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 9JLA2021032410176Aoa · defectiveTHE MAINTENANCE TEAM DISCOVERED THE LEFT AOA HEAT FAIL AMBER CAS MESSAGE ILLUMINATED WITH LEFT PROBE SWITCH ON. THE MAINTENANCE TEAM TROUBLESHOT AND DETERMINED THAT THE LEFT AOA TRANSMITTER WAS DEFECTIVE. THE AOA TRANSMITTER WAS REMOVED AND REPLACED WITH A NEWSDR HNAA2021021500051Computer · malfunctionedPDIS 669 27-36 2433571 13FEB21 SYR CLOSE
AFTER T/O GOT SPS2 INOP WITH SPS ADVANCED AND THE AOA FLAGGED ON F/O'S PFD.
FACT 13FEB21 14:01 SYR
R/R STALL PROTECTION COMPUTER IAW EMB AMM 27-36-02. OPS CHECK GOOD.SDR HNAA2021020800045Stall Warning · inoperativeSPS 1 INOP MASTER WARNING ON TAKE OFF ROLL REJECTED TAKE OFF. T/S SPS 1 INOP REF FIM 27-36-00-810-801-A FOUND TRAN SITORY CONDITION PERFORMED STALL PROTECTION SYS OPS CHECK IAW AMM 27-36-00 OPS CHECK GOOD A/C OK FOR SERVICE.SDR HNAA2021020400043Aoa · malfunctionedSPS1 INOP AND SPS ADVANCE EICAS MSG ON TAKE OFF ROLL. MAINTENANCE: FOLLOWED FIM TASK 27-36-00-810-807-A - NO DEFECTS. NOTED REINSTALLED CTOR,SPC,AND RACK./// TRANSCRIBED TO HA300 SEQ #4 ON WORK PACKAGE DATED 02/04/21. AIRCRAFT IS STILL IN WORK R/R #1 AOA VANE.SDR QXEA2021020100040Transducer · failedIN CRUISE AT 25000 'PUSHER SYST FAIL' CAUTION LIGHT ILLUMINATED. RAN E&A CHECKLIST TURNED OFF STICKER PUSHER SHUTOFF. NO LOW SPEED CUE ON AIRSPEED TAPE. AFTER LANDING ON ROLLOUT BOTH NR 1 & NR 2 STALL SYST FAIL CAUTION LIGHTS ILLUMINATED. REMOVED FROM SERVSDR SIMA20210118003Aoa · failedSPS-1 FAIL IN CLIMB 17,000-FL190 RAN QRH PROCEDURE, SPS 1-2 INOPERABLE MESSAGE. MECH SPS 1 FAILURE EMERGENCY DECLARED. CONTINUED TO ORD. C/A: R & R NR 1 AOA SENSOR, IAW EMB 145 AMM TASK 27-36-01. OPERATIONS CHECK GOOD.SDR SIMA20210118002Computer · failedSPS 1-2 INOPERABLE, STICK PUSHER FAIL, SPS ADVANCED MECHANICAL DECLARED EMERGENCY FLIGHT CONTINUED DTW. C/A: R & R SPC IAW AMM 27-36-02. OPERATIONS CHECK GOOD.SDR 3SDR20210216006Stick Shaker · faultedDURING FLIGHT, STICK PUSHER DID NOT ACTIVATE AND DID NOT GIVE ANY INDICATION OF A SYSTEM FAILURE.SDR GAJA01.04.21.01Detector · failedSTALL WARNING HORN ACTIVATED IN STRAIGHT AND LEVEL FLIGHT, PILOT CONTINUED NORMAL OPERATIONS AND LANDED SAFELY. UPON TROUBLESHOOTING, FOUND LIFT DETECTOR (ON-WING) TO HAVE INTERNALLY FAILED. REPLACED LIFT DETECTOR, ALL CHECKS GOOD.SDR 9JLA2020120220245Computer · defectiveA FLIGHT WAS CANCELLED WHEN THE FLIGHT CREW PERFORMING PREFLIGHT CHECKS DISCOVERED A FAULT WITH THE RIGHT STALL WARNING SYSTEM. THE MAINTENANCE TEAM TROUBLESHOT AND DETERMINED THE STALL WARNING COMPUTER WAS DEFECTIVE. THE DEFECTIVE COMPUTER WAS REMOVED AND ASDR DALA2020111903796Computer · inoperativeDIV- DIVERTED TO DEN DUE TO BOTH STICK SHAKERS CONTINUOUSLY ACTIVATED. ON ARRIVAL RIGHT STICK SHAKER ACTIVATED, RESET C/B. PERFORMED LT-RT SMYD COMPUTER BITE CHECKS, SMYD-1 FAULT 27-31009. SMYD-2 FAULT 27-32009 RECORDED. REPLACED RT AOA SENSOR AND SMYD-2SDR DALA2020111803772Module · malfunctionedIN CLB FL310 GOT AMBER IAS DISSAGREE BOTH PFD'S LEFT SIDE CA IAS BAD. F/O + STANDBY INDICATIONS BOTH AGREED, FEW MINUTES INTERMITTENT. CLACKER FOR 3 MIN, ALSO GOT A/T LIM INDICATION IN UPPER DU CTR. ALSO EEC THEN WENT TO ALT EEC. REMOVED & REPLACED AOA SENSDR UIEA2020111402393Circuit Card · malfunctionedADI FAILURE FLAG "SPD LIM". REMOVED AND REPLACED LEFT STALL WARNING M615 CARD, REF AMM 27-32-01. STALL WARN TEST PASSED.SDR AALA202011129015Sensor · inoperativeAIRCRAFT WAS GROUNDED. CLIMBING THROUGH FL225, ALTITUDE DISAGREE ILLUMINATED WITH BOTH SIDES IN ICING CONDITIONS (-3 DEGREES C). FLIGHT DECLARED EMERGENCY AND DIVERTED TO JFK, LANDED WITHOUT INCIDENT. REPLACED LT ANGLE OF ATTACK SENSOR WITH NEW, IAW AMM 34-SDR CALA2020103001228Aoa · damagedCAPT`S PITCH LIMIT INDICATOR CAME DOWN UPDATED MAA CODE FIX USING VENDOR MAA SCREEN, PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. UPDATED MAA CODE FIX USING VENDOR MAA SCREEN, PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. MAC RELATED WORK ORDER 00000000SDR IPXA2020102761735Aoa · inoperativeINSPECTION TYPE: N/A ATB NO EMERGENCY DECLARED. LANDED WITHOUT INCIDENT. IAS DISAGREE ALT DISAGREE AND STELL WARNING PLI SHOWED IN CAPTAINS FD STICK SHAKER WAS ON FOR ENTIRE FLIGHT IAS DISAGREE CHECKLIST WAS RAN. REMOVED AND REPLACED THE DAMAGED LEFT AOA VASDR CALA2020102301201Aoa · failedCREW REPORTS CAPT'S STALL WARNING GOING OFF TOO EARLY. DFCS TEST FAULTS SMYDC-1. BITE TEST OF SMYD-1 FAULTS AOA SIGNAL ERROR 27-31004, REF FIM 27-32-00-810-809. SENSOR ON ORDER. M&E 29-3412-9-0001. REPLACED ANGLE OF ATTACK SENSOR, PER AMM 34-21-05-400-801SDR VNAA2020102311102Transducer · failedEMERGENCY DECLARED FOR A STALL FAIL CAUTION MESSAGE. CREW ASKED FOR 36C FOR AN ABUNDANCE OF CAUTION DUE TO INCREASED LANDING DISTANCE AND ATC DECLARED FOR THEM. TRUCKS ROLLED. THE AIRCRAFT LANDED SAFELY AND TAXIED TO THE GATE WITH NO ISSUES. THE AIRCRAFT ISDR CALA2020100901167Computer · malfunctionedYAW DAMPER OFF AFTER TAKEOFF. WHEN RE-SELECTED RUDDER ENGAGED ABRUPTLY. FOUND POSITION 1 SMYD FAILED SELF TEST. REMOVED AND REPLACED POSITION 1 SYMD, PER AMM 27-32-42. ALL TESTS PASSED. S/N OFF 0869 COMPUTER, STALL OFF 29-2732-9-0003 0869 ON 29-2732-9-000SDR IPXA2020100661015Circuit Card · false activationINSPECTION TYPE: NA, DIVERSION, NO EMERGENCY DECLARED. SPD LIM ANNUNCIATED ON CAPT'S PFD BEFORE SPEED LIMIT IS APPROACHED. NO AIRSPEED LIMITS WERE APPROACHED OR EXCEEDED DURING FLT. REMOVED AND REPLACED LEFT STALL WARNING MODULE CARD ASSEMBLY, PER AMM 27-32SDR AALA202010059006Sensor · failedAIRCRAFT WAS GROUNDED: CAPTAINS AOA SENSOR FAILED DURING CLIMB OUT, CLIMBING THROUGH FL 350, OAT -42 DEGREES. REPLACED AOA SENSOR PER AMM 34-11-19.SDR HALA2020092800189Actuator · defectiveATB - AP1 DISCONNECTED DURING CLIMB WHEN RE-ENGAGED IN AP2. PLANE TURNED SEVERAL DEGREES OFF COURSE BEFORE FINDING COURSE AGAIN. PERFORMED FCC 1 & 2 BITE TEST, PER AMM 22-00-00 AND FOUND "A/P STICK PUSHER" SYS FAIL. REMOVED AND INSTALLED STICK PUSHER SERVO SDR SIMA202009064001Computer · malfunctionedON DESCENT SPS 2 INOPERABLE WARNING WENT AWAY, BUT CAME RIGHT BACK AS WE RAN THE QRH SPS 1 INOPERABLE AS WELL WE ALSO RECEIVED STICK PUSHER FAIL AND SPS ADVANCED MECH, SPS FAIL. EMERGENCY DECLARED C/A-REF FIM TASK 27-36-00-810-A. PERFORMED RESET OF STALL PROTSDR IPXA2020081959232Aoa · faultedAIR TURNBACK, NO EMERG DECLARED. ALT DISAGREE EICAS MESSAGE PASSING 6000'MSL, ALT DIFFERENCE OF 320' BETWEEN CAPT & F/O INST,COMPLETED AIRSPEED UNRELIABLE PROCEDURE(W/ALTN AIR DATA SELECTED(CAPT SIDE), CAPT & F/O A/S & ALT COMPARISON FL 280 ALT SPLIT 300' ASDR AALA202008049001Aoa · defectiveAIRCRAFT WAS GROUNDED: SPEED LIMIT ILLUMINATED ON CAPT. PFD FOR A FEW SEC. MULTIPLE TIMES EVERY MINUTE. THEN AUTO PILOT DISENGAGES FMA SHOWS CWS P MIN MANUVER SPEED YELLOW BAR DISPARES DURING SPD LIM.REPLACED LEFT AOA SENSOR PER AMM 3421-05.SDR AALA2020072879043Aoa · inoperativeAIRCRAFT WAS GROUNDED: ON TAKE OFF ROLL UPON ENGAGING TOGO AUTOTHROTTLES DISENGAGED AND TAKE OFF CONFIGURATION WARNING SOUNDED, REJECTED TAKE OFF AT APPROXIMATELY 45 / KNOTS. MAINTENANCE DETERINED THAT THE SPEED BRAKE TAKEOFF WARNING SWITCH WAS NOT ENGAGING USDR AALA2020072879042Aoa · inoperativeAIRCRAFT WAS GROUNDED: ON TAKE OFF ROLL UPON ENGAGING TOGO AUTOTHROTTLES DISENGAGED AND TAKE OFF CONFIGURATION WARNING SOUNDED, REJECTED TAKE OFF AT APPROXIMATELY 45 / KNOTS. MAINTENANCE DETERINED THAT THE SPEED BRAKE TAKEOFF WARNING SWITCH WAS NOT ENGAGING USDR AALA2020072749001Aoa · malfunctionedAIRCRAFT NOT GROUNDED - INTERMITTENT SPEED LIMIT INDICATION ON CAPTAIN'S PRIMARY FLIGHT DISPLAY (PFD). LOW AIRSPEED WARNING HOOK DISAPPEARS AT SAME TIME. REMOVED AND REPLACED LEFT ANGLE OF ATTACK (AOA) SENSOR PER AMM 34-21-05, ALL REQUIRED CHECKS PASS.SDR CALA2020062901026Aoa · reads highEEC ALTN MODE ON TAKEOFF ... AIRSPEED UNRELIABLE PER FLIGHT CREW VERBAL REPORT, CAPTAINS AIRSPEED INDICATION READS APPROXIMATELY 40KNOTS SPLITS BETWEEN THE STANDBY AND THE FO AIRSPEED INDICATOR. PERFORMED ALPHA VANE RIGGING TEST IAW AMM 22-11-00-820-809, FOUNSDR UIEA2020051201020Sensor · malfunctionedL AOA EICAS AFTER ENG START(<P>TRANSFERRED TO MDDR 128280 PER MEL 30-32-01, CAT 'C'.</P><P>LP 1131025: REMOVED AND REPLACED LEFT AOA SENSOR IAW AMM 34-12-03, OPS TEST OK. THIS CLEARS MDDR 128280.<BR /></P>)SDR RU3A202004216017Switch · faultySTALL FAIL CAME ON AFTER TAKEOFF. CAUSE WAS ACCELERATION SWITCH. REPLACED ACCELERATION SWITCH.SDR AALA202003309007Sensor · faultyAIRCRAFT WAS GROUNDED: SPD LIM FLAG ON CA PFD STICK SHAKER ACTIVATED,TWICE, AUTO SLAT FAIL, AIRSPEED INDICATIONS WERE,NORMAL, ALL HAPPENED ON CLIMBOUT. RETURNED TO BOS. ACCOMPLISHED SYMD BITE REF FIM 27-32-00-810-801 FOUND MX MSG 27-31004 AOA SIG ERROR T/S PERSDR YENA2020032070245Sensor · failedFLT 2020. FLL-ORH. DIVERTED TO JFK. EMERGENCY FLIGHT DECLARED. ADS 1 FAIL IN FLIGHT TO ADS3 RH WAS BLOCKED OUT WITH LINES QRH TO ADS 2 COMMON SOURCE ATARUAL CONTINED FOR DURATION COULD NOT RESET ; R & R #1 PITOT/STATIC/AOA SENSOR IAW AMM 34-13-01 PERFORMED OPSSDR SIMA202003098001Computer · malfunctionedHIGH SPEED ABT 105KTS DUE TO STALL PROTECTION 1 AND 2 INOP WARNING ON TAKE-OFF ROLL- REJECTED TAKE OFF-C/A-REF NRWC 677-ORD-04250 FOR CMC DOWNLOAD FOUND SPC FAIL ON CMC.T/S IAW EMB 145 FIM 27-36-00.RAR SPC IAW EMB 145 AMM 27-36-02. / PERFORMED OPS CHECK OF STSDR FDEA2020021080290Stick Shaker · inoperative"WARN ELEX" ON STATUS PAGE DURING PREFLIGHT TROUBLESHOOTING PER B767 FIM 27-32 FT803, WITH IRU'S ALIGNED THE WARN ELEX MSG CLEARS BUT PER BLK 2 WHEN THE LEFT STALL WARNING SWITCH IS TOGGLED THERE IS NO STICK SHACKER AND "WARN ELEX" APPEARS ON THE STATUSSDR VNAA2020021671101Warning Message · illuminatedSTALL FAIL AMBER CAUTUON ON TAKEOFF. MAINTENANCE INSPECTED AND CLEANED PITOT WATER TRAPS AND PUGED THE PITOT SYSTEM WITH NO FURTHER DEFECTS NOTED.SDR SIMA202001197007Aoa · malfunctionedINBND SDF DECLARED EMERGENCY ACCT MECH STICK PUSHER FAIL INDICATION.SPS 1 INOP IN FLIGHT-C/A-RAR NO 1 AOA SENSOR IAW EMB 140 AMM 27-36-01. OPS CHECKS GOOD.SDR IPXA2020010850753Stick Shaker · faultyINSPECTION TYPE:N/AAIR TURN BACK - ON TAKE OFF ROLL THRU 10,000 FT AIRCRAFT HAD A SEVERE SHAKING IN YOKE AND RUDDER ALL ECAM INDICATIONS NORMALISOLATED TO CAPTAINS STICK SHAKER WHEN PULL CAPTAINS STICK SHAKER CB THE SHAKING GOES AWAY & WHEN RESET SHAKING COMESDR RU3A20200108001Warning Light · activatedSTALL PROTECTION SYSTEM FAIL LIGHTS FLASHING IN FLIGHT.SDR HNAA2020010600013Computer · inoperativePDIS 650 27-36 2289051 05JAN20 PHL CLOSE
SPS 2 INOP AND SPS ADVANCED DURING REJECTED TAKEOFF
FACT 05JAN20 20:15 PHL
PERFORMED OPS CHECK IAW AMM 27-26-00. DETERMINED FAU
LT ON STALL PROTECTION COMPUTER. R&R SPC COULSDR AALA2019121879016Sensor · faultyAIRCRAFT WAS GROUNDED: ON DESCENT OUT OF FL300 IN IMC CONDITIONS GOT IAS DISAGREE. FOS AIRSPEED/MACH INDICATED 8 KIAS .5 MACH LOW. HAPPENED SEVERAL TIMES BETWEEN FL300 AND FL200 THEN CORRECTED. MAINTENANCE TROUBLESHOT IAW FIM 31-62-00. BITE CHECKED ADIRU AND CSDR HNAA2019121600386Relay · malfunctionedSPS 2 INOP DISPLAYED IN FLIGHT WITH AOA ANNUNCIATION ON F/O'S PFD. MAINTENANCE REMOVED AND REPLACED RELAYS K0357 AND K0359. PERFORMED STALL PROTECTION SYSTEM ADJUSTMENT AND TEST IAW E145 AMM 27-36-00 STALL PROTECTION SYSTEM OPERATION CHECK GOOD AT THIS TIME. ISDR SWIA2019111246760Transducer · faultyON DEPARTURE FOS LOW SPEED CUE WAS STUCK ON THE GREEN LINE. FLIGHT # 5066 CLOSED REMOVED AND REPLACED RH AOA TRANSDUCER IAW AMM. PERFORMED AOA OPS CHECK IAW AMM. OPS CHECK GOOD AT THIS TIME. PERFORMED FUNCTIONAL TEST OF STALL PROTECTION COMPUTER (GREEN ACCSDR COEA2019110753807Proximity Switch · faultyFLIGHT 1700, HNL-ITO AIR TURNBACK/APPROX. 14:15 DISCREPANCY: AFTER GEAR WAS RETRACTED, FLIGHT CONTROL LIGHT ON CAP AND STICK SHAKER LIGHTS ILLUMINATED. AIRCRAFT WAS RETURNED TO HNL. NO EMERGENCY DECLARED. LANDED WITHOUT FURTHER INCIDENT. CORRECTIVE ACTION: MASDR COEA2019110752807Aoa · faultyFLIGHT 1700, HNL-ITO/AIR TURNBACK AT APPROX.1045Z DISCREPANCY: FLIGHT CONTROL LIGHT ON CAP AND STICK SHAKER FAULT LIGHTS ILLUMINATED AFTER TAKEOFF. AIRCRAFT RETURNED TO HNL. NO EMERGENCY DECLARED. LANDED WITHOUT FURTHER INCIDENT. CORRECTIVE ACTION: MAINTENANCSDR COEA2019102541807Aoa · faultyFLIGHT 1700, HNL-ITO/ AIR TURNBACK DISCREPANCY: ON CLIMB OUT, THE STICK PUSHER/SHAKER FAULT LIGHT ILLUMINATED IN ADDITION TO THE MASTER CAUTION LIGHT. THE AIRCRAFT WAS RETURNED TO HNL. NO EMERGENCY DECLARED. LANDED WITHOUT FURTHER INCIDENT. CORRECTIVE ACTION:SDR SWAA2019091937021Sensor · inoperativeAIR DATA INSTRUMENTS DISAGREE ON TAKEOFF. TAKEOFF CONTINUED, RETURNED TO DAL. R&R AOA SENSOR IAW AMM.SDR DALA2019090205110Computer · malfunctionedSTALL INDICATION FAILURE MESSAGE ON EOAP ON GROUND. WOULD NOT CLEAR. MULTIPLE LOTS STALL WARN 2 CORD ON RESET BUT COMP HAS ELECT SMELL & TEST SW STICKS INTO IN NORMAL. R&R SAME. OPS NORMAL. REF AIM 34_19. COMPUTER, STALL OFF 88-3415-9-0001 S/N01946. (LP4623602SDR CA190802010Computer · malfunctioned(CAN) STALL ALT COMP LIGHT AND STALL FAIL ARE ANNUNCIATIED. FIELD SERVICE REPRESENTATIVE INPUT AUG 1, 2019: FAULT CLEARED THE NEXT MORNING. ADVISED CUSTOMER TO REPLACE THE STALL COMPUTER. (TC# 20190802010)SDR CA191003024Computer · faulted(CAN) AIR TURN BACK, ON CLIMB OUT, INTERMITTENT STALL FAIL CAUTION MESSAGE. CORRECTIVE ACTION: REMOVED AND REPLACED STALL PROTECTION COMPUTER W/A SERVICEABLE UNIT. (TC# 20191003024)
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