 - AFTER TAKEOFF MIA, CREW RECEIVED A NR 2 FIRE WARNING AND THROTTLE BECAME JAMMED. DISCHARGED FIRE BOTTLES AND SHUT ENGINE DOWN. AIR INTERRUPTED AND LANDED MIA WITHOUT INCIDENT. REPLACED ENGINE DUE TO DAMAGE CAUSED BY BLOWN PNEUMATIC DUCT. PSDR AALA981135Clamp · looseBOS - FLT 1527 - AFTER TAKEOFF BOS, TAIL COMPARTMENT HIGH LIGHT ILLUMINATED. TAIL COMPARTMENT HIGH LIGHT EXTINGUISHED AFTER PACK SWITCH TURNED OFF. RETURNED BOS AND LANDED WITHOUT INCIDENT. REMOVED LEFT HAND AUGMENTATION VALVE CLAMP, CLEANED VALVE SURFACE. SDR USAABB98059Duct · rupturedPIT - FLT 8876 - CLIMBING OUT OF PIT, CREW RECEIVED THE EICAS MESSAGE 'L ENG OVHT'. CREW REDUCED POWER AND THE MESSAGE EXTINGUISHED. THE MESSAGE REAPPEARED WITH POWER APPLICATION. THE BLEED SYSTEM HAD NO EFFECT ON THE MESSAGE. CREW REDUCED LEFT ENGINE POWESDR SCNA98052Duct · leakingDURING CLIMBOUT, HAD A NUMBER THREE STRUT OVERHEAT LIGHT COME ON AND LEFT PACK WAS UNABLE TO KEEP PRESSURE. DIVERTED AIRCRAFT TO IAH. TIGHTENED LOOSE DUCT CLAMPS IN THE NUMBER THREE STRUT. RAN UP NUMBER THREE ENGINE TO POWER WITH NO MORE LEAKS DETECTED. GRSDR EISA98127Clamp · looseCLIMGING THROUGH 16,000 FEET AT 91 PERCENT N1, GOT A NR 1 STRUT OVERHEAT LIGHT OUT WITH THROTTLE RETARDED. SWAPPED NR 1 AND NR 3 BLEEDS PER AOM WITH NO RECURRENCE IN-FLIGHT. GENERATED FROM PILOT REPORT. TROUBLESHOT SYSTEM TO LOOSE CLAMP. TIGHTENED CLAMP. SDR USAASB98128Clamp · looseCLT - FLT 338 - FLIGHT DEPARTED CLT AND RIGHT PACK ON MEL. SHORTLY AFTER LIFTOFF, THE LEFT WING BODY OVERHEAT LIGHT ILLUMINATED. FLIGHT RETURNED TO FIELD AT CLT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND BLOWING HOT ASDR 98UAL900225Valve · failedDIVERTED TO SFO DUE TO A BLEED VALVE PROBLEM. *S/D* LEFT ENGINE BLEED SYSTEM WAS CLOSING OFF DUE TO TEMPERATURE. LEFT ENGINE FAN AIR MODULATING VALVE TEMPERATURE SENSOR AND LEFT ENGINE AIR BLEED OVERTEMP SENSOR REPLACED. NO PNEUMATIC WRITE-UPS SINCE DIVERSSDR BJNA980504Clamp · looseLEFT WING BODY OVERHEAT LIGHT ILLUMINATED, FOLLOWED QRH PROCEDURE AND AFTER A FEW MOMENTS THE OVERHEAT LIGHT WENT OUT. RETORQUED CLAMP ON INBOARD END OF AIR CLEANER AT FORWARD END OF LEFT A/C BAY PER BMM 36-19-11, GRUOND CHECKS NORMAL. (M)SDR 98UAL900219Manifold · failedOVERTEMP LIGHT WENT ON NR 1 ENG, EGT 945 DEG. REDUCED POWER DURING CLIMB TO APPROX 108 PERCENT N1 AND LIGHT WENT OUT. APPROX 500 FEET DURING CLIMB, BOTH ENG FIRE LOOP LIGHTS ILLUM AND WARNING HORN ALARM SOUNDED. CHECKLIST FOR ENG FIRE ACCP AND FIRE LIGHT WENSDR 98FDEA00377Clamp · loose98-0145, NUMBER 3 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED IN FLIGHT WITH WING ANTI-ICE OFF, LIGHT WENT OUT WHEN THROTTLE WAS RETARDED. RAN ENGINE FOUND CLAMP ON DUCT COMING FROM THE PRECOOLER LEAKING. TIGHTENED CLAMP, RAN ENGINE AGAIN LEAK CHECKED GOOD. OPESDR HALA9800137Controller · failedFLT 10 - LAX - DURING CRUISE NR 3 MANIFOLD FAIL LIGHT CAME ON TEMP ABOUT 190 DEGRESS PSI AT 10 AFTER SHUT OFF. REPLACED MANIFOLD FAIL DET CONTROLLER, THE PNEU MANIFOLD FAULT INDICATOR, NO FAULT NOTED, OPS CHECKED OK. ON ENG RUN. (M)SDR HALA9800131Seal · leakedFLT 114 - HNL - ON FLIGHT FROM HNL TO OGG, THE TAIL COMPARTMENT WARNING LIGHT ILLUMINATED. AIRCRAFT RETURNED TO HNL, WHERE AN UNEVENTFUL LANDING WAS MADE. REPLACED LT PERI SEAL DUCTS. FOUND BOTH ARM PERI SEALS LEAKING. REPLACED RT AND LT PERI SEALS. GROUNSDR EISA98118Clamp · looseDURING CLIMB-OUT, ENGINE NR 1 STRUT OVERHEAT LIGHT ILLUMINATED. REDUCING THRUST EXTINGUISHED LIGHT. GENERATED FROM PILOT REPORT. TROUBLESHOT FOUND 8TH STAGE DUCT CLAMP LOOSE, DUCT MISALIGNED, TIGHTENED AND ALIGNED CAMP, RAN ENGINE. NO LEAKS NOTED. (M)SDR EISA98117Clamp · looseDURING CLIMB-OUT, NR 1 STRUT OVERHEAT LIGHT ILLUMINATED. REDUCING THRUST PER ABNORMAL CHECK LIST EXTINGUISHED LIGHT. GENERATED FROM PILOT REPORT. REPOSITIONED AND TIGHTENED CLAMP ON PNEUMATIC DUCT NR 1 ENGINE. RAN ENGINE, LEAK CHECK GOOD. (M)SDR COMA9860127Bracket · chafedDURING 'C' CHECK, FOUND RIGHT ENGINE 14TH STAGE BLEED AIR DUCT INSULATION DAMAGED. REPLACED HEAT BRACKET.SDR EISA98114Duct · looseCLIMBING OUT NR 1 ENGINE STRUT LIGHT ILLUMINATED. FOLLOWED PROCEDURES IAW ABNORMALS, LIGHT EXTINGUISHED WITH POWER REDUCTION. GENERATED FROM PILOT REPORT. REPOSITIONED AND TIGHTENED CLAMP ON 8TH STAGE DUCT. LEAK CHECK GOOD ON ENGINE RUN UP. (M)
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