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 2008UALA06411Shutoff Valve · faultyWITH RIGHT ENGINE BLEED SELECTED DO NOT GET GREEN BAR ON AIR PAGE TO OPERATE PACKS. PRSOV VALVE OPENS ONLY. STATUS MESSAGE R PRSOV BLEED. MAT MESSAGE 36-10380. FOUND R PRSOV MUSCLE LINE GALLED. REPLACED R PRSOV AND R PRSOV CONTROLLER. ENGINE RUN RIGHT BLESDR UALA2008111306359Duct · crackedWING BODY OVERHEAT LIGHT. RT FL DUE TO INCLEMENT WEATHER AT PLANNED DESTINATION. FAULT RECURRED ON NEXT FLIGHT OUT. PERFORMED TROUBLE SHOOTING, INTERROGATED M237 MODULE AND FOUND CODE 24 INDICATING LT A-C BAY OVERHEAT. INSPECTED LOOP AND COMPARTMENT. FOUND LASDR LR7A08122Duct · blownDURING CLIMB, FLIGHT CREW NOTED NR 3 ENGINE NACELLE OVERHEAT ANNUNCIATION AND PERFORMED ENGINE SHUTDOWN IAW AFM AT 14:28Z. REPLACED UPPER BLEED AIR MANIFOLD ON NR 3 ENGINE, LEAK CHECK GOOD PER SMP581 CH 36-10.SDR SWIA200820303Shutoff Valve · malfunctionedLEFT 14TH STAGE DUCT WARNING MESSAGE ON DESCENT, SECURED ENGINE. (FLT 4785)REPLACED LEFT PRSOV AND 14TH STAGE VALVES.SDR UALA2008111306307Regulator · blockedLOSS OF ALL WATER PRESSURE. FLIGHT DIVERTED. FOUND BLEED AIR PRESSURE REGULATOR BLOCKED. CLEANED AND NOW WATER PRESSURE TO LAV AND GALLEY NORMAL.SDR C2XA08RI165Switch · defectiveFLIGHT 2473 - EWR - FLIGHT CREW REPORTED NR 2 BLEED FAIL INDICATION ON CLIMBING. CREW PERFORMED AIR RETURN AND LANDED AIRCRAFT UNEVENTFULLY. EWR MX REMOVED AND REPLACED BLEED PUSHBUTTON AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO SDR 2008UALA06294Shutoff Valve · malfunctionedRT BLEED FAULT. RTFL. REPLACING PRSOV. RIGHT ENGINE BLEED LIGHT ILLUMINATED WITH BLEED SWITCH ON. REPLACED PRSOV. ACCOMPLISHED IDLE RUN, BLEED PRESSURE NORMAL. BLEED SWITCH-NORMAL OPERATION.
SDR HNAA0800310Bleed Air Sys · contaminatedAN ODOR WAS DETECTED WHEN THE BLEED SYSTEM DUCT TEMP EXCEEDS 20C. THE APU AND ENGINE BLEEDS WERE RUN ON THE GROUND AND ODOR DISSIPATED. SUSPECT RESIDUAL DE-ICE FLUID CONTAMINATION OF APU DURING MORNING DE-ICEING OF AIRCRAFT. AIRCRAFT WAS RELEASED FOR SERVICSDR 2008UALA06214Shutoff Valve · failedRT HIGH PRESSURE SHUTOFF VALVE FAILED. HPSOV FAILED. REPLACED WITH NEW VALVE. OP TESTS OKAY.SDR ASAA0853634Control Valve · faultyUPON DEPARTURE FROM HNL AIRFLOW FROM GASPERS WAS EXCESSIVELY HIGH NOISE LEVEL WAS 120 DBT AND TEMPERATURE IN CABIN WAS VERY COLD. AFTER APPROX 5 MIN AIRFLOW DB LEVEL AND TEMPERATURE RETURNED TO NORMAL. SUSPECT THAT A 9TH STAGE BLEED VALVE STUCK OPEN. NO OTHSDR 08FDEA04428Controller · failedPASSING FL 240, BOTH PACKS FAULTED, C/W ECAM PROCEDURE. PACK WOULD NOT RESET, DESCENDED TO 10,000 FOR REMAINDER OF FLIGHT. PASSING 14,000 ON WAY BACK DOWN PACK FAULTS MAGICALLY WENT AWAY AND CABIN BEGIN TO STABILIZE PERFORMED SUCCESSFUL BITE TEST OF NR 1 ASDR HALA0800815Isolation Valve · malfunctionedETOPS SIGNIFICANT SYSTEM - BTB - 36100301 - BTB - AFTER ENG START CLOSING LEFT ISLN VLV LIGHT REMAINED ILLUMINATED WITH LEFT ISLN VLV EICAS MSG. COULD NO RESET. REMOVED & REPLACED LT ISOLATION VLV PER AMM 36-11-04. OPS CHECK GOOD.SDR HALA0800812Switch · malfunctionedETOPS SIGNIFICANT SYSTEM - AFTER ENGINE START L ISN VALVE EICAS & OVERHEAD LIGHT ON. RTN TO GATE. PER FIM 36-10-00 RESET SW AND OPS CHECKED OK FOR SERVICE.SDR CHQA200800200Filter Element · dirtyFLIGHT 5941, CLE TO ORD. WHILE CLIMBING THROUGH FL190, THE FLIGHT CREW RECEIVED A BLD 1 OVERTEMP MESSAGE ON EICAS. THE QRH PROCEDURES WERE FOLLOWED AND BLEED 1 WAS DESELECTED AND CROSS BLEED WAS TURNED TO OPEN. THE FLIGHT ENCOUNTERED ICING CONDITIONS AND RESDR 2008UALA06095Shutoff Valve · malfunctionedLT ENG REACHED 490 DEG DURING SLUGGISH START. TAXI TEMPS ELEVATED ALSO CLIMB/CRUISE NORMAL. REPLACED NR 1 ENG HPSOV & HP CONTROLLER. OPS CHECK GOOD. REPLACED NR 1 ENGINE.
SDR DL76G081340Shutoff Valve · unserviceableIN FLIGHT EICAS MESSAGE RIGHT HPSOV ALONG WITH BLEED RIGHT LIGHT ON OVERHEAD PANEL. FWD TO MCO AND PLAC PER MEL 36-11-02.SDR C2XA008TY123Thermostat · malfunctionedENROUTE FROM IAH TO ORF WHEN THE CREW RECEIVED SEVERAL EICAS MESSAGES FROM BLEED NR 1 OVERTEMP FOLLOWED BY BLEED NR 2 OVERTEMP THROUGHOUT DESCENT TO EXIT, IN ADDITION TO ANTI-ICE FAIL AND ICE CONDITIONS. DIVERTED TO TYS, WHERE MX REMOVED R&R BOTH FWD FAN AIRSDR DL76G081335Shutoff Valve · malfunctionedRIGHT ENGINE HPSOV ANNUNCIATOR ILLUMINATED DURING FLIGHT ALONG W/ BLEED LT ON RIGHT PACK. DEACTIVATED RIGHT ENGINE HPSOV AND RIGHT THRUST REVERSER PER MEL 36-11-02 FWD TO MCO AND PLACARD.SDR COEA0801728Control Valve · failedFLT NR 7699 SEA TO BLI, DURING CLIMB OUT AT APPROXIMATELY 1000FT AGL THE BLEED AIR HEAT SYSTEM WAS SELECTED ON. AFTERWARD THE COCKPIT STARTED FILLING WITH BLACK SMOKE ALONG WITH A BURNT RUBBER ODOR. THE PILOT PIT ON HIS OXYGEN MASK AND TURNED OFF THE BLEED ASDR C2XA08IA222O-Ring · wornIAH FLIGHT 2160 THE CREW REPORTED A BLEED 2 LEAK MSG DURING CRUISE. THE ACFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MX R&R BLEED O-RINGS UNDER THE CARGO COMPARTMENT FLOOR. OPS AND LEAK CHECKED WITH NO DEFECTS AND THE ACFT WAS APPROVED FOR RETURN SDR AALA200802651Duct · leakingLAX - ON CLIMB THROUGH 1000 OVERHEAT LIGHT ILLUMINATED. CREW TURNED OFF ENGINE BLEED SYSTEM AND LIGHT EXTINGUISHED. RETURNED TO LAX AND LANDED WITHOUT INCIDENT. ON LANDING FOUND NUMBER ONE ENGINE ACCESS PANELS OPEN. REPLACED NUMBER ONE ENGINE HIGH PRESSURESDR SIMA200827302Precooler · malfunctionedON FLIGHT 3992 DURING CRUISE CREW ADVISES THAT THERE IS A BURNING RUBBER OIL ODOR IN THE CABIN. WHEN ON THE GROUND THE TEMPERATURE STABILIZED. ACFT REMOVED FROM SERVICE. C/A R&R NR 2 ENGINE PRECOOLER. OPS CHECK GOOD. ACFT RETURNED TO SERVICE.SDR YENA2008091Valve · leakingFLT NR 26 FLL-JFK AIR RETURN TO FLL, DUAL ENG BLEED FAULT 1 FAILED AT 1200`, 2 FAILED AT 11,200`. FOUND NR 1 ENG FAN AIR VALVE LEAKING FROM DIAPHRAGM. REMOVED AND REPLACED NR 1 FAN AIR VALVE IAW 36-11-54. OPS AND LEAK CHECK OK. ENG RUN-UP IAW AMM 71-00-00,SDR C2XA08IA214Valve · inoperativeIAH FLIGHT 2063. THE CREW REPORTED A BLEED 1 OVERTEMP IN FLIGHT. THE CREW CLOSED THE BLEED VALVE IN ACCORDANCE WITH THE QRH AND THE ACFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MX R&R THE ENGINE 1 FAN AIR VALVE. OPS CHECKED WITH NO DEFECTS NOTED SDR ABXR201072000023ACheck Valve · cracked(ABXR) DURING A MX INSP EVENT, WHILE DOING AN INSP OF THE NR 1 ENG 8TH STAGE CHECK VALVE IAW AD 90-12-02 IAW SB 36-2078, REV 2, FOUND APPROX A 1 INCH CRACK IN THE CONE SEAT AREA. R & R THE VALVE IAW MM.SDR 2008UALA05756Valve · faultySPLIT DUCTS AT 30000 RT 10 PSI HIGHER THAN LEFT AT CRUISE THRUST SMALLER SPLIT AT IDLE THRUST. NR 2 HIGH STAGE VALVE WEAK. REPLACED NR 2 HIGH STAGE VALVE. OPS CHECK ON GROUND RUN NORMAL.SDR HNAA0800290Switch · brokenNR 2 BLEED HOT CAUTION LIGHT ILLUMINATED IN FLIGHT. R&R NR 2 ENGINE HIGH PRESSURE BLEED SWITCH. REFERENCE MM 21-11-21. GROUND RUN OPS CHECK GOOD.SDR ASAA0853511Valve · leakingNR 1 ENGINE HIGH STAGE VALVE LEAKS AT BODY. REMOVED AND REPLACED NR 1 ENG HIGH STAGE VALVE IAW 737NG MM 36 11 06 000 801 STEP B&C AND MM 36 11 06 400 801 STEP E&F, PERFORMED W T W AAR 516368 D D 28DEC08, PERFORMED INSTALL TEST OF VALVE IAW 737NG MM 36 11 06 4SDR ASAA0853488Regulator · failedNR 1 ENGINE HIGH STAGE REGULATOR FAILED ENGINE BLEED AIR SYSTEM HEALTH CK. REMOVED AND REPLACED HIGH STAGE REF IAW 737NG MM 36 11 07 000 801 STEP B&C W MM 36 11 07 400 801 STEP E.SDR RAI2008F00000Precooler · malfunctionedDURING CLIMB, CREW RECEIVED A NR 2 BLEED OVERTEMP MESSAGE ON THE EICAS. MAINTENANCE REMOVED AND REPLACED THE NR 2 PRECOOLER AND PRECOOLER DUCT IAW AMM PROCEDURES. OPS CHECKED GOOD. (K)SDR 2009FA0000193Line · cutPREVIOUSLY REPORTED TO MFG, DURING THE SUPPLEMENTAL INSP FOR CONTINUED AIRWORTHINESS OF THE AIRPLANE. DURING SUPPLEMENTAL INSP NR 57-10-14 CARRY-THRU FWD SPAR CAP, FOUND MULTIPLE PNEUMATIC LINES SPLICED TOGETHER WITH STANDARD MIL-SPEC HOSE ON LT AND RT WINGS.SDR DL76G081129Shutoff Valve · failedRT ENGINE PNEUMATIC PRESSURE FLUCTUATING ON TAXI OUT. REMOVED PRSOV. INSTALLED PRSOV PER MM. PERFORMED OPS CK PER MM. ALL NML. PERFORMED HI PWR RUN CK OUT PER MM. ALL NORMAL.SDR C2XA08IA198O-Ring · blownJAN FLIGHT 3021. THE CREW REPORTED A BLEED 1 LEAK ON CLIMBOUT FROM BHM AT APPROXIMATELY 10,000 FEET. THE CREW SHUT DOWN THE NR 1 ENGINE AND DIVERTED TJAN WHERE IT LANDED WITHOUT INCIDENT. MX PLACED THE NR 1 BLEED SYSTEM ON MEL 36-11-05 CTL NR 153327 AND THESDR GLB2008F00016Regulator · malfunctionedACFT 240GL AIR RETURN FLT 5087 "DEN" 08/17/08 PILOTS REPORTED THE PNEUMATIC PRESSURE WAS EXCEEDING REDLINE DURING CLIMBOUT AT FULL POWER SETTINGS. MAINTENANCE ADJUSTED PNEUMATIC REGULATOR AS REQUIRED IAW 1900D MM 36-00-01. OPERATIONAL CHECK WAS GOOD.
SDR YENA2008080Thermostat · failedFLT 640, SFO-JFK, DIVERTED TO LGB, ENG 1 AND ENG 2 BLEED FAULTS DURING TAKEOFF DEPARTURE PHASE, ENG 2 BLEED FAULT OCCURRED FIRST. REPLACED NR 2 ENG THERMOSTAT FIN7170HM2. LEAK CHECK GOOD. REF AMM 36-11-06. REMOVED AND REPLACED NR 1 ENG FAN AIR VALVE THERMOSDR 2008UALA04273Shutoff Valve · fluctuatesDURING CLIMB R ENG HPSOV EICAS ON DUCT PRESS FLUCTUATES BETWEEN 25 - 40 PSI, OUT DURING CRUISE. FOUND HIGH PRESSURE SHUTOFF VALVE FAULTY. REPLACED VALVE. CHECKS OKAY FOR SVC.SDR 08FDEA03403Duct · crackedRT EXT FUSE NR 3 ENG FAN AIR EXH PORT ASSY IS FRETTED/CRACKED. REMOVED AND REPLACED FAN AIR EXH POT ASSY REF SRM 51-30-2 PG 1-32, REF MM 51-20-151-7 PG 1-5, REF MM 36-00-001-2 PG 1-4. THIS IS CLASSIFIED AS A MINOR REPAIR.SDR YENA2008077Shutoff Valve · failedFLT 447, BOS-TPA, DIVERTED TO JFK, BLEED 1 FAIL EICAS AT FL300, BLEED 1 PSI ABOUT 7 PSI, UNABLE TO MAINTAIN CABIN ALTITUDE. CLIMBING 800 FPM WITH CRUISE THRUST. FAULT CODE 36111200AM1 FOUND ON CMC. REMOVED AND REPLACED NACELLE PRSOV IAW AMM 36-11-03. OPERASDR 2008UALA04197Shutoff Valve · faultyLT ENGINE PRSOV NOT FULLY CLOSING AFTER ENGINE SHUTDOWN. REPLACED PRSOV, CHECKS GOOD. LT PRSOV & APU BLEED LIGHT WORK NORMALLY.SDR 2009FA0000196Line · cutPREVIOUSLY REPORTED DURING SUPPLEMENTAL INSP FOR CONTINUED AIRWORTHINESS OF THE AIRPLANE. DURING SUP INSP NR 57-10-14 CARRY-THRU FWD SPAR CAP FOUND MULTIPLE PNEUMATIC LINES SPLICED TOGETHER WITH STANDARD MIL-SPEC HOSE ON LT AND RT WINGS. LINES NOT AVAILABLE SDR COMA0870024Coupling · leakingON CLIMBOUT FROM CVG RECEIVED LT BLEED DUCT WARNING MSG, WARNING MSG CLEARED AND WAS REPLACED BY BLEED CAUTION MSG. ACFT RETURNED BACK TO CVG AND LANDED SAFELY. INSPECTED ACFT, SUSPECT LT ENG PYLON DUCT V-BAND COUPLING LEAKING. REMOVED AND REPLACED LT ENG PSDR UIEA200800281Relief Valve · leakingAT CRUISE NR 4 ENG HAD MULTPLE FIRE WARNINGS ON BOTH A&B. PERFORMED IN FLIGHT SHUT DOWN AND AIR TURNBACK. MAINTENANCE FOUND LEAKING PRESSURE RELIEF VALVE, WHICH WAS BLASTING HOT AIR ON THE DETECTORS. REPLACED OVER PRESSURE RELIEF VALVE PER 36-11-03, OPS CHESDR C2XA08RI113Line · leakingFLIGHT 2943 - EWR - FLIGHT CREW PERFORMED AIR RETURN DUE TO BLEED NR 2 LEAK ON EICAS DURING CLIMBOUT. MESSAGE CLEARED AFTER COMPLETION OF QRH PROCEDURES. CREW LANDED ACFT UNEVENTFULLY. EWR MAINTENANCE RESEALED BLEED LINE BETWEEN FRAME 70 AND 74. MAINTENANCSDR 2008UALA04066Modulating Valve · faultyNR 1 ENG FAMV STATUS MESSAGE. FOUND FAULTY FAN AIR MODULATING VALVE. REPLACED FAMV, OP CHECKED GOOD. AC OK FOR SERVICE.SDR RAIA00807022O-Ring · wornFLT 5529-STL-BLEED NR 2 LEAK MESSAGE ON THE EICAS. MAINTENANCE REMOVED AND REPLACED THE BLEED DUCT O-RINGS. SYSTEM OPS CHECKED GOOD. (S)SDR COMA086334Valve · failedON CLIMBOUT FROM CVG LT A/C PACK FAILED OFF, RT A/C PACK FLUCTUATING IN PRESSURE. ACFT RETURNED BACK TO CVG AND LANDED SAFELY. REMOVED AND REPLACED LT 10TH STAGE SHUT OFF VALVE. (S)SDR CALA2008072300099Clamp · missingCABIN PRESSURIZATION WAS UNCONTROLLABLE. PAX MASKS DEPLOYED. FOUND CLAMP MISSING FROM BOOT ON APU BLEED AIR DUCT LOCATED IN MLG WHEEL WELL KEEL BEAM. INSTALLED APU BLEED AIR DUCT CLAMP PER AMM 36-14-02. REFERENCE LOG PAGE 8036986 FOR AIRCRAFT CABIN PRESSURESDR RAIA00807013Precooler · leakingFLT 7905 - IAD - DURING CLIMBOUT, CREW RECEIVED A BLEED 2 LEAK ON THE EICAS. MAINTENANCE REMOVED AND REPLACED THE NR 2 PRECOOLER ASSEMBLY. SYSTEM OPS CHECKED GOOD. (A)SDR 2008FA0000545Bellows · rupturedTHE BELLOWS INSIDE THE BRADED CONNECTION CRACKED OUT LEAVING A HOLE ABOUT .75 IN IN DIA AT THE UP STREAM SIDE OF THE FLEXIBLE CONNECTOR. THE PROBLEM WAS DISCOVERED ON A MAINT RUN UP AT WHICH TIME THE FIRE DETECTION SYS WAS ACTIVATED FROM AN OVERHEAT SITUATIONSDR C2XA08ON159Valve · inoperativeFLT 0216 - ONT - FLIGHT CREW REPORTED BLEED 1 AND 2 OVERTEMP IN ICING CLIMBOUT. THRUST TO ELIMINATE MSG, ICING WAS AT 240. ALSO HAD A PACK 2 MEL OVERLOAD-AIR RUSHING IN COCKPIT. MX PERSONNEL REMOVED AND REPLACED PACK 2 OVERTEMP SWITCH AND NR 2 FAN AIR VALVE
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