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 CA971113071Clamp · loose(CAN) NR 1 STRUT OVERHEAT LIGHT CAME ON WHEN WING TAI WAS COMMANDED. STRUT OVERHEAT CONDITION CHECKLIST CARRIED OUT AND AIRCRAFT LANDED. CLAMP ON AIR SUPPLY LINE HAD FAILED. REPLACED.SDR 9718791157Bleed Duct · damagedAT ROTATION, THE NR 1 ENGINE FIRE LIGHT ILLUMINATED FOLLOWED BY THE REVERSER UNLOCK LIGHT. WITH POWER REDUCED TO IDLE ON THE NR 1 ENGINE, THE FIRE LIGHT WENT OUT. FUEL WAS DUMPED AND THE AIRCRAFT RETURNED WITHOUT INCIDENT. MAINTENANCE FOUND AN ENGINE BLEED SDR P5CA9701613Duct · crackedCRACKED NR 4 RIGHT LEADING EDGE DRIVE UNIT PNEUMATIC SUPPLY DUCT. REPLACED DUCT PER BAC MM 36-11-00.SDR P5CA9701611Pneumatic Duct · crackedCRACKED APU PNEUMATIC SUPPLY DUCT IN LOWER AFT CARGO COMPARTMENT AT STA 1540. REPLACED PNEUMATIC DUCT PAR BAC MM 36-11-01.SDR P5CA9701607Precooler · crackedCRACK ON NR 4 ENGINE PRECOOLER. WELDED PRECOOLER PER BAC PROCESS 5975.SDR P5CA9701606Precooler · crackedCRACK ON NR 3 ENGINE PRECOOLER. WELDED PRECOOLER PER BAC PROCESS 5975.SDR P5CA9701605Pneumatic Duct · crackedCRACKED PNEUMATIC DUCT IN NR 4 PYLON FOR NR 4 AIR DRIVEN HYDRAULIC PUMP TURBINE DRIVE. WELD REPAIRED AND PRESSURE TESTED DUCT PER BAC PROCESS 5975.SDR HEEA0011193Valve · leakBLEED VALVE LEAKS, 20 DEGREE DROP IN TOT.SDR HEEA0011192Valve · failedNO. 1 ENGINE HAD HIGH TOT. BLEED AIR VALVE FAILED.SDR 9718619965Clamp · leakingTAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED AFTER TAKEOFF. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND AIR LEAK AT FORWARD CLAMP ON PNEUMATIC CROSSFEED VALVE. REPOSITIONED CLAMP. LEAK AND OPERATIONAL CHECK NORMAL. AIRCRAFSDR 98ZZZX1950Blast Tube · looseMIA/TPA - FLT 7403 - PILOT REPORT: LEFT FIREWALL FUEL VALVE T-HANDLE ILLUMINATED DURING TAKEOFF. ABORTED TAKEOFF. RE-SECURED LOOSE BLAST TUBE ON LT COWLING, INBOARD SIDE.SDR SRAA970912Clamp · looseWHILE TAXIING, NR 1 NACELLE OVERHEAT WARNING LIGHT CAME ON, AIRCRAFT BLOCKED IN WITHOUT INCIDENT. INSPECTED NR 1 ENGINE AND FOUND CLAMP ON F-STACK BLEED AIR DUCT NOT ALIGNED. REMOVED CLAMP, RESEALED DUCT AND REINSTALLED CLAMP, OPS CHECKED AND LEAK CHECKED GOSDR 97ZZZX4375Tube · dentedRECEIVED NEW BLEED AIR TUBE ASSY FROM LEARJET WITH SEVERAL LARGE DENTS. RETURNED UNUSED TO LEARJJET FOR REPLACEMENT. RECEIVED 2ND TUBE ASSY WITH NO DAMAGE. INSTALLED ON AIRCRAFT AND RETURNED TO SERVICE. (PN 2655101-62).SDR PLGA970914AValve · malfunctionedFLT 4260 - ALB - ON CLIMB-OUT, THE LEFT BLEED AIR SHUTOFF VALVE LIGHT ILLUMINATED. AIRCRAFT RETURNED TO ALB AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED LEFT AIR VLV (GARRETT). SYSTEM CHECKED GOOD, AIRCRAFT RETURNED TO SERVICE. (M)SDR 9717649990Duct · crackedDURING CLIMB, THE LEFT ENGINE EXPERIENCED A FIRE WARNING INDICAITON. CREW REDUCED LEFT ENGINE POWER SETTING AND FIRE WARNING CEASED. AIRCRAFT RETURNED TO LGA AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE 13TH STAGE MANIFOLD ON THE LEFT ENGINSDR TWAA9711201Clamp · looseSTL - FLT 118 - DURING CLIMB, THE TAIL COMPARTMENT HIGH TEMPERATURE LIGHT ILLUMINATED. TIGHTENED CLAMPS ON THE LEFT HAND AUGMENTATION VALVE. OPERATIONAL CHECK NORMAL. CHECK C - 3-15-97 - JFK. (X)SDR 9717329959Duct · crackedDURING CLIMB, THE LEFT ENGINE EXPERIENCED A FIRE WARNING INDICATION. CREW REDUCED A LEFT ENGINE POWER AND FIRE WARNING CEASED. AIRCRAFT RETURNED TO MSP AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE 13TH STAGE MANIFOLD ON THE LEFT ENGINE, OPESDR WRLA97106Duct Coupling · leakingDURING INITIAL CLIMB-OUT, FLIGHT CREW RECEIVED NR 2 ENGINE FIRE WARNING. FLIGHT CREW REDUCED POWER ON ENGINE, AND INDICATION EXTINGUISHED. FLIGHT CREW ELECTED TO RETURN TO POINT OF DEPARTURE FOR MAINTENANCE TROUBLE-SHOOTING. AIRCRAFT RETURNED TO POINT OF DESDR REXA97250Bleed Air · leakRIGHT BLEED LEAK IN FLIGHT. GROUND RAN COULD NOT DUPLICATE DISCREPANCY. INSPECTED 'Y' CONNECTIONS IN WING ROOT, PERISEALS IN FLAP COVE, ASSOCATED PIPING. NO LEAKS NOTED AT THIS TIME. (M)SDR CKSA97494Bleed Valve · inoperativeACFT UNABLE TO MAINTAIN PRESSURIZATION. CRUISING FL24.0 CABIN ALT REACH 9500 FT WITH A CABIN RATE OF CLIMB STEADY AT 200 FPM. FLOW CONTROL KNOB WAS ALL THE WAY TO INCREASE. DESCENDED TO FL22.0 AND NO CHANGE TO THE STATUS. DESCENDED TO FL20.0 AND CABIN RATESDR 97FDEA00646Duct · leakedWITHIN 5 MINUTES OF SWITCHING OVER TO NR 2 ENGINE BLEED FOR NR 1 PACK LOWER AFT BODY OVERHEAT LIGHT CAME ON. LIGHT EXTINGUISHED WITHIN 30 SECONDS OF PLACING NR 2 BLEED SWITCH BACK OFF. RAN NR 1 AND NR 2 ENGINES TO POWER. COULD NOT DUPLICATE PROBLEM. LEAK CSDR 97FDEA00645Duct · leakedNR 3 ENGINE, FIRE WARNING INDICATION ON TAKEOFF ROLL. BOTH FIRE BOTTLES WERE DISCHARGED. FOUND 8TH STAGE DUCT NR 3 ENGINE BLOWN. REMOVED AND REPLACED DUCT AND BOTH FIRE BOTTLES, LEAK CHECKED GOOD. ENGINES RAN.SDR VNAA9709003Valve · failedDURING TAKEOFF ROLL, A BLEED WARNING MESSAGE ILLUMINATED. THE CREW ABORTED TAKEOFF AND RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE LEFT HIGH PRESSURE BLEED SHUTOFF VALVE IN ACCORDANCE WITH DORNIER MANTENANCE MANUAL 3SDR P5CA9701550Precooler · crackedCRACKED INTERNAL BRACKET ON NR 4 ENGINE PRECOOLER. REPLACED NR 4 ENGINE PRECOOLER PER BAC MM 36-12-01.SDR P5CA9701546Duct · crackedCRACKED STARTER PNEUMATIC DUCT ON NR 2 ENGINE. REPLACED DUCT PER BAC MM 36-11-01.SDR USAABB97103Mod Valve · failedPHL FL 18 - EN ROUTE LAX/PHL AT FL 410, CREW RECEIVED EICAS MESSAGE 'R ENG BLEED OFF' AND NOTED THAT THE DUCT PRESSURE READ 10 PSI. CREW THEN NOTED THAT THE RIGHT DUCT PRESSURE READ 45 AND THE LEFT DUCT PRESSURE WAS AT 10. DUCT PRESSURES BEGAN TO FLUCTUATE VSDR RAIA970908Seal · failedSTL - FLT 7492 - LEFT AIR OFF AND DUCT CAPTIONS ILLUMINATED DURING TAXI. MAINTENANCE REPLACED LEFT BLEED AIR DUCT SEALS. (X)SDR 9717099963Pneu Valve · leakingTAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED AFTER TAKEOFF. CREW DECLARED AN EMERGENCY AND RETURNED TO BNA, AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND LEAKING CROSSFEED PNEUMATIC VALVE IN RIGHT SYSTEM. REPLACED VALVE AND TEMPERATURE SENSOR, SDR EISA97182Duct · failedDURING CRUISE, FIRE WARNING BELL SOUNDED, NO VISUAL FIRE WARNING INDICATION. UNSCHEDULED LANDING. REMOVED AND REPLACED NR 2 ENGINE 6TH STAGE BLEED DUCT. LEAK TEST AND FIRE TEST GOOD. (M)SDR 97FDEA00599Clamp · failedON CLIMBOUT, APPROXIMATELY 5 MINUTES AFTER CLOSING NR 1 BLEED AND OPENING NR 2 BLEED AT 18,000 FT LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED. INITIATED CHECKLIST. AFTER SWITCHING TO NR 1 BLEED, LIGHT EXTINGUISHED. NOTED L-PACK AT 145 DEG C. PARTIALLY OPENEDSDR 97FDEA00594Clamp · looseLOWER AFT BODY OVERHEAT LIGHT CAME ON DURING FLIGHT. LIGHT CAME ON WHILE CLIMBING PAST FL240. THE CONFIGURATION WAS NR 1 BLEED CLOSED, NR 2 BLEED OPEN, NR 3 BLEED OPEN WITH BOTH PACKS ON. AS PER RED TABS, OPENED NR 1 BLEED AND CLOSED NR 2 BLEED. AFTER THISSDR CA970903005Duct Bleed Air · cracked(CAN) ON CLIMB THROUGH 1,500 FEET, THE TEMPERATURE ON NR1 ENGINE SUDDENLY INCREASED BY 100 DEGREES, POWER WAS REDUCED AND IN CRUISE THE NR1 ENGINE TEMPERATURE WAS 40 DEGREES HIGHER THAN THE NR2 ENGINE. ON LANDING THERE WAS NO THRUST REVERSERS AVAILABLE ON THE SDR 97FDEA00595Duct · leakingLOWER AFT BODY OVERHEAT LIGHT ILLUMINATED APPROX 5 MINS AFTER SWAPPING BLEEDS FROM NR 1 TO NR 2 ON THE ALTIMETERS CHECKLIST. RAN THE LOWER AFT BODY OVERHEAT LIGHT CHECKLIST AND THE LIGHT EXTINGUISHED AFTER SWAPPING BLEEDS BACK TO NR 1. CONTINUED FLIGHT WITH SDR SRAA970816Clamp · looseDURING CRUISE FOR FLIGHT 746 FROM AMS, AT FL 20.0 A LOUD BANG WAS HEARD FOLLOWED BY 2000 FPM CABIN RATE OF CLIMB, INITIATED EMERGENCY DESCENT TO A SAFE ALTITUDE. INSPECTED AIRCRAFT DURING FLIGHT AND FOUND THE PANEL FORWARD OF THE BALLSCREW IN THE RT WHEEL WELSDR PCAA9700528Bleed Line · brokenSPZ PANEL INDICATES 63 DEGREES OUTSIDE AIR TEMP. ACRID SMELL IN COCKPIT AND CABIN OF OVERHEATED PLASTIC. FOUND RIGHT BLEED LINE BROKEN JUST OUTBOARD OF HIGH TEMP SWITCH. REMOVED PIPE ASSEMBLY. INSTALLED NEW BLEED LINE ASSEMBLY. AIRCRAFT RETURNED TO SERVICSDR P5CA9701450Precooler · crackedNR 3 ENGINE HAD A OVERHEAT ON THE BLEED VALVE. VALVE CLOSED, THROTTLED BACK, LIGHT WENT OUT. FOUND NR 3 ENGINE PRECOOLER CRACKED APPROXIMATELY 5 INCHES LONG. REMOVED AND REPLACED PRECOOLER PER M/M 36-12-01.SDR USAAD97143Duct · rupturedEWR - FL 274 - AFTER TAKEOFF FROM LGA, CREW RECEIVED MASTER CAUTION AND THE LEFT ENGINE FIRE WARNING. THE FIRE WARNING EXTINGUISHED WHEN THE THROTTLE WAS RETARDED. FLIGHT DIVERTED TO EWR AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED A BLOWN 13THSDR CKSA97458Bleed Air Duct · leakingNUMBER 2 FIRE DETECTION FAULT LIGHT CAME ON IN FLIGHT BLEED VALVE WENT TO CLOSE POSITION AND A AND B INDICATORS SHOW 8.5 AND 7. TEMP WAS NORMAL ON ALL ENGINE PARAMETERS. SUSPECT A BLEED AIR LEAK AROUND B-LOOP. FOUND AIR LEAK AT FIRE LOOP 6 O'CLOCK POSITION SDR TC8A97043Clamp · looseENGINE NR 4 ON DESCEND HIGH POWER SETTING, FIRE WARNING LIGHT ON, OK CRUISE POWER. TIGHTENED LOOSE CLAMP ON THE PNEUMATIC STARTER DUCTING. RAN NR 4 ENGINE AT POWER, NO DEFECT NOTED ON GROUND IAW M/M 26-10-0. FIRE WARNING OK.SDR 97UAL900624Clamp · leakingENGINE NR 1 STRUT OVERHEAT ON CLIMBOUT. THROTTLED BACK AND LIGHT INTERMITTENT. RETURNED TO ORD ON AN AMBER ALERT. *S/D* FOUND PNEUMATIC LEAK AT PRECOOLER. REPLACED DISTORTED CLAMP, LEAK CHECKED OK.SDR 97FDEA00537Duct · failedLOWER AFT BODY OVERHEAT LIGHT CAME ON 40 MINUTES INTO FLIGHT. LIGHT WENT OUT AFTER SECURING LEFT PACK AND NR 1 AND NR 2 BLEED. THE LEAK IS BETWEEN THE BLEED VALVE AND THE PACK VALVE AS PER RED TABS. *S/D* REPAIRED DUCTS IN KEEL BEAM AND AFT CARGO AREAS. DSDR PLGA970807AController · malfunctionedBDL - FLT 4552 - DURING FLIGHT FROM MHT/LGA, THE RIGHT BLEED AIR LEAK LIGHT ILLUMINATED. CREW FOLLOWED PROCEDURES, AND SHUT DOWN THE RIGHT ENGINE. AIRCRAFT LANDED AT BDL WITHOUT INCIDENT. MAINTENANCE INSPECTED AIRCRAFT AND FOUND NO INDICATION OF A LEAK. ENSDR 9717126730Valve Bushing · under sizedDURING TAKEOFF, THE NR 4 ENGINE DID NOT REACH TAKEOFF POWER. ABORTED TAKEOFF AND RETURNED TO THE GATE. REPLACED THE HIGH STAGE CONTROL AND VALVE. OPERATIONAL CHECK GOOD.SDR 97FDEA00502Valve · leakingLOWER AFT BODY LIGHT ILLUMINATED IN FLIGHT. REMOVED AND REPLACED NR 1 CABIN AIR MODULATING VALVE PER MAINTENANCE MANUAL 36-00. RAN ALL THREE ENGINES PER B-727 JET RUN HANDBOOK. THE OVERHEAT LIGHT DID NOT ILLUMINATE. NO LEAKS FOUND.SDR AALA971398Duct Clamp · looseDFW - FLT 123 - AT ROTATIO DURING T/O, FIRE WARN AND RT HYD TEMP HIGHT LIGHTS ILLUMINATED FOR NR 3 ENG. ACCOMPLISHED SHUTDOWN OF NR 3 ENG AND FIRE WARNING LIGHT EXTINGUISHED. A/C DUMPED FUEL AND RETURNED TO DFW, LANDING WITHOUT INCIDENT. REPLACED NR 3 ENG. SDR P5CA9701381Cooling Manifold · crackedNR 3 ENGINE - HPT COOLING MANIFOLD ABOVE AND AFT OF ENGINE BLEED AIR PRECOOLER 11 O'CLOCK POSITION, CRACKED. WELDED IAW MM 36-12-01, BAC 5975 USING 3475.5 TIG ROD.SDR P5CA9701380Precooler · crackedNR 3 ENGINE PRECOOLER HAS CRACK AT LOWER FWD 'V' BAND CLAMP. WELDED IAW MM 36-12-01, BAC 5975 USING 625 TIG ROD.SDR 97FDEA00495Clamp · failedDURING CLIMBOUT AFTER 10 MINUTES OF FLIGHT, THE LOWER AFT BODY HEAT LIGHT CAME ON. CONFIGURATION WAS 1 AND 3 BLEEDS OPEN. PER RED TABS SECTION 2-7-14, NR 1 PACK AND BLEED WERE TURNED OFF. BEFORE NR 1 ENGINE COULD BE RETARDED THE LIGHT WENT OUT. THE OVERHEASDR 9714856634Seal · leakingDURING CLIMB, THE LEFT WING LEADING EDGE OVERHEAT LIGHT ILLUMINATED. AIRCRAFT DIVERTED TO MSP AND LANDED WITHOUT INCIDENT. REPLACED 'Y' DUCT SEALS IN NR 2 PYLON.SDR P5CA9701386Duct · leakingIN CRUISE FL 290 LEFT WING OVERHEAT LIGHT ILLUMINATED, COMPLIED WITH WING OVERHEAT PROCEDURE ISOLATED LEFT WING AND NR 1 AND NR 2 ENGINES WITH PYLON VALVES LIGHT WENT OUT. RETURNED THRUST TO NORMAL, LIGHT STAYED OUT. FOUND PNEUMATIC LEAK 1 FOOT INBOARD OF NR
Back to JASC 3610