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 ASMD200704013Augment Valve · failedRT PNEUMATIC SYSTEM FAILED DURING CLIMB, SO RT PNEUMATIC CABIN DEPRESSURIZED AND PASSENGERS OXYGEN MASKS WERE ACTIVATED. CAPTAIN PERFORMED ABNORMAL PROCEDURE DESCENDING AT 25,000 FEET. DURING MAINTENANCE CHECK, THE OXYGEN MASKS AND 25 OXYGEN GENERATORS WERE DESDR HALA0700173Pneumatic System · unknownETOPS SIGNIFICANT SYSTEM, LEFT PNEUMATIC SYSTEM IS NOT BEING PRESSURIZED BY L ENGINE. PERFORMED BITE OF AIR SUPPLY MODULE NO FAULTS NOTED. OPS CHECK OF L PNEUMATIC SYSTEM OPERATES NORMAL PER FIM 36-10-00 FIG 15 SHEET 1.SDR HALA0700175Unknown · unknownETOPS SIGNIFICANT SYSTEM, ON DESCENT LEFT ENG BLEED LIGHT ILLUMINATED AND L ENG PRV EICAS MSG ILLUMINATED. TURNED OFF LEFT ENG BLEED AIR SWITCH AND LEFT PACK CONTROL SELECTOR. PERFORMED TEST PER FIM 36-10-00 FIG 123. OPS CK'S NORMAL. NO FAULTS. NO MSG'S.SDR SWAA071861Duct · crushedAT FL 240, CABIN ALT HORN SOUNDED, ALT CLIMBED TO 15,000 FT AND MASKS DEPLOYED. FOUND AFT PRESSURE BULKHEAD APU PNEUMATIC DUCT CRUSHED. REMOVED AND REPLACED AFT PRESSURE BULKHEAD APU PNEUMATIC DUCT PER MM.SDR SIMA200710608Shutoff Valve · failedLEFT COWL ANTI-ICE DUCT WARNING ILLUMINATED, ENGINE SHUTDOWN. EMERGENCY DECLARED, DIVERTED TO BNA. REMOVED AND REPLACED PRESSURE SHUTOFF VALVE IAW CRJ AMM 36-12-05 WITH NO DEFECTS NOTED. REMOVED AND REPLACED LEAK TRANSDUCER IAW CRJ AMM 30-22-03 WITH NO DEFESDR HALA0700167Unknown · unknownETOPS SIGNIFICANT SYSTEM, LEFT PNEUMATIC SYSTEM IS NOT BEING PRESSURIZED BY L ENG. CYCLED L ENG VALVE SWITCH AND L PNEUMATIC SYSTEM OPERATES NORMAL PER FIM 36-10-00 FIG 115 SHEET 1.SDR DL76G070314Line · disconnectedON T/O ROLL AT 70KTS, HAD R ENG PRV CAUTION MESSAGE AND BEEPER. ABORTED T/O. FOUND SENSE LINE FROM PRC DISCONNECTED. SECURED LINE.SDR DXTA200702099Warning Light · illuminatedON TAKEOFF ROLL HP DUCT OVERPRESS RT AMBER CAS MESSAGE CAME ON AND REMAINED ON. [SUP 4-19-07] REMOVED AND REPLACED OVER OVER PRESS SWITCH IAW 760 MM 30-10-00 OPS END LEAK CHECK GOOD.SDR ASMF200704007Valve · failedAIRCRAFT AIR-TURNED BACK DUE TO RT ENGINE BLEED TRIP OFF LIGHT, TURNED ON. AT CUU, TECH PERSONNEL DEFERRED REPORT IAW MEL 36-8. DURING OVERNIGHT CHECK; RT HIGH STAGE PRECOOLER VALVE WAS REPLACED IAW MM 36-11-06, TESTED CORRECT. OVERWEIGHT INSPECTION WAS NOT RESDR HALA0700161Line · looseETOPS SIGNIFICANT SYSTEM, L ENG PRV WARNING CAME ON SEVERAL TIMES DURING DESCENT FRM FL 380. TROUBLESHOT PER FIM 36-10-00 FIG 123. FOUND LOOSE SENSE LINE TO PRE-COOLER. TIGHTENED LINE, RAN ENGINE AND PERFORMED OPERATIONAL TEST OF PRV PER AMM 36-11-18/501. SDR RAIA00704024O-Ring · damagedFLT 5496 - STL - FAILED PART 2, ANTI-ICE TEST FOLLOWED BY BLEED LEAK ENGINE 1 & 2 AND WING BURST MESSAGE. MAINTENANCE REMOVED AND REPLACED BLEED O-RING & CLAMP AT JOINT NR 10 DUE TO CLOSE PROXIMITY CAUSED BLEED 1 AS WELL. NO FURTHER LEAKS NOTED.SDR SIMA200709909Duct · crackedNUMBER 1 BLEED LEAK OCCURRED CLIMBING THROUGH 13,000 FEET, RETURNED TO ORD. REMOVED AND REPLACED T-DUCT BEHIND LEFT SIDE WALL IAW EMB 36-11-09. OPERATIONAL AND LEAK CHECK GOOD. RETURNED AIRCRAFT TO SERVICE.SDR 2007FA0000315Mixing Valve · out of toleranceDURING TAKEOFF ROLL CREW EXPERIENCED A RUSH OF WARM OILY SMELLING AIR IN THE COCKPIT. CREW ABORTED TAKEOFF AND RETURNED TO BASE. MAINTENANCE CREW RAN AIRCRAFT AND DUPLICATED PROBLEM FINDING THE DUCT OVRHT LIGHT AND LT BLEED LIGHT ON AT FULL POWER. FURTHER TROUSDR ABXA070073Flange · looseON CLIMBOUT, EICAS MESSAGE LEFT ENGINE OVERHEAT DISPLAYED WITH ENGINE OVERHEAT LIGHT ILLUMINATED. LIGHT REMAINED ILLUMINATED AFTER THRUST REDUCTION. ENGINE WAS SHUTDOWN. DID AIR TURNBACK TO STA SAL. OPENED NR 1 ENGINE COWL, INSPECTED BLEED AIR DUCTING. FOSDR CA070316002Line · broken(CAN) DURING ANNUAL INSPECTION, THE BLEED AIR LINE FOR THE CABIN HEATER WAS FOUND UNSECURED UNDER THE COCKPIT FLOOR. FURTHER INVESTIGATION FOUND THE MUFFLER FOR THE LINE BROKEN IN (2) PIECES AT THE FWD END. THE PARTS WERE REPLACED. THE REMAINING AIRCRAFT IN THSDR C1HA200778001Line · looseON CLIMB-OUT FROM DEN, NR 3 EPR STARTED SURGING UP AND DOWN 10 TO 15 PERCENT, SHUT OFF RT PACK, SURGING STOPPED. MADE PRECAUTIONARY LANDING BACK IN DEN CONFIRMED FAULT FOUND 10 SENSE LINES LOOSE ON RT FLOW CONTROL VALVE. TIGHTENED PER STD PRACTICES REF MM 36SDR 752006Regulator Valve · leakingNR 1 ENGINE MAXIMUM TAKEOFF POWER. PILOT'S PANEL ENGINE LOOP FAULT LIGHT ILLUMINATED INTERMITTENTLY FOLLOWED BY INTERMITTENT FIRE WARNING. NACELLE TEMPERATURE FLUCTUATED 5 TO FULL SCALE. SET CLIMB POWER. NACELLE TEMPERATURE A & B SETTLED TO 2.0. TAKEOFF POSDR MALA070051Tube · leakingRIGHT BLEED AIR LEAK CAUTION LIGHT ILLUMINATED. CLOSED BLEED VALVE AND BLEED AIR LEAK CAUTION LIGHT WENT OUT. CND PROBLEM. LEAK CHECK RIGHT BLEED SYSTEM. NO LEAKS FOUND. PER ENGINEERING REQUEST, REPLACED RIGHT BLEED TUBE. OPS AND LEAK CHECK GOOD.SDR COMA0760247Isolation Valve · failedFLIGHT 5199 - DURING CRUISE FLIGHT THE 10TH STAGE ISOLATION VALVE FAILED TO CLOSE. PERFORMED AN OPERATIONAL CHECK OF THE 10TH STAGE ISOLATION VALVE, DISCREPANCY COULD NOT BE DUPLICATED BY MAINTENANCE.SDR MALA070040Duct · leakingAIRCRAFT DID AN AIR RETURN FOR THE RT BLEED LEAK INDICATION COMING ON AFTER TAKEOFF. THE CREW FOLLOWED THE QRH AND LANDED WITHOUT FURTHER INCIDENT. REMOVED AND REPLACED RT ELBOW AT FWD DUCT (RED HOSE) IAW AMM 21-20-00. OPS CHECK GOOD.SDR NWAA070983263Seal · damagedAT FLIGHT LEVEL 190, AIR R WING LEAK ANNUNCIATED. LOST PRESSURIZATION DUE TO LEFT PACK PREVIOUSLY PLACED ON MEL. PER COM PROCEDURE AN EMERGENCY WAS DECLARED AND EMERGENCY DESCENT EXECUTED. SHORTLY FOLLOWING THE BLEED FAULT EXTINGUISHED, WITH SYSTEM RECOVERINSDR SIMA200706404Actuator · wornVIBRATION FELT IN BOTH IN CABIN AROUND ROW 6 AND FLIGHT DECK, NO VIBRATION IN FELT IN CONTROLS. REMOVED AND REPLACED NR 1 RAM AIR VALVE ACTUATOR ASSEMBLY, LEFT EMERGENCY VENT VALVE ASSEMBLY AND RIGHT EMERGENCY VENT VALVE ASSEMBLY IAW EMB AMM. OPERATIONAL CHESDR AMTA200700110Shutoff Valve · malfunctionedLT ENGINE BLEED OFF LIGHT ILLUMINATED AT TAXI INTO INDY WITH ASSOCIATED EICAS MSG. REPLACED PROSOV AND HIGH STAGE PILOT IAW AMM. RAN LT ENGINE, OPS CHECKED LT BLEED REF MM. BLEED OPERATION NORMAL. (K)SDR 2007FA0000294Mixing Valve · intermittentSHORTLY AFTER TAKEOFF, AIRCRAFT (LT BLEED AIR) WARNING ILLUMINATED, AND (RT BLEED AIR) WARNING ILLUMINATED APPROX 5 SEC LATER, SMELLED ODOR IN MAINTENANCE. UNABLE TO DUPLICATE MALFUNCTION ON GROUND RUN; LT MIXING VALVE WAS SUSPECTED, SO REPLACED. PERFORMED GSDR 2007FA0000205Mixing Valve · intermittentSHORTLY AFTER TAKEOFF, AIRCRAFT (L BLEED AIR) WARNING ILLUMINATED, AND (R BLEED AIR) WARNING ILLUMINATED APPROX 5 SEC LATER, SMELLED ODOR IN CABIN. REDUCED POWER AND WARNING WENT OUT. AIRCRAFT DIVERTED FOR MAINTENANCE. UNABLE TO DUPLICATE MALFUNCTION ON GROSDR 07FDEA00518Duct · disconnectedINTERMITTENT LEVEL 3 APU FIRE ALERT AFTER 150 EN ROUTE-SUSPECTED BLEED/DUCT LEAK-COMPLIED W/QRH, BOTTLE BLOWN. FOUND FLEX DUCT AT EXHAUST DISCONNECTED AND CLAMP MISSING, DUCT COMES FROM THE GEN COOLING SHROUD. RAN APU FOUND AIR LEAKING AT PRESS REG VALVE CLASDR 07FDEA00490Valve · malfunctionedNR 2 BLEED FAULT DURING CLIMB-OUT. FAULT DUE TO OVERHEAT. PRESSURED CHECKED MUSCLE LINE ON FAN AIR VALVE TO HP VALVE. CHECKED GOOD. REPLACED FAN AIR VALVE IAW MM 36-11-16-4-02. RAN NR 2 ENGINE AT POWER PER JRH. WITH ENGINE STABILIZED AT POWER THE BLEED PSDR CA070214005Line · broken(CAN) AFTER LANDING THE NR 1 PROP RPM WAS LOWER THAN NORMAL. MAINTENANCE FOUND THAT THE P3 LINE FROM THE P3 FILTER BOWL TO THE ENGINE WAS BROKEN PN 3035279. THE LINE WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. (TC NR 20070214005)SDR MALA070027Hose · rupturedRT BLEED AIR LEAK LIGHT CAUTION LIGHT ILLUMINATED DURING FLIGHT AT APPROXIMATELY 10,000, FT RAN THE QRH. CAUTION LIGHT WHEN OUT INITIALLY THEN CAME ON INTERMITTENTLY WITH BLEED AIR AND HP VALVES CLOSED, THIS CONTINUED UNTIL DESCENT, WHEN POWER WAS AT A LOW SESDR RAIA00702010O-Ring · wornFLT NR 5501 - STL - BLEED 2 LEAK INDICATION ON THE EICAS. MAINTENANCE REMOVED AND REPLACED THE BLEED LINE O-RINGS.SDR NOCA02907Shutoff Valve · malfunctionedLEFT REVERSER INTERLOCK STATUS MSG. REMOVED AND REPLACED NR 1 ENG PRSOV IAW MM 36-11-09. SYSTEM OPS CHECK OK.SDR UIEA20070039Duct · crackedNR 3 PYLON AIR VALVE INDICATES 10-PSI IN CRUISE WITH 95 PERCENT N1 SET IS NOT REGULATING CORRECTLY WITH ISOLATION VALVE OPEN. THE LEFT AND RIGHT MANIFOLD PRESSURE ONLY INDICATE 26-PSI. LEAK CHECK FOUND NO FAULT ON ENGINE AREA. SUSPECT CRACKED DUCT ON THE WISDR YENA2007004Valve · failedBLEED OVERPRESS AFTER T/O - BLEED NR 1 QRH PROCEDURE CLEARED MSG. A-I WING FAIL - EICAS MSG DURING CLIMBOUT. ACCOMPLISHED QRH PROCEDURE. MSG REMAINED. MSG CAUSED BY FAILURE OF FAN AIR VALVE REPLACED NR 1 ENG FAN AIR VALVE PER AMM 36-11-09. PERFORMED POWERSDR DL76L070062Shutoff Valve · unknownWITH LEFT HPSOV ON MCO. AFTER TAKEOFF LEFT ENGINE BLEED OFF STAYED ILLUMINATED.SDR DLM88070056Clamp · looseAFTER T/O OUT OF LGA. GOT A TAIL COMPARTMENT TEMP HIGH ANNUNCIATOR. RAN QRH AND LIGHT EXTINGUISHED WHEN LEFT THROTTLE RETARDED TO IDLE. DIVERTED TO JFK. REPOSITION CLAMPS ON LT AUGMENTATION VALVE, RETORQUE SAME. AS PER MM, PERFORM PROC 36-00-00201. AUG VSDR AWXA200700099Clamp · dislodgedFLIGHT 320: PHX - LAS - AT FL 240 NR 2 ENGINE (RT OVHT) ILLUM, EICA AND LOWER PANEL MSG. THE CREW COMPLIED W/QRH, SHUTDOWN NR 2 ENG, (CAPT STATED LIGHT EXTINGUISHED AFTER THROTTLE REDUCTION, AND ILLUMINATED AFTER POWERED BACK UP, THAT'S WHEN INITIATED AN IN-FSDR AALA20070074Line · looseMIA INFLIGHT T447/13JAN - LEFT ENGINE BLEED LIGHT ILLUMINATED ON TAKEOFF ROLL. WOULD NOT RESET. ENGINE BLEED RESET ON DESCENT. LANDED MIA WITHOUT INCIDENT. FOUND LOOSE LINE AT HIGH STAGE VALVE. SECURED LINE AND RESEATED CONNECTORS AT HIGH STAGE VALVE. SYSSDR RAIA00701018Duct · crackedFLT NR 5542-DSM-NR 1 BLEED LEAK INDICATION IN FLIGHT. MAINTENANCE REMOVED AND REPLACED THE BLEED DUCT SEALS AND REMOVED AND REPLACED THE T-DUCT.SDR 0700053274Thermostat · unknownAIR ENGINE NR 1 AND NR 2 BLEEDS FAULTED AT FLIGHT LEVEL 390. STARTED LOSING CABIN PRESSURIZATION, ATC CLEARED AND EXECUTED RAPID DESCENT, DURING WHICH CABIN ALTITUDE WENT TO 12500 FEET. BLEEDS RECOVERED AT 10,000 FEET. MASKS WERE NOT DROPPED, AND AIRCRAFT LSDR RYNA200700001Shutoff Valve · leakingAIR TURNBACK, AFTER DEPARTURE CLIMBING THROUGH FL370 LEFT BLEED TRIP LIGHT ILLUMINATED WHILE TRYING TO RESET, THE RIGHT BLEED TRIPPED. ALSO MANAGED TO RESET BOTH, BUT BOTH TRIPPED AGAIN. FINALY MADE AN AIR TURNBACK TO DTW. COMPLIED WITH FIM AND FOUND LEFT ESDR DL76G070016Isolation Valve · stuckL ISOLATION BLD VALVE EICAS MSG WITH OVERHEAD PANEL LIGHT ON. VALVE APPEARS TO BE OPEN. REPLACED L ISOLATION VALVE. VALVE WAS FROZEN IN MID POSITION RAN VLV, OPS NORMAL.SDR YENA200692Valve · failedENG 2 BLEED FAULT ON T/O, A/C CONTINUED FLIGHT. IN CRUISE, ENG 1 BLEED FAULT AT FL 360, NO LOSS OF CABIN PRESSURE, INITIATED EMERGENCY DESCENT. PER TSM TASK 36-11-54-05, FOUND NR 2 ENG FAN AIR VALVE AT FAULT, REMOVED AND REPLACED NR 2 ENG FAN AIR VALVE IAW ASDR AMTA200600740Control Valve · unserviceableHAD LT BLEED AIR TRIP OFF IN DESCENT, RESET OK IAW CHECKLIST. REPLACED PRECOOLER CONTROL VALVE. (K)SDR YENA200689Seal · leakingRIGHT BLEED AIR LEAK PASSING 10,000 FT. PERFORMED TSM TASK 36-22-00-810-802. FOUND ENGINE NR 2 BLEED DUCT SEAL LEAKING AT NR 2 ENGINE BLEED INTER RIB TO CLOSING RIB. REMOVED AND REPLACED DUCT SEAL IAW AMM 36-11-48. ALL OPS AND LEAK CHECK GOOD.SDR AMTA200600738Valve · unknownBLEED TRIP LIGHT WOULD NOT RESENT. REMOVED AND REPLACED PRSOV IAW AMM 36-11-04-4 RAN ENGINE AT HIGH POWER, OPS CHECK GOOD OK FOR SERVICE. (K)SDR 06FDEA04288Duct · rupturedT/O AT SJC NR 2 THROTTLE MUCH FURTHER FWD THAN 1 AND 3 EGT NR 2 CREEPING UP, MAX TEMP = 880' C PULLED NR 2 THROTTLE BACK EVEN W/ 1 AND 3 GOT FIRE WARN, THROTTLE IDLE. SHUT DOWN ENGINE, FIRED BOTTLE NR 1 AS A PRECAUTION. DIVERT TO KOAK. DURING T/O N2 FOR ALSDR AMTA200600735Shutoff Valve · unserviceableIN CRUISE, AT 390 FL, BLEED AIR DUCT LT INDICATORS SPLIT L=44, R=58, EPR NR 1=159, NR 2=158, N1 NR1 87.1, NR 2 87.9. REMOVED AND REPLACED PRSOV NR 2 ENG SYS CHECK NORMAL REF 36-11-09-2. (K)SDR C2XA06IA192Duct · blownDFW - FLIGHT 2536, THE CREW REPORTED AN ENGINE TWO FIRE INDICATION ON TAKEOFF. THE CREW SHUTDOWN THE NUMBER TWO ENGINE AS A PRECAUTION, AND RETURNED TO DFW WHERE THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, AND FOUND A BLOWN -Y- SDR UIEA200600305Relief Valve · faultyDURING CLIMB-OUT, NR 2 ENGINE FIRE WARNING. BOTH ENGINE NACELLE TEMPS ON NR 2 ENGINE READ 8.5. ALL OTHER INDICATIONS NORMAL. ENGINE FIRE HANDLE PULLED. FIRE LIGHT EXTINGUISHED AND NACELLE TEMPS RETURNED TO NORMAL. REPLACED NR 2 PRV PER AMM 36-11-19. REPLSDR SWAA064800Control Valve · faultyDIVERSION, RT BLEED TRIP OFF LIGHT ILLUMINATED DURING CLIMB, RESET, ILLUMINATED AGAIN. DURING CRUISE AT FL 390 CABIN WAS CLIMBING 200 FT PER MINUTE, DURING DESCENT CABIN CLIMBED AT 400 FT PER MINUTE, AUTO DID NOT APPEAR TO MAINTAIN CABIN ALT. FERRY FLIGHT TO
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