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 VNAA0202004Warning System · malfunctionedDURING TAKEOFF, THE CREW RECEIVED AN ANGLE OF ATTACK FAIL CAS MESSAGE AND ABORTED TAKEOFF. THE CREW CLEARED THE RUNWAY AND THE INDICATION CLEARED BY ITSELF. THERE WERE WINDY CONDITIONS AT THIS TIME. FLIGHT 4059 WAS CLEARED FOR ANOTHER TAKEOFF ATTEMPT. FLIGSDR G60A065Sensor · malfunctionedAFER TAKEOFF, STICK SHAKER STARTED AND THEN SLAT DISAGREE LIGHT CAME ON. RETURNED TO KMIA. REMOVED AND REPLACED AOA SENSOR P/N 2568A13, PER MM 22-33-01 AND NR 1 AT/SC COMPUTER P/N 2593342976 PER MM 22-31-01. STALL WARNING TESTS GOOD. (M)SDR COMA0260089ComputerFLIGHT 5996 - STICK SHAKER ACTIVATED AFTER T/O.RESET THE STALL COMPUTER - SYSTEM TEST SATISFACTORY.SDR VNAA0202001Stick Shaker · malfunctionedDURING TAKEOFF, THE CREW RECEIVED A SHAKER AND PUSHER FAIL MESSAGE AND ABORTED TAKEOFF, THE MESSAGE CLEARED BY ITSELF. THERE WAS CONSIDERABLE WIND GUSTS. FLIGHT 4020 WAS CLEARED FOR ANOTHER TAKEOFF ATTEMPT AND DEPARTED WITH NO FURTHER INCIDENTS.SDR VNAA0201017Stick Shaker · malfunctionedDURING TAKEOFF, THE CREW RECEIVED A LEFT HAND SHAKER FAIL MESSAGE AND ABORTED TAKEOFF. THE MESSAGE CLEARED AND MAINTENANCE CONTROL CLEARED FLIGHT 4050 FOR ANOTHER TAKEOFF ATTEMPT. FLIGHT 4050 THEN DEPARTED WITH NO FURTHER INCIDENTS.SDR RAIA00201026Sensor · faulty5512-STL LEFT STALL CAPTION LIGHT ILLUMINATED DURING TAXI. MAINTENANCE REMOVED AND REPLACED THE LEFT AOA SENSOR.SDR SWIA200210557Control Panel · faultySTALL WARNING MAP ILLUMINATED ON TAKEOFF. ABORTED TAKEOFF. LEFT STALL WARNING. INSTALLED SERVICEABLE TEST PANEL. OPS CHECK GOOD.SDR RAIA00201024Stall Warning · malfunctioned5303- PIT- FLAP FAIL/STALL PROTECTION SYSTEM ADVANCED MESSAGE AFTER TAKEOFF. MAINTENANCE RESET FLAP SYSTEM, SYS OPS CHECK OK.SDR RAIA00201023Stall Warning · malfunctioned5281-TOL- STALL PROTECTION SYSTEM NR 2 INOP ALERT MESSAGE ON TAKEOFF ROLL. MAINTENANCE INSPECTED AOA VANE AND OPERATIONAL CHECKED SYSTEM, NO DEFECTS NOTED.SDR VNAA0112019Warning System · malfunctionedDURING THE TAKEOFF, THE CREW RECEIVED A SHAKER AND PUSHER FAIL MESSAGE AND ABORTED TAKEOFF. AS FLIGHT 4023 CLEARED THE RUNWAY THE MESSAGE CLEARED AND FLIGHT 4023 WAS CLEARED FOR ANOTHER TAKEOFF ATTEMPT. FLIGHT 4023 THEN DEPARTED WITH NO FURTHER INCIDENTS.SDR 2002F00231Warning Horn · false activationON DECEMBER 22, 2001, THE STALL WARNING HORN SOUNDED IMMEDIATELY AFTER TAKEOFF. THE PILOT REPORTED THAT THE HORN WOULD NOT SILENCE, AND THEN RETURNED THE AIRCRAFT TO ICT WITHOUT ANY FURTHER INCIDENT. MAINTNANCE CORRECTED THE PROBLEM, AND RETURNED TO THE AIRCSDR AUS20011360Computer · faulty(AUS) SPURIOUS STALL WARNINGS RESULTED IN NR 1 AND NR 2 LIFT COMPUTERS BEING REPLACED.SDR C2XA01TY188Motor · failedTYS DURING A SCHEDULED INSPECTION THE CAPTAINS STICK PUSHER FAILED OPERATIONAL CHECKS. MAINTENANCE REMOVED AND REPLACED THE CAPTAINS STICK PUSHER MOTOR IAW EMB-145 27-36-04, OPERATIONAL CHECKS WERE SATISFACTORY. THE AIRCRAFT RELEASED FOR SERVICE.SDR VNAA0111002Warning System · malfunctionedAT THE BEGINNING OF THE TAKEOFF ROLL, THE CREW RECEIVED A PUSHER CAS MESSAGE AND ABORTED TAKEOFF. AFTER CLEARING THE RUNWAY THE MESSAGES CLEARED. THE CREW AND MAINTENANCE FELT THE STRONG WINDS HAD CAUSED THESE INDICATIONS AND FLIGHT 4032 WAS CLEARED FOR ANOTSDR VNAA0110020Warning System · malfunctionedDURING TAKEOFF, THE CREW RECEIVED A PUSHER FAIL AND AOA CAS MESSAGES AND ABORTED TAKEOFF. THE MESSAGES WENT OUT ALMOST IMMEDIATELY AND THE CREW ATTEMPTED ANOTHER TAKEOFF. FLIGHT 4052 THEN DEPARTED WITH NO FURTHER INCIDENTS.SDR SWIA200110274Computer · faultyON TAKEOFF ROLL SYSTEM NR 1 STALL WARNING LIGHTS ILLUMINATED. ABORTED TAKEOFF. REPLACED NR 1 STALL WARNING COMPUTER. OPS CHECK GOOD.SDR CNMA200100034Sensor · malfunctionedON ROTATION GOT THE STICK SHAKER AND AURO SLAT EXTENDED, PULLED STALL WARNING CIRCUIT BREAKERS ACCORDING TO CHECKLIST. DUMPED 20,000 LBS OF FUEL AND RETURNED TO AIRPORT. REMOVED AND REPLACED AOA SENSOR IAW MM 22-33, OPS CHECKED GOOD.SDR VNAA0110011Stall Warning · malfunctionedDURING THE TAKEOFF ROLL, THE CREW RECEIVED AN ANGLE OF ATTACK CHIME AND FAILURE. ABORTED THE TAKEOFF. AS FLIGHT 4138 CLEARED THE RUNWAY THE MESSAGE CLEARED. THE CREW CONTACTED MAINTENANCE CONTROL AND WAS CLEARED FOR ANOTHER TAKEOFF ATTEMPT. FLIGHT 4138 THESDR COMA0160767Transducer · faultyFLIGHT #5078. STALL FAIL CAUTION MESSAGE DUIRNG CLIMB OUT OF MCO, AIRCRAFT RETURNED TO THE FIELD.REPALCED THE # MACH. TRANSDUCER.SDR GLBA2001207Vane · dirtySTALL WARNING WOULD NOT SILENCE. CLEANED STALL VANE, OPS CHECKED SYSTEM SATISFACTORY.SDR COMA0160721Pitot LineFLIGHT #5680. DURING CLIMB OUT OF CVG RECEIVED A STALL FAIL CAUTION MESSAGE ACCOMPANIED WITH STICK SHAKER AND LOW AIRSPEED INDICATION ON CO-PILOTS SIDE, AIRCRAFT RETUREND TO THE FIELD.PURGED WATER FROM THE #1 AND #2 STANDBY PITOT STATIC SYSTEM.SDR DHL2001721006Stall Warning · malfunctionedOVERSPEED WARNING SOUNDED ON CLIMBOUT APPROX 10 KTS BEFORE BARBER POLE AND STICK SHAKER SOUNDED ON DESCENT AT 210 KTS CLEAN CONFIGURATION. PERF ADJ/ TEST STALL WARNING SYS PER MM 34-18-01. OPS CKS NORMAL. PLACED BOTH MACH METERS (CAPT & F/O ) TO MODE B. PESDR AUS20010929Computer · faulty(AUS) STALL COMPUTER FAULTY.SDR CA010828008Sensor · failed(CAN) ON 3 OCCASIONS AUGUST 24, 2000, SEPT 13 2000, AND SEPT 20 2000 "ALPHA FLOOR" (MAX AUTO THROTTLE) WAS ENGAGED ON APPROACH AND DEPARTURE. PROBLEM WAS INTERMITTANT AND TROUBLESHOOTING LEAD TO AOA SENSOR. SENSOR REPLACED, PROBLEM CLEARED.SDR RAIA00108024Vane · failed7092-STL-RIGHT STALL CAPTION ILLUMINATED DURING TAXI. MAINTENANCE INSPECTED AND REPLACED THE RIGHT AOA VANE.SDR COMA0160632Trim Switch · faultyFLIGHT #5877. DURING CRUISE FLIGHT RECEIVED A STALL FAIL MESSAGE WHILE ABOVE STALL SPEED.REPLACED THE FLIGHT OFFICERS PITCH TRIM SWITCH.SDR COMA0160608ComputerFLIGHT #5235. DURING TAXI OUT RECEIVED A STALL FAIL CAUTION MESSAGE, AIRCRAFT RETURNED TO THE GATE.RESET THE STALL PROTECTION COMPUTER.SDR 2001F00262Sensor · failedAFTER DEPARTING BQN, SLATS WOULD NOT RETRACT, STALL WARNING AND STICK SHAKER ACTIVATED AT 175 KNOTS. DUMPED APPROXIMATELY 38,000 LBS OF FUEL AND RETURNED TO BQN. AIRCRAFT LANDED NORMAL. CHECKED AND FOUND CODE 71 AND NR 1 PITCH TRIM AND NR 1 AOA SENSOR FAILESDR MWEA011097Transducer · failedWINDSHEAR AND STALL INDICATION FAILURE ANNUNCIATOR LIGHTS CAME ON WHEN AIRCRAFT WAS IN FLIGHT MODE. BOTH LIGHTS EXTINGUISHED AT GROUND SHIFT MODE. REMOVED AND REPLACE RIGHT, AND LATER LEFT, ANGLE OF ATTACK TRANSDUCERS.SDR 2001FA0000229Detector · inoperativeUPON INSTALLING NEW LIFT DETECTION, NOTED THAT WHEN WIRED AS ORIGINALLY REMOVED FROM AIRCRAFT, WITH HEAT TURNED ON, DETECTION WAS INOPERATIVE. GROUND FOR HEATER WAS INSTALLED ON COMMON FOR DETECTION; CAUSING A NO POTENTIAL WHEN HEATER TURNED ON.SDR 2001F00248Detector · inoperativeUPON INSTALLING NEW LIFT DETECTION NOTED THAT WHEN WIRED AS ORIGINALLY REMOVED FROM AIRCRAFT, WITH HEAT TURNED ON, DETECTION WAS INOPERATIVE. GROUND FOR HEATER WAS INSTALLED ON COMMON FOR DETECTION; CAUSING A NO POTENTIAL WHEN HEATER TURNED ON.SDR AUS20010690Detector · faulty(AUS) LIFT DETECTOR FAULTY. INVESTIGATION FOUND THAT THE AIRCRAFT WIRING (WIRE NO A2K4S-20P3) HAD BEEN CUT APPROXIMATELY 76.2MM (3IN) UP FROM THE FORWARD SIDE CONSOLE CONNECTOR AND CONNECTED TO THE STALL WARNING HORN. PERSONNEL/MAINTENANCE ERROR. UNAPPROVED MOSDR SWIA20019997Control Unit · malfunctioned30 SECONDS AFTER T/O, ''STALL WARNING'' CAUTION MESSAGE. COMPLIED WITH QRH & RETURNED TO SLC.REPLACED STALL PROTECTION UNIT. STALL PROBLEM OPS CHECKS GOOD IAW MM 27-35-01.SDR AUS20010655Detector · faulty(AUS) LIFT DETECTOR FAULTY. SWITCH OPERATES IN OPPOSITE SENSE.SDR UPS01236195Wire · brokenINSPECTION TYPE:C, AT ROTATION STICK SHAKER BEGAN AND CONTINUED UNTIL AIRCRAFT LANDED AND NOSE WHEEL TOUCHED DOWN. REPAIRED BROKEN WIRE W1129-301-22R AT STA 560 PER WDM 20-30-12 OP CHECKED STALL WARNING SYSTEM PER MM 34-18-00, OPS CHECKED GOOD.SDR UPS01236193Wire · brokenINSPECTION TYPE:N/A AT ROTATION STICK SHAKER BEGAN AND CONTINUED UNTIL AIRCRAFT LANDED AND NOSE WHEEL TOUCHED DOWN. REPAIRED BROKEN WIRE W1129-301-22R AT STA-560 PER WDM-20-30-12. OP CHECKED STALL WARNING SYSTEM PER MM 34-18-00. OPS CHECKS GOOD.SDR AUS20010656Detector · faulty(AUS) LIFT DETECTOR FAULTY. DETECTOR MICROSWITCH OPERATES IN OPPOSITE SENSE. SWITCH SPRING LOADED UP. PERSONNEL/MAINTENANCE ERROR.MANUFACTURING ERROR.SDR CHQA200158613Computer · faultyA/C ABORTED TAKEOFF DUE TO RT STALL LIGHT. MAINTENANCE REMOVED AND REPLACED STALL WARNING COMPUTER.SDR CA010621039Computer · failed(CAN) THE FLIGHT CREW REPORTED NR 2 STALL WARNING /STICK PUSH CAUTION LIGHT ILLUMINATED DURING FLIGHT. THE STALL WARING COMPUTER WAS REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE. THESTALL WARNING COMPUTER HAD BEEN REPAIRED 194 HOURS PREVIOUS TO THIS OCCUSDR SWIA972620Computer · malfunctionedAFTER TAKE OFF, DURING FLAP RETRACTION, THE STALL FAIL CAUTION MESSAGE CAME ON. POWERED DOWN A/C, POWERED UP A/C. PERFORMED SELF TEST OF FLAP CONTROL, PASSED TESTS. RESET STALL COMPUTER. OPS CHECK GOOD AT THIS TIME.SDR SIMA200115002Sensor · defectiveORD - FLT 4431 - CREW REPORTED SPS TWO WARNING ON EICAS. AIRCRAFT WAS RETURNED TO ORD. MAINTENANCE REMOVED AND REPLACED THE NR 2 AOA SENSOR. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WS RETURNED TO SERVICE. (M)SDR JBXA000284Transducer · failedSTALL FAIL CAUTION MESSAGE ON CLIMBOUT. COULD NOT GET TO RESET IN AIR. AIRCRAFT RETURNED TO RDU. REMOVED AND REPLACED NR 1 ANGLE OF ATTACK TRANSDUCER IAW CRJ AMM 27-35-05. RESET STALL PROTECTION COMPUTER MEMORY IAW CRJ AMM 27-35-01. PERFORMED OPERATIONAL SDR SWIA972591Stall Warning · malfunctionedSYSTEM 1 STALL WARNING CAME ON DURING TAKEOFF. REPLACED LAMP IN STALL WARNING PANEL. RERACKED NR 1 STALL COMPUTER. STALL WARNING OPS CHECK GOOD.SDR 2001UALA00771Computer · malfunctionedSTICK SHAKER ACTIVATION ON TAKE-OFF. SUPPLEMENTAL DATA UPDATE REPLACED NR 1 AND NR 2 STALL MANAGEMENT COMPUTERSDR 2001F00042Computer · inoperativeGSO - FLT 4020 - DURING CLIMB, CREW REPORTED THE SPS 1 FAIL INTERMITTENTLY. CREW THEN RECEIVED AN SPS ADVANCE MESSAGE AN AT THAT POINT BOTH FAIL MESSAGES STAYED ON. CREW FOLLOWED AOM PROCEDURES AND RETURNED TO FIELD. EMERGENCY WAS DECLARED AND AIRCRAFT WAS SDR SIMA20011397Vane · faultyGSO - FLT 4020 - DURING CLIMB, CREW REPORTED THE SPS 1 FAIL INTERMITTENTLY. CREW THEN RECEIVED AN SPS ADVANCE MESSAGE AND AT THAT POINT BOTH FAIL MESSAGES STAYED ON. CREW FOLLOWED AOM PROCEDURES AND RETURNED TO FIELD. EMERGENCY WAS DECLARED AND AIRCRAFT WASSDR MALA010494Transmitter · defectiveRT STALL FAIL LIGHT ILLUMNATES MULTIPLE TIME INFLIGHT. LIGHT ILLUMINATES MASTER CAUTION AND SINGLE CHIME. LIGHT GOES OUT ON OWN AFTER ABOUT ONE SECOND. CAME ON APPROXIMATELY THIRTY TIMES. AIR RETURN TO DTW. MAINTENANCE REPLACED RT ANGLE OF ATTACK TRANSMITSDR 01FDEA00369Stall Warning · faultyON SHORT FINAL GOT STICK SHAKER. AMBER SLATS WERE ILLUM ON PFD. PREF RTS ON FCC NR 1 AND 2 AOA TESTS AND AUTOLAND TESTS ALL PASSED OK TO CONTINUE.SDR SWIA972540Stall Warning · false activationSTALL FAIL CAUTION MESSAGE ON EICAS DURING CLIMBOUT. FOLLOWED QRH PROCEDURES. RETURNED TO SLC. RESET CIRCUIT BREAKERS CBP1, Q2 AND CBP4, C7. STALL FAIL MESSAGE WENT AWAY. OPS CHECK GOOD.SDR SWAA011278Sensor · malfunctionedABORTED TAKEOFF, STALL WARNING CONTROL COLUMN SHAKER ACTIVATED. R&R AOA VANE PER MM.
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