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 DXTA2024092200593Flow Valve · corrodedBLEED LOOP FAULT CYAN CAS: AT 43000FT CYAN BLEED LOOP FAULT CAS MESSAGE FOLLOWED SHORTLY AFTER WITH A RED PACK LEAK MESSAGE. FOLLOWING CHECKLIST WE DESCENDED AND AT AROUND 30000FT RED CABIN ALTITUDE ILLUMINED CAUSING PAX O2 MASKS TO DEPLOY. CORRECTIVE ACTION:SDR V7PA202402270001Pressure Valve · failedCREW REPORTED A LH ENGINE FIRE WARNING IN FLIGHT WHILE CLIMBING THRU 12,000 FEET.. PULLED THROTTLE TO IDLE AND WARNING STOPPED. CREW DECLARED EMERGENCY AND RETURNED TO TTN. MAINTENANCE PERSONNEL TROUBLESHOT THE DISCREPANCY AND FOUND THE LH ENGINE PRESSURE SHSDR CALA2024090500574Controller · faultyDUCT PRESSURE INDICATION L AND R POINTERS NOT THE SAME (SPLIT), WITH EITHER POINTER BELOW 18 PSIG DURING TAKEOFF, CLIMB AND CRUI SE; THE ENGINE IS THE BLEED SOURCE REMOVED AND REPLACED THE #2 ENG BLEED AIR REGULATOR (BAR) COMPLIED WITH. IAW AMM 36-11-03. STILLSDR DALA2024082708481Pneumatic System · contaminated(LOG 0519782) PACK AND PNEUMATIC SYSTEM CONTAMINATED WITH HYD FLUID. R/R AIR PRESSURE FILTER ASSY REF B737 AMM 29-09 REF B737 AMM 21-00 FOR CONTAMINATION REMOVAL FROM AIR COND SYS CLEANED AS REQUIRED R/R RECIR FILTERS REF B737 AMM 21-25 REMOVED DUCT RT PACK BESDR NACA202408270001Sense Line · looseR ENG HPSOV AND ASSOCIATED STATUS ON FINAL APPROACH, EICAS MESSAGE CLEARED AFTER 30 SECONDS. ACCOMPLISHED AIR SUPPLY MODULE BITE TEST FOUND NORMAL IAW MM 36-23-00, FOUND HPSOV SENSE LINE LOOSE, TIGHTENED RH HPSOV SENSE LINE IAW AMM 36-11-07 THUMB TEST GOOD.SDR HALA20240820234Sense Line · misinstalledETOPS - WHILE PERFORMING T/C E36-24-01-32 FOUND HPV SENSE LINE & UNION CROSS THREADED. INSTALLED NEW MUSCLE SENSE LINES FOR HPV PER AMM 36-11-49 OPS CHECK & LEAK CHECK GOOD IDLE RUN SUCCESSFULSDR 2024F00198Regulator · failedQRF TO SLCB AFTER TAKEOFF DUE TO DUCT PRESSURE DROPED TO CERO (CROSSIING 15.000FT) AND THE RIGHT DUCT WAS UNNABLE TO MANTAIN PRESSURIZATION CONTROL. CLIMB 1000FT/MIN. CORRECTIVE ACTION: AT ENGINE #1 WAS REPLACED BAR AND PERFORMED PRESSURIZATION CONTROL SYSTEM SDR CVGA20240812001Pneumatic System · malfunctionedL-R BI AIR FAIL, AT FL190 L-R BLEED AIR CAS ANNUNCIATION ILLUMINATED, PULLED OUT PILOT CHECKLIST AND FOLLOWED THE PROCEDURE. CABIN CLIMBED TO 10,500FEET ON THE DESCENT TO 9000FT WHERE CABIN WAS TOTALLY UNPRESSURIZED. LANDED AT NEAREST SUITABLE AIRPORT. EMERGENSDR CALA2024081200405Shutoff Valve · faultyENGINE NUMBER ONE ENG ANTI ICE LIGHT ILLUMINATED IN FLIGHT. FOUND E1 PI SENSOR FAULT 36-21010. PLACED ON MEL IAW CARD 36070. REMOVED AND REPLACE PRSOV IAW 36-11-04. NO HELP WITH ISSUE. FURTHER TROUBLE SHOOTING REQ.SDR DALA2024073007638Union · leakingSHIP 5049 - DIV - TO BWI DUE TO AIR R WING LEAK ECAM MESSAGE. CORRECTIVE ACTION: FOUND LEAK AT PNEUMATIC CONNECTOR UPSTREAM OF WAI VALVE. REPLACED TAPPING SEALS AT THIS CONNECTOR AND DUCT ASSEMBLY. NO LEAKS NOTED. (LP 6081992)SDR AALA202407300088Regulator Valve · low pressureAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: IMMEDIATELY AFTER TAKEOFF, NOTICED LEFT PNEUMATIC DUCT PRESSUREWAS LOW INDICATING APPROXIMATELY 5PSI. NO ASSOCIATED PNEUMATIC ANNUNCIATIONS OCCURRED. AIRCRAFT CABIN PRESSURIZED NORMALLY; AIRCRAFT AIR INTSDR AALA202407306695Bleed Valve · low pressureAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: IMMEDIATELY AFTER TAKEOFF, NOTICED LEFT PNEUMATIC DUCT PRESSUREWAS LOW INDICATING APPROXIMATELY 5PSI. NO ASSOCIATED PNEUMATIC ANNUNCIATIONS OCCURRED. AIRCRAFT CABIN PRESSURIZED NORMALLY; AIRCRAFT AIR INTSDR 4DPA2024072300001Thermostat · failedCREW REPORTED CLIMBING THROUGH 10,000, BLEED 2 LEAK MASTER WARNING. RAN QRH AND MSG DISAPPEARED AFTER 3 MINS. REPOSITION FLIGHT, SO NEVER CLIMBED ABOVE 12,000. CAB ALT REMAINED AT 800 AT ITS HIGHEST, ON SCHEDULE. NO OTHER ISSUES AND CONTINUED THE REPOSITION. CSDR MASA2024071500085O-Ring · inoperativeLT BLEED DUCT WARNING MESSAGE IN FLT/R&R 90 DEGREES PIPE ASSEMBLY O-RING ON ACM, OPS CHECK GOOD.SDR DALA2024071707217Clamp · looseSHIP 3224- PRES/DIV - TO FSD DUE TO LOSS OF PRESSURIZATION (CAB PR EXCESS CAB ALT AND AIR ENG 2 BLEED LEAK ECAM MESSAGES). CORRECTIVE ACTION: FOUND MULTIPLE BLEED LEAKS. PRV CLAMP LOOSE, PRSOV CLAMP, OVER PRESSURE VALVE FLAPPER COVER LOOSE PER A320 AMM 36-11. SDR HNAA2024070900536Thermostat · faultedBLD 2 VLV CLSD AFTER TAKEOFF MSG CLSD AFTER LANDING. FACT 09JUL24 00:03 PHL T/S IRW FIM 36-00-810-808-A DUE TO CMC PRECOOLER 2 TEMP CTL SYS FAIL MSG. R/R E2 FAN AIR CONTROL THERMOSTAT IAW AMM 36-11-06 R/R E2 BLD VLV IAW AMM 36-11-05 PERFORMED OPS CHECK IAWSDR DALA2024070806895Pneumatic System · leakingSHIP 3137 PNEUMATIC LEAK ON AIR CYCLE MACHINE RH PACK. CORRECTIVE ACTION: REPLACED AIR CYCLE MACHINE RH PACK PER A319 AMM 21-52-21-000-001-A. (0430943)SDR DXTA2024070312250Duct · blownAT 39,000 FEET WHILE IN CRUISE WE HEARD A LOUD BANG. AT THAT TIME, CABIN ALTITUDE BEGAN RISING 750' PER MINUTE. WE WERE AT AROUND 9.0 PSI DIFFERENTIAL AROUND 6000 FEET CABIN ALT. WITHIN MINUTES WE KEPT CLIMBING TO 14000' CABIN ALTITUDE. EMERGENCY DESCENT ANDSDR YENA2024070100929Sense Line · brokenFLT#2468, CHS-BOS. (AIRCRAFT DIVERTED TO JFK). 'BLEED 2 FAIL AT 3000 FEET RESET WORKED THEN CAME BACK; FOUND PRSOV SENSE LINE TO BE BROKEN REMOVED AND REPLACED PRSOV SENSE LINE REF AMM 36-11-03. OPS CHECK OK. ENG #2 BLEED SUPPLY OK.'SDR HALA20240617161Clevis · faultedETOPS - ENG 1 BLEED FAULT AFTER ENG START. REMOVED AND REPLACED CLEVIS AND SCREW PIN OF ELECTROPNEUMATIC ACTUATOR ON ENG1 PERFORMED OPS TEST OF BMC 1 TEST PASSED. PERFORMED ENG RUN OF ENG 1 NO ECAM MESSAGES ENG RUN GOOD OK TO CONTINUE PER AMM 36-11-504-400-802SDR YENA2024062500904Sense Line · faultedFLT#278, SFO-FLL. (ETOPS) 'CLASS II AIR BLEED ( CLASS II MAINTENANCE MESSAGES DISPLAYED ON ECAM STATUS PAGE OF ECAM SYSTEM DISPLAY 1) FAULT(S) INDICATED BY AIR BLEED ); DURING TROUBLESHOOTING ECS BLEED LINE TO PYLON (FWD) WAS LEAKING. PER TSM 36-11-00-810-A15-SDR DALA2024060405754Seal · leakingSHIP 5012 - ATB - DUE TO AIR L WING LEAK ECAM MESSAGE. CORRECTIVE ACTION: FOUND LEAK COMING FROM TAPPING SEALS ON LEFT WING ANTI-ICE DUCT. R/R TAPPING SEALS AT LEFT WING ANTI-ICE DUCT. NO LEAKS NOTED. (LP 5662400)SDR DXTA2024060311936Unknown · odorWHEN BLEEDS ARE SWITCHED FROM APU TO ENGINES AFTER TAKEOFF THERE IS AN ODOR FOR ABOUT 5-10 MINUTES FROM THE AIR VENTS PAX SAID IT WAS A SMOKY TYPE ODOR CAN BE SMELLED ON CABIN AND COCKPIT. RAN ENGINES BEFORE AND AFTER INSPECTIONS, APU START UP AND RUN WAS NORMSDR NACA2024052000003Shutoff Valve · failedR ENG HPSOV APPEARED ON EICAS NUMEROUS TIMED BELOW 10,000' ON ARRIVALS. REPLACED #2 ENG HPSOV IAW AMM 36-11-07. OPS CHECK AND LEAK CHECK GOOD. UNIT UNKNOWN TO TRAXSDR NACA2024052000001Sensor · failedAPU PNEUMATIC AIR NOT WORKING. DEFERRED PER MEL 49-11-01-A. PERFORMED FIM FAULT TREE 49-11-987. FOUND P2 SENSOR FAILED. REMOVED AND REPLACED P2 SENSOR, TEST OK IAW AMM 49-61-04.SDR YENA2024052100770Seal · leakingFLT#2672, TPA-EWR. 'LEVEL 2 CABIN ODOR EVENT DURING CRUISE/ DESCENT DID NOT RESOLVE ON EITHER PACK AFTER FOLLOWING ISOLATION GUIDE. ODORS OBSERVED BY ALL FLIGHT CREW AND PERSISTED UNTIL LANDING; FOLLOWED TSM 71-00-00-810-801-A. FOR SMOKE AND OIL SMELL IN THE CSDR CALA2024052001517Warning Message · illuminatedL ENG BLEED OFF CAS AFTER ENG START BLEED PSI PULSING UP AND DO WN 15 PSI DEBRIEF CREW. LEFT ENG BLEED PULSING AT ENG START WITH BLEED OFF INDICATION. EVEN WHEN ADDING POWER STILL PULSING. EVENTUALLY BLEED OFF INDICATION EXTINGUISHED BUT ENGINE BLEED STILL FLSDR I5PA2024051775703Pilot Valve · inoperativeFLT NO: N/A (MX INSP.) ESI - R ENG HPSOV SEURED CLOSED. MEL 36-11-02. R/R R ENG HS PILOT PER AMM 36-11-08. OPS CHECK NORMAL.SDR NACA2024050300001Pneumatic System · low pressureAPU PNEUMATIC PRESS DROP TO 10 PSI. PERFORMED APU INSPECTION AND FOUND TUBINE BLADES BROKEN. REMOVED AND REPLACED APU IN REF AMM 49-11-01 NO LEAKS ALL NORMAL.SDR NACA2024050100001Controller · no testPERFORM RH AND LH PNEUMATIC HEALTH CHECK. PERFORMED RH AND LH PNEUMATIC HEALTH CHECK IAW AMM 36-00-22. REPLACED HPC PN# 773289-15 SN# 200008067 4659FH 1488 FC. REPLACED PRVC PN# 792755-16 SN# 910169 FH AND FC UNKNOWN. REPLACED PRV PN# 820170-10 SN# A95030012 4SDR CALA2024042901263Sense Line · leakingL ENG BLEED OFF EICAS MSG ON TO ROLL REJECT TO AT APPROX 75KTS PERFORMED HEALTH CHECK ON FAN AIR MODULATING VALVE REF. TO AMM 36-00-23-705-153-001. FAN AIR TEMPERATURE SENSOR FAILED THE HEALTH CHECK. RECOMMENED CHANGING THE FAN AIR TEMPERATURE SENSOR. FOUND SESDR JJBA20240422059Valve · inoperativeBLEED 1 AND 2 OVERTEMP MESSAGE ON EICAS. REMOVED AND REPLACED LH FAN VALVE AND CLEANED RH FAN AIR VALVE FILTER. OPS/LEAK CHECK SATSDR DALA2024041704517Engine · contaminatedSHIP 6822 LAST 30 MIN OF FLIGHT COCKPIT AND CABIN EXPERIENCED WET SOCK TYPE ODOR. CORRECTIVE ACTION: PERFORMING BSI OF #1 ENGINE. FOUND OIL EVIDENCE IN 2.5 BLEED PORTS. REMOVED AND REPLACED RECIRCULATION FILTERS PER B757 AMM 21-25. REPLACED NO. 1 ENGINE IN ACCSDR CALA2024040800998Pressure Valve · inoperativeR BLEED OFF EICAS ON IN CRUISE. RESET OK. LOCKED DUE TO DIVERSION UNLOCKED AFTER REPLACEMENT OF PRSOV CREW REPORTS BLEED TRIPPED OFF AGAIN AND WOULD NOT RESET. WITH BLEED SWITCH IN OFF POSITION " BLEED OFF" AND "PACK OFF" LIGHTS ILLUMINATED YET RIGHT DUCT PRESSDR ABXA2024032766Shutoff Valve · inoperativeRT ENGINE HPSOV MSG DURING CRUISE FLIGHT. (REASON FOR DIVERSION TO IND: HPSOV MESSAGE (NO ICING)- ICING AT CVG/JFK) ACCOMPLISHED THUMB TEST ON HPSOV FROM CONTROLLER SIDE OF SENSE LINE, NO FAULTS PRESENT. REPLACED HPSOV IAW B767 AMM 36-11-07 AND RH BLEED CONTROSDR NACA2024022700001Shutoff Valve · warning messageR ENG HPSOV EICAS MSG. DEFERRED R ENG HPSOV IAW MEL 36-11-02-02 CAT C ON 2/28/24@0325ZSDR HALA20240220045Valve · inoperativeETOPS - ENG 2 PRV INOP. REMOVED & REPLACED #2 ENG PRV IAW AMM 36-11-52-000-804-A & 36-11-52-400-804-A OPS CHECK GOOD NO FAULTS NOTED.SDR NACA2024020900002Isolation Valve · failedISOLATION VALVE EICAS MESSAGE. NO DUCT PRESSURE. REPLACED CENTER ISOLATION VALVE IAW AMM 36-11-04 OPS CHECK GOOD. PART UNKNOWN TO TRAX.SDR DALA2024020601620Seal · leakingSHIP 1028 - DIV - TO PHX DUE TO AIR R WING LEAK ECAM MESSAGE. CORRECTIVE ACTION: FOUND LEAK AT CLAMP BETWEEN OZONE CONVERTER AND FLOW CONTROL VALVE, AND AT CLAMP BETWEEN ACM AND SECONDARY HEAT EXCHANGER. REPLACED SEALS. LEAK CHECK GOOD. (LP 5398286)SDR NACA2024020500005Warning Message · intermittentLEFT ENG HPSOV EICAS MESSAGE INTERMITTENT. PERFORMED TS IAW FIM 36-20 FT 804. NO DISCREPANCIES NOTED. NO MX OR STATUS MESSAGE NOTED.SDR HALA20240205037Transducer · faultedETOPS - AIR ENG L HPV NOT OPEN ANNUNCIATION UPON DESCENT. REMOVED AND REPLACED ENGINE #1 BLEED TRANSFERRED PRESSURE-TRANSDUCER, PE RAMM 36-11-15. BITE TEST AND LEAK CHECK GOOD. OK FOR SVC. REMOVED AND REPLACED #1 ENGINE HP VALVE, PER 36-11-51. OPS AND LEAK CHESDR YENA2024012200077Valve · failedFLT#2334, PBI-DCA. (AIRCRAFT PERFROMED AN AIR TURN BACK TO PBI) 'BLEED 2 FAIL; PERFORMED FIM TASK 36-11-00-810-816-A, FOUND FAN AIR VALVE AT FAULT. REMOVED & REPLACED FAN AIR VALVE W/ REF TO EMB AMM 36-11-09. OPS CHECK GOOD, A/C OK FOR SERVICE.'SDR NACA2024011800001Shutoff Valve · intermittentR ENG HPSOV EICAS INTERMITTEINT IN CRUISE. STATUS MESSAGE REMAINED AFTER SHUTDOWN. PERFORMED FIM 36-00 FAULT TREE 803 NO FAULT FOUND.SDR SCNA20240116014Unknown · odorDEFECT 765927: - - FLT ATTENDANTS REPORT BURN RUBBER SMELL THROUGHOUT THE CABIN. - - RESOLUTION: (IN PROGRESSSDR CALA2024011000075Duct · damagedBLEED LOSS BODY EICAS ON TAKEOFF ROLL. FOUND BLOWN PNEUMATIC DUCT IN THE LH MAIN WHEEL WELL, SEE ATTACHED IMAGE. MINIMUM REQUIRED PARTS HIGHLIGHTED, UNTIL FURTHER EVALUATION IS ACP. INITIAL EVALUATION PARTS INFO ADDED. REF IPC 29-11-16-01 ITEMS 100 AND 105, ASDR NACA202401040003Unknown · unknownDUCT PRESSURE FLUCTUATES BETWEEN 20 AND 40 LEFT AND RIGHT DURING CLIMB AFTER TAKEOFF. PERFORMED PNEUMATIC HEALTH CHECK TO FAN VALVE FOUND NORMAL PER AMM 36-00-21SDR I5PA2023122288802Valve · failedFLT NO.: N/A (MX FINDING). ESI - LEFT ENGINE HIGH STAGE SYSTEM PNEUMATIC HEALTH CHECK REQUIRED. ACCOMPLISHED PNEUMATIC HEALTH CHECK OF THE LH HPSOV AND HS PILOT PER AMM. HS PILOT FAILED. REPLACED PER AMM.SDR DALA2023122110481Unknown · unknownSHIP 3357 - ATB/DE - DUE TO AIR ENG 1 BLEED FAULT. CORRECTIVE ACTION: T/S. FOUND DEACTIVATION SCREW ON FAV LOOSE AND ORING DAMAGED. REPLACED FAV, PRSOV AND FAN AIR THERMOSTAT. (5151360)SDR CALA2023122103707Sensor · faultyDURING CLIMB/CRUISE L DUCT PRESSURE 15PSI AND R DUCT PRESSURE 41 . SENSOR, PRECOOL OFF 29-3626-9-9001 0008 ON 0000 SENSOR, PRECOOL OFF 29-3626-9-9001 0008 ON 29-3626-9-9001 1039 PERFORMED #1 ENGINE PNEUMATIC HEALTH CHECK PER AMM 36-11-00-700-801 IN CONJUNCTIONSDR YENA2023112901502Unknown · unknownFLT#2220, LHR-JFK. (ETOPS) 'ENG 1 OVER PRESSURE VALVE LEAKING AIR FROM LOWER CLAMP WITH APU BLEED AIR ON; REPLACED ENG 1 OVER PRESSURE SEAL PER AMM 36-11-53. OPS CHECK GOOD OK FOR SVC.'FLT#2220, LHR-JFK. (ETOPS) 'ENG 1 OVER PRESSURE VALVE LEAKING AIR FROM LOWE
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