JASC 3241
Service difficulty reports · 1,310
Reports filed under 3241 · Brake Anti-Skid Section, newest first.
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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 ABXA9600511Control Box · defectiveBRAKES FAILED WITH ANTI-SKID SYSTEM ARMED WITH AIRCRAFT BELOW 15 KIAS ON LANDING. REPLACED ANTI-SKID CONTROL BOX IAW DC8 MM CHAPTER 32-43-6 AND OPS CHECK WAS GOOD.SDR IXXA9688Control Valve · intermittentANTI-SKID FAIL LIGHT ILLUMINATED ON TAKEOFF ROLL DEPARTING ICT TO OKC. GEAR WAS RECYCLED AND THE LIGHT EXTINGUISHED. AIRCRAFT LANDING AT OKC WAS UNEVENTFUL. MX REPLACED THE RIGHT OUTBOARD ANTI-SKID DUAL CONTROL SERVO VALVE. THE SYSTEM OPERATIONALLY CHECKEDSDR 96ZZZX3455Circuit Board · failedTHE CIRCUIT BOARD MAINTENANCE RELEASE TAG WAS IDENTIFIED WITH PN 42-15919NL, SN 351, ACTUAL UNIT WAS IDENTIFIED WITH PN 42-15919NL, SN 341. AFTER CIRCUIT BOARD WAS INSTALLED IN CONTROL BOX, IT WAS FOUND DURING SYSTEM CHECK-OUT THAT BOARD HAD A HARD FAILURE.SDR 96ZZZX3053Control Box · pins corrodedIMPROPER ANTI-SKID OPERATION AND INVALID TEST. FOUND OXIDIZATION ON CONTROL BOX CONNECTOR J1 AND J2 PINS. BOX, SN 137, ORDERED EXCHANGE BOX AND EXCHANGE BOX SHIPPED. ALSO, HAD OXIDIZED PINS. BOX, SN DASH 064. CLEANED OXIDIZATION FROM PINS, MALE AND FEMALESDR ORJA9626Drive Studs · inopWHEEL NOT TURNING LIGHT CAME ON SHORTLY AFTER BEGINNING TO ROLL. RETURNED TO GATE. REINSTALLED DRIVE COUPLING STUDS ON NR 3 ANTI-SKID TRANSDUCER. OPS CHECK NORMAL. (M)SDR REXA96015Transducer · failedBRAKE INOP ON TAXI AFTER LANDING. REMOVED AND REPLACED RHIB ANTI-SKID TRANSDUCER. (M)SDR USAAD96056Transducer · failedFLT NR 1846 - MCO-PIT - 'WHEEL NOT TURNING' LIGHT CAME ON AT 85 KNOTS. REPLACED OUTBOARD RIGHT WHEEL TRANSDUCER. (M)SDR CA960524018Flywheel · improper lube(CAN) WRONG LUBRICATION IN FLYWHEEL SIDE.SDR AU960519Indicator · faulty(AUS) BRAKING SYSTEM ANTI-SKID INDICATOR/TEST PANEL FAULTY DUE TO SUSPECTED SHORTING TEST SWITCH - AUTO-BRAKE SYSTEM WOULD NOT OPERATESDR 96ZZZX2545Transducer Pins · looseSEA - FLT 350 - DURING THE TAKEOFF ROLL AT APPROXIMATELY 40 KNOTS, THE 'WHEEL NOT TURNING' LIGHT ILLUMINATED. THE TAKEOFF WAS ABORTED. REINSTALLED TRANSDUCER PINS. OPERATIONAL CHECK AND BITE CHECK NORMAL. CHECK C-1D - 11/3/95 - JFK.SDR 96ZZZX1967Transducer · corrodedTRANSDUCER IS CORRODED (SEVERELY PITTED). THIS CORROSION APPEARS TO START AT THE ETCHING USED TO INSTALL PART NUMBER OR SERIAL NUMBER. THE CORROSION NORMALLY SPREADS ONTO CONNECTOR PLUG AND TENDS TO TRANSFER ONTO AXLE, CORRODING IT. S/N 406 AND S/N 431.SDR VNAA9600013Control Unit · malfunctionedPIT - FLT 4169 - DURING TAKEOFF ROLL, THE CREW WAS ALERTED BY A C.A.S. MESSAGE THAT BRAKES WERE HOT. CREW ABORTED TAKEOFF AND RETURNED TO THE GATE. PIT MX RE-RACKED THE ANTI-SKID CONTROL UNIT IAW MM 32-43-10. ALSO, ALLOWED SEVERAL MINUTES FOR THE BRAKES TOSDR 9607529860Anti-Skid Comp · failedDURING LANDING WITH ANTI-SKID ON MEL, THE NR 2 AND NR 3 TIRES BLEW, NO DAMAGE TO AIRFRAME. CHANGED NR 2 AND NR 3 TIRES. REPLACED NR 1 ANTI-SKID VALVE AND ANTI-SKID COMPUTER. ANTI-SKID SYSTEM OPERATIONALLY CHECKED GOOD.SDR ORJA96019Transducer Pins · failedAT 50 KTS ON TAKEOFF ROLL, WHEEL NOT TURNING LIGHT ILLUMINATED. REPLACED ANTI-SKID TRANDUCER PINS IN NR 2 WHEEL AXLE. OPS CHECKED GOOD. (M)SDR CA960416006Line · cracked(CAN)DURING WALKAROUND HYDRAULIC FLUID NOTED DRIPPING FROM #1 NACELLE. SYSTEM PRESSURIZED AND FLUID FOUND DRIPPING FROM END OF HYDRAULIC LINE AT ANTI SKID CONTROL VALVE. CRACK NEAR FLARE.SDR 96ZZZX2368O-Ring · leakingO-RING AT T-FITTING AN917-6D WHERE ANTI-SKID PUMP PRESSURE SWITCH IS LOCATED WAS LEAKING. THE ACCUMULATOR PRESSURE WOULD DROP AND COULD CAUSE BRAKING PROBLEMS. TIGHTENED B-NUT AT FITTING AND PRESSURE CHECKED. MARKED WITH TORQUE SEAL. SUBMITTER STATED ALL TSDR 9604586628Control Unit · failedDURING TAKEOFF, ANTI-SKID LIGHTS ILLUMINATED ON BOTH THE PILOTS AND SECOND OFFICER'S PANEL. ABORTED TAKEOFF AND RETURNED TO THE GATE. REPLACED THE ANTI-SKID CONTROL UNIT AND OPERATIONAL CHECK GOOD.SDR 9603999963Anti-Skid · malfunctionedBOTH THE LEFT MAIN GEAR TIRES BLEW ON LANDING INTO GRR. AIRCRAFT REMAINED ON RUNWAY AND PASSENGERS WERE DEPLANED VIA STAIRS. AIRCRAFT WAS TOWED TO THE GATE WITH BOTH TIRES FLAT. MAINTENANCE REPLACED BOTH LEFT MAIN ANTI-SKID VALVES, ALL FOUR ANTI-SKID TRANSDSDR RAIA960148Transducer · faultySUX - FLT 7213 - ANTI-SKID LIGHT ILLUMINATED ON TAKEOFF ROLL. MAINTENANCE REPLACED RIGHT OUTBOARD WHEEL TRANSDUCER. (X)SDR P5CA9600001Control Box · failedDEPARTING KHV, TOWER ADVISED RUBBER LEFT ON RUNWAY. ON ARRIVAL ANC, DISCOVERED NR 11 TIRE BLOWN, HOLE IN WING-BODY FAIRING, 18 OF CONDUIT MISSING FROM RT BG STRUT. REPLACED ANTI-SKID BOX DUE TO FAILED BITE CHECK IAW MM 32-42-00, 3 TIRES IAW MM 32-45-01. PERSDR SWAA960031Anti-Skid Valve · malfunctionedAFTER GEAR RETRACTION, UPON GEAR HANDLE BEING POSITIONED TO OFF, INBOARD GEAR ANTI-SKID LIGHT ILLUMINATED. LIGHT EXTINGUISHES WITH HANDLE IN UP OR DOWN POSITIONS. AIRCRAFT DIVERTED TO BNA AND MADE AN UNEVENTFUL LANDING. AT HOU, REPLACED RT INBOARD ANTI-SKIDSDR 95UAL900357Anti-Skid Module · inoperativeOUTBOARD ANTI-SKID WARNING LIGHT ILLUMINATED AT 100 KNOTS ON TAKEOFF ROLL. TAKEOFF WAS ABORTED WITH VERY LITTLE BRAKING USED. REPLACED ANTI-SKID CONTROL MODULE, CHECKS OK.SDR DL72E954787Transducer · faultyIR - RT BRAKE EXTREMELY WEAK. NR 3 BRAKE AT FAULT, TURNED OFF ANTI-SKID BRAKES, OPS NORMAL. REPLACED NR 3 TRANSDUCEDR ANTI-SKID, OPS NORMAL.SDR DLM88954723Transducer · failedON LANDING ROLLOUT, BRAKING EFFECTIVENESS ON THE LEFT SIDE WAS ALMOST NON-EXISTENT, SOMEWHAT MORE EFFECTIVE AT TAXI SPEEDS. RESET LEFT GEAR IN LINE FUSE, VERIFIED BRAKES ARE OPERATING AT GATE, PERFORMED HIGH SPEED TAXI, FOUND ANTI-SKID INOP. OPERATES NORMAL SDR COMA9511995Control Box · defectiveRIGHT ANTI-SKID INOPERATIVE WARNING AFTER LANDING GEAR WAS RETRACTED. REPLACED THE ANTI-SKID CONTROL BOX.SDR COMA9511993Relay · failedWHEN THE LANDING GEAR WAS SELECTED UP, THE RIGHT INBOARD ANTI-SKID FAILED. REPLACED RELAY K0021.SDR 95ZZZX6359Anti Skid Sys · malfunctionedKTUS/KDAY - FLT 011 - ON LANDING ROLL-OUT, BRAKES FADE WITH ANTI-SKID ON, HYDRAULIC PRESSURE DROPPED TO 2,000 PSI. MAINTENANCE PERFORMED AN OPERATION CHECK OF THE ANTI-SKID SYSTEM IAW MM CHAPTER 32. NO DEFECTS WERE NOTED. BRAKE SERVICE LIMITS WERE CHECKED BSDR CAL950942Transducer · inoperativeEWR - FLT 0293 - LOW SPEED TAKEOFF ABORT. SUPPLEMENT - TAKEOFF WAS ABORTED DUE TO A LOUD POPPING NOISE FOLLOWED BY A JOLT. THE ANTI-SKID SYSTEM WAS TROUBLESHOT AND ALL ANTI-SKID VALVES CHECKED GOOD. MAINTENANCE FOUND THE RT ANTI-SKID TRANSDUCER CONNECTOR PISDR WWMA950070Cap · defectivePILOT REPORTED, THE BRAKES FAILED ON THE CAPTAIN'S SIDE, BOTH PEDALS. CYCLED THE BRAKE ANTI-SKID SWITCH WITHOUT RESTORING THE BRAKE EFFECTIVENESS. THIS WAS THE SECOND OCCURANCE OF THE SAME PROBLEM ON THE SAME DAY. MAINTENANCE FOUND THE NR 4 MAIN LANDING GEASDR 9515362275Anti-Skid Cntrl · failedAFTER LANDING ROLLOUT, ANTI-SKID WAS PULSING CAUSING BRAKES TO RELEASE DURING RUNWAY TURN OFF. CREW ABORTED TURN OFF. MAINTENANCE REPLACED ANTI-SKID CONTROL BOX AND OPERATIONAL CHECK NORMAL.SDR ASAA9540058Anti-Skid Light · out of adjustSEA - FLT NR 479 - CREW REPORTED, ANTI-SKID INOP LIGHT ILLUMINATED AFTER GEAR RETRACTION WITH GEAR HANDLE IN UP OR OFF POSITIONS. CYCLED GEAR AND LIGHT EXTINGUISHED WITH GEAR DOWN. ILLUMINATED WITH GEAR UP. LIGHT FINALLY EXTINGUISHED PASSING 20,000 FEET. LSDR REXA95061Transducer Assy · malfunctionedBRAKES OCCASIONALLY FAIL TO STOP AIRCRAFT UNLESS ANTI-SKID SYSTEM IS TURNED OFF. SEPT 11, 1995 TO SEPT 18, 1995, THREE WRITE-UPS. SEPT 11, OHMED ALL WHEEL SPEED TRANSDUCERS AND NO DEFECTS NOTED. SEPT 14, REPLACED LEFT AND RIGHT INBOARD WHEEL SPEED TRANSDUCESDR WTAA950263Anti-Skid · malfunctionedPSP - LEFT ANTI-SKID INOP LIGHT ILLUMINATED DURING TAKEOFF ROLL. ABORTED TAKEOFF WITHOUT INCIDENT. MAINTENANCE DEFERRED ANTI-SKID SYSTEM PER MEL 32-42-2. AIRCRAFT RETURNED TO SERVICE. SUBSEQUENTLY MAINTENANCE CLEARED THE DEFERRAL AFTER ACCOMPLISHING AN INSSDR WWMA950061Transducer · defectiveFLT 5090 - BPT-DFW - AFTER LANDING PILOT APPLIED THE BRAKES AND THE ANTI-SKID LIGHT CAME ON. THE CONTROL TOWER REPORTED SMOKE, THE ANTI-SKID WAS TURNED OFF AND THE BRAKES WORKED NORMALLY. UPON INVESTIGATION MAINTENANCE INSPECTED THE NR 4 BRAKE AND REPLACED TSDR 9513572202Transducer · malfunctionedAFTER LANDING, TOWER REPORTED SMOKE EMITTING FROM LEFT MAIN GEAR. FIRE DEPARTMENT INSPECTED AND FOUND NR 2 TIRE FLAT. AIRCRAFT WAS TOWED TO THE GATE. MAINTENANCE REPLACED NR 1 TIRE, NR 2 BRAKE, TIRE AND ANTI-SKID TRANSDUCER. OPERATIONAL CHECK NORMAL.SDR 95ZZZM500Control Box · looseFLT EWW262 - KMIA-KFLL - ON LANDING ROLL OUT AT KFLL, THE BRAKES FADE WITH ANTI-SKID ON. MAINTENANCE RESECURED THE ANTI-SKID CONTROL BOX. TESTED THE ANTI-SKID SYSTEM PER MM CHAPTER 32-43-0. NO DEFECTS WERE NOTED. (M)SDR REXA95052Computer · failedNO BRAKES WHILE TAXIING. REMOVED AND REPLACED ANTI-SKID COMPUTER IAW SAAB AMM. (M)SDR AALA951445Anti-Skid Contlr · malfunctionedIAH - FLT 2063 - DURING LANDING ROLL-OUT, NR 1 AND NR 2 MLG TIRES EXPERIENCED BLOW OUTS WHEN BRAKES WERE APPLIED. AIRCRAFT STOPPED WITHOUT INCIDENT. REPLACED NR 1 AND NR 2 MLG WHEELS AND BRAKES AND PLACARDED ANTI-SKID SYSTEM. AIRCRAFT MAINTENANCE FERRY IAH/SDR SIMA952191Screws · brokenCRP - FLT NR 3857 - BLUE AND GREEN HYDRAULIC SYSTEM LOW LEVEL LIGHT ON INFLIGHT, LANDING GEAR EXTENDED MANUALLY, ZERO FLAPS LANDING. CFR CALLED OUT. (M)SDR F3LA95015Anti-Skid Contl · failedBZN - UPON LANDING, FLIGHT CREW REPORTED LOSS OF LEFT MAIN LANDING GEAR BRAKES. MAINTENANCE INSPECTED AND BLED THE BRAKE SYSTEM AND PERFORMED AN OPERATIONAL CHECK. SYSTEM CHECKED OK. A FAULT WAS FOUND ON THE ANTI-SKID MODULE TEST AND THE LEFT OUTBOARD ANTI-SDR COM60528Control Box · defectiveANTI-SKID SYSTEM FAIL, CIRCUIT BREAKER TRIPPED. REPLACED ANTI-SKID CONTROL BOX.SDR CAL950593Anti-Skid Contl · inoperativeEWR - FLT 0223 - WHEN FIRST APPLYING THE BRAKES ON LANDING AT EWR, THERE WAS LITTLE BRAKING AVAILABLE. ALL GAUGE PRESSURES WERE NORMAL. MAXIMUM APPLICATION OF BRAKES WAS REQUIRED TO BRING THE AIRCRAFT TO A STOP. ALL FOUR ANTI-SKID TRANSDUCERS CHECKED GOOD. SDR 9510346614Anti-Skid Module · leakingDURING CLIMB AND GEAR RETRACTION, THE NR 4 HYDRAULIC SYSTEM QUANTITY DECREASED TO 1 GALLON. THE CREW DUMPED APPROXIMATELY 100,000 LBS OF FUEL, RETURNED TO MSP, AND LANDED WITHOUT INCIDENT. REPLACED THE LEFT BODY GEAR ANTI-SKID CONTROL MODULE, LEAK AND OPERASDR 95ZZZX3375Connector · looseKDAY/KFLL - FLT 032 - NO BRAKING ACTION ON LANDING WITH ANTI-SKID ON. MAINTENANCE RESECURED RECEPTACLE ON THE ANTI-SKID CONTROL BOX. BLED BRAKES, AND PERFORMED A REAR WHEEL SPIN-UP TEST IAW MM, CHAPTER 32-00. OPERATIONAL CHECKS OF THE ANTI-SKID AND MLG BRAKSDR COM60495Pseu · defectiveANTI-SKID CAUTION MESSAGE IS ON WHEN PARKING BRAKE IS RELEASED. REPLACED THE PROXIMITY SENSOR ELECTRONIC UNIT.SDR USAA950544Control Unit · failedBWI - FLT 126 - FLIGHT EN ROUTE MCO TO DCA WHEN ANTI-SKID INOP LIGHT ILLUMINATED. FLIGHT DIVERTED TO BWI DUE TO RUNWAY LENGTH. MAINTENANCE REPLACED ANTI-SKID CONTROL UNIT. (M)SDR REXA95040Anti-Skid Syst · brokenLOST BRAKES WHEN TAXIING INTO RAMP. TURNED OF ANTI-SKID BRAKES, RETURNED. REMOVED AND REPLACED LT I/B AND O/B TRANSDUCER. REMOVED AND REPLACED I/B AND O/B HUB CAPS, BOTH CLIPS WERE BROKEN. ACFT OK FOR SERVICE. (Z)SDR REXA95039Anti-Skid Syst · malfunctionedON TAXI INTO GATE, LOST BRAKE'S. TURNED ANTI-SKID OFF, BRAKES RETURNED. CHECKED AND CLEANED ALL ELECTRICAL CONNECTORSREF AMM 32-43-00. NO FAULTS DETECTED, OPS CHECKED GOOD ACFT OK FOR SERVICE. (Z)SDR COM60470Control Unit · defectiveANTI-SKID CAUTION MESSAGE ON EICAS. REPLACED THE ANTI-SKID CONTROL UNIT.SDR COM11887Relay · defectiveANTI-SKID INOP LIGHTS ILLUMINATED DURING LANDING GEAR RETRACTION. REPLACED RELAY KO255.
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