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.
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
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 COEA2016030801803Unknown · malfunctionedFLIGHT 7299 BRAKE INOPERATIVE WO 159364 DISCREPANCY. DURING TAXI, THE FIRST OFFICERS RT BRAKE FAILED. ACFT WAS TAXIED BACK TO RAMP. OPERATIONS CHECKED BRAKES IAW JIC 32-42-00 OPT 10000-001 & ENG RUN & TAXI CHECKLIST. NO FAULT FOUND. OPERATIONS CHECKED GOOSDR SIMA20160304003Shutoff Valve · faultyBRAKE RT FAULT, HAPPENED ON FINAL, CAUSED GO AROUND & EMER DECLARED. READ & ACCESSED CMC TEST PAGE IAW AMM 45-45-45. TEST & RESET BRAKE CONTROL SYS IAW AMM 32-41-00 WITH NO BRAKE MSGS OF ANY KIND. R & R THE INBD BRAKE SOV, COMPLIED WITH WR 2016-03-05 23-004SDR E07A2016030700001Control Unit · inoperativeON TAXI OUT TO TAKEOFF, CREW HAD A BRAKE FAILURE. ACFT DEPARTED TAXI WAY & STOPPED WHEN THE RT GEAR SANK INTO THE DIRT. ACFT WAS RECOVERED & INSPECTED FOR DAMAGE. NO DAMAGED NOTED BUT DETERMINED THAT BRAKE CONTROL UNIT FAILED. INSTALLED REPAIRED BRAKE CONTSDR A6WA201643637Unknown · not reportedNOTICED PUDDLE TO THE LT OF RT MAIN GEAR & LT NR 3 TIRE SMOKING.SDR VNAA2016030100004Brake · failedCREW REPORTED RECEIVING A RT OTBD BTMS MASTER WARNING AT FL160. DECLARED AN EMERGENCY, RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R THE BRAKE ASSY. MAINTENANCE PERFORMED CHECKS IAW THE AMM AND THE ACFT WAS RELEASED FOR SERVSDR A6WA201643622Tire · smokeON POST FLIGHT SMOKE COMING FROM RT MLG TIRE BTMS 4, 4, 5, 5 WAS 4,4,6,6.SDR C77A20160222017Fuse · failedEMERGENCY PARKING BRAKE HYD FUSE FOR NR 1 HYD SYS OTBD BRAKES FAILED OPERATIONAL TEST OF TASK CARD 32-40-00-001. R & R LT EMER HYD BRAKE FUSE IAW AMM 32-41-15 ON WO 20091921M2. OPERATIONS CHECKED GOOD.SDR CA160226006Brake · cracked(CAN) DURING A GENERAL VISUAL INPECTION OF THE NOSE LANDING GEAR IT WAS DISCOVERED THAT A CRACK HAD DEVELOPED ACROSS THE SPIN BRAKE ASSEMBLY TWO LOWER MOUNTING HOLES. THIS AIRCRAFT HAS 3315.7 HRS AND 2898 CYCLES. NO OTHER DAMAGE WAS NOTED.SDR WX0A2016022373093Brake Sys · contaminatedDURING DECELERATION PASSING 70 - 60 KNOTS, WHEN TRANSITIONING TO PEDAL BRAKES, BOTH BRAKES GET VERY GRABBY. HAD TO TAP THE BRAKES A FEW TIMES TO LOOSEN THEM UP. WILL NOT BE ABLE TO DUPLICATE DURING SLOW TAXI CHECKS. REF LOG PAGE 635331 IAW MOC REQUEST PERFOSDR CA160222004Check Valve · failed(CAN) UPON ACFT SHUTDOWN, CAS MESSAGE, BRAKE ACCUMULATOR, DISPLAYED. BRAKE ACCUMULATOR PRESSURE WOULD NOT HOLD RENDERING PARK BRAKE INEFFECTIVE. ACFT HAD AN IDENTICAL PROBLEM 18 MONTHS EARLIER THAT WAS THE RESULT OF A FAILED HYD CHECK VALVE, PN L95H07-202 UPSDR FDEA201602050457Line · misinstalledON ARRIVAL, FOUND NR 10 TIRE BLOWN. ON FLT CREW DEBRIEF, THEY HEARD OR FELT NOTHING. ASCU FAULTED WHEEL NR 10 NOT TURNING. TROUBLESHOT IAW FIM 32-40-01, FOUND LINE CROSSED AT NR 9 & 10 FWD BRAKE PORT. CORRECTED FWD BRAKE LINE IAW FIM 32-40-01. PERFORM ASDR CALA2016020495086Line · leakingON THE RNWY FOR TAKEOFF, FOLLOWING ACFT REPORTED FLUID PUDDLE UNDER RT MLG & SIGNS OF VISIBLE FOG. REPLACED 2 RT NR 4 MLG BRAKE LINES WITH NEW LINES. BLEED BRAKES IAW AMM 32-41-00. OPERATIONS CHECKED GOOD.SDR WX0A2016020473087Servo Valve · failedTHE CREW WAS USING AUTO BRAKES FOR LANDING. THE AUTO BRAKES WERE DISENGAGED BETWEEN 120 - 100 KTS BY APPLYING MANUAL BRAKING. WHEN THE AUTO BRAKE SYS WAS DISENGAGED THE CREW FELT A JOLT BUT THE ACFT STAYED ON THE CENTERLINE THROUGHOUT THE ROLLOUT. THE ACFT SDR HYIA20160205001Cotter Pin · brokenPILOT REPORTED LT BRAKE FAILED. RUDDER PEDAL APPEARS DISCONNECTED FROM CYLINDER. INSPECTED & FOUND THE CONNECTING CLEVIS PIN HAD FALLEN OUT DUE TO BROKEN COTTER PIN. MX THEN RE-CONNECTED LT RUDDER PEDAL TO BRAKE CYLINDER IAW MM CH 20-10-01.SDR SIMA20160128010Check Valve · failedRETURN LINE CHECK VLV OF THE EMER & PARKING BRAKE SYS FAILED OPERATIONAL CHECK. R & R EMER & PARKING BRAKE SYS RETURN LINE CHECK VLV IAW AMM 32-44-08. LEAK CHECKED GOOD.SDR DALA2016020900946Brake · lockedEXPERIENCED THE NR 1 BRAKE LOCKING UP DURING TAXI OUT TO THE RUNWAY. ACFT RETURNED TO BLOCKS. MAINTENANCE FOUND THE NR 1 BRAKE ASSY AND BEARING DAMAGE. REPLACED NR 1 BRAKE ASSEMBLY AND NR 1 TIRE ASSY. INSPECTED AXLE WITH NO DAMAGE FOUND.SDR IPXA2016012798536Valve · inoperativeAFTER LEVELING AT FL 320 HOT BRAKE ECAM. BRAKE TEMPS ON ALL 4 TIRES INDICATED 300 AND CLIMBING . DESCENT TO FL200 TO EXTEND GEAR. TEMPS CONTINUE TO CLIMB TO 485. THEN COOLED TO NORMAL TEMPS, EMERGENCY DECLARED UPON LANDING. FOUND CODE 81 & 82 IN BTCU R&R SDR SIMA20160118002Shuttle Valve · inoperativeNUMBER 1 HYD QTY LOW ADVISORY ON EICAS UPON TAKEOFF & LG RETRACTION INDICATION IN THE AMBER. FOUND HYD 1 LOW & HYD 2 TO BE HIGH, INSPECTED HYD SYS 1 FOR LEAKS, NO LEAKS NOTED. R & R 1 & 4 BRAKE SHUTTLE VLVS IAW AMM 32-49-03. OPERATIONS CHECKED GOOD & LEAK CSDR ASOA20160117002RTransducer · shortedPILOT REPORTED AFTER LANDING AND EXITING ON HIGH SPEED TAXIWAY THEY EXPERIENCED A COMPLETE BRAKE FAILURE AND COULD NOT STOP THE ACFT. EMERGENCY BRAKE WAS PULLED TO STOP ACFT SAFELY. MAINTENANCE R & R THE PILOT LT BRAKE PEDAL POSITION TRANSDUCER WITH OPS CHECSDR QXEA2016011600036Brake Sys · malfunctionedMAIN BRAKES ARE NOT RESPONSIVE, WITH OR WITHOUT THE ANTI-SKID BEING ON. PERFORMED VISUAL INSPECTION OF BRAKES AND BRAKE LINES, CONNECTIONS FOR LEAKS WITH NO LEAKS NOTED. C/W BLEED THE BRAKES WITH MAIN BRAKE SYS, REF Q400 AMM TASK 32-42-00-870-801. TAXIED ACFSDR SIMA20160112001Sensor · defectiveBRAKE OVERHEAT, WARNING MSG OCCURRED AT ROTATION SPEED ON TAKEOFF. LT OTBD BRAKE TEMP CONTINUED RISING TO 18, BEFORE SLOWLY DROPPING BACK TO NORMAL. R & R THERMOCOUPLE SENSOR IAW AMM TASK 32-46-01. OPERATIONS CHECKED GOOD.SDR 29GA2016010900002Brake Sys · malfunctionedCOMING TO GATE, BRAKES FELT SPONGY. BLEED BRAKE ASSY IAW 32-42-00-MM, OPS CHECK OK IAW 32-40-05 MM.SDR 29GA2016010700002Brake Sys · malfunctionedWHEN PRESSURE TO BRAKE, DELAYING IN BRAKING ACTION. BLED THE BREAK SYS IAW AMM 32-42-00-02. BREAKING SYSTEM FUNCTIONS PROPERLY. OPS CHECKED GOOD.SDR ANCF2016010401Control Unit · malfunctionedAFTER POS 4 BACK, THE PARKING BRAKE DIDN'T WORK. AFTER CB'S RESET, ECAM MSG BRAKES ALTN BRK FAULT APPEARED. IAW AMM 32-43-34-000-+001400-001A THE ALTERNATE CONTROL UNIT, ABSU, WAS R & R. OPERATIONAL TEST WAS SATISFACTORY. PN E21328002, SN OFF S01420 & SN OSDR DXTA2016010406149Brake Cable · brokenLEFT BRAKE PEDAL ON LT SEAT HAS NO PRESSURE. LT WEAR PIN WILL MOVE WHEN LT BRAKE ON THE RT SEAT IS PRESSED. FOUND PILOT'S LT MIDDLE BRAKE CABLE BROKEN. R & R CABLE WITH NEW IAW MM 32-44-10. RIGGED & SAFETIED CABLE, TAXI CHECKED GOOD AT THIS TIME.SDR DXTA2015123006148Control Unit · malfunctionedBRAKE FAIL CAS MSG ON LANDING ROLL OUT, STILL HAD RT BRAKE WITH NO ANTI-SKID. ODOR NOTICED IN COCKPIT OF PLANE. ACFT WAS TOWED FROM TAXIWAY. TROUBLE SHOT BRAKE FAIL, FOUND RT MLG WST & WOW HARNESS DEFECTIVE. REPLACED RT WOW & WST HARNESS, PN 2317-1146-401,SDR ASMF201602003Coupling · leakingDURING TRANSIT CHECK, IT WAS DETECTED A HYD LEAK IN THE MAIN BRAKE NR 4. PERFORMED REVISION DETECTING HYD LINE COUPLE LEAKING OF THE MAIN BRAKE NR 4, THE HYD LINE COUPLE & PACKING SEAL WERE REPLACED IAW AMM 32-41-11, TESTED CORRECT.SDR FISA2016122900005Stator · brokenRIGHT BRAKE LOCKED UP AFTER LANDING WAS COMPLETED, WHILE TRYING TO TURN AROUND ON RUNWAY.SDR FISA2016122900004Stator · brokenLEFT BRAKE LOCKED UP AFTER LANDING WAS COMPLETED WHILE TRYING TO TURN ONTO TAXI WAY.SDR CA160105009Brake Assy · seized(CAN) AFTER AN EXTENDED TAXI AND SHUTDOWN OF ACFT, WHILE DEBOARDING PASSENGER PILOT HEARD A SUDDEN BLAST OF AIR COMING FROM RT SIDE OF THE ACFT. PILOT FOUND RT TIRE DEFLATED. WHEN INSPECTED BY ENGINEER, FOUND TIRE FUSE PLUGS MELTED AND BRAKE ASSEMBLY SEIZED. SDR CA160125013Brake · malfunctioned(CAN) THE FOLLOWING HAS BEEN REPORTED TO MFG: FOLLOWING A NORMAL START AND RUN UP TO 100 PERCENT NR, THE PARKING BRAKE HANDLE WAS THEN RELEASED BY PLACING PRESSURE ON THE TOE BRAKES AND PUSHING THE BRAKE HANDLE DOWN. NO CAS MESSAGES ILLUMINATED PRIOR TO OR DSDR 29GA2015122100002Valve · malfunctionedCAPTAINS SIDE BRAKE AUTHORITY IS MINIMAL REQUIRES EXCESSIVE PRESSURE. REPLACED BRAKE VALVE, OPS CHECK GOOD.SDR 7GMB2015121720151Control Valve · inoperativeAFTER STARTING NR 2 ENG, BRAKE INBD INOPERATIVE MSG APPEARED ON EICAS. TROUBLE SHOT & FOUND INBD BRAKE CONTROL VLV INOPERATIVE. REPLACED INBD BRAKE CONTROL VLV. OPERATIONS CHECK & LEAK CHECK TESTED GOOD. THE ACFT WAS RETURNED TO SERVICE.SDR 2015FA0000650Relay · failedAT APPROXIMATELY 12:28 THE PILOT INFORMED THE TOWER THAT HE HAD A LOW POWER BRAKE ENUNCIATOR LIGHT. THEY ASKED HIM IF HE WANTED THE EQUIPMENT OUT AND HE STATED YES. DURING THE DEBRIEF HAD A VIBRATION IN THE ACFT, HE DECIDED TO KEEP FLYING THE ACFT HERE. APPRSDR O2GA2015121080801Hose · defectiveLEFT BRAKE INOPERATIVE DURING TAXI. REPLACED THE COPILOTS SIDE MASTER CYLINDER & HOSE. TAXI CHECK COMPLIED WITH. ACFT RTS.SDR AALA20151211001Transducer · damagedAIRCRAFT WAS GNDED. DURING TAKEOFF ROLL, WHEEL NOT TURNING LIGHT ILLUMINATED. TAKEOFF ABORTED PRIOR TO 80 KNOTS. FOUND BROKEN PINS AT NR 2 WHEEL SPEED TRANSDUCER. R & R TRANSDUCER IAW AMM 32-43-02.SDR 29GA2015120200004Brake · out of limitsWHILE EXITING THE HIGH SPEED TAXIWAY AFTER LANDING, AT APPROXIMATELY 40 KNOTS, LIGHT BRAKES WERE APPLIED. PLANE DID NOT SLOW DOWN WITH INCREASED BRAKING, PLANE DID SLOW DOWN APPROXIMATELY 1 TO 2 SECONDS AFTER APPLYING INCREASED PRESSURE ON BRAKES. ACFT DECELSDR DXTA2015111306128Brake Assy · failedAIRCRAFT LANDED WITH FROZEN BRAKES. LT MAIN HAS DAMAGE TO TIRES & WHEELS. RT SIDE DAMAGE TO TIRES ONLY. CHANGED ALL 6 WHEELS AND TIRES. CHANGE ALL 4 MAIN BRAKES. INSPECTED LT AND RT ENGINES FOR FOD DAMAGE. DID A DETAILED INSPECTION OF ALL THE LANDING GEAR.SDR AALA201511239004Warning System · false activationON TAKEOFF GOT RED ECAM CONFIG PARKING BRAKE ON PARK, BRAKE WAS NOT ON. ACFT ABORTED TAKEOFF AT ABOUT 50 KNOTS & RETURNED TO GATE WITHOUT FURTHER INCIDENT. INSPECTED & CYCLED THE BRAKE SYS SEVERAL TIMES WITH NO FAULTS BEING NOTED.SDR CA151203006Valve · failed(CAN) ECAM YELLOW SYS LOW PRESSURE IN FLIGHT. 10 SECONDS AFTER, LOSS OF MOST OF THE YELLOW SYSTEM HYDRAULIC FLUID AND ASSOCIATED PITCH FEEL, SPOILER, YAW DAMPER 2 AFS.SDR K5SR2015112327126Brake Assy · crackedWHILE PERFORMING THE NR 1 AND NR 2 WHEEL AND TIRE CHANGE. UPON REMOVING THE WHEEL ASSEMBLIES FROM THE ACFT FOUND NR 1 AND NR 2 BRAKE ASSEMBLY CARBON ROTOR ASSEMBLIES TO BE CRACKED AND BROKEN OFF FROM THE KEY WAY GUIDES IN SEVERAL PLACES. R & R NR 1 AND NR 2 SDR QXEA2015111900611Module · malfunctionedT/O WARNING TEST ACCOMPLISHED ON TAXI OUT WAS OK. WHILE HOLDING SHORT OF THE RUNWAY WITH PARK BRAKE ON, CLEARED FOR TAKEOFF PARK BRAKE WAS RELEASED WHILE ROLLING ONTO THE RUNWAY, PARK BRAKE CAUTION, ILLUMINATED THEN WHEN OUT. TAKEOFF WARNING TEST ACCOMPLISHESDR AALA201511189007Control Unit · malfunctionedWHILE ADVANCING THRUST FOR TAKEOFF, RECEIVED BRAKE SYS 1 FAULT. DISCONTINUED TAKEOFF AT APPROX 20 KNOTS. PERFORMED BSCU ADJUSTMENT & TEST IAW AMM 32-46-00. ALL CHECKED GOOD.SDR SIMA20151114001Sensor · failedBRAKE OVERHEAT ON EICAS AFTER TAKEOFF, RT INBD INDICATOR IN AMBER, COMPLIED WITH AOM VOL 1. PROCEDURES RETURNED, NOT AN OVERWEIGHT LANDING SINK RATE 300FT PER MIN. DEFERRED RT INBD BRAKE INDICATION. R & R BRAKE TEMP SENSOR IAW AMM 32-47-01. OPERATIONS CHECSDR COZA20151112061Metering Valve · leakingLEFT BRAKE METERING VLV LEAKING FLUID FROM VLV BODY. REPLACED VLV & NO LEAKS FOUND.SDR 7GOR20151130001Module · failedLOSS OF BRAKE ACTUATION.SDR AALA20151106006Sensor · faultyRECEIVED HOT BRAKES MSG DURING TAKEOFF ROLL. TAKEOFF ABORTED AT APPROX 80 - 90 KNOTS. FOUND NR 4 BRAKE TEMPERATURE SENSOR FAULTY. R & R NR 4 BRAKE TEMPERATURE SENSOR IAW AMM 32-47-15. ACCOMPLISHED ACFT TAXI. BRAKE TEMPERATURE INDICATION CHECKED NORMAL IAWSDR CA151106002Switch · damaged(CAN) ON TAKEOFF ROLL FLIGHT CREW REJECTED TAKEOFF AT APPROXIMATELY 103 KTS DUE TO A TO CONFIGURATION WARNING. ON TAXI BACK TO TERMINAL CREW NOTICED, PARKING BRAKE, ON CREW ALERT PANEL WITH THE PARKING BRAKE NOT ENGAGED, NO OTHER WARNINGS ON THE CAP DURING THESDR 29GA2015110900001Brake Sys · unresponsiveON TAXI-IN AFTER LANDING, APPLY BRAKES WITH NO RESPONSE. TURN ANTI-SKID SWITCH OFF AND BRAKES WORK. BLED ALL BRAKES AND PERFORMED OPS CHECK OF BRAKES WITH ANTI-SKID ON AND OFF SYSTEM OPS CHECKS GOOD.SDR SIMA20151104001Control Unit · failedAFTER LANDING, THE INBD BRAKES WERE IN THE AMBER WITH THE NR 3 RT INBD BRAKE, CAUSING A BREAK OVERHEAT ON THE EICAS. THE NR 1 & 4, BOTH OTBD BRAKES WERE SHOWING IN THE GREEN RANGE, AS THOUGH THEY HAD DONE NO BRAKING. R & R BRAKE CONTROL UNIT IAW AMM 32-41-02
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