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.

SDR 042703Brake Assy · failedWHILE TAXING ON THE RAMP, BOTH BRAKES AND STEERING FAILED. CREW USED EMERGANCY BRAKES TO STOP THE AIRCRAFT. NOSE OF AIRCRAFT BUMP INTO THE RAILING. MAINTENANCE SUSPECTS ANTI-SKID SYSTEM.Apr 27, 2003 · N72LL · Lear 35ASDR DXTA200300012Brake · malfunctionedDURING TAXI OUT FOR DEPARTURE CO-PILOT FELT THE BRAKES MOMENTARILY DISENGAGED. PILOT TOOK CONTROL AND HAD SAME EXPERIENCE. AIRCRAFT RETURNED TO BLOCK. PERFORMED ANTI-SKID SYSTEM CHECK ON GROUND AND SYSTEM PERFORMED NORMALLY.Apr 20, 2003 · N313QS · Cessna 560CESSNASDR P5CA0300784Control Unit · inoperativeON PUSHBACK RT WING FRONT ANTI-SKID LIGHT ILLUMINATED. DE-ACTIVATED NR 14 BRAKE & DEFERRED ITEM. ONE DEFECTIVE CHANNEL WITHIN CONTROL UNIT.Mar 20, 2003 · N505MC · Boeing 7472D3BSDR KPVA200314Warning Light · illuminatedFLT 1550 - HNL - INBOARD AND OUTBOARD ANTI-SKID CAUTION LIGHTS ILLUMINATED ON TAXI. PERFORMED ANTI-SKID SELF TEST. NO MALFUNCTION DEFECT CODES NOTED. TESTED SYSTEM IAW DHC-8 MM 32-46-00, PARAGRAPH 3, PAGE 3. (M)Mar 19, 2003 · N808WP · Dhav DHC8103SDR DXTA200300008Pressure Switch · failedBRAKE PUMP RUNS CONTINUOUSLY WHEN BRAKES ARE APPLIED. LOW BRAKE PRESS ANNUNCIATOR ILLUMINATES.Mar 14, 2003 · N323QS · Cessna 560CESSNASDR MWEA030132Control Box · inoperativeWHILE ARMING ANTI-SKID RIGHT OUTBOARD AND INBOARD LIGHTS REMAINED ON. REMOVED AND REPLACED ANTI-SKID CONTROL BOX.Mar 13, 2003 · N209ME · Doug DC932SDR ARWA20030302Wire · damagedON FINAL ANTI-SKID LIGHT STAYED ON WITH LFI INDICATION. CHECKED ANTI-SKID WIRING IAW W/D 32-3-0. FOUND BROKEN WIRE GOING TO LT IN-BOUND VALVE, REPAIRED WIRE IN ACCORDANCE WITH MM 20-50-1, OPERATIONAL CHECKED ANTI-SKID SYSTEM IAW MM 32-43-0. OPERATIONAL CHECKMar 11, 2003 · N441J · Doug DC863FSDR CA030312023Warning Light · illuminated(CAN) DURING APPROACH, ANTI-SKID INOP ANNUNC ILLUM. EMERG SYS WAS UTILIZED FOR FINAL BRAKING. ILLUM OF ANTI-SKID ANNUNC, NORMAL BRAKING, ANTI-SKID OR POWER BRAKES ARE BLOCKED, ARE NOT AVAILABLE BY DESIGN. EMER BRAKING MUST BE UTILIZED. A/C WAS RETURNING FROMar 8, 2003 · Cessna 550SDR GAIA03011OPControl Box · inoperativeON LANDING, ALL FOUR TIRES WERE BLOWN. REMOVED AND REPLACED ANTI-SKID CONTROL BOX AND ALL 4 MAIN WHEEL ASSEMBLIES. INSPECTED AIR FRAME AND ENGINES FOR DAMAGE. NO DAMAGE FOUND. AIRCRAFT WAS RETURNED TO SERVICE.Feb 26, 2003 · N6808 · Boeing 727223SDR UO22003F00000Control Box · malfunctionedANTISKID TEST PROBLEM. INTERMITTENTLY, THE RIGHT LIGHT WOULD NOT COME ON DURING TEST. DISCONNECTED THE LT AND RT INPUT CONNECTORS FROM THE ANTISKID CONTROL BOX. ALL INPUTS TO THE BOX WERE CHECKED. NO DEFECTS WERE FOUND. TRIED ANTISKID TEST PUSHBUTTON. WHFeb 25, 2003 · N20CF · Amd FALCON10SDR ARWA20030203Valve · failedPRIOR TO 80 KTS. ANTI-SKID LIGHT CAME ON. NOTE: REJECTED TAKEOFF AT KMIA. CHECKED ELECTRICAL SYSTEM IAW MM 32-3-0 SMT 1 & 2 FOUND SYSTEM WORKED NORMAL. REMOVED AND REPLACED LAMP CONTROL BOX IAW MM 32-43-7; PENDING OPERATIONAL CONTROL CHECK. ALSO REMOVED ANFeb 7, 2003 · N784AL · Doug DC863FSDR ARWA20030202Control Box · failedANTI-SKID INOPERATIVE. REMOVED AND REPLACED CONTROL BOX IN ACCORDANCE WITH MM 32-43-6. OPERATIONAL CHECKED GOOD IAW MM 33-43-0.Feb 7, 2003 · N784AL · Doug DC863FSDR 03FDEA00057Valve · failedWHEN LOWERING THE GEAR FOR LANDING GEAR WAS DOWN AND LOCKED. WE HAD ANTI-SKID FAIL WARNING ON CONFIG PAGE. WENT AROUND RECYCLED GEAR DID NOT GET THE WARNING THE SECOND TIME. ALSO TRIED RECYCLING ANTI SKID SWITCH WITH GEAR DOWN DID NOT PUT THE WARNING LIGHT Jan 20, 2003 · N566FE · Doug MD1010FSDR MEX2003330Control Valve · failedFLT 464 - CUL-HMO - AIRCRAFT RETURNED TO PLATFORM, DURING TAXI ANTI-SKID LIGHTS CAME ON. DURING REVISION, DETECTED FAILURE OF DUAL PRESS CONTROL VALVE. THE DUAL PRESSURE CONTROL VALVE AT LEFT INTERIOR SIDE WAS REPLACED IAW MM 32-43-02, ALL TESTS CORRECT. (MJan 8, 2003 · N751RA · Doug DC987SDR DHL2002807014Connector · dirtyAFTER GEAR EXTENSION ANTI-SKID INOP LIGHT CAME ON. GEAR WAS CYCLED, THEN WHEN GEAR WAS PUT DOWN AGAIN ANTI-SKID LIGHT REMAINED EXTINGUISHED. CLEANED CANNON PLUG CONNECTORS AND PERFORMED OPS CHECK OF ANTI-SKID SYSTEM IAW 32-43-4. OPS CHECKED NORMAL.Dec 10, 2002 · N807DH · Doug DC873FSDR MWEA020726Control Box · malfunctionedAUTO BRAKES WERE ARMED, THE MASTER CAUTION LIGHT AND AUTO BRAKE FAIL LIGHTS CAME ON. REMOVED AND REPLACED ANTISKID CONTROL BOX.Dec 8, 2002 · N808ME · Doug DC982SDR COMA0260609WireFLIGHT 5625 T/O ABORTED DUE TO ANTI SKID CAUTION MESSAGE.REPAIRED DEFECTIVE WIRE CONNECTION AT THE R/H OUTBD WHEEL SPEED TRANSDUCEROct 26, 2002 · N932CA · Cndair CL6002B19SDR COMA0260608Connector · brokenFLIGHT 5537 ANTI SKID INOP MESSAGE DURING T/O.REPLACED THE WIRING CONNECTOR AT THE R/H OUTBD WHEEL SPEED TRANSDUCER.Oct 25, 2002 · N932CA · Cndair CL6002B19SDR 02FDEA00753Conduit · out of positionON CLIMBOUT FROM ANC "RED UNSAFE" INDICATION ON PRIMARY INDICATING SYSTEM AND "CONFIGURATION PAGE" AS WELL FOR LEFT MAIN GEAR UNSAFE ON RETRACTION. FOUND FWD ANTI SKID CONDUIT LOOSELY ROUTED THROUGH THE FWD HOSE AND CONDUIT GUIDE ASSY SUSPECT UNDER AIR LOAD AOct 18, 2002 · N586FE · Doug MD11SDR S2YA02039Control Unit · faultyFLT 2151 - BWI-MKE - DURING TAKEOFF, WHEN THE A/C REACHED ABOUT 40 KNOTS THERE WAS INDICATION OF ALTERNATE ANTI-SKID. THE CREW ABORTED THE TAKEOFF CLEARED THE MESSAGE AND TRY AGAIN ONLY TO ABORT THE SECOND ATTEMPT. THE CREW CONSULTED MX A THIRD ATTEMPT OF TAOct 14, 2002 · N360SK · Dorner DO328300SDR COMA0260545Connector · defectiveFLIGHT 6039 ANTI SKID CAUTION DURING T/O.REPLACED THE L/H OTB WHEEL SPEED TRANSDUCER CONNECTOR.Sep 27, 2002 · N959CA · Cndair CL6002B19SDR 2002UALA01449Transducer · failedAIRCRAFT RECEIVED ANTI SKID EICAS MSG ON TAKEOFF ROLL. REPLACED NR 5 ANTI-SKID TRANSDUCER. OP CHECK NORMAL.Sep 23, 2002 · N178UA · Boeing 747422SDR 00043Switch · failedLANDING AT KYIP AIRCRAFT HAD NO BRAKING ACTION ON SYSYTEM NR 1 , CAPT TOOK CONTROL OF AIRCRAFT AND WENT TO SYSTEM NR 2 , AIRCRAFT BEGAN TO SLOW, CAPT TURNED AIRCRAFT THRU GRASS AND BACK ON TO THE TAXI WAY TO HELP SLOW THE AIRCRAFT. NO DAMAGE TO AIRCRAFT OR AISep 18, 2002 · N165TW · Amd FALCONSDR 02090901Hydraulic Line · burstJust prior to takeoff, the "R Hyd Press" EICAS Msg. came on and right hyd qty had dropped to "0.45RF". Aircraft returned to the gate. further investigation revealed the right aft outboard (#8) Brake flex line had ruptured. Line was removed and replaced as per Sep 5, 2002 · N513NA · Boeing 7572T7SDR VNAA0208012Control Unit · faultyDURING THE CLIMBOUT, THE CREW RECEIVED MULTIPLE ERRATIC BRAKE TEMPERATURE INDICATIONS AND RETURNED TO PIT. MAINTENANCE INSPECTED AND REPLACED THE ANTI SKID CONTROL UNIT IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-00-00. OPERATIONAL CHECKS WERE PERFORMEDAug 9, 2002 · N437JS · Dorner DO328100SDR VNAA0208011Warning System · malfunctionedDURING TAKEOFF, THE CREW RECEIVED A BLUE ANTI-SKID CAS MESSAGE AND ABORTED TAKEOFF. THE CREW RECYCLED THE AIRCRAFT POWER AND THE MESSAGE CLEARED. FLIGHT 4181 WAS CLEARED FOR ANOTHER TAKEOFF ATTEMPT AND DEPARTED WITHOUT ANY FURTHER INCIDENTS.Aug 8, 2002 · N470PS · Dorner DO328100SDR SWIA200211104Anti-Skid Sys · malfunctionedUPON LANDING GEAR EXTENSION AT SBA RECEIVED ANTI-SKID INBOARD AND OUTBOARD EICAS MESSAGES. FOLLOWED QRH PROCEDURE. FOUND THAT AVAILABLE LANDING DISTANCE WAS VERY NEAR BOOK LIMIT WITH BOTH ANTI-SKID INOP. DIVERTED TO LAX. PULLED AND RESET BOTH ANTI-SKID CB'Jul 30, 2002 · N431SW · Cndair CL6002B19SDR USA2002F00068Control Unit · faultyUPON LANDING, CREW REPORTED THE NORMAL BRAKES WERE VERY SOFT AS THE ANTISKID SYSTEM WAS ON MEL. BRAKE PEDALS HAD TO BE COMPLETELY DEPRESSED TO MAKE TURNOFF. FLIGHT TAXIED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE ANTISKID COJul 27, 2002 · N620AU · Boeing 7572B7SDR SWIA200211028Warning System · activatedLEFT ANTISKID INOP ON APPROACH TO LANDING. ON SECOND APPROACH THE LEFT ANTISKID FAILED AGAIN FOLLOWED BY THE RIGHT ABOUT 10 SECONDS LATER. RETURNED TO FAT. INSPECTED ANTISKID SYSTEM, UNABLE TO DUPLICATE DISCREPANCY AT THIS TIME. REMOVED AND REPLACED LEFT AJul 9, 2002 · N234SW · Emb EMB120ERSDR HEEA080252Crosstube · corrodedCROSSTUBE CORRODED BEYOND LIMITS..Jun 27, 2002 · N467PH · Bell 407SDR GAIA02068OPAccessory Unit · inoperative(LANDING GEAR ACCESSORY) SCHEDULED FLIGHT, DURING GEAR RETRACTION, THE PARKING BREAK ILLUINATED. CREW RECYCLED THE GEAR WITH ON CHANGE IN INDICATION. CREW DECLARED AN EMERGENCY LANDING. AT ABOUT 1000 FEET THE LIGHT EXTINGUISHED AND THE AIRCRAFT LANDING WEMay 31, 2002 · N916PG · Boeing 727287SDR GAI2002F00001Accessory Unit · inoperative(LANDING GEAR ACCESSORY) SCHEDULED FLIGHT, DURING GEAR RETRACTION, PARKING BRAKE LIGHT ILLUMINATED. CREW RECYCLED THE GEAR WITH NO CHANGE IN INDICATION. CREW DECLARED AN EMERGENCY LANDING. AT ABOUT 1000 FEET THE LIGHT EXTINGUISHED AND THE AIRCRAFT LANDING May 31, 2002 · N916PG · Boeing 727287SDR AUS20020508Control Box · faulty(AUS) ANTISKID CONTROL BOX FAULTY.May 27, 2002 · Emb EMB120SDR Z972002F00000Transducer · failedANTI-SKID TRANSDUCER FAILED (LOCK UP) CAUSING THE MAIN WHEEL BEARING TO HEAT-UP INTURN CAUSED LEFT MAIN WHEEL BEARING FAILURE CAUSING SEVERE DAMAGE TO AXLE, LOWER FORK, WHEEL HALVES. ALL NEW PARTS INSTALLED.May 20, 2002 · N118MP · Israel 1124ASDR C1HA200284001Control Valve · malfunctionedMAIN GEAR ANTI-SKID OUTBOARD ANNUNCIATOR CAME ON AFTER TAKEOFF - INTERMITTENT. RETURNED BACK TO MSP. REMOVED AND REPLACED LT O/B ANTI-SKID CONTROL VALVE IAW MM. OPS CHECKS NORMAL.May 20, 2002 · N684CA · Boeing 7272S7SDR 0201599969Valve · leakingDURING START WHEN THE CREW ATTEMPTED TO PRESSURIZE THE RIGHT HYDRAULIC SYSTEM, THE HYDRAULIC PRESSURE INDICATION DID NOT RISE AND THE HYDRAULIC QUANTITY INDICATION DROPPED TO ZERO. FLIGHT ABORTED THE START AND RETURNED TO THE GATE. MAINTENANCE FOUND THE RIGHMay 14, 2002 · N9333 · Doug DC931SDR AUS20020441Connector · loose(AUS) RT INBOARD ANTI-SKID TRANSDUCER CONNECTOR PLUG LOOSE.May 13, 2002 · Dhav DHC8102SDR QXEA0200672Warning System · malfunctionedSEA- OUTBOARD ANTI-SKID CAUTION LIGHT ILLUMINATED AFTER TAKING IT OUT OF START/FEATHER FOR TAXI. AFTER COMPLETING EMERGENCY CHECKLIST, RECYCLED ANTI-SKID. INBOARD ANTI-SKID ILLUMINATED AND OUTBOARD EXTINGUISHED. RAN ENGINES. PERFORMED ANTI-SKID SYSTEM SELFApr 19, 2002 · N345PH · Dhav DHC8202SDR SWIA200210771Connector · dirtyANTISKID INOP MESSAGE ON LEFT SIDE ILLUMINATED DURING TAKEOFF ROLL. ABORTED TAKEOFF. CLEANED CANNON PLUGS AT ANTISKID HARNESS AND SWAPPED RIGHT SIDE TRANSDUCERS INBOARD TO OUTBOARD TRANSDUCERS. GROUND OPS CHECKS GOOD.Apr 8, 2002 · N251YV · Emb EMB120ERSDR GTIA020274Control Box · malfunctionedDTW - FLT 909 - AT 80 KIAS ON TAKEOFF WHEEL NOT TURNING LIGHT CAME ON ABORTED TAKEOFF. REMOVED AND REPLACED ANTI-SKID CONTROL BOX. BITE TEST AND SYSTEM CHECK OK IAW MD80 MM 32-43-00. (M)Apr 1, 2002 · N814NK · Doug DC983SDR MEX2002046Control Valve · failedHMO-LAS - WHEN LANDING GEAR GOT DOWN, ANTI-SKID IGHTS TURNED ON. AS CONSEQUENCE OF SPARE PARTS MISSING, AN AIRCRAFT CHANGE TOOK PLACE. LEFT ANTI-SKID DUAL CONTROL VALVE WAS REPLACED IAW MM 32-43-02, TESTS WERE PERFORMED OK.Feb 21, 2002 · N214AM · Doug DC987SDR 02FDEA00089Control Unit · failedDURING FLIGHT TEST BRAKE LAND ALL MAIN LANDING GEAR TIRES BLEW (10) EACH. REMOVED AND REPLACED ALL MLG WHEEL AND TIRE ASSY. REMOVED AND REPLACED ANTI-SKID CONTROL UNIT PER AMM 32-45-01-2.Jan 26, 2002 · N311FE · Doug DC1030FSDR MALA020138Control Box · failedDURING FLIGHT 2868 BRAKES FAILED BUF, WORKED AFTER PUMP SET TO OVERRIDE. NO INTERRUPTION OF FLIGHT. MAINTENANCE REPLACED ANTI-SKID CONTROL BOX PER TECH REP. ALL CHECKS GOOD AT THIS TIME.Jan 23, 2002 · N68XJ · Saab SF340ASDR CA020207003Brake · malfunctioned(CAN) DURING TAXI- ANTI-SKID TEST FAILURE - WIRES BG15B20BLU & GB30B20WHT - SUSPECT CYCLIC FAILURE.Jan 18, 2002 · Cndair CL6012A12SDR AWXA200200022Warning System · malfunctionedPHX - ABORTED T/O - FLT 644 - S - UPON RELEASE OF BRAKES FLIGHT CREW RECEIVED AMBER WARNING MESSAGES FOR INBOARD AND OUTBOARD ANTI-SKID CHANNELS INOPERATIVE AND AUTO-BRAKES, AIRCRAFT ABORTED TAKEOFF AND RETURNED TO GATE. AT GATE MAINTENANCE ISSUED A DPI, MEL Jan 12, 2002 · N184AW · Boeing 737277SDR P5CA0200629Wire · brokenRT BODY GEAR LEFT REAR (NR 11) ANTI-SKID LIGHT CAME ON AND WOULD NOT RESET. WHEEL ASSY RETORQUED FOR PRECAUTION PER MM 32-45-01. NR 11 BRAKE DEACTIVATED PER MEL. REPAIRED BROKEN WIRES AT TRANSDUCER ELECT CONNECTION PER MM STANDARD PRACTICES. REACTIVATED NRJan 11, 2002 · N806FT · Boeing 747249FSDR DL757011999Module · faultyAFTER T/O ANTI-SKID INOP LIGHT EICAS ANTI-SKID ADVISORY AND STATUS MSGS ALTN ANTI-SKID AND NORM ANTI-SKID. PERFORMED BITE CHECK FAULTS NR 2 XDCR. FOUND BACKSHELL LOOSE AND SECURED SAME. REPLACED ANTI-SKID MODULE. NO CURRENT FAULTS.Dec 31, 2001 · N685DA · Boeing 757232SDR C2XA01TY215Service difficultyTYS DURING A SCHEDULED 1-C INSPECTION THE EMERG./PARKING BRAKE SYSTEM FAIL A OPS. CHECK. MAINTENANCE R/R THE #2 BRAKE CONTROL VALVE AND PERFORMED A LEAK AND OPS. CHECK.ALL WORK WAS ACCOMPLISHED IAW EMB 135 AMM 32-41-06 AND WILL BE REL. UPON COMPLETION OF THE CDec 29, 2001 · N14514 · Emb EMB135LRSDR 2001UALA02444Transducer · malfunctionedPLANE DIVERTED TO LAX DUE TO ANTISKID PROBLEM, AND SHORT RUNWAYS AT BUR. SUPPLEMENTAL DATA UPDATE REPLACED LEFT MLG INBOARD ANTI-SKID TRANSDUCER.Dec 20, 2001 · N377UA · Boeing 737322SDR ARWA20011208Control Box · faultyON TAKEOFF ROLL ANTI-SKID LIGHT ILLUMINATED ON SKID CONTROL MONITOR, RF2 AND LF1 LIGHTS WERE ON. ABORTED TAKEOFF AT 65 KNOTS. AIRCRAFT RETURNED TO BLOCKS. REMOVED AND REPLACED ANTI-SKID CONTROL BOX IAW 32-43-6. OPS CHECK NORMAL IAW MM 32-43-0. AIRCRAFT REDec 15, 2001 · N441J · Doug DC863F
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