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 DXTA2023092696430Motor · failedWHILE HOLDING SHORT OF RUNWAY, HEARD A POP COME FROM LT CIRCUIT BREAKER PANEL. WAS THE POWER BRKS CIRCUIT BREAKER. LOOKED UP AT ANNUNCIATOR PANEL & ANTI-SKID INOP LIGHT WAS ILLUMINATED. ASKED ATC FOR A TAXI BACK TOWARD THE FBO. LEFT CIRCUIT BREAKER OUT & PLASDR FDEA202309131589Module · misinstalledREPEAT WRITE UP. ON MAINWHEEL TOUCHDOWN, THE NOSE TRACKED TO THE LEFT SIDE OF THE RUNWAY BEFORE NOSE WHEEL TOUCHDOWN. AN AGGRESSIVE AMOUNT OF RIGHT RUDDER WAS REQUIRED TO MAINTAIN CENTERLINE. FLAPS WERE 35, AUTO BRAKES WERE SELECTED TO MEDIAN. WINDS WERESDR UIEA2023082600798Transducer · unknownINFLIGHT ANTISKID EICAS MESSAGE AND OVERHEAD LIGHT ILLUMINATED(<P>PERFORMED FIM TASK 32-42 FT 803. FOUND WHEEL SPEED TRANSDUCER FAULTY. REMOVED AND REPLACED WHEEL SPEED TRANSDUCER IAW AMM 32-42-06. OPS CHK GOOD</P>)SDR DALA2023081406585Unknown · unknownSHIP 9576 -MISC/DE- THE FLIGHT CREW DECLARED AN EMERGENCY WITH ATC DUE TO THE "ANTI-SKID FAIL' MESSAGE ILLUMINATING DURING APPROACH. THE LANDING WAS UNEVENTFUL, AND THE AIRCRAFT TAXIED TO THE GATE. CORRECTIVE ACTION: MAINTENANCE FOUND THE ANTI-SKID CONNECTOR #SDR CALA2023081102491Brake Assy · disengagedNO6 BRAKE FOUND DESINTEGRATED ON ARRIVAL LHR. BRAKE PISTON STATOR MISSING, CARBON ROTOR FOUND WORN INDICATING STATOR MISSING FOR SOME TIME 32-46-01-004-011. TASK 32-11-20-404-011-004. BRAKE ROD INSTALLATION TO BE INSPECTED UNDER IDT REF GMM 09-10-05. 1 (10). PSDR IPXA2023080932999Anti-Skid Sys · warning message*DIVERSION* THE ANTISKID SYSTEM IN OPERATION (NORMAL + ALTERNATE) HAS A FAILURE. ANTISKID EICAS ADVISORY MESSAGE ILLUMINATED DURING CRUISE. C/W FIM 32-42 FAULT TREE 806 AND 807. OPS CHECK GOOD NO FAULTS FOUND.SDR DXTA2023080792380Unknown · unknownUPON LANDING ON A DRY RUNWAY AND INITIAL BRAKE APPLICATION NOTICED THE BRAKES WOULD GRAB AND RELEASE. WHEN WE SLOWED DOWN TO EXIT RUNWAY THE BRAKES KEPT GRABBING AND RELEASING AT TAXI SPEEDS AND EVEN AT SLOWER SPEEDS ON THE FBO RAMP ALL THE WAY DOWN TO A COMPLSDR SWAA2023071478505Unknown · unknownANTI SKID INOP LITE ILLUMINATED<[01] BIT CHECK SHOWS ?PWR A/B?. USING IFIM TASK 32-42-00-810-842; NO FAULTS WERE FOUND. OK FOR SERVICE.SDR 2023F00222Anti-Skid Valve · failedANTISKID INOP LIGHT ON, BEFORE LANDING AND DURING APPROACH. FLIGHT DIVERTED TO CBB (ROUTE VVI-LPB). CORRECTIVE ACTION: HAS BEEN REPLACED ANTISKID VALVE LESFT. IN GROUND TEST NORMALSDR QXEA2023062900099Unknown · unknownAFTER LANDING WHILE EXITING THE RUNWAY @ APPROX 10 KTS, EICAS MESSAGES "BRK LH FAULT" AND "BRK RH FAULT" ILLUMINATED. BRAKES FELT MUSHY FOR ABOUT 4 SECONDS AND THEN RETURNED TO NORMAL FEELING AT WICH POINT EICAS MESSAES DISAPPEARED. REMOVED FROM SERVICE. INTERSDR VNAA202306161111Control Unit · unserviceableLH INBD BRAKE MASTER WARNING AT 10500FT. GEAR RETRACTED. (5MIN) ONCE ON GROUND INDICATED 01 BUT BOX WAS RED. REPLACED LH IB BRAKE TEMPERATURE SENSOR IAW CRJ900 AMM 32-46-01-000/400-801-A01-PSA AND REPLACED ANTI-SKID CONTROL UNIT IAW CRJ900 AMM 32-44-06-000/40SDR FDEA202305220916Unknown · unknownON CLIMB OUT OF ICN TIRE PRESS EICAS. RAN CHECKLIST AND GEAR SYNOPSIS SHOWED RIGHT NOSE GEAR TIRE PRESSURE AT 54 PSI. IT EVENTUALLY WENT TO 0. LANDED AT CAN AND MX TOWED AC TO THE GATE. EMERGENCY DECLARED. CHECK FOUND THE RIGHT NOSE PUNCTURED.REMOVED AND SDR DALA2022120607829Unknown · unknownON CLIMB OUT OF ICN TIRE PRESS EICAS. RAN CHECKLIST AND GEAR SYNOPSIS SHOWED RIGHT NOSE GEAR TIRE PRESSURE AT 54 PSI. IT EVENTUALLY WENT TO 0. LANDED AT CAN AND MX TOWED AC TO THE GATE. EMERGENCY DECLARED. CHECK FOUND THE RIGHT NOSE PUNCTURED.REMOVED AND SDR DXTA2023051986610Unknown · unknownON TAKE OFF ROLL, IMMEDIATELY AFTER THROTTLES WERE SET TO TAKE OFF POWER, RECEIVED A NO TAKE OFF MESSAGE. NO TAKE OFF WAS ACCOMPANIED BY WHITE BRAKE FAULT CAS MESSAGE. DURING TAXI THE BRAKES FELT NORMAL. PERFORMED EMERGENCY PARKING BRAKE OPS CHECK. IAW MM 32SDR SWAA2023051748491Brake · stoppedDURING TAXI AIRCRAFT SHUDDERED THEN CAME TO A STOP. UNABLE TO MOVE UNDER POWER. TRIED AS HIGH ADS 60% N1.<[01] FOUND #3 MAIN BRAKE ASSEMBLY SEIZED. THERMAL PLUGS STILL INTACT. METAL SHAVINGS BETWEEN BRAKE DISKS AND ON BRAKE PUCKS. SEE ATTACHED PHOTOS. PERFORMESDR DALA2023042403171Unknown · unknownSHIP 0659 -BRAKE/TIRE- MULTIPLE LMLG TIRES BLOWN, AND BRAKES LOCKED DURING LANDING. CORRECTIVE ACTION: REPLACED ANTISKID AUTOBRAKE CONTROL UNIT, LT NML ANTISKID VALVE MODULE, LMLG DAMAGED WHEELS AND BRAKES, HYD DISCONNECT BRACKET AND #1-WHEEL SPEED TRANSDUCER SDR CALA2023042101208Transducer · inoperativeW/GEAR HANDLE IN UP POS ANTI SKID INOP LIGHT ON. W GEAR HANDLE I N OFF AND DN ANTI SKID LIGHT OFF REMOVED AND REPLACED #2 MLG ANTI-SKID TRANSDUCER IAW AMM 32-42-11. PERFORMED OPS CHECK W/ REF TO AMM 32-42-00 OPS CHECK GOOD. NO FURTHER DEFECTS NOTED. PARTS USEDSDR HALA2023040300075Unknown · unknownOTHER - UPON LANDING AND DECELRATION #5 TIRE WAS DEFLATED TO ZERO PRESSURE. AIRCRAFT WAS DIFFICULT TO MANUVER AND WE WERE UNABLE TO TAXI. SHUT A/C ENGINES DOWN AND TOWED TO GATE. FOUND #5 TIRE WITH BLOW OUT. PERFORMED A330 AMM TASK 05-51-15-200-801-A. NO DAMAGSDR CALA2023032700903Brake Assy · unknown#1 MLG BRAKE REQUIRES REPLACEMENT DUE TO BROKEN RIVETS R/R BRAKE ASSY (DISCOVERED RIVETS MISSING) IAW AMM 32-41-41. OPS CK GOOD. PARTS USED: 1932685,QTY :1 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1932685 SN OFF 6479 IPC REFERENCE # 32-41-41-01 BRAKE, MLG, SDR CALA2023032700902Brake · unknown#2 MLG BRAKE REQUIRES REPLACEMENT DUE TO BROKEN RIVETS REMOVED AND REPLACED BRAKE PER REF AMM 32-41-41 NO LEAKS NOTED ROTABLE PARTS CHANGE WAS INDICATED - TT # 1932727 SN OFF 7860 BRAKE, MLG, CAR OFF 60-3241-9-0001 7860 ON 60-3241-9-0001 8010SDR YENA2023031700254Unknown · unknownFLT#776, JFK-ORH. 'LH RH BRAKE FAULT ON TAXI OUT; INTERROGATED CMC FOUND 1 OCCURRENCE, NO CORRELATION MSGS. RESET BMC 1 AND BMC 2 IAW 32-41-00. DE-ENERGIZE/ENERGIZE AIRCRAFT IAW 32-42-02. PERFORMED BRKS OPERATIONAL CHECK IAW 32-41-00. NO FAULTS NOTED, COULD NOSDR DALA2023030301588None · noneSHIP 196 - MISC/DE - DUE TO ANTI-SKID FAIL MESSAGE. CORRECTIVE ACTION: REPLACED #3 WHEEL SPEED TRANSDUCER. (9462552)SDR CALA2023021000385Wheel · unknownDUE TO REPORT FROM UPLINE STATION, PLEASE CHECK MLG WHEELS AND VERIFY ALL MLG WHEEL BOLTS INTACT REF AMM 32-41-00. UPDATED MAA CODE FIX USING VENDOR MAA SCREEN CONTRACT MX V939360 SHELDAHL , BRIAN INSPECTED ALL 4 MLG WHEELS CHECK MLG WHEELS AND VERIFY ALL MLG SDR AALA202301277677Transducer · defectiveAIRCRAFT WAS GROUNDED: ON LANDING ROLL OUT LEFT BRAKE/ ANTISKID CONTINUED TO PULSATING BELOW 80 KNOTS AFTER BEING OFF BRAKING. MAINTENANCE REPLACED THE LEFT-HAND BRAKE FAN MANIFOLD PER AMM 32-42-16 (AALA202301279633) AND REPLACED BOTH TRANSDUCERS PER AMM 32-41SDR AALA202301271267Transducer · defectiveAIRCRAFT WAS GROUNDED: ON LANDING ROLL OUT LEFT BRAKE/ ANTISKID CONTINUED TO PULSATING BELOW 80 KNOTS AFTER BEING OFF BRAKING. MAINTENANCE REPLACED THE LEFT-HAND BRAKE FAN MANIFOLD PER AMM 32-42-16 (AALA202301279633) AND REPLACED BOTH TRANSDUCERS PER AMM 32-41SDR AALA202301279633Manifold · defectiveAIRCRAFT WAS GROUNDED: ON LANDING ROLL OUT LEFT BRAKE/ ANTISKID CONTINUED TO PULSATING BELOW 80 KNOTS AFTER BEING OFF BRAKING. MAINTENANCE REPLACED THE LEFT-HAND BRAKE FAN MANIFOLD PER AMM 32-42-16 (AALA202301279633) AND REPLACED BOTH TRANSDUCERS PER AMM 32-41SDR DXTA2023012479060Selector Valve · faultedDURING TAXI FEELS LIKE THE BRAKES DRAGGING. TAKES AN ABNORMAL AMOUNT OF THRUST TO MAINTAIN TAXI SPEED. BRAKE PEDALS HAVE ABOUT AN INCH OF FREE PLAY BEFORE FEELING FIRM. WITH ALL HYDS OFF & PRESSURE BLEED OFF BY CYCLING BRAKES & FLT CONTROLS, BRAKE PEDALS CAME SDR DALA2023019200429Shuttle Valve · faultedCREW ELECTED DE DUE TO RT HYD QTY EICAS MESSAGE AND QUANTITY INDICATION LOW. C/W QRH AND LANDED NORMALLY. R/R LT AND RT ANTISKID SHUTTLE VALVES. A/C RTS.SDR DALA2023011700345Transducer · faultedCREW DECLARED EMERGENCY DURING APPROACH DUE TO NML AND ALTN ANTISKID EICAS MESSAGES AND ASSOCIATED ANTISKID DISCREET LIGHT ILLUMINATED. R & R NR 4 & 8 TRANSDUCER WIRING FROM TRANSDUCERS TO LG JUNCTION BOX. R & R NR 8 TRANSDUCER AND ANTISKID - AUTO BRAKE CONTROSDR VNAA202301131111Transducer · faultedA/SKID OUTBD CAUTION MSG AND OB GND SPLR FAULT STATUS MSG AFTER TAKE OFF. REMOVED AND REPLACED RH OB WHEEL TRANSDUCER IAW AMM 32-44-01-00/400-801-A01. OPS TEST GOOD AT THIS TIME.SDR CALA2023010600039Tire · failedNUMBER 3 TIRE FAILURE REPLACED #3 TIRE DUE TO COMPLETE TIRE FAILURE PER AMM 32-41-11-400-066-A. TIRE PRESSURE CHECK GOOD. ADJACENT TIRE PRESSURE GOOD AS WELL. PARTS USED: 1791401,QTY :1 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1791401 SN OFF 0655 IPC REFERSDR CALA2022123003524Control Module · faultedANTISKID LIGHT ON DURING TAKEOFF ROLL 70 KNOTS CREW HAD SKID LIGHT ON AND OFF 3 TIMES DURING ROLL. AACU PER FIM 32-42 TASK 807 RESISTANCE IS 400 - 600 OHMS NEXT STEP IS CONSISTANTLY FAILS A/B CNTL PER 32-42 TASK 801. A/B CNTL FIM IS TO REPLACE SERVO VALVE PRESDR IPXA2022122189205Anti-Skid Sys · inoperativeINSPECTION TYPE:NA ON LANDING A/C DECELERATED NORMALLY W/ AUTO BRAKES WHEN BRAKES WERE DISARMED A/C CONT BRAKING 50% N1 REQUIRD TO EXIT RUNWAY ATTEMPTED SHORT TAXI, HIGH POWER REQUIRD. A/C PULLED SLIGHTLY TO RIGHT ON TAXI SHUT DOWN SHORT OF RAMP REQUESTED MAINSDR AALA202212216359Control Unit · warning lightAIRCRAFT WAS GROUNDED: ECAM AUTO BRAKE FAULT AFTER TAKEOFF. EMERGENCY DECLARED. FLIGHT RETURNED TO PHX LANDING SAFELY. MAINTENANCE REPLACED BRAKE / STEERING CONTROL UNIT (BSCU) PER AMM 32-42-34 AND ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.SDR HALA2022122100011Control Unit · malfunctionedATB - ANTI SKID FAIL ALERT ON APPROACH WITH LANDING GEAR IN DOWN POSITION. AIR TURN BACK TO HNL. PERFORMED FIM 32-45 TASK 807 - NO FAULTS. PERFORMED AMM 32-45-00-741-001 ANTI-SKID SHUT-OFF VALVE TEST - NO FAULTS. REMOVED AND REPLACED BCU PER AMM 32-45-01-000SDR IPXA2022121629946Warning Message · false activationANTISKID- EICS MESG BRAKE LIMITER + ANTI-SKID STATUS MSG PRFORMED BRAKE SYSTEM BITE TEST IAW M/M 32-42-00-715-297 BITE CHECKED GOOD.SDR DALA2022121308049Warning Message · illuminatedMISC/DE, CREW DECLARED EMERGENCY DURING APPROACH DUE TO ALTN AND NML ANTISKID EICAS MESSAGE AND ASSOCIATED ANTI-SKID DISCREET LIGHT ILLUMINATED. R & R AS/AB CONTROL UNIT IAW AMM NO HELP. DEF NR 7 BRAKE.SDR YENA2022111101117None · failedFLT#42, PBI-LGA. (AIRCRAFT DIVERTED TO JFK) 'BRAKE RH FAULT AND BRAKE LH FAULT; REMOVED AND REPLACED MAIN BRAKE CONTROL VALVE 4. OPS AND LEAK CHECKS ARE GOOD. REF TO AMM 32-41-09.'SDR DALA2022110307120None · noneSHIP 3226 - DIV - TO IAD DUE TO A BRAKES SYS 1 FAULT. CORRECTIVE ACTION: BRAKES SYSTEM 1 PLACED ON MEL 32-42-03A. TROUBLESHOT SYSTEM. BITE TEST OF BCSU 1 WAS GOOD. NO TROUBLE FOUND. NO HISTORY. OK FOR SERVICE. MEL/PLAC REMOVED. (9192090)SDR DALA2022110307124None · noneSHIP 3324 BRAKE RELEASE NO.4 WHEN GEAR DOWN, COMPLED WITH ECAM AND QRH. CORRECTIVE ACTION: R&R WHEEL SPEED TACHOMETER REF A330 AMM 32-42. (9222948)SDR CALA2022103103004Brake · smokeRIGHT MAIN WHEELS SMOKING AFTER LANDING SUSPECT HYD OIL ON NO. 4 BRAKE FROM LEAK/EARLER REMOVED AND REPLACED #4 BRAKE IAW AMM 32-45-11-400-801. OPS CHECK IS GOOD. ADD EMP:006402, 308509, ADDING PARTS INFO ROTABLE PARTS CHANGE WAS INDICATED - TT # 1873924 SN OSDR I5EA2022110300003Transducer · failedANTISKID LIGHT ILLUMINATED IN FLIGHT, EMERGENCY DECLARED INTO KIWA. REMOVED AND REPLACED #4 WHEEL TRANSDUCER AND ANTISKID CONTROL BOX IAW B737 AMM 32-42-11 AND 32-42-21, SYSTEM OPS CHECKS GOODSDR 3EJA956101522Anti-Skid Sys · failedON APPROACH TO ASA FOLLOWING GEAR EXTENSION AMBER ANTI-SKID FAIL CAS MESSAGE ILLUMINATEDSDR YENA2022092600964None · failedFLT#52, MCO-BOS. (AIRCRAFT DECLARED AN EMERGENCY) 'DURING FLIGHT, BOTH BRAKE FAULT LIGHTS ILLUMINATED, UPON LANDING ONLY THE INBOARD BRAKES ACTIVATED; REPLACED BRAKE CONTROL MODULE 1 MAU 1 SLOT 5. NO ACTIVE MESSAGES REF AMM CHAPTER 32-41-07.'SDR DALA2022083005810None · noneSHIP 3146 -ATO- AT 20 KTS DUE TO A BRAKE SYS 2 FAULT. CORRECTIVE ACTION: RESET BSCU 2. REPLACED. (8968192)SDR QXEA2022071800252Brake Assy · wornWHILE TAXIING NOTICED MORE ENG POWER REQUIRED TO TAXI AND PARK. NOTICE LEFT BRAKES MUCH HOTTER THAN NORMAL. FELT LIKE POTENTIALLY LEFT CALIPER IS HUNG UP? NOT SURE TEMP STAYED IN THE YELLOW NO OVERHEATED. REMOVED FROM SERVICE. PERFORMED GVI OF THE L/H AND R/H SDR CALA2022070401644Brake Assy · cracked#2 MAIN BRAKE ASSY KEYS CRACKED. REMOVED AND REPLACED #2 MLG BRAKE ASSY. BLEEDING AND INSTALLATION TEST GOOD.SDR CALA2022070401642Brake Assy · cracked#1 MAIN BRAKE ASSY KEYS CRACKED. REMOVED AND REPLACED # 1 BRAKE ASSY.SDR DALA2022070504637None · noneSHIP 3114 - ATO - DUE TO BRAKE SYSTEM 2 FAULT MESSAGE RECEIVED WHEN ADVANCING THROTTLES. CORRECTIVE ACTION: BSCU CHANNEL 2 DEFERRED PER MEL. REPLACED BOTH NOSEWHEEL STEERING HANDWHEEL TRANSMITTERS (1GC AND 2GC). OPS CHECK GOOD.(8343918)SDR FDEA202206261566Tire · delaminatedPDIS 880 32-41 3226 26JUN22 MEM FACT U SUSPECTED TIRE FAILURE ON TAKEOFF IN OSAKA. LANDED WITHOUT INCIDENT. TIRE DID INCUR FURTHER DAMAGE. NEED CHANGE RH NOSE WHEEL ***EMERGENCY DECLARED*** RH NOSE TIRE FOUND TO HAVE A COUPLE STRANDS OF CO
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