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 SWIA971988Warning Light · illuminatedANTI-SKID OUTBOARD INOP LIGHT ILLUMINATED DURING APPROACH, LIGHT EXTINGUISHED DURING GO-AROUND. RETURNED TO LAX. CHECKED OUTBOARD WHEEL SPEED TRANSDUCER FOR SECURITY. JACKED AIRCRAFT AND CYCLED GEAR 10 TIMES. UNABLE TO DUPLICATE PROBLEM. OPS CHECK GOOD.SDR SWIA971983Selector Valve · malfunctionedANTI SKID OUTBOARD AND MAP BRAKE LIGHT CAME ON, BASE TO FINAL TURN ON APPROACH (2 APPS) ALL INOP LIGHTS GO OUT WHEN GEAR IS RAISED. DIVERTED FROM SBA TO SMX. REMOVED AND REPLACED LANDING GEAR SELECTOR IAW 32-31-03. PERFORMED GEAR SWINGS. OPS CHECKS GOOD. SDR MWEA00772Control Box · malfunctionedMKE - FLT 5 - 'WHEEL NOT TURNING'. ANNUNCIATOR CAME ON DURING TAKEOFF. DISCONTINUED AT 60 KNOTS. RETURNED TO GATE. MAINTENANCE PERFORMED TROUBLESHOOTING PROCEDURE PER MM 32-43-00. INSPECTED ALL TRANSDUCERS, NO DEFECTS NOTED. REMOVED AND REPLACED ANTI-SKISDR MWEA00757Connector · looseFLT 930 - MKE - WHEEL NOT TURNING LIGHT CAME ON AT 70-80 KNOTS. ABORTED TAKEOFF AND RETURNED TO GATE. LIGHT WENT OUT AFTER CLEAR OF RUNWAY. MAINTENANCE INSPECTED AND FOUND NO EVIDENCE OF WHEEL LOCK-UP. ALL TIRES CHECKED NORMAL. FOUND BOTH INBOARD ANTI-SKISDR 20000829SH006Control Valve · failedANTI-SKID CONTROL VALVE FAILED WITHOUT ANY COCKPIT INDICATION. NR 1 LEFT MAIN GEAR TIRE BLEW ON LANDING, EXCESSIVE RESULTING HEAT CAUSED NR 2 LT MLG TIRE TO BLOW ON ROLL-OUT. TROUBLESHOOTING INDICATED THE ANTI-SKID CONTROL VALVE SOLENOID WAS FUNCTIONING, HOWSDR AALA20001275Control Box · failedIAH - FLT 1854 - ON TAXI OUT BRAKES WENT TO FLOOR AND AIRCRAFT DID NOT STOP. REPLACED ANTI-SKID CONTROL BOX. ALSO, REPLACED LT/RT WINDOW HEAT CONTROLLERS. CONTROLLER ELECTRO MAGNETIC INTERFERENCE IS KNOWN TO CAUSE ANTI-SKID AND BRAKING PROBLEMS. ALL OPS CHSDR CA000828003Line · leaking(CAN) ON 2/8/2000 WHILE EN ROUTE BOTH HYDRAULIC FLOW LIGHTS ILLUMINATED. CREW CALLED EMERGENCY, & UNEVENTFUL LDG MADE. A/C SUBSEQUENTLY TOWED FROM RWY. INSP SHOWED THAT HYDRAULIC CONTENTS WERE LOW BUT NO EVIDENCE OF HYDRAULIC LEAK COULD BE FOUND. HYDRAULIC SYSDR SWIA971908Warning Light · illuminatedON APPROACH ABOUT TWO MINUTES AFTER GEAR DOWN RIGHT ANTI SKID 'INOP' BECAME ILLUMINATED (TWO TIMES). ON GEAR RETRACTION LIGHT EXTINGUISHED. DIVERTED FROM ACV TO FAT DUE TO FIELD LENGTH RESTRICTIONS AT ACV. DEFERRED PER MEL 32-42-2.SDR SWAA001323Control Box · inoperativeDIVERSION, ANTI-SKID LIGHT ILLUMINATED. REMOVED AND REPLACED ANTI-SKID CONTROL UNIT AND LT I/B WHEEL SPEED TRANSDUCER PER MM.SDR DHL2000707029Warning Light · illuminatedON TACK OFF ROLL THE RIGHT INBD MAIN LANDING GEAR ANTI-SKID LIGHT ILLUMINATED AT 60 KTS,REJECTED TAKE OFF. PLACED ON D M I PER MEL 32-05.SDR SIMA1833Transducer · inoperativeHOU - FLT 3624 - AFTER TOUCHDOWN AT APPROX 65 KNOTS PILOT APPLIED BRAKES AND RECEIVED AN ANTI-SKID WARNING AND FELT A LURCH TO THE LEFT. MAINTENANCE REMOVED AND REPLACED NR 1 WHEEL TRANSDUCER IAW SAAB MM 32-43-15 AND CORRECTLY INSTALLED ANTI-SKID WIRING ON LESDR RAIA0006005Sensor · failed7628-STL- CREW REPORTS, DURING TAXI LOUD GRINDING AND THUMPING NOISE COMING FROM UNDER COCKPIT FLOOR. MAINTENANCE INSPECTED AND FOUND ANTI SKID UNIT CYCLING DUE TO NR 3 WHEEL SPEED SENSOR. MAINTENANCE REPLACED NR 3 WHEEL SPEED SENSOR.SDR OZIA003125004Control Valve · malfunctionedLEFT BRAKE DRAGGING; HAD TO USE RIGHT BRAKE ONLY ON LANDING. LEFT BRAKES INDICATE HOT; RIGHT BRAKES INDICATE COLD. NOSE STEERING WAS ADJUSTED AND NORMAL BRAKE ANTI-SKID CONTROL VALVE WAS REPLACED PRECAUTIONARY.SDR C2XA00CL038Brake · failedROC - FLT 4398 - THE CREW REPORTED THE BRAKES LOCKED UP SEVERLY ON TAXI. MAINTENANCE REMOVED AND REPLACED NR 3 BRAKE ASSY IAW EMB MM 32-41-05. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. (M)SDR VNAA0005003Control Box · failedTHE CREW REPORTED THAT THE BRAKES WERE COMPLETELY INEFFECTIVE WHILE TAXIING. FLIGHT 4102 RETURNED TO THE GATE WHERE MAINTENANCE BLED THE BRAKES AND REPLACED THE ANTI-SKID CONTROL UNIT IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-00-00. OPERATIONAL CHECKSSDR HNAA0000037Control Valve · failedAFTER LANDING AND CLEARING THE RUNWAY IN FLO ON REPOSITIONING FLIGHT, THE A/C HAD AN UNCOMMANDED AND UNCONTOLLABLE TURN TO THE LEFT. NORMAL BRAKES WOULD NOT FUNCTION. CREW STOPPED THE AIRCRAFT USING THE PARKING BRAKE. AFTER ENGINE SHUTDOWN NR 4 TIRE WAS FOUSDR CA000505003Valve · failed(CAN) LT INNER ANTI-SKID VALVE FOUND LEAKING. VALVE REPLACED AND AIRCRAFT RETURNED TO SERVICE.SDR RRXA000262Transducer · inoperativeON LANDING ANTI-SKID FAILED. FOUND RFO TRANSDUCER TO BE INOP. REMOVED AND REPLACED RFO TRANSDUCER IAW DC-8 MM CH 32-43. PERFORMED SPIN UP ANTI-SKID, OPS CHECKS GOOD, NO DEFECTS NOTED.SDR 20000413SH046Control Box · failedDURING TAH, PRIOR TO TAKEOFF, FOOT BRAKES APPLIED, NO BRAKING ACTION TOOK PLACE. BRAKE SYS PRE-SELECTED TO THE ATTACHED MODE. INVEST REVEALED WITH ANTI-SKID SELECTED THE FAULT LIGHT WAS OUT WITH BRAKES APPLIED. INITIALLY, BRAKES WENT ON, BUT RELEASED AND STSDR RAIA0004015Transducer · failedFLT 6214-DCA, ANTI SKID FAILED DURING TAXI. MAINTENANCE INSPECTED AND DEFERRED PER MEL. MAINTENANCE REPLACED LEFT INBOARD MAIN WHEEL SPEED TRANSDUCER.SDR USAASB00084Valve · failedCLT - FLT 1403 - EN ROUTE FROM TPA-LGA, THE ANTI-SKID INOPERATIVE LIGHT ILLUMINATED. FLIGHT DIVERTED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE LEFT OUTBOARD MAIN LANDING GEAR ANTI-SKID VALVE HAD FAULTED. REMOVED AND REPLACED THE LEFTSDR COMA0060265Warning System · activatedANTI-SKID CAUTION MESSAGE WHEN GEAR SELECTED DOWN. COULD NOT DUPLICATE. NO FAULT CODES IN COMPUTER. AIRCRAFT RETURNED TO SERVICE.SDR MALA000177Indicator · illuminatedAIR TURNBACK. CREW REPORTED THE ANTI-SKID LIGHT ILLUMINATED AFTER THE GEAR WAS SELECTED DOWN. MX REPLACED THE ANTI SKID CONTROL VALVE. PERFORMED FUNCT. CHECK IAW32-40-00.SDR AWXA0000107Control Unit · failedABORTED TAKEOFF ROLL AT 60KTS, DUE TO VERY HARD PULL TO LEFT, TOWER REPORTED SMOKE FROM LT MLG AFTER STOPPING ON RUNWAY WITH HEAVING BRAKING APPLIED. A/C TOWED TO GATE. REPLACED ANTI-SKID CONTROL UNIT. HIGH ENERGY INSPECTION NOT REQUIRED. TT 0003675, M+E =SDR AU000251Valve · leaking(AUS) LT ANTI-SKID VALVE INTERNAL SEAL LEAKING.SDR USAAF00012Control Box · malfunctionedCLT-ROA - FLT 1687 - AFTER TAKEOFF THE ANTI-SKID MESSAGE ANNUNCIATED, SHORTLY AFTER THERE WAS A STAB TRIM 2 MESSAGE. THE ANTI-SKID MESSAGE EXTINGUISHED AFTER THE LANDING GEAR WAS EXTENDED PRIOR TO LANDING. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUSDR AU000166Control Box · faulty(AUS) ANTI-SKID CONTROL BOX AND RELAYS K0021 AND K0420 FAULTY.SDR AT0000009O-Ring · defectiveDURING TAKEOFF, THE HYDRAULIC INDICATOR WENT TO ZERO AND EMERGENCY GEAR HANDLE WOULD NOT RAISE TO UP POSITION. REPLACED O-RING ON RIGHT MAIN LANDING GEAR BRAKE METERING VALVE IAW 737 MM 32-41.SDR 2000ZZZX665Ecc · inoperativeDURING LANDING, THE POWER LEVERS WOULD NOT GO INTO REVERSE PITCH. WHEN THE BRAKES WERE APPLIED, THEY LOCKED UP. THE ANTI-SKID ELECTRONIC CONTROL UNIT AND BOTH MAIN LANDING GEAR AIR/GROUND PROXIMITY SWITCHES, PN 20505, WERE REPLACED. (X)SDR COMA9910186Brake Rotor · brokenLEFT INBOARD BRAKE MAKING LOUD NOISE DURING TOWING. FOUND BRAKE ROTOR BROKEN, LEFT INBOARD BRAKE. INSTALLED SERVICEABLE BRAKE.SDR QXEA9902351Brake · malfunctionedSEA - DURING LANDING ROLL, BREAKING EFFECTIVNESS DIMINISHED NOTICEABLY. INSPECTED ANTI SKID SYSTEM. NO DEFECTS NOTED. OPERATIONAL CHECK GOOD.SDR CA991209038Line · misinstalled(CAN) ON ONE OCCASION BRAKE CHATTER APPEARS ON RT SIDE. FOUND TWO HYDRAULIC LINES CROSSED, REPAIRED.SDR HALA9900199Valves · inoperativeHNL - LEFT OUTBOARD TIRE BLEW WHILE TURNING OFF RUNWAY. POSSIBLE ANTI-SKID FAILURE. DAMAGE TO FLAP ARTICULATING ELBOW AND FLYING GEAR DOOR. REPLACED NR 1 AND NR 2 MAIN TIRES. CDL FOR FLY DOOR AND MEL FOR ANTI-SKID FERRIED PLANE W/GEAR DOWN TO HNL. ON ARRISDR AALA991544Connector · looseSAT - FLT 1636 - DURING TAKEOFF ROLL, MAIN LANDING GEAR WHEEL NOT TURNING ANNUNCIATOR LIGHT ILLUMINATED. TAKEOFF ABORTED AND AIRCRAFT RETURNED TO GATE WITHOUT INCIDENT. RESECURED LOOSE CONNECTOR TO NR 1 MAIN LANDING GEAR ANTI-SKID TRANSDUCER. SYSTEM GROUND SDR GAIA99152Connector · dirtyFLT 563 - EWR-DFW - AFTER LANDING AT DFW ON ROLL OUT THE LEFT BRAKE WOULD NOT APPLY. THE BRAKE OPERATED NORMALLY WITH THE ANTI-SKID OFF. THE AIRCRAFT TAXIED TO PARKING WITHOUT INCIDENT. CLEANED CANNON PLUG ON BOTH DUAL SERVO VALVES IN LEFT WHEEL WELL. OPS SDR RAIA9910009Transducer · failed7102 - STL - RIGHT BRAKE DOESN'T WORK. MAINTENANCE REPLACED RIGHT BRAKE ANTI-SKID TRANSDUCER.SDR USAASB99235Valve · failedORD - FLT 2704 - AFTER TAKEOFF FROM BWI, THE INBOARD ANTI-SKID LIGHT ILLUMINATED AND DID NOT EXTINGUISH AFTER GEAR RETRACTION. FLIGHT DIVERTED TO ORD FOR MAINTENANCE AND LONGER RUNWAYS. LIGHT REMAINED ON WHEN LANDING GEAR WAS DOWN AS WELL. FLIGHT LANDED WITSDR AALA991200Valve · defectiveDFW - FLT 1597 - EN ROUTE FROM ORD-MEX, RIGHT HYDRAULIC FLUID QTY DECREASED TO .56 WHILE LEFT HYDRAULIC FLUID QTY INCREASED TO 1.35. RIGHT HYDRAULIC PUMPS DEACTIVATED AND AIRCRAFT LANDED DFW WITHOUT INCIDENT. REPLACED LEFT AND RIGHT ANTI-SKID SHUTTLE VALVES.SDR 99UAL900417Control Unit · failedDIVERTED TO JFK DUE TO ANTISKID EICAS MESSAGE. *S/D* PERFORMED BITE TEST AND FOUND CARD 2-6 DISPLAYED. REPLACED ANTISKID AUTOBRAKE CONTROL UNIT.SDR MALA976532Control Box · malfunctionedYELLOW SYSTEM ANTI-SKID INOP LIGHT CAME ON DURING FLIGHT, SELECTED GREEN SYSTEM AND LIGHT WENT OUT AND WORKED NORMALLY. MAINTENANCE REPLACED ANTI SKID CONTROL BOX IAW AMM 32-41-47. PERFORMED OPS CHECK, ALL TESTS PASS.SDR HEEA063406Pad · corrodedRIGHT PAD ASSEMBLY HAD CORROSION BEYOND LIMITS. REPLACED WITH SERVICEABLE PART.SDR HEEA063405Pad · crackedPAD CRACKED AND CORRODED. REPLACED WITH SERVICEABLE PART.SDR HEEA063404Pad · crackedPAD CRACKED AND CORRODED. REPLACED WITH SERVICEABLE PART.SDR HEEA063403Pad · corrodedPAD CORRODED BEYOND LIMITS. REPLACED WITH SERVICEABLE PART.SDR 99FDEA00281Contrl · inopON LAND WITHOUT AUTOBRAKES ARMED, MAX BRAKES WERE APPLIED BY AUTOBRAKE SYSTEM. BRAKE APPLIED, GREEN STRIP IN MAX. AUTOBRAKES SWITCH WAS CYCLING ON & OFF. TOE BRAKES USED TO RELEASE BRAKES. REMOVED AND REPLACED AUTOBRAKE SYS CONTROL UNIT AMM 32-42-72-4. RESDR CA990728006Control Box · shorted(CAN) ERROR CODE 54 LEAD TO REPLACEMENT OF ANTI-SKID CONTROL UNIT WHICH WAS SHORTED INTERNALLY.SDR JBXA9900089Transducer · failedFLT 118 RDU TO SWF, ON TAKEOFF ROLL HAD LIFT DUMPER FAULT. ABORTED TAKEOFF AND RETURNED TO GATE. REMOVED AND REPLACED NR 2 MAIN LANDING GEAR WHEEL SPEED TRANSDUCER IAW F-100 MM 32-45-22. NO DEFECTS NOTED, OKAY FOR SERVICE.SDR VNAA9906005Metering Unit · failedANTISKID FAILED ON TAXI OUT. AIRCRAFT RETURNED TO GATE. MAINTENANCE REPLACED BRAKE METERING UNIT.SDR SWIA971509Transducer · failedRIGHT INBOARD ANTI-SKID LIGHT CAME ON UPON GEAR DOWN. RECYCLED AND LIGHT REMAINED ON. RETURNED TO LAX DUE TO RUNWAY LENGTH RESTRICTIONS WITH ANTI-SKID INOP. REMOVED AND REPLACED NR 2 WHEEL SPEED TRANSDUCER WITH SERVICEABLE UNIT. OPS CHECK GOOD.SDR 99ZZZX2353Valve · malfunctionedTHE ANTI-SKID SERVO VALVE WIRES (POSITIVE AND NEGATIVE) WERE CROSSED ON THE REPLACEMENT OF THE POWER BRAKE VALVE. THIS PREVENTED THE ANTI-SKID SYSTEM FROM ACTUATING THE VALVE TO UNLOAD THE BRAKE HYDRAULIC PRESSURE WHEN A SKID OCCURRED ON LANDING RESULTING IN
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