JASC 3241
Service difficulty reports · 1,310
Reports filed under 3241 · Brake Anti-Skid Section, 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 = '3241' 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 = '3241' 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 AWXA200600388Power Supply · malfunctionedDURING DESCENT RECEIVED BRAKE ANTI-SKID NWS FAULT. TRIED TO CYCLE ANTI-SKID & NW STEERING SWITCH WITH NO HELP. DECLARED EMERGENCY LANDING. ON GROUND, CYCLED CIRCUIT BREAKERS. RECEIVED STEERING BACK. MX REPLACED BSCU, NO HELP. BSCU CHANNEL 1 DEFERRED. ORISDR BSYA200600007Control Valve · weakTAXING OUT OF AIRNETS RAMP AT LCK AIRPORT AIRCRAFT TAXIED OFF RAMP INTO THE MUD. AIRCRAFT RETURNED TO AIRNETS RAMP. MAINTENANCE REMOVED AND REPLACED TIRE AND WHEEL ASSY.ADJUSTED NOSE STEERING COMPUTER. A FEW DAYS LATER CHANGED ANTI SKID CONTROL VALVES FOR WEAKSDR WX0600010Control Box · malfunctionedLAS - FNL, CREW REPORTED THE WHEEL NOT TURNING LIGHT CAME ON DURING THE TAKEOFF ROLL AT 80 KNOTS THEN WENT OUT DURING ROLL OUT AFTER ABORTED TAKEOFF. AIRCRAFT RETURNED TO GATE. MAINTENANCE REMOVED AND REPLACED THE ANTI-SKID CONTROL BOX. OPERATIONALLY CHECKESDR DXTA200501168Relay · inoperativeON TAXI INTO FBO, PARTIAL BRAKE PRESSURE LOST WITH PWR BRAKE LOW PRESSURE AND ANTI SKID INOP ANNUCIATOR LIGHTS ON. TRIED TURNING ANTI-SKID OFF, AND ALL BRAKE PRESSURE LOST. TURNED ANTI-SKID ON RECLAIMED PARTIAL PRESSURE. TROUBLESHOT A/S BRAKE SYS, REPLACED BRSDR AU510002070Anti-Skid Sys · faultyFOLLOWING TWO BURST TIRES ON NR 1 MAIN WHEEL, MAINTENANCE CHANGED THE GREEN SYSTEM ANTI-SKID VALVE FOR NR 1 WHEEL POSITION. INVESTIGATION CONTINUING.SDR AALA20050811Valve · inoperativeSTL - WHEEL NOT TURNING LIGHT ON AT APPROXIMATELY 130 KNOTS DURING TAKEOFF. EXTINGUISHED AFTER LIFT OFF. NOTED BURNED RUBBER SMELL IN COCKPIT AND CABIN THAT DISSIPATED QUICKLY. ALL BRAKE TEMPS BELOW 50 DEGREES. REPLACED LEFT HAND INBOARD AND OUTBOARD ANTI-SDR COMA0560631Computer · malfunctionedFLIGHT 5836 - DURING BOS APPROACH RECEIVED AN A/SKID CAUTION MESSAGE AFTER EXTENDING THE LANDING GEAR, APPROACH WAS ABORTED AND MESSAGE CLEARED AFTER 15 SECONDS. SECOND ATTEMPT WAS WITHOUT DIFFICULTY. PERFORMED AN OPERATIONAL TEST OF THE A/SKID SYSTEM, DISCRESDR DXTA200501090Accumulator · lowUPON LANDING, AFTER APPLYING BRAKES, LOW BRAKE PRESS AND ANTI SKID INOP. MASTER CAUTION LAMPS ON FOR 6 SECONDS THEN EXTINGUISHED. ALSO BRAKES GRABBY LT MORE THAN RT. FOUND POWER BRAKE ACCUMULATOR PRECHARGE FLAT SERVICED WITH N2 TO PRECHARGE PRESSURE CHECKEDSDR MALA050834Valve · failedEN ROUTE ANTI-SKID INOP ILLUMINATED. AIR RETURN TO MSP, CHANGED VALVE.SDR MALA050828Valve · inoperativeANTI-SKID YELLOW SYSTEM NR 4 VALVE INOP. REPLACED VALVE.SDR 2005UALA01273Warning Light · intermittentAN INTERMITTENT EICAS ANTI-SKID WARNING LIGHT CAUSED A DIVERSION DUE TO CONCERNS WITH A SHORT RUNWAY AT PLANNED DESTINATION. REPLACED ANTISKID-AUTOBRAKE CONTROL UNIT PER MM 32-42-01. OPS CHECK NORMAL.SDR AU510002021Control Valve · failedRT MAIN LANDING GEAR NR 2 WHEEL LOCKED UP ON LANDING CAUSING THE TIRE TO BURST. INVESTIGATION FOUND THE RT MAIN LANDING GEAR AXLE HAD WATER INGRESS AND THE ANTI-SKID WIRING HAD HIGH RESISTANCE. THE WIRING WAS REPLACED BUT THE ANTI-SKID SYSTEM WAS STILL INOPESDR ASMF200511006Control Valve · failedAIRCRAFT RETURNED TO PLATFORM, PARKING BREAK CONTROL BREAKER M-36 WAS THROWN OUT CAUSING ALL ANTISKID LIGHTS TO TURN ON. DURING OVERNIGHT CHECK, THE ANTISKID SYSTEM DUAL SERVO VALVE OF THE INNER RT SIDE WAS REPLACED IAW MM 32-43-03, TESTED CORRECT.SDR AALA20050730Control Box · inoperativeORD - AFTER LANDING GEAR WAS EXTENDED THREE OUT OF FOUR ANTI-SKID LIGHTS ILLUMINATED. LEFT INBOARD LIGHT REMAINED OUT. CYCLED THE SYSTEM AND TESTED. NO CHANGE OF LIGHTS. LANDED ORD WITHOUT INCIDENT. FOUND ANTI-SKID CONTROL BOX INOPERATIVE. REPLACED ANTI-SDR DXTA200501062Case · crackedBRAKE PRESS LOW AND ANTI-SKID INOP LIGHTS ON BEFORE LANDING, BRAKES INOP. PEDALS TO FLOOR ON LANDING, USED BOTTLE TO STOP. BRAKE FLUID COMING OUT ALL OVER NOSE WHEEL. REMOVED LEFT NOSE BAGGAGE FLOOR PANELS TO GAIN ACCESS TO ANTI-SKID SYS. FOUND ANTI-SKID SSDR COMA0560583Anti-Skid Sys · warning lightFLIGHT 5904 - PARKING BRAKE SOV AND ANTI/SKID CAUTION. RESET SYSTEM. NO DEFECTS NOTED.SDR DXTA200501041Transducer · malfunctionedCAPT LEFT BRAKE PEDAL INTERMITTENTLY LOSES PRESSURE IN TURNS. REMOVED AND REPLACED LT ANTI SKID TRANSDUCER IAW CE 560 MM 32-42-07.SDR TSAA0532050Anti-Skid Sys · deactivatedON CLIMB OUT, PILOT OBSERVED THE LT ANTI-SKID LIGHT ON AND STAYED AND RETURNED BACK TO DEPARTURE. THE ANTI-SKID SYSTEM WAS MEL’D WAITING FOR AN ANTI-SKID CONTROL BOX. THE ANTI-SKID SYSTEM AND ANTI-SKID BRAKES WERE DEACTIVATED.SDR AALA20050687Shuttle Valve · inoperativeJFK - AUA - DURING CRUISE CREW REPORTED UNCOMMANDED RIGHT HYDRAULIC SYSTEM TRANSFERRING TO LEFT HYDRAULIC SYSTEM. REMOVED AND REPLACED THE LEFT AND RIGHT ANIT-SKID SHUTTLE VALVE. SYSTEM GROUND CHECKED NORMAL OPERATION.SDR DXTA200501017Filter · failedON TAXI OUT A/C WAS UNRESPONSIVE ON BRAKE CHECK CAPT. SIDE: FULL PRESSURE WITH NO BRAKING AVALIBLE. F/O SIDE: PEDALS COMPLETLY FLOORED WITH NO PRESSURE. - REMOVED & REPLACED ANTI-SKID CONTROL FILTER & BLEED BRAKE SYSTEM IAW CE 560 MLM 32-42-00. COMPLIED WITH TSDR 138910092005Anti-Skid Sys · malfunctionedNR 1 TIRE BLEW ON LANDING.SDR AALA20050652Transducer · inoperativeMIA - INFLIGHT AFTER TAKEOFF UPPER EICAS ANTI-SKID MESSAGE AND LIGHT CAME ON ANNUNCIATOR PANEL. AFTER GEAR DOWN, LIGHT AND MESSAGE STAYED ON THROUGH ROLL OUT. BOTH ARE INTERMITTENT. REPLACED NUMBER 7 TRANSDUCER FOR ANTI-SKID AUTOBRAKE CONTROL UNIT. SYSTEM SDR AWXA200501124Warning System · activatedLAS - ABORTED TAKEOFF - FLT 421 - AIRCRAFT ABORTED TAKEOFF FOR POSSIBLE AUTO BRAKE PROBLEM. SAFETY EVENT REPORT REVEALS THAT TAKE OFF WAS ABORTED, UNDER 60 KNOTS, DUE TO TAKE OFF CONFIGURATION WARNING. CREW NOTICED SPEED BRAKE LEVER NOT FULLY IN DETENT AFTERSDR DXTA200500978Anti-Skid Sys · malfunctionedUPON LANDING, EXPERIENCED "HARD PEDALS" AND NO BRAKES FOR ABOUT 6 SECONDS. JUST BEFORE USING EMER BRAKING THE BRAKES SUDDENLY GRABBED VIOLENTLY. AFTER THAT THEY WORKED NORMALLY. GAINED ACCESS TO ANTI-SKID FAULT INDICATORS IN NOSE BAGGAGE AREA. FOUND NO FAUSDR COMA0560511Control Unit · malfunctionedFLIGHT 4940 - INBOARD ANTI-SKID CAUTION. RESET THE ANTI-SKID CONTROL UNIT.SDR DJFA2005140Transducer · intermittentTHE CREW REPORTED THAT THE AIRCRAFT BRAKING FAILED UPON EXITING THE RUNWAY AFTER LANDING. WHEN THE ANTI-SKID SYSTEM WAS TURNED OFF, NORMAL BRAKING POWER WAS RESTORED. MAINTENANCE REPLACED BOTH ANTI-SKID WIRING HARNESSES, AND DISCOVERED BOTH MAIN LANDING GEARSDR DXTA200500938Brake · malfunctionedON LANDING ROLL AND DURING TAXI THE BRAKES ARE VERY TOUCHY AND APPLY AT DIFFERENT RATES. NOT POSSIBLE TO TAXI WITHOUT CONSTANT PULLING LEFT AND RIGHT. PERFORMED TROUBLESHOOTING OF BRAKE SYSTEM, INCLUDING ANTI-SKID SYSTEM FUNCTIONAL CHECK IS GROUND MODE. FUNCSDR AALA20050557Control Unit · inoperativeLAX INFLIGHT T1677 - ANTI-SKID MESSAGE IN FLIGHT. AIRCRAFT DIVERTED FROM SNA TO LAX AND LANDED WITHOUT INCIDENT. REPLACED ANTI-SKID CONTROL UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION.SDR DXTA200500933Transducer · inoperative" ANTI-SKID OFF " LIGHT ILLUMINATED DURING TAXI OUT, PRESSED TO RESET AND APPROX 1 MIN LATER IT ILLUMINATED, CYCLED ANTI-SKID CB'S AND IT AGAIN ILLUMINATED AND CONTINUED TO CYCLE ON /OFF APPROX EVERY MIN. REMOVED TRANSDUCER ON NR 4 WHEEL P/N: 606568 S/N: OLT0SDR DXTA200500904Anti-Skid Sys · malfunctionedANTI SKID ACTIVATES INTERMITTANTLY BELOW 5KTS. COMPLETELY ACTIVATES WITH MODERATE BRAKE PRESSURE, RESULTING IN NO BRAKES AT ALL. ANTISKID OFF BRAKES NORMAL. ALL ELECTRICAL SIGNALS CHECK OK IAW 560 M/M WIRING 32-48-01. BIT CHECK, CHECKS OK IAW 560 MM 32-40-0SDR DXTA200500899Warning Light · illuminatedON LANDING THE ANTISKID LIGHT ILLUMINATED AND ON TAXI IN THE LOW BRAKE PRESSURE LIGHT ILLUMINATED AND THE PNEUMATIC BRAKES HAD TO BE USED TO STOP THE PLANE. C/W BRAKE SYSTEM BLEED, BIT TEST & AN ANTISKID FUNCTIONAL TEST. NO FAULTS FOUND AT THIS TIME, WORK DOSDR XN0A1254Brake Assy · vibratesON TAXIOUT, BRAKES VIBRATE WHEN APPLIED. BLED BRAKES AS REQ'D IAW B727 MM REF 32-41-0, SYSTEM OPS CHECKS GOOD.SDR COMA0560429Transducer · malfunctionedFLIGHT 5553 - ANTI SKID CAUTION DURING T/O. REPLACED WHEEL SPEED TRANSDUCER.SDR ASMF200508003Control Box · inoperativeAIRCRAFT REJECTED TAKEOFF (WHEEL NOT TURNING) LIGHT TURNED ON. ANTISKID CONTROL BOX WAS REPLACED IAW MM 32-43-00, TESTED CORRECT.SDR ASMF200508001Socket · damagedDURING TRANSIT SERVICE, PERFORMED ANTISKID TEST, THE CIRCUIT BREAKER R-41 WAS ACTIVATED AND WOULD NOT RESEAT IT. ANTISKID VALVES CONNECTORS WERE DISCONNECTED AND TRANSDUCERS WERE CHECKED OF 4 MAIN WHEELS AND FAIL CONTINUE. ANTISKID CONTROL BOX WAS REPLACED ISDR G41A200500001Anti-Skid Sys · malfunctionedAFTER LANDING, MIDLAND TX, APPROX 13:49 PM TO DROP OFF PAX`S, SCHEDULED TO PROCEED TO DALLAS TO DROP OFF REMAINING PAX`S, THE PILOT EXPERIENCED A VIBRATION DURING TAXI. INSPECTION OF A/C REVEALED RT OUTBOARD MAIN TIRE HAD A BLOW OUT DUE TO A POSSIBLE LOCKUP OSDR CA050728002Control Unit · failedAN AIRCRAFT EXPERIENCE LT MLG NR 1 TIRE BURST ON LANDING, THEN THE LT MLG NR 2 TIRE BURST DURING TAXI. MAINTENANCE REPLACED LT MLG WHEELS REPLACED, ASCU AND LT GEAR A/S CONTROL VALVE. PERFORMED A/S SYSTEM TEST. AIRCRAFT RTS.SDR DXTA200500857Transducer · inoperativeON TAKEOFF ROLL, APPROACHING 60K MASTER CAUTION LIGHT ILLUMINATED WITH ANTI-SKID ANNUNCIATOR LIGHT SWITCHES PROPER POSITION, TAKEOFF ABORTED. T/S TO BAD RT WHEEL TRANSDUCER. INSTALLED NEW TRANSDUCER OP'S CHECKS SATISFACTORY AT THIS TIME. ALL WORK DONE IAW CSDR SIMA200520901Brake Assy · failedDURING LANDING, ANTI SKID CYCLED ABNORMALLY. AIRCRAFT WOULD NOT STOP IN NORMAL DISTANCES. REPLACED BRAKE CONTROL UNIT. OPERATIONAL CHECK GOOD. AC RETURNED TO SERVICE. (K)SDR QXEA200501124Warning Light · illuminatedGEG - ON FLIGHT 2367, RETURNED TO GATE. OUTBOARD ANTI SKID CAUTION LIGHT ILLUMINATED DURING TAXI, PLACED ON MEL.SDR COMA0560397Warning Light · illuminatedFLIGHT 5877- LEFT OUTBD ANTI SKID CAUTION. CND, SYSTEM CHECKS NORMAL, NO FAULTS FOUND.SDR DXTA200500830Warning Light · illuminatedBRAKE LIGHT ILLUMINATED IN FLIGHT, DOWNLOADED FAULT CODE 335. RESEARCHED COOL CODE: CHECK RT WHEELS. WHEELS CHECK GOOD. NO DEFECTS DETECTED. WORK PERFORMED IAW CHAPTERS 45-308 AW 32-404 OF THE FALCON 2000 M/M.SDR DXTA200500821Pump · malfunctionedANTI-SKID AND POWER BRAKE FAILURE. PUMP RUNNING CONTINUOUSLY (BOTH LIGHTS ON). REMOVED BRAKE PUMP AND INSTALLED NEW PUMP. OPERATIONAL CHECKS GOOD. LEAK CHECK GOOD. WORK PERFORMED IAW CH 32-42-06 OF CESSNA 560XL MM.SDR ASMF200506024Control Box · failedAIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF RIGHT INBOARD ANTISKID LIGHT TURNED ON. AT PLATFORM, BITE TO ANTISKID CONTROL BOX WAS PERFORMED DETECTING FAILURE IN THE RIGHT INTERIOR DOUBLE SERVO VALVE. VALVE WAS REPLACED IAW MM 32-43-04, TESTED CORRECT.SDR DXTA200500795Anti-Skid Sys · malfunctionedPILOTS LEFT BRAKE IS MUSHY AND HAS TO BE PUMPED UP TO OPERATE. CO-PILOTS RIGHT BRAKE DOES THE SAME THING. DRAINED AND FLUSHED RESERVIOR AND BRAKE LINES. BLED ANTI-SKID BRAKE SYSTEM WITH SKYDROL 500-B-4.SDR DXTA200500752Transducer · inoperativeDURING TAXI BOTH PEDALS ON RT SEAT BECAME SOFT, ANTI-SKID LIGHTS CAME ON. AFTER PUMPING THE PEDALS THE LIGHT WENT OUT, AND THE BRAKES FELT NORMAL. THIS HAPPENED THREE SEPERATE TIMES DURING TAXI. REPLACED LT ANTI-SKID TRANSDUCER AND BLED BRAKES. OPS CHECK GSDR AALA20050375Valve · faultyJFK - AFTER AUTOBRAKES WERE SELECTED FOR LANDING, ANTI SKID INOPERATIVE LIGHT CAME ON AND STAYED ON UNTIL AFTER LANDING. LIGHT WENT OFF WHEN ENGINES WERE SHUT DOWN. FOUND ANTI SKID VALVES 3/4 FAULTED. REPLACED 3/4 ANTI SKID VALVES. SYSTEM GROUND CHECKED NOSDR CA050603005Valve · unserviceable(CAN) ON INSPECTION, LT ANTI-SKID VALVE FOUND UNSERVICEABLE. LT ANTI-SKID VALVE REPLACED.SDR ASMF200505022Control Unit · malfunctionedAIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF ANTI SKID LIGHTS TURNED ON. THE CIRCUIT BREAKER AND ANTI SKID MODULE WERE RESEATED WITH NEGATIVE RESULTS, THE AUTO BRAKE SYSTEM WAS RESEATED IAW MM 32-43-00, TESTED CORRECT. DURING OVERNIGHT SERVICE, THE ANTISDR DXTA200500709Annunciator · illuminatedDURING OCF TAKEOFF ROLL, AT 70 KIAS, THE ANTI-SKID ANNUNICATOR ILLUMINATED. ABORTED TAKEOFF. LIGHT WENT OUT AFTER WE EXCITED THE RUNWAY. TROUBLESHOT ANTI-SKID LIGHT ILLUMINATED. TROUBLESHOT TRANSDUCER. ALL VOLTAGES AND OHMS READ CORRECTLY. TROUBLESHOT WI
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