JASC 3418
Service difficulty reports · 1,641
Reports filed under 3418 · Stall Warning 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 = '3418' 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 = '3418' 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 AUS20020925Bearing · sticking(AUS) ANGLE OF ATTACK TRANSMITTER VANE BEARINGS STICKING.SDR MEX2002264Computer · failedAIRCRAFT RETURNED TO PLATFORM DUE TO AUTO SLAT FAIL LIGHT ON. IN THE EOAP APPEARED A MESSAGE OF AUTO SLAT FAIL. PERFORMED A BITE CHECK TO THE STALL COMPUTERS, BOTH OF THEM RECORDED THE SAME FAILURE. AIRCRAFT WAS SHUT DOWN TO DISCONNECT BOTH AUTO-ACTURATORS SDR CA020816001Sensor · missing(CAN) LEFT ALPHA AIR DATA SENSOR HEAT OFF LEGEND CAME ON IN FLIGHT. ON ARRIVAL IT WAS FOUND THAT THE AOA VANE WAS MISSING. AN INSPECTION OF THE WING AND STABILIZERS WAS C/O, NO DAMAGED WAS FOUND. THE AOA SENSOR WAS REPLACED, AND TESTED SERVICEABLE. AIRCRAFT WASDR WRNA200200003Stall Warning · activatedIN CLIMBOUT, CLEAN CONFIGURATION ABOVE 250 KTS VIOLENT SHUDDER WITH STALL WARNING AND STICK SHAKER. A/C WT 335 ALT FL 200, ENGINE PARAMETERS AND FLT CONTROL INDICATION NORMAL. SYS PARAMETERS NORMAL. AIRCRAFT RETURNED TO AIRPORT. PERFORM OP'S CK OF AOA SENSSDR GLBA2002118Transducer · faultySTALL WARNING HORN SOUNDED SEVERAL TIMES DURING CLIMB. REMOVED AND REPLACED STALL TRANSDUCER, PERFORMED CALIBRATION TEST FLT OP/C GOOD.SDR AUS20020924Transmitter · corroded(AUS) ANGLE OF ATTACK TRANSMITTER VANE BEARINGS CORRODED.SDR GLBA2002105Computer · malfunctionedSTALL WARNING SOUNDED AT 220 KNOTS INDICATED AIR SPEED AOG IN DEN. REPLACED STALL WARNING COMPUTER, OPS CHECKED SYSTEM SATISFACTORY.SDR MEX2002258Computer · failedAIRCRAFT RETURNED TO PLATFORM AS DUE TO AUTO SLAT FAIL LIGHT ON, BOTH STALL WARNING COMPUTERS WERE FOUND WITH FAILURES, PROXIMITY SWITCH AND "C" AND "D" SENSORS WERE TESTED AND FAIL CONTINUE. EXCESSIVE GREASE WAS DETECTED IN OUTBOARD SLATS ACTUATORS. ACTUATOSDR SWIA200211032Computer · malfunctionedCAPTAIN'S STICK PUSHER DOES NOT WORK. REMOVED AND REPLACED THE STALL PANEL COMPUTER. NR 1 SPC OPERATES NORMALLY.SDR MEX2002198Transducer · failedAIRCRAFT RETURN TO PLATFORM AS A CONSEQUENCE OF AUTO SLAT FAIL LIGHT AND TRI COMPUTER OUT OF SERVICE. SLAT SYSTEM RECYCLE WAS PERFORMED IAW MM TESTS, OK. IN RELATION TO TRI COMPUTER WAS RESTED ON BOTH DFGC, TESTS OK IAW MM. DURING TRANSIT IN MEX WERE CHANGESDR AUS20020922Transmitter · corroded(AUS) ANGLE OF ATTACK TRANSMITTER VANE BEARING CORRODED AND STICKING.SDR SWIA200210957Connector · looseFIRST OFFICER'S STICK SHAKER NOT WORKING ON FIRST FLIGHT OF THE DAY CHECK. FOUND CONNECTOR LOOSE ON SHAKER UNIT. TIGHTENED CONNECTOR. OPS CHECK PER 27-60-00 GOOD.SDR AUS20020660Transmitter · faulty(AUS) RT ANGLE OF ATTACK TRANSMITTER FAULTY. INVESTIGATION FOUND THAT THE INTERNAL POTENTIOMETER WAS OPEN CIRCUITED. AIRCRAFT IS A RAAF FALCON 900 A26-076.SDR GLBA2002080Transducer · intermittentSTALL WARNING INTERMITTENT. REPLACED TRANSDUCER.SDR ZW0A205901Computer · failedON TAKEOFF OUT OF STL LT AND RT GEAR UNSAFE LITES AND SLAT DISAGREE LIGHTS ON INTERMITTENTLY WITH A SLAT OVRSP WARNING ON CLIMB OUT THRU 11000 FT. RETURN TO STL. PROX BOX 90348 -TWA-8-336-04 FAILURE. R&R PROX BOX SELF TEST STALL WARNING COMPUTERS CHECKED WOW ASDR SWIA200210903Computer · malfunctionedSTICK SHAKER CAME ON DURING TAKEOFF ROLL. ABORTED TAKEOFF. REPLACED NR 1 STALL WARNING COMPUTER SYSTEM. OPS CHECK GOOD.SDR SWIA200210867Computer · malfunctionedSTALL FAIL MESSAGE INFLIGHT. RETURNED TO SLC. RESET MEMORY ON CH1 & CH2 IN STALL COMPUTER IAW MM 27-35-01. PERFORMED TEST OF STALL SYSTEM. OPS CHECK GOOD, NO FAULTS NOTED.SDR SWIA200210852Transducer · malfunctionedAFTER TAKEOFF, THE STALL FAIL CAUTION MESSAGE CAME ON. COMPLIED WITH QRH. RETURNED TO SLC. REMOVED AND REPLACED NR 1 MACH TRANSDUCER. OPS CHECKS GOOD IAW 27-35-25.SDR AUS20020661Transmitter · faulty(AUS) RT ANGLE OF ATTACK TRANSMITTER FAULTY. INVESTIGATION FOUND THAT THE INTERNAL POTENTIOMETER WAS SHORT CIRCUITED. AIRCRAFT IS A RAAF FALCON 900 A26-073.SDR MWEA020327Computer · faultySTALL FAILURE LIGHT ILLUMINATED, LIGHT CAME ON AND OFF AFTER SELECTING FLAPS. REMAINED OUT FOR DURATION OF FLIGHT. REMOVED AND REPLACED NR 2 STALL COMPUTER SYSTEM, TEST GOOD.SDR GTIA020506Cam · out of adjustDTW - FLT 563 - SLACK IN THE CG ADJUSTMENT WHEEL OF TAKEOFF CONDITIONING COMPUTER. TAKEOFF WARNING HORN DURING INITIAL POWER UP FOR TAKEOFF TAXIED OFF OF RUNWAY. FOUND STABILIZER TAKEOFF WARNING ROLLER CAM OUT OF ADJUSTMENT. ADJUSTED CAM POSITION IAW MD80 MSDR MEX2002256Switch · failedAIRCRAFT RETURNED TO PLATFORM AS DUE TO AUTO SLAT FAIL LIGHT, THE STALL COMPUTER WAS REPLACED AND FAILURE CONTINUED, THE CONNECTORS OF STALL COMPUTER WERE CLEANED AND BOTH ACTUATOR CONNECTORS WERE RESEATED, TESTS WERE PERFORMED OK. DURING TAXI THE SAME LIGHTSDR SWIA200210836Computer · malfunctionedAFTER TAKEOFF, STALL FAIL CAUTION MESSAGE APPEARED. RETURNED TO SLC. RESET STALL PROTECTION COMPUTER (SPC) CIRCUIT BREAKERS AND RESET SPC MEMORY. MESSAGE CLEARED. OPS CHECK GOOD.SDR VNAA0205001Stall Warning · malfunctionedDURING TAKEOFF, THE CREW RECEIVED A PUSHER, SHAKER CAS MESSAGE AND ABORTED TAKEOFF. WINDS WERE GUSTING TO 40 KNOTS. AS THE AIRCRAFT EXITED THE RUNWAY, THE MESSAGE CLEARED. FLIGHT 4083 WAS CLEARED FOR ANOTHER TAKEOFF ATTEMPT AND THEN DEPARTED WITH NO FURTHERSDR VNAA0204022Stall Warning · malfunctionedDURING TAKEOFF, THE CREW RECEIVED A STICK SHAKER FAIL AND ABORTED TAKEOFF. THE WINDS WERE GUSTING TO 18 KNOTS. AS THE AIRCRAFT EXITED THE RUNWAY, THE MESSAGE CLEARED BY ITSELF. THE CREW CALLED MAINTENANCE CONTROL WHO ADVISED THE CREW TO ATTEMPT ANOTHER TAKESDR S2YA02014Stick Shaker · inoperativeJUST AFTER TAKEOFF OF FLIGHT, THERE WAS A CAS MESSAGE FOR STICK PUSHER FAIL. THE CREW DID AN AIR TURN BACK. MECHANIC REPLACED THE STICK PUSHER AND OPERATIONAL CHECK THE SYSTEM.SDR 2002FA0000536Sensor · misinstalledAOA SENSOR, AN ANGLE OF ATTACK (AOA) SENSOR WAS IMPROPERLY INSTALLED ON AN AIRCRAFT BY INSTALLING IT ONE HOLE OFF IN THE COUNTER CLOCKWISE DIRECTION. THE IMPROPER INSTALLATION OF THE AOA SENSOR RESULTED IN A FALSE STALL WARNING INDICATION DIRECTLY AFTER TAKESDR GUU2002F00003Computer · malfunctionedDURING TAKE OFF STALL WARNING WENT OFF. REMOVED AND REPLACED STALL WARNING COMPUTER, OPERATIONAL CHECK NORMAL. TEST FLIGHT SATISFACTORY.SDR 2002F00489Connector · looseFLT 5717 - IN GSP, ABORTED TAKEOFF ROLL DUE TO SPS 1 AND 2 INOPERATIVE AND STICK SHAKER FAIL MESSAGE. MAINTENANCE RESEATED CONNECTOR PLUG TO STICK SHAKER AND REMOVED AND REINSTALLED SPSP COMPUTER. MESSAGE CLEARED. SYSTEM OP CHECKS GOOD. AIRCRAFT WAS RETURNSDR SWAA020732Sensor · brokenAIR TURNBACK, DURING ROTATION AT ABOUT 10 DEGREES NOSE UP BOTH STICK SHAKERS ACTIVATED, A/C FLEW NORMAL. FOUND AOA SENSOR BROKEN. REMOVED AND REPLACED AOA SENSOR PER MM.SDR CA020502009Computer · failed(CAN) STALL FAIL CAUTION MESSAGE SHORTLY AFTER TAKEOFF, QRH PROCEDURE APPLIED WITHOUT SUCCESS - MESSAGE DID NOT CLEAR. FOUND TO BE THE STALL PROTECT COMPUTER AT FAULT. REPLACED COMPUTER, SYSTEM CHECK SERVICEABLE.SDR 700HH40302Indicator · faultyAOA INDICATOR NEEDLE WILL NOT FOLLOW AOA PROBE MOVEMENT THROUGH FULL RANGE OF TRAVEL. NEEDLE STAYS IN UPPER (RED ARC) OF INDICATOR.SDR VNAA0203045Stall Warning · malfunctionedAFTER TAKING THE RUNWAY THE FLIGHT RECEIVED A PUSHER FAIL WARNING MESSAGE ON THE EICAS DISPLAY. THE FLIGHT CREW EXITED THE RUNWAY AND RETURNED TO THE GATE. MAINTENANCE RESET THE STALL PUSHER SYSTEM IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 27-30-00. OPSDR SWAA020586Vane · bentAIR TURNBACK, CAPT'S STALL WARNING CONTROL COLUMN ACTIVATED. FOUND AOA VANE BENT. REMOVED AND REPLACED AOA VANE PER MM.SDR RAIA00203099Vane · inoperative5576 STL- RIGHT STALL ANNUNCIATOR ILLUMINATED ON TAXI OUT. MAINTENANCE REMOVED AND REPLACED THE RIGHT STALL VANE, OPS CK OK.SDR VNAA0203024Stall Warning · malfunctionedTHE FLIGHT WAS ON THE TAKEOFF ROLL WHEN THE FLIGHT CREW RECEIVED A STALL PUSHER FAIL WARNING MESSAGE ON THE EICAS DISPLAY. THE FLIGHT CREW ABORTED THE TAKEOFF AND EXITED THE RUNWAY. ONCE CLEARING THE RUNWAY THE WARNING MESSAGE CLEARED ITSELF WITH NO ACTION FSDR AUS20020921Transmitter · faulty(AUS) ANGLE OF ATTACK TRANSMITTER VANE BEARING CORRODED.SDR COMA0260193ComputerFLIGHT 5529 STALL FAIL MESSAGE AFTER T/O.RESET THE STALL COMPUTER - SYSTEM CHECK NORMAL.SDR COMA0260177Sensor · malfunctionedFLIGHT 6013 STALL FAIL MESSAGE AFTER T/O.REPLACED THE #1 AOA SENSOR.SDR CA020318007Computer · failed(CAN) DURING CLIMB AFTER TAKEOFF CREW WAS UNABLE TO SELECT AUTOPILOT. INVESTIGATION FOUND RT STICK SHAKER REGISTER GROUNDED ON NR 2 INTEGRATED COMPUTER. REPLACED STALL WARNING COMPUTER.SDR VNAA0203010Sensor · malfunctionedDURING TAKEOFF, THE CREW RECEIVED AN ANGLE OF ATTACK CAS MESSAGE AND ABORTED TAKEOFF. AS THE AIRCRAFT CLEARED THE RUNWAY THE MESSAGE CLEARED BY ITSELF, THE CONDITIONS WERE EXTREMELY WINDY. FLIGHT 4049 WAS CLEARED FOR ANOTHER TAKEOFF ATTEMPT AND DEPARTED WITHSDR COMA0260154Service DoorFLIGHT 5469 LOUD BUZZING NOISE AND STALL FAIL CAUTION PLUS IAS MESSAGE.FOUND 02 SERVICE DOOR OPEN - CLOSED DOOR.SDR MEX2002059Computer · failedFLT 601 - ATL-MEX - THERE WAS A FAIL IN THE STALL WARNING COMPUTERS IAW MM 34-19-00. AT RON MEX 07/08 TESTS WERE PERFORMED IAW MM 34-19-00. (M)SDR GTIA020222Vane · damagedDTW - FLT 1258 - AUTOTHROTTLE WORKED IN UNTIL REACHING CRUISE AT 29,000 THEN WENT OFF LINE COULD NOT RE-ENGAGE. REMOVED AND REPLACED RIGHT AOA VANE PER MD80 MM 34-19-01, SYSTEM OPS CHECK GOOD. (M)SDR GTIA020213Vane · failedDTW - FLT 1258 - AUTOTHROTTLE WORKED UNTIL REACHING CRUISE AT 29,000 THEN WENT OFF LINE COULD NOT RE-ENGAGE. REMOVED AND REPLACED RIGHT AOA VANE PER MD80 MM 34-19-01, SYSTEM OPS CHECK GOOD. (M)SDR VNAA0203002Warning System · malfunctionedAT 80 KNOTS THE CREW RECEIVED A PUSHER-SHAKER FAIL CAS MESSAGE AND ABORTED TAKEOFF. AFTER EXITING THE RUNWAY THE MESSAGE CLEARED ITSELF. FLIGHT 4015 WAS CLEARED FOR ANOTHER TAKEOFF ATTEMPT AND DEPARTED WITH NO FURTHER INCIDENTS.SDR USAASB02030Vane · damagedBUF - FLT 437 - ON ROTATION OUT OF BUF, EN ROUTE TO PHL, THE FIRST OFFICER REPORTED THE AIRCRAFT WENT INTO A CONTINUOUS STICK SHAKER MODE. CAPTAIN CHECKED FLAP SETTINGS AND FOUND NO INDICATIONS OF ANY OTHER ABNORMALITIES OTHER THAN THE STICK SHAKER WARNING. SDR VNAA0202013Warning System · malfunctionedDURING TAKEOFF, THE CREW RECEIVED A PUSHER FAIL CAS MESSAGE AND ABORTED TAKEOFF. AFTER EXITING THE RUNWAY THE MESSAGE CLEARED. FLIGHT 4021 WAS CLEARED FOR ANOTHER TAKEOFF ATTEMPT AND DEPARTED WITH NO FURTHER INCIDENTS.SDR SWIA200210650Stall Warning · false activationON ROTATION RECEIVED STALL FAIL CAUTION MESSAGE. PERFORMED APPROPRIATE QRH PROCEDURE. RETURNED TO SLC. RESET STALL COMPUTER CIRCUIT BREAKERS CBP-1 Q2 CBP-4 C7 AND CLEARED THE MEMORY. OPS CHECK GOOD.SDR COMA0260088Computer · malfunctionedFLIGHT 5045 STALL FAIL CAUTION MESSAGE.REPALCED THE STALL COMPUTER.
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