JASC 3240

Service difficulty reports · 6,462

Reports filed under 3240 · Landing Gear Brake 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 = '3240'
  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 DLM11020040Brake · unserviceableON T/O ROLL NOTICEABLE PULL TO RIGHT. DURING CLIMBOUT CHECKED BRAKE TEMP NO. 8 READ 280 ALL OTHERS AT 60. 20 MINS INTO CLIMB TEMP BEGAN TO INCREASE RAPIDLY. TEMP DIFF LIGHT ALSO ILLUM MAX TEMP AT 475 DEG.__REMOVED AND REPLACED NBR 8 BRAKE ASSY. BLEED NBR 8 BRJan 11, 2002 · N812DE · Doug MD11SDR CA020102002Stator · broken(CAN) DISASSEMBLED BRAKE UNIT AND FOUND STATOR DISC P/N 133-89302 CHG "B" BROKEN. (SEE ATTACHED PHOTO'S).Jan 2, 2002 · Cessna 550SDR 2002UALA00011Monitor · malfunctionedCREW REPORTS HOT BRAKES ON CLIMB OUT WITH GEAR DOWN. SUPPLEMENTAL DATA UPDATE ORIG INDICATION 370 DEG, CLIMBED TO 425 DEG. SUSPECTED INDICATION PROBLEM, BRAKE TEMP CHECKS NORMAL. BSCU BITE CHECK AND PREVIOUS LEG REPORT FAULT BRAKE TEMPERATURE MONITORING UNIT Jan 1, 2002 · N462UA · Airbus A320232SDR DLM90011959Controller · failedFLT DIV- AFTER GEAR EXTENSION UNABLE TO ARM AUTO-BRAKES. AUTO-BRAKE FAIL MSG ON OAP. ANTI-SKID FAULT DISPLAYED ON OAP. REPLACED ASAB CONTROLLER.Dec 19, 2001 · N903DA · Doug MD9030SDR COMA0260039Wheel · crackedVISUAL INSPECTED WHEEL ASSY FOR LEAKAGE AND FOUND I/B SUBASSEMBLY CRACKED AT BOTTOM OF DISK KEY BOSS.Dec 17, 2001 · N729CA · Cndair CL6002B19SDR CA011217022Control Unit · intermittent(CAN) EICAS MESSAGE LT / RT INBOARD BRAKE FAULT (INTERMITTENT).Dec 10, 2001 · Lear 45LEARSDR XC42001F00000Stator · defectiveBRAKE ASSEMBLY (PN 2-1661) FAILED PREMATURELY. NR 1 STATOR CRACKED THROUGH IN 2 PLACES CAUSING SIGNIFICANT DAMAGE TO TORQUE TUBE AND WHEEL ASSEMBLY. PIECE OF STATOR 8 INCHES LONG MISSING. NOTE: MOST RECENT CONFIGURATION OEM PARTS INSTALLED (KIT NR 304-289 CDec 10, 2001 · N504 · Skrsky S58ESDR 2003F00017Brake Assy · contaminatedMOS - FLT 8706 - LEFT BRAKE SPONGY. AIR ENTRAPMENT IN THE LEFT BRAKE SYSTEM. REQUIRES BLEEDING SERVICE, INSPECTION, AND OPS CHECK. BLEED LEFT BRAKE SEVERAL TIMES. BRAKE PEDAL PRESSURE IS GOOD. NO LEAKAGE EVIDENT AT THIS TIME. (M)Dec 4, 2001 · N827FE · Cessna 208SDR AUS20011270Shuttle Valve · faulty(AUS) HYDRAULIC FLUID TRANSFERRED FROM GREEN HYDRAULIC SYSTEM TO YELLOW HYDRAULIC SYSTEM. INVESTIGATION FOUND THAT THE MAIN WHEEL BRAKE SHUTTLE VALVES WERE THE CAUSE OF THE PROBLEM.Nov 28, 2001 · Bac 146200ASDR AUS20011281Brake · missing(AUS) AIRCRAFT NOSE SPAT AND PITOT TUBE DAMAGE WHEN AIRCRAFT RAN INTO THE SIDE OF THE HANGAR WHILE BEING TAXIED FOR REFUELLING. INVESTIGATION FOUND THAT THE PILOT WAS SITTING IN THE RH SEAT AND THAT THE BRAKES HAD BEEN REMOVED FROM THE RH SIDE POSITION. THE RENov 27, 2001 · Parten P68BSDR AALA20012067Manifold · defectiveORD - FLT 795 - EN ROUTE PHL-ORD, SHORTLY BEFORE LANDING LEFT MLG WOULD NOT LOCK IN THE DOWN POSITION. AFTER A SECOND ATTEMPT, LANDING GEAR LOCKED DOWN SUCCESSFULLY. LANDED ORD WITHOUT FURTHER INCIDENT. REPLACED BRAKE SWIVEL MANIFOLD. SWUNG GEAR. SYSTEM GNov 24, 2001 · N1445B · Fokker F28MK0100SDR 2001FA0000612Brake Assy · malfunctionedTHE PILOT STARTED THE AIRCRAFT ENGINE, THE AIRCRAFT STARTED TO ROLL, AT WHICH TIME THE PILOT APPLIED THE BRAKES. THE LEFT BRAKE WAS OPERATIONAL BUT THE RIGHT WAS FLAT. THIS CAUSED THE AIRCRAFT TO SWERVE TO THE LEFT HITTING A CESSNA CARAVAN DAMAGING BOTH AIRCNov 23, 2001 · N9541J · Cessna A188BSDR 2001FA0000679Housing · crackedHOUSING IS CRACKED INSIDE ONE OF THE BOLT MOUNTING HOLES. FATIGUE, DEFECT IN THE IN THE CASTING OF THE HOUSING AND /OR OVERTORQUING OF BOLT ON INSTALLATION.Nov 20, 2001 · Boeing 737*SDR AALA20012048Detector · malfunctionedLHR - FLT 101 - BRAKE HOT LIGHT ILLUMINATED IN CRUISE FLIGHT. ECAM INDICATIONS ON WHEELS 1, 2, 5 AND 6 WERE 400-420 DEGREES. ACCOMPLISHED PROCEDURES IAW OPERATING MANUAL. INDICATIONS REMAINED UNCHANGED. REPLACED BRAKE DETECTION UNIT AND LEFT GEAR BRAKE TEMNov 18, 2001 · N18066 · Airbus A300B4605RSDR DHL2001803016Control Cable · failedNO BRAKE ON BOTH CAPT AND F/O LEFT BRAKE PEDAL. REMOVED AND REPLACED 85/86AA BRAKE CABLE FOR THE LT BRAKES AS PER DACO MM 32-41-0. PERFORMED OPS CHECK, NO FAULTS NOTED. OPS CHECKED OK.Oct 26, 2001 · N803DH · Doug DC873SDR IU62001F00017Housing · crackedHOUSING IS CRACKED INSIDE ONE OF THE BOLT MOUNTING HOLES. LEAKS AT PROOF PRESSURE. FATIGUE, DEFECT IN THE CASTING OF THE HOUSING AND/OR OVERTORQUING OF BOLT ON INSTALLATION.Oct 23, 2001 · Boeing 737*SDR USAASB01295Selector Valve · defectiveLGA - FLT 579 - ON CLIMB-OUT FROM LGA, ENROUTE TO CLT, THE A/C EXPERIENCED A SEVERE VIBRATION THROUGH BOTH THE FIRST OFFICERS AND CAPTAINS RUDDER PEDALS. THE FORWARD CABIN AREA, EXPERIENCED VIBRATION AS WELL. NO VIBRATION IN AFT CABIN AREA. TURNING OFF YAW DAOct 13, 2001 · N420US · Boeing 737401SDR 2001FA0000381Line · chafedRIGHT BRAKE LINE ROUTED UNDER CO-PILOT SEAT PEDISTAL AREA IS CHAFFING ON HEAT DUCT TUBING. SLIDING A 193-6 LOW PRESSURE HOSE OVER THE BRAKE LINE WILL KEEP THE BRAKE LINE FROM DEVELOPING A HOLE.Sep 11, 2001 · N2702L · Cessna 414ASDR 2001FA0000380Line · chafedBRAKE LINE ROUTED UNDER THE CO-PILOTS SEAT PEDESTAL AREA IS CHAFFING ON HEAT DUCT TUBING. SLIDING A 193-6 LOW PRESSURE HOSE OVER THE BRAKE LINE WILL KEEP THE BRAKE LINE FROM DEVELOPING A HOLE.Sep 11, 2001 · N414AN · Cessna 414ASDR 2002F00280Valve · malfunctionedDURING LANDING, THE RIGHT BRAKE WAS INEFFECTIVE FOR SEVERAL APPLICATIONS, THEN PEDAL PRESSURE INCREASE AND THEN BECAME SPONGY. REPLACED NR 4 BRAKE LOCKOUT DEBOOST VALVE IAW MM 33-41-21. OPS CHECKED NORMAL, AIRCRAFT OK FOR SERVICE. (M)Sep 8, 2001 · N760AT · Boeing 7272B7SDR 2001FA0000382Bolt · missingLEFT LANDING GEAR WOULD NOT EXTEND IN FLIGHT. AIRCRAFT WAS HOISTED UP AND THE GEAR EXTENDED AND LOCKED. FOUND A BOLT MISSING FROM THE LEFT BRAKE CYLINDER. PERFORMED SEVERAL GEAR RETRACTIONS AND OPS CHECKED OK.Sep 6, 2001 · N81JD · Cessna 172RGSDR DL73K011465Warning System · malfunctionedUPON INITIAL T/O ROLL EWR, AUTOBRAKE DISARM LIGHT ILLUMINATED. CYCLED RTO SWITCH AND THE AUTOBRAKE LIGHT ILLUMINATED AGAIN. PERFORMED AUTOBRAKE TEST PER M/M. UNABLE TO DUPLICATE.Sep 1, 2001 · N316DL · Boeing 737232SDR 2001FA0000421Housing · crackedHOUSING IS CRACKED INSIDE THE MOUNTING BOLT HOLE. FATIGUE, DEFECT IN THE CASTING OF THE HOUSING AND/OR OVER TORQUE OF BOLT ON INSTALLATION.Aug 21, 2001 · Boeing 737SDR 2001FA0000420Housing · crackedHOUSING IS CRACKED ALONG THE TOP CASTING SEAM. FATIGUE, DEFECT IN THE CASTING OF THE HOUSING AND/OR OVER TORQUE OF BOLT ON INSTALLATION.Aug 21, 2001 · Boeing 737SDR 2001FA0000419Housing · crackedHOUSING IS CRACKED INSIDE THE MOUNTING BOLT HOLE. FATIGUE, DEFECT IN THE CASTING OF THE HOUSING AND/OR OVER TORQUE OF BOLT ON INSTALLATION.Aug 20, 2001 · Boeing 737SDR 2001FA0000456Line · chafedRIGHT BRAKE LINE HAD A HOLE CHAFFED IN IT FROM BEING IN CONTACT WITH THE LINE HEATER DUCT LINE UNDER THE CO-PILOTS SEAT. THE BRAKE LINE RUNS UNDER THE HEAT DUCT AND IS VERY DIFFICULT TO SEE. THIS IS AN ORIGINAL PART.Aug 15, 2001 · N36887 · Cessna 414ASDR AKG2001F00000Line · chafedRIGHT BRAKE LINE HAD A HOLE CHAFFED IN IT FROM BEING IN CONTACT WITH THE HEATER DUCT LINE UNDER THE COPILOTS SEAT. THE LINE RUNS UNDER THE HEATER DUCT AND IS VERY HARD TO SEE.Aug 15, 2001 · N36887 · Cessna 414ASDR COMA0160591BrakeDURING LANDING AT BNA THE AIRCRAFT PULLED TO THE LEFT DURING APPLICATION OF BRAKES, AIRCRAFT TAXIED SAFELY TO THE GATE.INSPECTED BRAKES AND PERFORMED OPERATIONAL CHECK, NO DEFECTS NOTED.Aug 11, 2001 · N937CA · Cndair CL6002B19SDR CA011109002Line · chafed(CAN) ONE OF THE TWO BRAKE LINES THAT RUN DOWN THE LEG CHAFED THROUGH AT THE TOP CLAMP. BRAKES WERE SOFT ON THAT SIDE.Aug 8, 2001 · Bnorm BN2A27SDR RAIA00108003Tire · failed5266-PIT-UPON LANDING IN MEM, ALL FOUR MAIN TIRES FAILED. M,AINTENANCE INSPECTED AND REPLACED ALL FOUR MAIN TIRES, PERFORMED OPERATIONAL CHECK, SYSTEMS CHECKED GOOD. PERFORMED CMC MAINTENANCE DOWNLOAD, NO FAULTS FOUND.Aug 4, 2001 · N809HK · Emb EMB145ERSDR DL76K011266Rod · brokenLANDING GEAR DISAGREE WITH GEAR DOOR ADVISORY WHEN GEAR HANDLE PLACED UP AFTER T/O. NR 8 BRAKE ANTI-ROTATION ROD BROKE. REPLACED BRAKE AND LINE.Jul 30, 2001 · N176DZ · Boeing 767332SDR SIMA200120704Brake · malfunctionedDFW - FLT 3726 - CREW REPORTED NO TOE BRAKES ON CAPTAINS SIDE. AIRCRAFT WAS STOPPED WITH EMERGENCY BRAKES. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)Jul 26, 2001 · N541AT · Aerosp ATR72212ASDR C2XA01CL178Control Unit · defectiveCLE FLIGHT 4172 THE CREW REPORTED THE BRAKES ARE GRABBING EXTREMELY HARD. MAINTENANCE REPLACED THE BRAKE CONTROL UNIT. OPERATIONAL CHECKS WERE GOOD.Jul 25, 2001 · N15912 · Emb EMB145LRSDR AWXA0002044Packing · damagedBDL- EMERGENCY LANDING - FLT 402 - EN ROUTE FROM PHX RO BDL THE CREW FOUND YELLOW HYDRAULIC QUANTITY DECREASING AND TURNED THE YELLOW SYSTEM HYD PUMP OFF PRIOR TO GETTING A RESERVOIR LOW LEVEL WARNING. ON APPROACH THE YELLOW HYD SYSTEM WAS LOST AND THE CREW CJul 23, 2001 · N652AW · Airbus A320232SDR SIMA200119913Sensor · faultyLBB - FLT 3668 - ABORTED TAKEOFF, NR 1 BRAKE TEMP INDICATOR FLUCTUATED. REMOVED AND REPLACED NR 1 BRAKE TEMP SENSOR IAW AMM. OPS CHECK GOOD. (M)Jul 18, 2001 · N628AE · Emb EMB145LRSDR 2001F00226Tube · crackedPRIOR TO TAKEOFF, RUPTURED LEFT MAIN WHEEL BRAKE EXPANDER TUBE. THE RUPTURE CAUSED A HYDRAULIC FLUID LOSS AND SUBSEQUENT LEFT BRAKE LOSS. THE AIRCRAFT WAS STOPPED WITH REVERSE THRUST AND THE ENGINES SHUTDOWN. NORTH OPS WAS ADVISED OF THE SITUATION BY VICTORJul 14, 2001 · N376AS · Doug DC3CSDR DHL2001803566Control Cable · frayedC CHECK - FIRST OFFICER'S LT. BRAKE NR 85 RUN CABLE FRAYED. REMOVED AN REPLACED FRAYED RUN CABLE NR 85 AND PERFORMED ADJUSTMENT AN TEST OF WHEEL BRAKE SYSTEM IAW. MM 32-41-0 PAGE 201-205.Jul 10, 2001 · N803DH · Doug DC873SDR 2002FA0000049Shuttle Valve · malfunctionedRT OUTBOARD BRAKE LOCKED UP DURING TAXI AND CAUSED BRAKE FIRE. VALVE WAS PLACED ON TEST STAND AND REPEATEDLY TESTED VIGOROUSLY FOR 50 MINUTES PER OEMS ATP. NO PROBLEMS WERE NOTED. VALVE WAS THEN TORN DOWN AND INSPECTED. ONLY IRREGULARITY FOUND WAS LOOSE SCJul 5, 2001 · N347PH · Dhav DHC8202SDR BTV2001F00002Rotor · failedDURING A ROUTINE SCHEDULED BRAKE INSPECTION IT WAS NOTED THAT NR 3 BRAKE, OUTBOARD DRIVE ROTOR KEYS WERE FRACTURED. AFTER REMOVING THE WHEEL IT WAS NOTED THAT ALL EIGHT FORWARD SIDE DRIVE CLIPS WERE FAILED. MFG IS INVESTIGATING. A SERVICEABLE BRAKE WAS INSTJun 29, 2001 · N588GA · Gulstm GULFSTREAMGVSDR RRXA010056Pad · failedON DEPARTURE GEAR HANDLE UP NOSE GEAR HAD EXTREME NO ISE AS IF NOSE WHEELS WERE SPINNING AND RUBBING. ALSO HAD EXTREME VIBRATION, GEAR HANDLE PUT BACK DOWN, VIBRATION CONTINUED WITH GEAR DOWN, WHEN ACFT BANKED IN FLT NOSE GEAR HAD LOUD BANG. BOTH GEAR UP INDIJun 27, 2001 · N831AL · Doug DC873FSDR IU62001F00005Housing · crackedHOUSING IS CRACKED INSIDE THE MOUNTING HOLE. FATIGUE, DEFECT IN THE CASTING OF THE HOUSING AND/OR OVERTORQUING OF BOLT INSTALLATION. IMPROVE DESIGN OR CHANGE THE MATERIAL OF THE HOUSING FOR INCREASED STRENGTH AND RELIABILITY.Jun 27, 2001 · Boeing 757*SDR UPS01136160Brake Assy · malfunctionedINSPECTION TYPE:N/A AIRCRAFT PULLED RIGHT ON LANDING WHEN BRAKES APPLIED AND RIGHT BRAKE TEMP ROSE TO 300 DEGREES MORE THAN LEFT. PERFORMED INSPECTION/CHECK OF BRAKES AND ANTI SKID SYSTEM. BLED BRAKES. PERFORMED NORMAL HIGH SPEED TAXI CHECK, USING GREEN ANDJun 22, 2001 · N129UP · Airbus A300F4622RSDR 01FDEA00467Control Unit · failedDURING BLOCK IN WITH PEDALS FULLY DEPRESSED, A/C WOULD NOT STOP. USED PARKING BRAKE TO STOP. BRAKE ANTI-SKID SEL IN NORMAL/ON. REMOVED AND REPLACED BRAKE CONTROL UNIT (29GG) MM 32-42-72-4.Jun 19, 2001 · N455FE · Airbus A310222SDR JGV2001F00002Disk · brokenWHILE PERFORMING ROUTINE INSPECTION ON AIRCRAFT, IT WAS DISCOVERED THAT THE OUTBOARD ROTATING DISK ON THE LEFT BRAKE WAS BROKEN INTO THREE PIECES. THE PIECES FELL OUT OR THE BRAKE ASSEMBLY WHEN THE WHEEL WAS REMOVED FROM THE AIRCRAFT.Jun 15, 2001 · N810SS · Cessna 525SDR DXT2001F00001Brake · looseSPECIAL BOLTS BETWEEN STRIKER AND PISTON HOUSING WERE LOOSE AND WERE BACKED OFF APPROX 114 INCH. BRAKE TORQUE BUTTON HAS WORN A GROOVE AROUND THE INNER CIRCUMFERENCE AT THE WHEEL.Jun 14, 2001 · N979QS · Cessna 750SDR DLM88010990Transducer · failedLANDED WITH AUTOBRAKES SELECTED MAX- VREF WAS 131 AND A/C LANDED ON SPEED IN THE TOUCHDOWN ZONE- AUTOBRAKES SEEMED TO ENGAGE NORMAL BUT AS THE BRAKES WERE SELECTED TO MED BOTH LEFT MAIN TIRES BLEW. REPLACED #2 ANTI-SKID TRANSDUCERJun 14, 2001 · N909DL · Doug MD88SDR HEED073512Brake · wornWORN BRAKES. S/NOS: DEC-82-217, AND NOV-3-467. REPLACED UNIT. S/NOS: JAN 80-286, AND MAR 84-677.Jun 14, 2001 · N278X · Skrsky S76CSDR AUS20010637Manifold · cracked(AUS) LH MAIN LANDING GEAR BRAKE SERVO MANIFOLD CRACKED. INVESTIGATIONFOUND A CRACK IN THE FILTER CHAMBER THREADS. CRACK LENGTH 19.05MM (0.75IN).Jun 7, 2001 · Airbus A320*SDR AUS20010624Manifold · cracked(AUS) LT MAIN LANDING GEAR BRAKE SERVO MANIFOLD LEAKING FROM AREA OFFILTER CAP. INVESTIGATION FOUND A 19.05MM (0.75IN) CRACK IN THE FILTER CHAMBER THREADS.Jun 7, 2001 · Airbus A320*SDR AUS20010590Manifold · cracked(AUS) LT BRAKE MANIFOLD LEAKING. INVESTIGATION FOUND A CRACK LOCATEDBETWEEN PORT A (SUPPLY LINE) AND FILTER CHAMBER.Jun 4, 2001 · Airbus A320*
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