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 SIMA20150509004Computer · failedSPS 1 INOPERATIVE. WARNING ON EICAS PLU SPS ADVANCED CAUTION ON EICAS, ON CAPTAINS PFD AOA INDICATION BUTTON LT CORNER. R & R SPS COMPUTER IAW AMM 27-36-02. OPERATIONS CHECKED GOOD.SDR SIMA20150509003Stall Warning · false activationSPS 1 INOPERATIVE. WARNING & SPS ADVANCED CAUTION ON EICAS. PERFORMED STALL PROTECTION. OPERATIONAL CHECKED IAW AMM 27-36-00. OPERATIONS CHECKED GOOD.SDR FDEA201504171253Stick Shaker · activatedMOMENTARY STICK SHAKER ACTIVATION AT FL 360, 242KIASDUE TO MODERATE TURBULENCE. AUTOPILOT WAS ENGAGED & AUTO THROTTLES WERE ENGAGED. CLEAN CONFIGURATION. COMPLIED WITH TURBULENCE INSPECTION IAW AMM 05-51-01-6, NO DEFECTS NOTED.SDR AALA20150415011Aoa · faultySTALL WARNING SYS FAILED DURING CLIMB. AN EMERGENCY WAS DECLARED & FLIGHT RETURNED LANDING OVERWEIGHT WITHOUT INCIDENT. R & R LT AOA SENSOR IAW AMM 34-21-05 WITH GOOD OPERATIONAL CHECK.SDR HNAA2015041000125Stick Shaker · malfunctionedPUSHER SYSTEM FAIL CAUTION LIGHT ILLUMINATED ON TAKEOFF ROLL FOR APPROXIMATELY 5 SECONDS. NR 1 AND 2 STALL SYSTEM CAUTION LIGHT ILLUMINATED INTERMITTENTLY. CREW POWERED DOWN ACFT FOR APPROXIMATELY 5 MINUTES SYS, OPS CHECKED, OPS AND SELF TEST NORMAL ON POWERSDR CA150323013Computer · malfunctioned(CAN) UNEXPECTED SPC FAIL OUTPUT ACTIVATION. AN UNEXPECTED ACTIVATION OF THE SPC NON-SINGLE CHANNEL FAIL OUTPUT OCCURS WHEN THE LATERAL ACCELERATION INPUT, FROM THE ACCELEROMETERS, EXCEEDS A CERTAIN THRESHOLD, APPROXIMATELY. THIS BEHAVIOR IS NOT IAW DESIGN.SDR HNAA2015031600095Transducer · failedON DEPARTURE CLIMB OUT, STALL/STICK SHAKER ACTIVATED CONTINUOUSLY, COULD NOT CANCEL. FOUND NR 2 LIFT TRANSDUCER BAD AND BOTH LT AND RT STALL SYS OUT OF CALIBRATION. R & R NR 2 LIFT TRANSDUCER AND ADJUSTED LT AND RT SIDES IAW MM 27-33-00. SYSTEM OPS CHECKED SDR SIMA20150223004Stall Warning · activatedSPS ADVANCE EICAS MSG ON TAKEOFF. PERFORMED OPERATIONS CHECK OF STALL PROTECTION SYS IAW FIM 27-36-00-810-806-A. PROBLEM STILL EXISTS IAW 4 OF THIS LOG PAGE FOR DISCREPANCY.SDR I5EA201502210001Aoa · malfunctionedRTO AT 100K 97.000LBS TEMP -12C BRAKE COOLING REQUIRED 48 MINUTES. REASON FOR RTO GOT STICK SHAKER. R & R LT AOA SENSOR OPS CHECK GOOD.SDR A6WA201542385Stall Warning · activatedSTALL FAIL CAUTION IN FLIGHT. COMPLIED WITH QRH & RETURNED.SDR I5EA0201511300024Squat Switch · malfunctionedSTALL WARNING SHAKER ON JUST PAST 80K ON T/O ROLL. R & R CIRCOIL CARD M990 GROUND SENSING SQUAT SW. FUNCTIONAL CHECK OF CARD AND RELATED SYSTEM GOOD. STALL WARNING TEST GOOD.SDR AALA20150114013Sensor · defectiveAIR INTERRUPT & RETURNED. AIRSPEED INDICATION ON CAPTAINS PRIMARY FLIGHT DISPLAY WENT BLANK THEN RETURNED MULTIPLE TIMES. TROUBLE SHOT SYS IAW FIM 34-21-00 & FOUND BAD LT ANGLE OF ATTACH SENSOR. R & R SENSOR IAW AMM 34-21-05. SYS CHECKED NORMAL.SDR SIMA20150109004Sensor · failedDURING STALL PROTECTION TEST THE STALL PROTECTION FAILED, SPS 2 INOPERATIVE & SPS ADVANCED WARNING & CAUTION MSGS PRESENTED ON EICAS. SYS FAILED, SAME WAY MULTIPLE TIMES. TRANSFERRED TO NRWC 608-ORD-01965. IAW NRWC 608-ORD-01965 R & R RT & LT AOA SENSOR IAWSDR WX0A2014120172281Transducer · inoperativeREJECTED TAKEOFF AT 120 KTS FOR A STALL WARNING. R & R LT AOA TRANSDUCER IAW MM 34-19-01. PERFORMED STALL WARNING TEST IAW 34-19-00 & RTS IAW 22-01-05. OPERATIONS CHECKED GOOD. PERFORMED HIGH ENERGY STOP INSPECTION IAW MM 05-57-00. NO FAULTS FOUND.SDR SWIA201440006Computer · malfunctionedRETURNED TO FIELD DUE TO STALL FAIL MESSAGE. REMOVED AND REPLACED STALL PROTECTION COMPUTER IAW AMM. OPS CHECKED GOOD.SDR N6WA2014111202Stall Warning · false activationSTALL FAIL CAUTION MSG. INSPECTED DRAIN TRAPS & PERFORMED OPERATIONS TEST OF STALL SYS IAW AMM 27-35-01. NO DEFECTS NOTED.SDR CA141014011Warning Horn · inoperative(CAN) STUDENT TESTED STALL WARNING ON THE GROUND AND FOUND IT TO BE NOT WORKING. MAINTENANCE FOUND THE REED HAD COME ADRIFT FROM THE HORN. IT APPEARED AS THOUGH THERE WAS A DAB OF SOME SORT OF GLUE ORIGINALLY HOLDING THE REED INTO THE HORN. THE REED WAS SNAPPESDR CA140917019Computer · failed(CAN) PILOT REPORT OF CAS, PUSHER, INDICATION IN FLIGHT AND SYSTEM WOULD NOT TEST/RESET. AIRCRAFT RETURNED TO BASE. ON TROUBLESHOOTING, FOUND STICK PUSHER COMPUTER WOULD NOT CLEAR AND RESET. STICK PUSHER COMPUTER REPLACED WITH SERVICEABLE UNIT. STICK PUSHESDR SIMA20140901003Computer · failedUNCOMMANDED FWD PUSH OF THE ELEVATOR FELT ON THE YOKE WHILE ON FINAL APPROACH & WITH THE AUTO PILOT DISCONNECTED, HAND FLYING. R & R STALL PROTECTION COMPUTER IAW AMM 27-35-01. OPERATIONAL TEST, PRE-FLIGHT TEST GOOD. ACFT RELEASED FOR FCF PURPOSES ONLY.SDR 9JLA201409107929Vane · defectiveTHE RT AOA HEAT FAILED IN FLIGHT. THE RT AOA VANE WAS FOUND TO BE DEFECTIVE & WAS REPLACED WITH NEW PN 6627308500-803.SDR 9JLA201408137927Computer · defectiveTHE STALL WARNING SYS WAS GIVING FALSE STALL INDICATIONS WHILE IN FLIGHT. TROUBLESHOOTING DETERMINED THAT THE DUAL STALL WARNING COMPUTER WAS DEFECTIVE. REMOVED THE DEFECTIVE STALL WARNING COMPUTER PN 6627308500-013 SN 320 & INSTALLED A REPAIRED UNIT. FUNCTSDR EPUA20140730001Insulator · unsecurePILOT REPORTED A BURNING ELEC SMELL DURING TAKEOFF. INSPECTED COCKPIT ELEC HARNESS & SECURED STALL WARNING HORN INSULATORS & TERMINALS.SDR SIMA20140723002Computer · malfunctionedSPS 2 INOPERATIVE ON EICAS UPON LANDING STICK SHAKER ACTIVATED. R & R STALL PROTECTION COMPUTER IAW AMM 27-36-02. OPERATIONS CHECKED GOOD.SDR 9JLA2014091003904Computer · faultyA RT STALL WARNING FAIL CAS MSG INTERMITTENTLY BEING DISPLAYED DURING FLIGHT. THE CREW COMPLETED THE REQUIRED CHECKLIST ITEMS, BUT CORRECTIVE ACTIONS DIDN'T CORRECT THE ISSUE. TROUBLE SHOT THE RT STALL WARNING SYS & FOUND THE DUAL STALL WARNING COMPUTER FAUSDR CA140501001Transducer · unserviceable(CAN) DURING B-CHECK SCHEDULED INSPECTION, FOUND STALL VANE STICKING TO THE AFT POSITION. DURING A FUTURE STALL, FLIGHT CREW COULD NOT BE WARNED OF THE STALL AND STICK PUSHER WOULD NOT OPERATE.SDR QXEA2014040500298Aoa · failedPUSHER SYS FAILED DURING CLIMBOUT AT 16K AND RT AOA VANE HEAT CIRCUIT BREAKER TRIPPED AT THE SAME TIME. RETURNED TO FIELD. LANDED UNEVENTFUL. REMOVED AND REPLACED THE RT AOA VANE IAW AMM 27-33-26-000-801 AND AMM 27-33-26-400-801. FUNCTIONALLY TESTED GOOD. SDR USAA2014033100004Nut Plate · failedFLIGHT ATTENDANT REPORTED A STRONG HIGH PITCHED SOUND AROUND ROW 2. FLIGHT DIVERTED TO PHL & LANDED WITHOUT INCIDENT. FOUND A BAD DOME NUTPLATE AT FIRST OFFICER'S AOA. R & R BAD DOME NUTPLATE & ACCOMPLISHED ACFT PRESSURIZATION TEST. NO LEAKS NOTED, ACFT OKSDR RU3A20140331012Computer · failedSTALL FAIL CAS MSG ILLUMINATED. REPLACED STALL PROTECTION COMPUTER.SDR GBBR20140331001Aoa · faultySTICK SHAKER ACTIVATED AFTER TAKEOFF. PILOT FLEW A CLOSE PATTERN AND LANDED AT DEPARTURE AIRPORT. PROBLEM WAS TRACED TO DEFECTIVE RT AOA SENSOR.SDR CALA2014031090572Unknown · unknownSTALL WARNING TEST, WITH RT AOA SENSOR CB OPEN F31 & FLIGHT OFFICER`S ALT AIR DATA SELECTED, ELEX WARNING STATUS WILL NOT CLEAR & THEREFORE NO STICK SHAKER. SWAPPED STALL WARNING CARDS M938, M615 & TRIED AIR DATA COMPUTER. NO HELP. SUSPECT CAPTAIN`S AOA SENSDR AALA20140306001Aoa · failedMIA CREW REPORTED AFTER TAKEOFF AIRSPEED SPLIT BETWEEN THE CAPTAIN & FIRST OFFICER. EMERGENCY DECLARED FLIGHT RETURNED MIA LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED LT ANGLE OF ATTACK SENSOR. SYS GND CHECKED NORMAL, OPERATION CLOSED.SDR QXEA2014022000148Module · failedLOW AIRSPEED CUE INTERMITTENT ON CAPTAIN`S PDF. RETURN TO FIELD. LANDING UNEVENTFUL. CHECKED CDS AND FOUND FAULT CODE SPM1. R & R SPM1 IAW T/C 6273301. OPS CHECK GOOD. CUE CAUTION MESSAGE DID NOT RETURN, AND SPM1 FAULT NOT PRESENT. RETURNED TO SERVICE.SDR SIMA20140104004Stall Warning · malfunctionedDURING STICK PUSHER TEST WE RECEIVED SPS 1 - 2 INOPERATIVE WARNINGS & STICK PUSHER FAIL CAUTION. TRIED 4 UNSUCCESSFUL ATTEMPTS. TROUBLESHOOT IAW FIM TASK 27-36-00-810-808-A & FOUND TO BE A TRANSITORY CONDITION. SYS OPERATIONS CHECKED GOOD IAW AMM 27-36-00.SDR QXEA2014010300002Transducer · failedPUSHER SYSTEM FAIL CAUTION LIGHT ILLUMINATED DURING FLIGHT AND RT AOA VANE HEAT CIRCUIT BREAKER TRIPPED. RETURNED TO FIELD, LANDED UNEVENTFULLY. R & R RT AOA TRANSDUCER IAW MM TASK 27-33-26-000-801/400-801. COMPLIED WITH MAINTENANCE 6273302 FOR CAT3, RETURN SDR HNAA2013122300626Computer · malfunctionedSTICK SHAKER ACTIVATED AT 130 KNOTS ON CLIMB OUT, AGAIN DURING RETURN TO FIELD, FLAPS TOO LOW VERBAL WARNING SOUNDED. FIRST FLIGHT AFTER SPAR REPAIR WAS COMPLETED. R & R STALL WARNING COMPUTER AND LIFT TRANSDUCER IAW AMM 27-33-00. OPS CHECKED GOOD.SDR SIMA20131219001Stall Warning · false activationFLIGHT 2848 AFTER SHUTDOWN, WITH BOTH ENGINES OFF APU ON, GPU OFF, SPS1 INOP, SPS ADVANCED ALERTS ON EICAS & AOA COMPARATOR LIGHT ON PFD1 APPEARED. MASTER WARNING & CATION LIGHTS ALSO ALERTED & COULD NOT CLEAR OR SILENCE. WITH GPU ON, APU OFF WE WERE ABLE TOSDR 9JLA201401153095Computer · defectiveDURING PREFLIGHT OPERATIONS IT WAS DISCOVERED THAT THE RT STALL WARNING SYS HAD FAILED. THE DEFECTIVE DUAL STALL WARNING COMPUTER SN 283 WAS REMOVED & AN INSPECTED STALL WARNING COMPUTER WAS INSTALLED IAW AMM 27-31-02.SDR HALA2013092600122Circuit Card · failedWARN ELEX ADVISORY DISPLAYED IN FLIGHT ALONG WITH AMBER SPLIM ON F/O ADI SPEED TAPE WITH LOSS OF RED SPEED TAPE INDICATOR BAR. REPLACED RT WARNING ELEX STALL WARNING CARD. OPS CHECK OK IAW FIM 27-32-00, FIG 105.SDR SIMA20130916005Control Panel · smokeSMOKE SEEN COMING FROM STALL PROTECTION TEST PANEL. SMOKE AND ELECTRIC ODOR PRESENT IN COCKPIT. SMOKE ALSO SEEN COMING FROM STALL PROTECTION TEST BUTTON. R & R STALL PROTECTION PANEL IAW AMM 20-13-10. OPS CHECKED GOOD IAW AMM 27-36-00.SDR CA131104008Transmitter · unresponsive(CAN) THE STICK SHAKER AND PUSHER SYSTEM WAS TESTED PRIOR TO DEPARTURE AS REQUIRED TO CLEAR THE CAWS DISPLAY OF THE PUSHER INDICATION AND INDICATED A SERVICEABLE SYSTEM. DURING TAKE OFF THE SHAKER SYSTEM WAS ACTIVATED AND THE AIRCRAFT RETURNED TO BASE WITHOUT SDR CALA2013083090874Screw · looseVERY LOUD SQUEAL ROW 1-2 NEAR WALL-FLOOR. PRESSURIZED ACFT IAW AMM 05 -53-00-780-03. FOUND CAPTAINS AOA SENSOR ATTACHMENT SCREWS LOOSE, SECURED. FIRST OFFICERS AOA BLANKING PLATE CLOCKED WRONG. REINSTALLED IAW MM. NO NOISE NOTED.SDR CALA2013082990844Screw · looseLOUD SQUEAL ABOVE SEAT 2A. REMOVED PSU ABOVE SEATS 2A & 2B, REMOVED SIDEWALL CEILING PANELS ABOVE ROWS 2 & 3 LT SIDE. AIR ESCAPING FROM RISER DUCT WHERE IT ATTACHES TO INDIVIDUAL AIR SUPPLY DUCT ABOVE SIDEWALL AT ROW 3, ADJUSTED & SECURED CLAMP, NO NOISE NOTSDR CA130823012Computer · failed(CAN) AOA SYSTEM FAIL LIGHT ILLUMINATED IN FLIGHT. AOA COMPUTER FOUND TO BE FAILED.SDR REXA2013070401331Stall Warning · false activationSTALL FAIL ENROUTE. QRH COMPLETED. PERSISTED WHOLE FLIGHT. FOUND OXYGEN SERVICING PANEL DOOR WAS LEFT OPEN. INSPECTED & SECURED OXYGEN SERVICE PANEL DOOR CLOSED IAW AMM 52-45-26. PERFORMED OPS CHECK OF STALL PROTECTION SYS IAW AMM 27-35-01. OPS CHECKED GSDR AALA20130629006Computer · inoperativeSLAT DISAGREE LIGHT ILLUMINATED ALONG WITH AUTO SLAT FAIL LIGHT. EMERGENCY DECLARED FLIGHT LANDED DFW WITHOUT INCIDENT. REPLACED NR 1 STALL WARNING COMPUTER. SYSTEM GROUND CHECKED NORMAL.SDR REXA2013061901197Stall Warning · contaminatedSTALL FAIL CAUTION MESSAGE WITH A IAS FLAG ON ISIS AND A YELLOW SSEC MESSAGE. REMOVED WATER FROM STANDBY SYSTEM, TRAP BLEW OUT STANDBY SYSTEM WITH NIT. PERFORMED PITOT STATIC LEAK CHECK OF THE STANDBY SYSTEM IAW AMM 34-11-00. LEAK CHECKS GOOD.SDR REXA2013056021060Stall Warning · activatedSTALL FAIL MASTER CAUTION ON CLIMBOUT, MESSAGE PERSISTED FOR DURATION OF FLIGHT.SDR REXA2013060101061Stall Warning · false activationSTALL FAIL MASTER CAUTION ON CLIMB OUT, MESSAGE PERSISTED FOR DURATION OF FLIGHT IAW MOC PERFORMED FIM PROCEDURE PIT TEST MESSAGE CLEARED. OK FOR SERVICE.SDR UALA2013050703209Circuit Card · failedCONTINUOUS STICK SHAKER ON GROUND AT GATE. REMOVED AND REPLACED A STALL WARNING PRINTED CIRCUIT CARD, OPS CHECKED OK.SDR UALA2013050203054Aoa · failedAIRCRAFT HAS A PITCH OSCILLATION WITH ANY AUTOPILOT IN COMMAND AND MODE SELECTED. FOUND RT AOA SENSOR FAILED MESSAGE INTERMITTENT IN CRUISE. REPLACED RT AOA SENSOR IAW AMM.
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