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.

SDR AUS20020925Bearing · sticking(AUS) ANGLE OF ATTACK TRANSMITTER VANE BEARINGS STICKING.Aug 14, 2002 · Pilats PC12SDR 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 Aug 13, 2002 · N162PL · Doug MD88SDR 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 WAAug 10, 2002 · Lkheed 10113853SDR 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 SENSAug 7, 2002 · N501TR · Airbus A300B4203SDR GLBA2002118Transducer · faultySTALL WARNING HORN SOUNDED SEVERAL TIMES DURING CLIMB. REMOVED AND REPLACED STALL TRANSDUCER, PERFORMED CALIBRATION TEST FLT OP/C GOOD.Aug 7, 2002 · N208GL · Beech 1900DSDR AUS20020924Transmitter · corroded(AUS) ANGLE OF ATTACK TRANSMITTER VANE BEARINGS CORRODED.Jul 22, 2002 · Pilats PC12SDR GLBA2002105Computer · malfunctionedSTALL WARNING SOUNDED AT 220 KNOTS INDICATED AIR SPEED AOG IN DEN. REPLACED STALL WARNING COMPUTER, OPS CHECKED SYSTEM SATISFACTORY.Jul 10, 2002 · N179GL · Beech 1900DSDR 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. ACTUATOJul 8, 2002 · N945AS · Doug MD83SDR SWIA200211032Computer · malfunctionedCAPTAIN'S STICK PUSHER DOES NOT WORK. REMOVED AND REPLACED THE STALL PANEL COMPUTER. NR 1 SPC OPERATES NORMALLY.Jul 7, 2002 · N587SW · Cndair CL6002B19SDR 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 CHANGEJun 26, 2002 · N169PL · Doug MD88SDR AUS20020922Transmitter · corroded(AUS) ANGLE OF ATTACK TRANSMITTER VANE BEARING CORRODED AND STICKING.Jun 19, 2002 · Pilats PC12SDR 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.Jun 8, 2002 · N214SW · Emb EMB120ERSDR 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.Jun 4, 2002 · Amd FALCON900SDR GLBA2002080Transducer · intermittentSTALL WARNING INTERMITTENT. REPLACED TRANSDUCER.Jun 4, 2002 · N247GL · Beech 1900DSDR 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 AJun 2, 2002 · N958U · Doug DC982SDR SWIA200210903Computer · malfunctionedSTICK SHAKER CAME ON DURING TAKEOFF ROLL. ABORTED TAKEOFF. REPLACED NR 1 STALL WARNING COMPUTER SYSTEM. OPS CHECK GOOD.May 28, 2002 · N297SW · Emb EMB120ERSDR 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.May 23, 2002 · N439SW · Cndair CL6002B19SDR 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.May 17, 2002 · N427SW · Cndair CL6002B19SDR 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.May 15, 2002 · Amd FALCON900SDR 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.May 15, 2002 · N809ME · Doug DC982SDR 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 MMay 14, 2002 · N812NK · Doug DC982SDR 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 LIGHTMay 8, 2002 · N491SH · Doug DC982SDR 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.May 4, 2002 · N432SW · Cndair CL6002B19SDR 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 FURTHERMay 2, 2002 · N433JS · Dorner DO328100SDR 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 TAKEApr 25, 2002 · N433JS · Dorner DO328100SDR 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.Apr 17, 2002 · N357SK · Dorner DO328300SDR 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 TAKEApr 16, 2002SDR GUU2002F00003Computer · malfunctionedDURING TAKE OFF STALL WARNING WENT OFF. REMOVED AND REPLACED STALL WARNING COMPUTER, OPERATIONAL CHECK NORMAL. TEST FLIGHT SATISFACTORY.Apr 14, 2002 · N38537 · Beech 1900DSDR 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 RETURNApr 5, 2002 · N825MJ · Emb EMB145LRSDR 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.Apr 5, 2002 · N610WN · Boeing 7373H4SDR 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.Apr 3, 2002 · Cndair CL6002B19SDR 700HH40302Indicator · faultyAOA INDICATOR NEEDLE WILL NOT FOLLOW AOA PROBE MOVEMENT THROUGH FULL RANGE OF TRAVEL. NEEDLE STAYS IN UPPER (RED ARC) OF INDICATOR.Apr 3, 2002 · N700HH · Braero HS125700ASDR 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. OPMar 29, 2002 · N461PS · Dorner DO328100SDR SWAA020586Vane · bentAIR TURNBACK, CAPT'S STALL WARNING CONTROL COLUMN ACTIVATED. FOUND AOA VANE BENT. REMOVED AND REPLACED AOA VANE PER MM.Mar 19, 2002 · N339SW · Boeing 7373H4SDR RAIA00203099Vane · inoperative5576 STL- RIGHT STALL ANNUNCIATOR ILLUMINATED ON TAXI OUT. MAINTENANCE REMOVED AND REPLACED THE RIGHT STALL VANE, OPS CK OK.Mar 17, 2002 · N560HK · Jetair JETSTM4101SDR 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 FMar 16, 2002 · N426JS · Dorner DO328100SDR AUS20020921Transmitter · faulty(AUS) ANGLE OF ATTACK TRANSMITTER VANE BEARING CORRODED.Mar 14, 2002 · Pilats PC12SDR COMA0260193ComputerFLIGHT 5529 STALL FAIL MESSAGE AFTER T/O.RESET THE STALL COMPUTER - SYSTEM CHECK NORMAL.Mar 14, 2002 · N735CA · Cndair CL6002B19SDR COMA0260177Sensor · malfunctionedFLIGHT 6013 STALL FAIL MESSAGE AFTER T/O.REPLACED THE #1 AOA SENSOR.Mar 10, 2002 · N981CA · Cndair CL6002B19SDR 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.Mar 8, 2002 · Lear 45LEARSDR 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 WITHMar 8, 2002 · N433JS · Dorner DO328100SDR COMA0260154Service DoorFLIGHT 5469 LOUD BUZZING NOISE AND STALL FAIL CAUTION PLUS IAS MESSAGE.FOUND 02 SERVICE DOOR OPEN - CLOSED DOOR.Mar 8, 2002 · N719CA · Cndair CL6002B19SDR 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)Mar 7, 2002 · N168PL · Doug MD88SDR 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)Mar 5, 2002 · N810NK · Doug DC981SDR 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)Mar 5, 2002 · N810NK · Doug DC981SDR 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.Mar 3, 2002 · N433JS · Dorner DO328100SDR 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. Feb 10, 2002 · N408US · Boeing 737401SDR 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.Feb 10, 2002 · N433JS · Dorner DO328100SDR 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.Feb 10, 2002 · N439SW · Cndair CL6002B19SDR COMA0260088Computer · malfunctionedFLIGHT 5045 STALL FAIL CAUTION MESSAGE.REPALCED THE STALL COMPUTER.Feb 5, 2002 · N932CA · Cndair CL6002B19
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