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 TSAA9534126Aoa Sensor · malfunctionedITO/HNL - FLT 437 - PILOT REPORT. DURING TAKEOFF, ROLL 'WINDSHEAR INOP' LIGHT CAME ON. TAKEOFF CONTINUED, AND AFTER BECOMING AIRBORNE, STICK SHAKER BEGAN. AIRSPEED APPROXIMATELY 140 KNOTS TO 150 KNOTS. MOVING STALL WARNING SWITCH TO 'TEST' POSITION STOPPEDSDR 95ZZZX3970Stall Warn Mod · malfunctionedITO/HNL - FLT 437 - PILOT REPORT. DURING TAKEOFF, ROLL 'WINDSHEAR INOP' LIGHT CAME ON. TAKEOFF CONTINUED, AND AFTER BECOMING AIRBORNE, STICK SHAKER BEGAN. AIRSPEED APPROXIMATELY 140 KNOTS TO 150 KNOTS. MOVING STALL WARNING SWITCH TO 'TEST' POSITION STOPPEDSDR 95ZZZX3415Lift Detector · failedFLIGHT CREW REPORTED THAT STALL WARNING CAME ON IN-FLIGHT AND REMAINED ON. MAINTENANCE CREW REPLACED INBOARD STALL WARNING SWITCH (LIFT DETECTOR) DUE TO AN INTERNAL SHORT AND AIRCRAFT WAS RELEASED AFTER A SUCCESSFUL TEST FLIGHT. THIS OPERATOR HAS FOUND THIS SDR AWXA9500381Aoa Sensor · brokenFLT 515 - PHX-OMA - ON CLIMB-OUT, THE STICK SHAKER ACTIVATED. PULLED AC STALL WARNING AND DC BREAKER TO SILENCE STICK SHAKER. AIRCRAFT RETURNED TO PHX WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED CAPTAINS SIDE AOA VANE PER MM 27-32-11, PG 401/SDR VTZA95197Lift Transducer · failureFLT NR 6435 - IAD-EWR - RETURNED TO IAD DUE TO THE STICK SHAKER COMING ON AFTER ROTATION. AIRCRAFT RETURNED TO IAD WITH NO FURTHER INCIDENTS. MAINTENANCE RECALIBRATED THE LEFT WING TRANSDUCER AND REPLACED AND RECALIBRATED THE RIGHT WING TRANSDUCER. AIRCRAFTSDR RAIA950605Summing Unit · failedSTL - FLT 7393 - RT STALL LIGHT ILLUMINATED, HORN SOUNDED. MAINTENANCE REPLACED RT STALL WARNING SUMMING UNIT. SYSTEM TEST REVEALED NORMAL OPERATIONAL. (M)SDR SWIA95588Stall Warn Pnl · malfunctionedON TAKEOFF ROLL, THE STALL SYSTEM ACTIVATED. ABORTED TAKEOFF. RT SYSTEM FAILS TO TEST PROPERLY. DEFERRED PER MEL 27-36-2. REMOVED STALL WARNING PANEL AND REPLACED IT WITH A SERVICEABLE ONE, IAW MM 27-34-08, OPS CKS GOOD, SEE F/L 75803.SDR MALA954477Computer · failedMSP - FLT 3352 - ON CLIMB-OUT FROM MSP, THE GEAR WARNING HORN BEGAN TO SOUND. THE AIRCRAFT RETURNED TO MSP. MAINTENANCE WAS UNABLE TO DUPLICATE THE DISCREPANCY. AS A PRECAUTION, MAINTENANCE REPLACED THE SAS COMPUTER. SYSTEM OPERATED SATISFACTORILY DURING ASDR COM11905Computer · defectiveDURING TAKEOFF ROLL, THE STALL WARNING CAME ON. REPLACED STALL WARNING COMPUTER.SDR 95UAL737072Aoa Sensor · missingIMMEDIATELY AFTER TAKEOFF FLAP RETRACTION, STICK SHAKER CAME ON CONTINUOUSLY. STICK SHAKER SOUNDED ALL THE WAY TO THE GATE. LEFT AOA SENSOR WAS FOUND MISSING.SDR COM20371Sas Servo · defectiveTHERE IS BINDING IN THE CONTROLS WHEN PULLING AFT ON THE CONTROL YOKE. REPLACED THE SAS SERVO AND CAPSTAN.SDR COM20368Sas Control · defectiveSAS ARM INDICATOR REMAINED ON ABOVE 145 KNOTS. REPLACED THE SAS CONTROL BOX.SDR BUFA9513Lift Transducer · defectiveFLT 792 - STALL WARNING CAME ON RIGHT AFTER ROTATION, STALL WARNING STILL ON AT 220 KTS IN LEVEL FLIGHT, ALL OTHER INDICATIONS NORMAL. RETURNED TO MMMX. REMOVED AND REPLACED STALL WARNING LIFT TRANSDUCER, SYSTEM OP CHECK NORMAL PER MM 34-16. (W)SDR COM60472Stall Unit · defectiveSTALL FAIL MESSAGE ON EICAS. REPLACED THE STALL PROTECTION UNIT.SDR 9507169969Stall Transducer · malfunctionedSTALL WARNING SYSTEM ACTIVATED ON ROTATION. PULLED STALL WARNING COMPUTER CIRCUIT BREAKERS AND RETURNED TO DTW WITHOUT INCIDENT. FOUND NR 2 TRANSDUCER PIN POPPED. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE.SDR COM11874Servo · defectiveAUTOPILOT SERVO APPEARS TO ENGAGE WITH AUTOPILOT OFF. REPLACED THE STICK PUSHER SERVO MOTOR.SDR 9506579966Computer · malfunctionedSTALL GLARESHIELD LIGHT AND STICK SHAKER ACTIVATED AFTER TAKEOFF. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. REPLACED NR 1 STALL WARNING COMPUTER AND TRANSDUCER. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE.SDR 95ZZZX2513Lift Detector · shortedFLIGHT CREW REPORTED STALL WARNING CAME ON DURING CRUISE FLIGHT. PULLED CIRCUIT BREAKER. MIANTENANCE REPLACED OUTBOARD STALL WARING VANE/SWITCH. DEFECTIVE SWITCH WAS REPAIRED BY THE MANUFACTURER PREVIOUSLY. AIRCRAFT WAS FLOWN THROUGH MOISTURE ON THIS DATE.SDR 95ZZZX2517Lift Detector · failedAT 100 KNOTS, AIRSPEED STALL WARNING CAME ON WHEN FLAPS WERE EXTENDED. MAINTENANCE REPLACED OUTBOARD STALL WARING SWITCH. NOTE: AIRCRAFT WAS FLOWN IN MOIST WEATHER ON THIS DATE.SDR 95ZZZX2516Lift Detector · failedSTALL WARNING SOUNDED WHEN FLAPS SELECTED TO 10 DEGREES ON GROUND. MAINTENANCE REPLACED INBOARD STALL WARNING SWITCH. NOTE: AIRCRAFT WAS OPERATED IN MOIST WEATHER ON THIS DATE.SDR 95ZZZX2515Lift Detector · shortedCREW REPORTED STALL WARNING OCCURRED WHEN SELECTING FLAPS FROM 10 DEGREES TO 20 DEGREES. MAINTENANCE REPLACED OUTBOARD STALL WARNING SWITCH. NOTE: THIS AIRCRAFT WAS FLOWN THROUGH MOIST WEATHER ON THIS DATE.SDR 95ZZZX2514Lift Detector · shortedSTALL WARNING OCCURRED AFER TAKEOFF FROM GEN AIRPORT. CREW PULLED APPLICABLE CIRCUIT BREAKER AND REMAINDER OF FLIGHT FLOWN FLAPS UP. MAINTENANCE REPLACED FAILED INBOARD STALL WARNING SWITCH. THIS AIRCRAFT WAS FLOWN THROUGH MOIST WEATHER ON THIS DATE. THIS SDR MWEA95170Aoa Transducer · malfunctionedPILOT REPORTS DURING CLIMB, STALL INDICATION FAIL AND WINDSHEAR INOP ANNUNCIATOR ILLUMINATED. STALL ANNUNCIATOR FINALLY WENT OUT WHEN FLAPS WENT TO 40 ON LANDING. WINDSHEAR STAYED ILLUMINATED. MAINTENANCE FOUND LT ANGLE OF ATTACK TRANSDUCER TESTING BAD. RESDR COM20362Sas Wire · chafedSAS FAULT LIGHT FLASHING IN FLIGHT. REPAIRED CHAFED WIRE AT INSTRUMENT PANEL GLARE SHIELD.SDR COM20360Ann Panel · malfunctionedSAS FAULT LIGHT FLICKERED IN FLIGHT. DISABLED SYSTEM PER CHECKLIST. REMOVED AND REPLACED MASTER ANNUNCIATOR PANEL WITH SERVICEABLE UNIT.SDR WTAA950153Lift Transducer · failedPSC - STALL WARNING SYSTEM ACTIVATED AT 70 KTS. DURING TAKEOFF ROLL, TAKEOFF ABORTED WITHOUT INCIDENT. AIRCRAFT FERRIED TO SEA FOR MAINTENANCE. FOUND WIRES TO RT WING LIFT TRANSDUCER SHORTING AT CONNECTION. REPOSITIONED WIRE HARNESS AND RESECURED. STALL WSDR COM60452Actuator · defectiveSCRAPING NOISE HEARD WHEN CONTROL YOKE MOVED FORE AND AFT. STALL WARNING ACTIVATED. REPLACED THE STICK PUSHER ACTUATOR.SDR C2XA95CL054Angle Of Attack · malfunctionedFLT NR 3724 - EWR- STICK PUSHER/SHAKER FAULT IN FLIGHT. AIR RETURNED TO EWR. MAINTENANCE REMOVED AND REPLACED RIGHT AOA PROBE. AIRCRAFT WENT ON A SATISFACTORY TEST FLIGHT AND RETURNED TO SERVICE. (W)SDR VTZA95117Stall Warning · out of adjustIAD/CRW - FLT 6378 - DURING CLIMB-OUT AT 1830 HRS ON 3-27-95, THE STICK SHAKER ACTIVATED. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE ADJUSTED THE STALL SIGNAL SUMMING UNITS. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (XSDR 9504869959Stall Warning · malfunctionedSTALL WARNING INDICATION FAILURE LIGHT ILLUMINATED UPON APPLICATION OF TAKEOFF POWER. TAKEOFF WAS ABORTED. A SUCCESSFUL TAKEOFF WAS ACCOMPLISHED ON SECOND ATTEMPT. RECYCLED SYSTEM ON GROUND. ALL CHECKED OK. AIRCRAFT RETURNED TO SERVICE.SDR COM60443Computer · defectiveTHE STICK SHAKERS ACTIVATED DURING FINAL APPROACH. REPLACED THE STALL WARNING COMPUTER.SDR WTAA950116Stall Vane · failedSEA - RT STALL WARNING AND STICK SHAKER CAME ON IN-FLIGHT. AIRCRAFT LANDED WITHOUT INCIDENT. AIRCRAFT FERRIED TO EUG. MAINTENANCE RPELACED RT STALL VANE. STALL SYSTEM OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (X)SDR COM11814Computer · defectiveNR 2 STALL WARNING SYSTEM RED LIGHT IS ON. REPLACED THE NR 2 STALL COMPUTER.SDR WTAA950094Transducer · malfunctionedEUG - LEFT STALL PROTECTION SHAKER AND HORN ACTIVATES WHEN STALL SYSTEM TURNED ON. MAINTENANCE REPLACED LEFT LIFT TRANSDUCER. STALL SYSTEM OPERATIONAL, CHECK NORMAL ON GROUND. AIRCRAFT RETURNED TO SERVICE. (X)SDR 9502709753Stall Computer · malfunctionedSTALL WARNING INDICATION FAILURE LIGHT ILLUMINATED AFTER FLAP RETRACTION ON TAKEOFF AND REMAINED ON AT SPEEDS UP TO 340 KTS. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. DISCREPANCY COULD NOT BE DUPLICATED ON GROUND. REPLACED BOTH NR 1 AND NR 2 STALLSDR LOSA9512Stall Computer · malfunctionedPILOT REPORTED STICKSHAKER BRIEFLY ENGAGED IN FLIGHT ABOVE 200 KNOTS AND ALSO ENGAGED BRIEFLY DURING FLIGHT ABOVE STALL SPEED. MAINTENANCE REPLACED LEFT STALL VANE ASSY FOR EXCESSIVE UNADJUSTABLE VOLTAGE, REPLACED SAS CONTROL BOX AND LT SAS COMPUTER. OPERATISDR COM11786Stall Computer · defectiveDURING TAKEOFF, STALL AURAL WARNING, STICK SHAKER AND STICK PUSHER ACTIVATED. REPLACED THE STALL COMPUTER.SDR 9502699155Stick Shaker · malfunctionedSTALL INDICATION FAILURE LIGHT AND STICK SHAKER ACTIVATED ON FINAL APPROACH INTO DTW. PERFORMED STALL RECOVERY AND ACCOMPLISHED GO-AROUND PROCEDURES. NORMAL INDICATIONS WERE ACHIEVED ON SECOND APPROACH. AIRCRAFT LANDED WITHOUT INCIDENT. DISCREPANCY COULD NSDR 9501959754Stall Transducer · failedSTALL INDICATION FAILURE LIGHT ILLUMINATED AFTER TAKEOFF WHEN FLAPS AND SLATS WERE RETRACTED. PERFORMED PRECAUTIONARY FLIGHT PROCEDURES AND NR 2 SYSTEM TESTED BAD. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REPLACED THE RIGHT STALL WARNING TRANSDUCSDR WTAA950024Transducer · malfunctionSFO - RT STALL IDENT LIGHT ILLUMINATED AND STICK SHAKER ACTIVATION REPORTED AT 150 KTS. MAINTENANCE ADJUSTED REPLACED AND ADJUSTED RIGHT STALL SYSTEM LIFT TRANSDUCER. STALL SYSTEM OPERATIONAL CHECK NORMAL ON GROUND. AIRCRAFT RETURNED TO SERVICE. (Z)SDR WTAA950018Transducer · req'd adjFAT - EN ROUTE SFO TO VIS AT 12,000 FEET, STALL IDENT LIGHT ILLUMINATED FOLLOWED BY STICK SHAKER AND STALL WARNING HORN ACTIVATION. AIRCRAFT DIVERTED TO STATION, LANDING WITHOUT INCIDENT. MAINTENANCE ADJUSTED LEFT AND RT STALL SYSTEM LIFT TRANSDUCER. STALL
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