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 SIMA20160517004Shutoff Valve · trippedBRAKE INBD INOPERATIVE MSG PRESENTED UPON GEAR EXTENSION. PERFORMED GO AROUND & COMPLETED AOM 1 PROCEDURES, NORMAL LANDING, ALL BRAKE TEMPS INDICATOR REMAINED IN THE GREEN 324M3800. FOUND INBD SOV TRIPPED, RESET INBD BRAKES OPERATIONS CHECKED OK. R & R BCU SDR E07A2016051300001Brake Assy · warpedRIGHT OTBD NR 4 MAIN TIRE, BRAKE LOCKED UP AND FLAT SPOTTED TIRE TILL IT DEFLATED.SDR 29GA2016051200004Brake Sys · malfunctionedACFT REQUIRES MORE THAN NORMAL BRAKE PEDAL PRESSURE AT MODERATE TAXI SPEEDS. ALL BRAKE AND HYDRAULIC INDICATIONS APPEAR NORMAL. BLED BRAKES IAW AMM 32-42-00-02. SERVICED HYD FLUID SYSTEM IAW AMM 12-10-29-03. OPS CHECKS GOOD.SDR ASMF2016072600002Brake · failedAIRCRAFT RETURNED TO PLATFORM DUE TO DURING PUSH BACK, THE MESSAGE IN EICAS AND STATUS AUTO BRAKE SYSTEM FAIL AND AUTO BRAKE / BRAKE NUMBER 7. MAINTENANCE PERSONNEL PERFORMED FIM DMC-B787-A-32-40-F1-U7A-421A-A PROCEDURE, NO CONFIRMING FAILURE AND THE MESSAGE OSDR 29GA2016051200003Brake Sys · weakSTIFF AND WEAK BRAKES. BLED BRAKES IAW AMM 32-42-00-02. OPS CHECK GOOD.SDR HYIA20160511002Fitting · loosePILOT REPORTED LT BRAKE INOPERATIVE & LARGE AMOUNT OF HYD FLUID NOTED ON POST FLIGHT INSPECTION. PERFORMED VISUAL INSPECTION OF LT BRAKE SYS & WW, FOUND CALIPER TO WW FLEXIBLE HOSE TOP FITTING LOOSE. RE-TORQUED CALIPER TO WW FLEXIBLE HOSE TOP FITTING IAW MM SDR NTF2016F00000Adjuster · looseDURING POST FLIGHT INSPECTION, ADJUSTER ASSEMBLY WAS LOOSE. FURTHER INSPECTION FOUND NUT, BALL, AND THE TUBE WERE MISSING. THE ADJUSTER ASSY WAS INOPERATIVE.SDR DXTA2016050606235Printed Ckt Board · defectiveAFTER TAXING & BRIEFLY SETTING THE PARKING BRAKE, THE AMBER BRAKE ANNUNCIATOR & LT BRAKE MINELCO WERE INDICATING. NO OTHER BRAKE ABNORMALITIES WERE OBSERVED. COMPUTER CODES, LT 325 PEDAL SWITCH FAILURE. REMOVED A DEFECTIVE LT BRAKE PCB PN FE422 & SN 4475. SDR 2016FA0000354Brake Sys · malfunctionedNR 2 BRAKE IS APPLIED WITHOUT PILOTS INPUT. THIS HAS HAPPENED FOUR TIMES IN THE LAST FOUR YEARS. RESULTS ARE TIRE BLOW OUTS, OVERHEATED BEARINGS, BRAKES OVER HEATED, MELTED TRANSDUCER AND HARNESS. REJECTION OF LOWER AXLE ASSEMBLY. THIS IS A SERVE SAFETY ISSUE SDR 29GA2016050400002Brake · unknownPARKING BRAKE VERY HARD TO SET, BRAKES FEEL MUSHY, PEDALS GO ALL THE WAY TO THE FLOOR. PERFORMED FUNCTIONAL CHECK OF PARKING BRAKE IAW AMM 32-42-00. OPS CHECK SATISFACTORY.SDR 29GA2016050400001Brake Sys · malfunctionedBRAKES ARE SOFT, PARKING BRAKE IS VERY HARD TO SET. BLED THE BRAKES IAW AMM 32-42-00-02. OPS CHECK GOOD.SDR E07A2016050300001Control Valve · inoperativeUNCOMMANDED BRAKE APPLICATION FOLLOWED BY BRAKE FAIL CAS MESSAGE.SDR QXEA2016042900286Transducer · malfunctionedBRAKING ACTION FOR ACFT, MARGINAL AT HIGH SPEEDS. BRAKES MUSHY AT ALL SPEEDS INCLUDING TAXI SPEEDS. R & R NR 4 MLG WHEEL SPEED TRANSDUCER IAW AMM TASK 32-46-11-000/400-801. ALL TEST GOOD BRAKES NO LONGER MUSHY NO FURTHER DEFECTS, RETURN TO SERVICE.SDR AALA201604299010Control Unit · defectiveAIRCRAFT WAS GNDED. AUTO BRAKE INOPERATIVE, ALSO LOST NORMAL BRAKING ON TAXI INTO GATE BUT NORMAL BRAKING QUICKLY RETURNED. REPLACED THE BRAKE STEERING CONTROL UNIT & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 32-42-34 & 22-97-00.SDR 9JLA201610179068Check Valve · leakingCREW REPORTED THAT AFTER AIRCRAFT SHUTDOWN WITH THE PARK BRAKE SET THE BRAKE ACCUMULATOR WOULD NOT HOLD PRESSURE. TROUBLESHOOTING IDENTIFIED THE EMERGENCY BRAKE CHECK VALVE WAS LEAKING INTERNALLY. THE VALVE WAS REPLACED WITH A NEW UNIT.SDR AALA201604269007Circuit Breaker · openDIVERTED, ACFT WAS NOT GNDED. FLIGHT CREW REPORTED A BRAKE ALTN BRK FAULT ACCU GUAGE SHOWS ZERO MSG & DIVERTED TO MCO WHERE THE AIRCRAFT LANDED SAFELY WITH NO FURTHER INCINDENTS. ACCOMPLISHED TSM 32-43-00-810-832-A DC POWER SUPPY, TSM LOSS OF BRAKE PRESSURE,SDR HALA2016042200030Brake · overheatedTHE CREW SAFELY ABORTED THE TAKEOFF AT 65 KNOTS DUE TO BRAKES HOT MESSAGE ON DEPARTURE ROLL. THE NR 5 WAS BRAKE SHOWING 300 DEGREES. THE BRAKES WERE COOL AND A SPIN CHECK SHOWED NO DRAGGING. DISCONNECTED NR 5 BRAKE AND REPLACED NR 5 BRAKE ASSY.SDR ESMR2016042001Line · leakingTHE PILOTS RT POWER BRAKE VALVE HAS A RIGID ALUMINUM LINE FOR THE SYS PRESSURE LINE PORT. THIS LINE WHEN TIGHTENED MOVES THE LINE TOWARD THE RIGHT RUDDER PEDAL. OVER MANY YEARS THE RUDDER PEDAL HAD CHAFED THE HYDRAULIC SUPPLY LINE AND EVENTUALLY CAUSED A PIN SDR R61A201604190255Warning Message · false activationWITH AUTO BRAKES SELECTED TO MEDIUM AND GEAR DOWN, THE AUTO BRAKES TURNED OFF AND BREAK LT AND BREAK RT FAULT MESSAGES APPEARED. AN EMERGENCY WAS NOT DECLARED AND CREW LANDED WITHOUT INCIDENT. CREW RECEIVED BRAKE OVERTEMP CAUTION MESSAGE. AFTER BRAKES COOLEDSDR FDEA201604181255Crank Assy · defectiveCAPTAIN DURING POST FLIGHT DEBRIEF REPORTED, RT BRAKE PEDAL EXCESSIVE TRAVEL & SLOW TO ACTUATE. R & R CAPTAINS RT BRAKE FEATHERING CRANK IAW EA 8-2720-TO324787.SDR VNAA2016041400015Brake · overheatedBRAKE OVERHEAT MESSAGE DURING APPROACH. THE CREW DECLARED AN EMERGENCY, CONTINUED THE APPROACH, AND LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED CHECKS IAW THE AMM.SDR CALA2016041895277Warning System · false activationAUTO BRAKE FAULT DISPLAYED ON UPPER ECAM SCREEN. TRIED NEW BSCU, SAME FAULTS, NO HELP. ACCOMPLISHED WIRING CHECK OF TACHOMETER WHEEL 4, 22GG, IAW AWD 32-11-02 & AWD 32-42-06. ALL CHECKED OK.SDR UHLA201604140176Warning Message · false activationPARKING BRAKE NOT RELEASED, MESSAGE IN FLIGHT. DECLARED EMERGENCY, RETURNED TO FIELD, LANDED WITHOUT INCIDENT. SERVICED EMERGENCY PARKING BRAKE SYSTEM 1 ACCUMULATOR, INSPECTED BOTH EMERGENCY PARKING BRAKE PRESSURE SWITCHES, NO DEFECTS FOUND. CLEANED AND RESSDR QXEA2016041200258Brake · overheatedAFTER LANDING DURING POST FLIGHT INSPECTION FOUND THE LT OTBD MAIN WHEEL SMOKING. EXCESSIVE BRAKING WAS NOT USED. PERFORMED INSPECTION AND FOUND SIGNS OF OVERHEATING ON THE BRAKE. REPLACED THE TIRE AND THE BRAKE AND PERFORMED EXCESSIVE BRAKING INSPECTION IAWSDR FDEA201604071155Connector · defectiveAFTER TAKEOFF, RECEIVED LEVEL 2, BRAKE OVERHEAT, MAX TEMP 692. LEVELED OFF AT 17,000 SLOWED, LOWERED GEAR FOR 10 MINUTES. RAISED GEAR, TEMP STARTED TO RISE. DIVERTED & LOWERED GEAR AT FL 200, LANDED FLAPS 50. R & R NR 6 BRAKE TEMP CONNECTOR IAW AMM 20-30-0SDR UHLA201604060164Accumulator · underservicedPARKING BRAKE NOT RELEASED MESSAGE IN FLIGHT. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. SERVICED EMERGENCY/PARKING BRAKE ACCUMULATOR IAW AMM 12-12-05. CLEANED EMERGENCY/PARKING BRAKE PRESSURE SWITCH CONNECTOR IAW AMM 32-44-09. OPS TEST GOOD.SDR 29GA2016040700001Brake Sys · malfunctionedCAPTAIN BRAKE PEDALS WENT ALMOST ALL THE WAY TO THE FLOOR FOR BRAKE EFFECTIVENESS. ALL HYD PRESSURES WERE IN THE GREEN. PERFORMED BLEEDING OF THE BRAKES IAW AMM 32-42-00-02, PERFORMED OPS CHECKS, OPS CHECK IS SATISFACTORY.SDR QXEA2016040500243Brake Sys · weakON LANDING FO NOTED THAT THE BRAKES DID NOT SEEM TO BE RESPONDING TO PEDAL INPUTS. CAPTAIN NOTICED THAT BRAKES DID NOT SEEM TO GRAB. AT THE GATE THE BRAKES FELT SPONGY. ACFT DID NOT PULL IN ANY DIRECTION. FOUND ALL BRAKES ROUGHLY THE SAME TEMPERATURE UPON ASDR R61A201604040235Control Module · inoperativeCREW REPORTED THAT THE BRAKES STOPPED WORKING ON LANDING AND TAXI TO GATE. MAINTENANCE R & R BCM MAU 1 SLOT 5 ALONG WITH RT PRESSURE TRANDUCER IAW AMM AND OPS CHECKED GOOD.SDR 29GA20160404001Brake Sys · weakBRAKES SPONGY. CHECKED HYD QTY, ACCUMULATOR PRESSURE, BRAKES FOR WEAR. BLED BRAKES IAW AMM CHAPTER 32-42-00-02 LOW SPEED MAINTENANCE TAXI GOOD, HIGH SPEED CREW TAXI CHECK GOOD.SDR WX0A2016040173123Tachometer · faultyDURING CLIMB OUT BRAKES AUTO BRAKE FAULT & BRAKE RELEASED ECAM POSTED ON LANDING ROLL OUT, NOTICED NR 2 BRAKE REMAINED RELEASED. PERFORMED TSM 32-42-00, FOUND 21GG TACH INOPERATIVE. REPLACED NR 2 MLG WHEEL SPEED TACH & OPERATIONS CHECKED GOOD IAW AMM 32-42-5SDR 29GA2016032900002Brake Sys · malfunctionedAIRCRAFT REQUIRES EXCESSIVE BRAKE PRESSURE AND MAKES A GRINDING NOISE INTERMITTENTLY. BLED THE BRAKE SYSTEM IAW AMM 32-42-00-02 AND OPS CHECKED IAW AMM 32-42-40-05. NO DEFECT NOTED. OPS CHECK GOOD.SDR 29GA2016032800004Brake Sys · weakBRAKES INTERMITTENTLY USE FULL PEDAL TRAVEL WITHOUT BRAKING SUFFICENTLY. BLEEDED ACFT BRAKE SYSTEM IAW AMM 32-42-00-02. NO FAULT NOTED AFTER, OPS CHECK NORMAL.SDR 29GA201603260001Brake Sys · malfunctionedNO BRAKES ON PARKING WITH ANTI-SKID SWITCH OFF ABLE TO STOP AIRCRAFT. INSPECTED AND TROUBLESHOT ANTI-SKID IAW TI NR: 340B-3243-2013-002, WM 32-43-00, AND AMM 32-34-00. OPS CHECK GOOD UNABLE TO DUPLICATE DISCREPANCY ON TAXI WITH ANTI-SKID SWITCH OFF.SDR DJFA20160324001Transducer · malfunctionedAIR TURN BACK DUE TO BURNING SMELL IN ACFT AFTER TAKEOFF. CAS MSG, BRAKE NOT RELEASED. LANDED WITH NORMAL BRAKING & NO INDICATIONS OF DRAGGING BRAKES. R & R EMER & PARKING BRAKE PRESS TRANSDUCER IN LT NOSE COMPARTMENT. OPERATIONS CHECKED GOOD.SDR AALA201603259003Accumulator · low pressureAIRCRAFT WAS NOT GNDED. AFTER STOPPING AT THE GATE, ENGS OFF, MAIN BRAKES SET, RUDDER PEDALS FULL DEPRESSED WOULDN'T KEEP THE ACFT FROM ROLLING BACK. PARKING BRAKE ENGAGED TO STOP ACFT. GOOD PSI ON TRIPLE INDICATOR. PERFORMED OPERATIONAL TEST OF NORMAL BRASDR SIMA20160322005Warning System · false activationBRAKE LT FAULT & BRAKE RT FAULT ADVISORY MSG ON APPROACH, DECLARED EMER. MSGS ON EICAS WHEN GEAR SELECTED DOWN. REPEAT WRITE UP. CORRELATED CMC FAULT MSGS =324411001BCM & 32411005BCM, OT PR PULSE FLTS. PERFORMED IBIT BCM1 PR PULSE INT TEST IAW FIM 32-41-00SDR 29GA2016032300002Brake Sys · weakLOSS OF BRAKES DURING TAXI. BRAKES DID NOT WORK DURING A CRAWLING TAXI SPEED. PERFORMED BRAKE BLEED ON NR 1 BRAKE IAW AMM 32-42-00. TAXI OPS CHECK IS GOOD.SDR SIMA20160322001Warning System · false activationUPON APPROACH, WE HAD AN ADVISORY BRAKE LT FAULT & BRAKE RT FAULT. WE PLACED THE GEAR IN THE UP & RAN THE APPROPRIATE CHECKLIST ON OUR NEXT APPROACH. THE MSGS WERE NOT THERE WHEN THE GEAR WAS PLACED IN THE DOWN POSITION. WE HAD DECLARED AN EMER & THE LANDINSDR WX0A2016032373111Selector Valve · faultyON ROLL OUT AFTER LANDING, AFTER ENGAGING MANUAL BRAKING, ALLOWED AUTO BRAKES LO TO SLOW ACFT TO 60 KTS. BRAKES STARTED SLIPPING AT APPROX 48 KTS GND SPEED DOWN TO ABOUT 15 KTS GND SPEED. R & R SELECTOR VLV ALT BRAKE IAW AMM 32-42-11*-PB 40. OPERATIONS CHECSDR 29GA2016032200002Brake Sys · weakDURING TAXI, AFTER LANDING, BRAKES FELT MUSHEY AND LATE TO RESPOND TO PEDAL PRESSURE. BLED THE BRAKE SYS IAW AMM 32-42-00-05, LEAK CHECK AND OPS CHECK NORMAL.SDR 29GA2016032200001Brake Sys · weakWHILE PARKING, BRAKES FELT SOFT. PERFORMED PROCEDURE TO BLEED THE WHEEL BRAKE SYSTEM IAW AMM 32-42-00-02, LEAK CHECK GOOD.SDR SIMA20160319002Unknown · malfunctionedBRAKE INBD INOPERATIVE WHEN LOWERING GEAR FOR LANDING, MSG REPEATED, SUBSEQUENT APPROACH COLD INBD BRAKE TEMP & AMBER OTBD TEMPS AFTER LANDING. TROUBLE SHOT IAW FIM TASK 32-41-00-810-802 NO RELATED CMC MSGS FOUND. OPERATIONS CHECKED MAIN BRAKE SYS IAW AMM 32SDR WX0A2016031673104Tachometer · faultyREPOSITION FLIGHT, NO PAX ONBOARD. ONCE CLIMBING OUT, THE ECAM STATUS MSG OF BRAKE RELEASE CAME BACK. LOOKED IN THE QRH & THE AOM, IT LED THE CREW TO THE INFORMATION OF AT LEAST 1 WHEEL BRAKE WOULD NOT FUNCTION DEPENDING ON WHICH HYD SYS WAS AFFECTED. EVEN SDR DJFA20160314001Unknown · malfunctionedON LANDING, CREW REPORTED LOSS OF BRAKES. ACFT EXITED THE END OF THE RUNWAY & WAS DAMAGED. THIS SDR WILL BE UPDATED UPON COMPLETION OF THE CORRECTIVE ACTION.SDR C77A20160311021Fuse · failedNUMBER 1 HYD SYS EMER BRAKE FUSE FAILED OPERATION TEST OF TASK CARD 32-40-00-001. R & R LT EMER HYD BRAKE FUSE IAW AMM 32-41-15 ON WO 20093701M3. OPERATIONS CHECKED GOOD. .SDR WX0A073103Brake Sys · malfunctionedAUTO BRAKE INOP, WAS APPLIED TO THE ACFT. DURING FLIGHT THE CREW RECEIVED AN ECAM STATUS MSG OF BRAKE RELEASE. QRH & AOM LED THE CREW TO THE INFORMATION OF AT LEAST 1 WHEEL BRAKE WOULD NOT FUNCTION DEPENDING ON WHICH HYD SYS WAS AFFECTED. THE FLIGHT DIVERSDR DALA2016031401932Brake · fireAFTER LANDING THE NR 3 MLG BRAKE WAS SHOWING HOT. MLG NR 1, LOW BRAKE 250 DEGREES. NR 2, LT BRAKE 270, NR 3, RT BRAKE 510 DEGREES. NR 4, RO BRAKE 360 DEGREES. UPON WALK AROUND FLAMES WERE OBSERVED FROM MLG NR 3, RT BRAKE. PORTABLE FIRE EXTINGUISHER USED. SDR AALA20160310005Rod · brokenAFTER TAKEOFF, WITH GEAR SELECTED UP, EICAS MSGS, GEAR DOORS, & GEAR DISAGREE, WITH VIBRATION. NORMAL INDICATION WITH GEAR DOWN. NO EMER WAS DECLARED & THE FLIGHT RETURNED WITHOUT FURTHER INCIDENT. INSPECTED LT MLG & FOUND NR 2 ANTI-ROTATION BRAKE ROD BROKESDR DXTA2016030806195Control Module · failedON LANDING ROLL OUT, WHEN BRAKING APPLIED TO DECELERATE, BRAKE FAIL MSG ILLUMINATED ON CAS. ZERO BRAKING ACHIEVED USING NORMAL BRAKES. EMERGENCY BRAKE SYS USED. BOTH MLG TIRES FAILED. REMOVED LT & RT WHEEL & TIRE ASSEMBLY. INSTALLED REPAIRED LT & RT WHEEL
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