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 CA110608003Computer · intermittentPILOT REPORTED THAT WHEN PERFORMING "STICK PUSHER TEST" THAT TEST WAS NOT CORRECT AND "PUSHER" CAWS LIGHT WOULD NOT EXTINGUISH. STICK PUSHER COMPUTER REPLACED, FUNCTIONAL TEST PERFORMED. STICK PUSHER SYS FUNCTIONED NORMAL.SDR UALA2011060302730Stick Shaker · malfunctionedSTICK SHAKER X4 WITH FLAPS DOWN & THROTTLES AT IDLE. TEST FLOWN FOR SHAKER.OPS NORMAL. SHAKER CHECKED AT FLAPS 0' 5 AND 30. NOTED FOR SFOEG. DIAGNOSTIC TEST FLIGHT: DUE TO REPEAT GRIPES OF THE STICK SHAKER GOING OFF AT VARIOUS FLAP SETTINGS, A DIAGNOSTIC TESTSDR MASA2011053102905Transducer · malfunctionedLEFT STALL WARNING IN FLIGHT. R & R NR 1 LIFT TRANSDUCER.SDR MASA2011053002896Aoa · malfunctionedSTALL FAIL CAUTION IN FLIGHT. R2 RT AOA AND SPC.SDR MASA2011052702868Stall Warning · malfunctionedSTALL FAIL CAUTION AFTER TAKEOFF. RESET NFAR RESET SYSTEM PER FIM 27-35-00. OP CHECK GOOD PER CFM.SDR REXA201100293Stall Warning · activatedAIRCRAFT DID AIR RETURN DUE TO STALL FAIL AFTER GEAR RETRACTION, NO EMERGENCY DECLARED.SDR C2XA11TY060Sensor · inoperativeTYS - A/C WAS FERRIED FROM CHS TO TYS WHEN CREW GOT A SPS 2 INOP ACCOMPANIED BY A AOA AMBER FLAG ON FO PFD. MAINTENACE REMOVED AND REPLACED THE NR 2 AOA VANE SENSOR IAW EMB 145 AMM 27-36-01. OPS CHECK GOOD AND WAS RELEASED.SDR TRBA2011054Probe · failedSTICK PUSHER SHAKER FAULT LIGHT ILLUMINATED AFTER TAKEOFF. EMERGENCY DECLARED AND RETURN TO BASE. RAI LT AOA PROBE IAW AMM 27-36-15 (NOTE MFC CODE SHOW LT AOA FAULT). RELEASED ACFT FOR FCF PURPOSES ONLY. FCF FOUND SATISFACTORY.SDR TRBA2011053Probe · failedSTICK PUSHER SHAKER FAULT LIGHT ILLUMINATED JUST AS ACFT ROTATED, ALL CONTROL INPUTS WERE NORMAL. EMERGENCY DECLARED AND RETURN TO BASE. R & R ANGLE OF ATTACK PROBE PILOT SIDE IAW JIC 27-36-15 RAI 10000. OPS CHECK GOOD.SDR QXEA2011041900285Stick Shaker · malfunctionedON LANDING RECEIVED PUSHER SYS FAIL CAUTION LIGHT. DID NOT CLEAR WITH EMERGENCY CHECKLIST PROCEDURE. COMPLIED WITH SL DH8-400-SL-31-005 FOR NUISANCE PUSHER SYS FAIL CAUTION LIGHT. RESET BREAKERS AND ALL CHECKED GOOD. RETURNED TO SERVICE. NO PARTS REPLACED.SDR CA110408001Servo · intermittent(CAN) PILOT REPORTED A PUSHER CAS MSG DURING CRUISE FLIGHT. UPON LANDING THE STALL WARNING 1 & 2 BREAKERS WERE OPENED & CLOSED IN AN EFFORT TO EXTINGUISH THE CAS MSG, HOWEVER THE MSG REMAINED. WHILE MX WAS PERFORMING AN OPERATIONAL TEST, THE PUSHER SERVO WASSDR CA110406001Computer · malfunctioned(CAN) DURING CLIMB, THE MASTER CAUTION ILLUMINATED AND PUSHER SYS FAIL AND RT STALL WARNING CAUTION LIGHTS ILLUMINATED. THE QRH WAS ACTIONED AND THE COMPANY ADVISED. RETURN TO BASE. NR 2 STALL WARNING COMPUTER REPLACED.SDR UALA2011030201028Module · faultySTALL WARNING OPS CHECK FAILS STEP B8, ALL OTHER STEPS CHECK OKAY. CAPT'S SIDE DOES NOT DISPLAY PITCH LIMIT INDICATOR AND NO STICK SHAKER WITH AIR DATA SWITCH IN ALT. FOUND 115V AC ON PIN 5 WITH SOURCE SWITCH IN ALT. FOUND 115V AC AT PIN 6 WITH SOURCE SWITCSDR AALA20110211TUL05Vane · brokenSAL - CREW REPORTED ANGLE OF ATTACK AND AIRSPEED FAILED. EMERGENCY DECLARED FLIGHT RETURNED SAL LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND FIRST OFFICERS AOA VANE BROKEN. PLANNED REPLACE FIRST OFFICERS ANGLE OF ATTACK VANE. SYSTEM GROUNSDR VNAA2011020100013Transducer · failedCREW REPORTED A STALL FAIL MESSAGE IN FLIGHT AFTER DEPARTURE FROM CLT. CREW RETURNED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT THE AIRCRAFT, REMOVED AND REPLACED THE RIGHT AOA TRANSDUCER AND PERFORMED CHECKS USING THE AIRCRAFT MAINTENANCE MSDR UALA2011010400043Sensor · faultyICING ISSUE, FLIGHT DIVERTED. CAPTAIN'S ANGLE OF ATTACK PROBE HEATER INOPERATIVE. RESET, NO HELP. ACCOMPLISHED CFDS PHC TEST. AOA SENSOR 3FP1 FAILS TEST. REPLACED AOA SENSOR 3FP1 IAW AMM, CHECKED OK.SDR QXEA2010122900948Stick Shaker · malfunctionedDURING THE TAKE OFF ROLL, THE PUSH SYS FAIL CAUTION ILLUMINATED, TAKEOFF WAS ABORTED AT 50 KTS. C/W OPS CHECK OF THE ELEVATOR CONTROL STICK PUSHER IAW TASK 27-33-710-802, NO DEFECTS NOTED. COULD NOT DUPLICATE. RETURNED TO SERVICE. NO PARTS REPLACED.SDR QXEA2010121700903Computer · malfunctionedSTALL FAIL CAUTION MESSAGE DURING CLIMBOUT. EMERGENCY AND ABNORMAL CHECKLIST COMPLIED WITH; CAPT STALL PROTECTION SWITCH TURNED OFF. RETURNED TO FIELD. LANDING UNEVENTFUL. R & R STALL PROTECTION COMPUTER AS A PRECAUTIONARY MEASURE. AMM TASKS 27-35-01-000-71SDR IPXA0163740Computer · inoperativeAFTER ROTATION GOT A MASSIVE VIBRATION IN THE CAPT & F/O YOKE. CREW DID AIR TURN BACK. NO INDICATIONS ON ECAM OR ROUND DIALS. DURING RETURN NUMEROUS ECAM MESSAGES WITH STICK SHAKER. AFTER LANDING ROLLOUT STICK SHAKER REMAINED ON. REPLACED 48FU1 RELAY. SDR O2GAN118RHWarning Light · illuminatedSTALL WARNING LIGHT ENROUTE TO DESTINATION, QRH FOLLOWED AND LANDED AT PLANNED DESTINATION, NOT PROBLEMS.SDR UALA2010112904360Module · faultyRT STALL WARNING INOP. REPLACED BITE MODULE.SDR HNAA2010112200247Computer · malfunctionedON ROTATION, STICK SHAKER ACTIVATED FOR REMAINDER OF FLIGHT. R & R NR 1 COMPUTER AND CALIBRATED IAW MM 27-33-00. RECONNECTED SHAKERS, OPS CHECKED GOOD.SDR CA101029002Stall Warning · failed(CAN) NOTE: AOA ASSEMBLY TSI AND TSN = 19155 CSI AND CSN = 9062. IAS DISAGREE MESSAGE AT APPROX 70 KTS FIRST OFFICER SIDE AND 60 KTS CAPTAIN SIDE. FIM 31-62-876 ACCOMPLISHED NFF AND PITOT STATIC SYSTEM TEST ACCOMPLISHED IAW 34-21-00 NFF LEFT HAND AOA VANE RSDR NSVA2010182Stall Warning · malfunctionedDURING FIRST FLIGHT OF THE DAY CHECKS STALL 2 DID NOT TEST PROPERLY AND WHEN BOTH STALL TEST SWITCHES ARE PUSHED UP THE PUSHER DID NOT ACTUATE. PERFORMED STICK PUSHER RESET PROCEDURE AND PERFORMED OPS CHECK, FOUND GOOD IAW AMM 27-35-00-05.SDR REXA20100146Computer · malfunctionedWINDSHEAR FAIL STATUS MSG ALONG WITH STICK SHAKER CAME ON AND OFF JUST AFTER LIFT OFF. REMOVED AND REPLACED STALL PROTECTION COMPUTER IAW AM 27-35-01. OP CHECK GOOD. GPWS OP CHECKS GOOD IAW AMM 34-42-01.SDR NSVA2010163Vane · damagedRIGHT AFTER TAKEOFF FLIGHT ENCOUNTERED MULTIPLE BIRD STRIKES (3 CROWS) DAMAGE FOUND TO THE RIGHT AOA VANE, RIGHT LANDING LENS AND RIGHT PROP BLADE NR 1. REPLACED RIGHT AOA VANE, REPLACED RIGHT PROP BLADE NR 1, AND REPAIRED SKIN DAMAGE AREA'S.SDR GUUA93327072810AAoa · malfunctionedUPON TAKEOFF AFTER LANDING GEAR UP STALL WARNING CAME ON AND SOUNDED UP TO 500 FEET ON AND OFF. SECURED AND CLEANED STALL WARNING VANE. TEST FLIGHT SATISFACTORY.SDR COMA2010062570018Stall Warning · malfunctionedDURING APPROACH INTO MEM RECEIVED STALL FAIL CAUTION MSG. FOLLOWED QRH, EMERGENCY DECLARED A/C LANDED SAFELY. PERFORMED CRJ FIM TASK 27-81-00-810-802, CLEARED INHIBITS. OPS CHECK GOOD, NO FURTHER DEFECTS.SDR HALA2010060300243Circuit Card · malfunctionedETOPS SIGNIFICANT SYS- ALTITUDE ALERT LIGHT FAILED TO ILLUMINATE ON DESCENT. R & R ALTITUDE ALERT WARNING DCA CARD IAW AMM 31-51-04, OPS CHECK OK.SDR AALA20100602SAT01Stick Shaker · faultySAT - INFLIGHT DFW-MEX. CREW REPORTED AIRCRAFT VIBRATIONS ON THE FLIGHT CONTROLS. FLIGHT DIVERTED SAT LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED FIRST OFFICERS STALL SHAKER AND STALL WARNING COMPUTER. SYSTEM GROUND CHECKED NORMAL OPSDR UALA2010052401776Circuit Card · faultyDURING CLIMB AFTER FLAP RETRACTION, CAPTS ADI DISPLAYED THE STALL SPEED WHISKERS TILL FL200. ACCOMPLISHED FIM, NO FAULTS NOTED. BOTH STALL WARNING CARDS REPLACED ON APR-26. FAULT CHANGED TO LEFT SIDE ONLY. REPLACED LEFT STALL WARNING MODULE, ALL SUBSEQUENT TESSDR 2010FA0000534Sensor · unsecure((JGVR)) RECEIVED UNIT, AS A REPAIRED UNIT. SENSOR HSG FOUND, NOT SECURED. SENSOR COULD BE ROTATED (RECLOCKED) GIVING IMPROPER READINGS. DISCOVERED WHEN TECH ATTACHED MOUNTING BRACKETS, TEMPORARILY INSTALLED SENSOR IN ACFT, ROTATED SENSOR TO CLOCK POSITION SDR 2010FA0000448Stall Warning · malfunctionedDURING PREFLIGHT STICK PUSHER WOULD NOT TEST THE FIRST TIME THE STALL WARNING SYSTEM WAS TESTED AFTER APPLYING ELECTRICAL POWER TO THE AIRPLANE. SUBSEQUENT TESTS WERE NORMAL.SDR UALA2010042601382Circuit Card · failedSTALL WARNING, RTFL. ACP FIM MM TASK TO FIG.103 SHT 4, BLOCK 7, REFERRED TO FIM MM PSEU BITE CHK FIG 103 SHT 3 BLOCK 2, CODE 007 CARD FAILED. REPLACED PSEU CIRCUIT CARD IAW MM AND CONT FIM. REPLACED L & R STALL WARNING MOD IAW MM. ACFT OK FOR SERVICE.SDR SWIA201024085Actuator · malfunctionedON ROTATION AND FLARE, EXCESSIVE ELEVATOR BACK-PRESSURE REQUIRED. (FLT 4686) PERFORMED OPERATIONAL CHECK OF THE ELEVATOR CONTROL SYSTEM, INSPECTED CABLES AND ELEVATOR AND FOUND NO DEFECTS. PERFORMED FORCE GAUGE CHECK OF THE RIGHT AND LEFT ELEVATORS FORCES ASDR DL75E100940Sensor · out of limitsABORTED T/O DUE TO F/O AIRSPEED IND FAILING TO RISE 80KAIS ABORT. VISUAL INSPECTED PITOT TUBES FOUND NO DEFECTS. FOUND F/O AOA SENSOR OUT OF CONFIGURATION. REPOSITION TO NORMAL CONFIGURATION AND PERFORM MACH AIR SPEED TEST PER M/M 34-12-00-715, NO TROUBLE FSDR HALA2010032600136Warning Light · false activationON SHORT FINAL 04R/800'/AP & AT OFF FLAPS 40 DEG STABILIZED AT 147 KTS. THE AMBER & RED FOOT OF SPEED TAPE ZOOMED UP TO 160 KTS CAUSING STALL WARNING & STICKSHAKER TO TURN ON. IMMEDIATELY ADDED POWER, AFTER 3-5 SECONDS & AMBER & RED FOOT WENT BACK TO NORMAL LSDR COMA2010031690001Stall Warning · malfunctionedEN ROUTE FROM JFK TO ORD RECEIVED STALL FAIL CAUTION MSG. QRH COMPLETED, EMERGENCY DECLARED. A/C LANDED SAFELY AT ORD. PERFORMED CIRCUIT BREAKER RESET OF STALL PROTECTION SYSTEM, ALSO PERFORMED PER-FLIGHT TEST OF STALL PROTECTION SYSTEM. NO DEFECTS NOTED.SDR HNAA2010031700068Switch · malfunctionedON CLIMB-OUT, BOTH STALL WARNING STICK SHAKERS ACTIVATED AND FIRST OFFICER'S FAST SLOW INDICATOR SHOW 10 TO 20 KNOTS SLOW. PULLED AND COLLARED CIRCUIT BREAKERS STALL WARNING AND HEATER NR 2, STALL FAIL MON 2, STALL TRANSPONDER AND HEATER 2. REMOVED AND REPLASDR AWKA7570311Indicator · inoperativeSHORTLY AFTER TAKE-OFF, WHILE CLIMBING THROUGH FL180 THE FLIGHT CREW REPORTED HAVING AN ELECTRICAL (SMOKE) ODOR IN THE COCKPIT. THE FLIGHT CREW DECIDED TO RETURN TO DEPARTURE. A SAFE, UNEVENTFUL LANDING WAS ACCOMPLISHED. SERVICE CENTER WAS CONTRACTED TO INSPSDR MASA2010030600180Stall Warning · malfunctionedMIS RTG STALL FAIL CAUTION ON T/O 90KT. RESET STALL PROTECTION SYSTEM.SDR MASA2010030200169Aoa · malfunctionedDIVERT LT AOA HEAT CAUTION. REPLACED LT AOA.SDR CA100225001Transmitter · malfunctioned(CAN) ON TAKEOFF, ONCE THE WEIGHT ON WHEELS SIGNAL WAS PRESENT, THE STICK SHAKER WARNING ACTUATED. PILOT RETURNED FOR LANDING. ACFT SPEED WAS REPORTED AS CORRECT. THE LT AOA TRANSMITTER WAS FOUND TO BE SENDING A SHAKER RANGE SIGNAL TO THE FCWU REGARDLESS OF SDR 2010FA0000239Computer · intermittentSTALL WARNING FAILS INTERMITTENT. UNIT WAS REMOVED AND SENT FOR REPAIR. UNIT WAS REINSTALLED AND FAILED ON FIRST FLIGHT. UNIT SHOWS SIGNS OF PREVIOUS REPAIR BUT NO LOG ENTRY WAS MADE.SDR 2010FA0000238Transducer · intermittentSTALL WARNING FAILS INTERMITTENT. UNIT WAS REMOVED AND SENT FOR REPAIR. UNIT WAS REINSTALLED AND FAILED ON FIRST FLIGHT. UNIT SHOWS SIGNS OF PREVIOUS REPAIR BUT NO LOG ENTRY WAS MADE.SDR DHLA20100005Transducer · malfunctionedFLT NR 981, AT THE START OF THE TO ROLL (A/S <60 KTS) THE STICK SHAKER ACTIVATED. TROUBLESHOT FOUND LIFT TRANSDUCER BAD. R & R LIFT TRANSDUCER IAW MM 34-16-1 PERFORMED ADJUSTMENT TEST OF STALL WARN SYS IAW MMS 34-16-00 & 34-16-01, OPS NORMAL. ACFT WAS GROUNDSDR DHLA20100004Stick Shaker · malfunctionedSTICK SHAKER ACTIVATED ON TAKEOFF ROLL, AT 60 KTS REJECTED TAKEOFF. PERFORMED STALL WARNING SYS TROUBLESHOOTING IAW MM 34-16-0. NO DEFECTS NOTED. FOUND NOSE STRUT AT 9 INCHES. SERVICED NOSE STRUT IAW MM 32-21-12. W&B NOTED TO BE ON THE AFT SIDE OF THE CG. HADSDR 2010FA0000166Switch · erraticTHE STALL WARNING SYS ACTIVATES ERRATICALLY. INCIDENTS SURROUNDING THE STALL WARNING SYS ANOMALIES: SITTING MOTIONLESS ON THE GROUND, ENGINES NOT RUNNING. SITTING MOTIONLESS ON THE ENGINE RUNNING. DURING CLIMB, IN CLEAR AIR, BETWEEN 108 AND 140 KIAS. AT CSDR A6WA201040082Computer · malfunctionedSTALL FAIL CAUTION AFTER TAKEOFF. QRH COMPLETED. STALL FAIL MESSAGE REMAINS. R & R STALL PROTECTION COMPUTER IAW AMM 27-35-01-000-400-801. OPS CK GOOD IAW AMM 27-35-01-710-801.SDR MASA2010012600080Stall Warning · false activationABORTED TAKEOFF FOR STALL FAIL CAUTION DURING HIGH WIND GUSTS. WIND GUSTS WERE DETERMINED TO BE THE CAUSE OF THE STALL FAIL INDICATION. STALL SYSTEM TEST OPS NORMAL, NO FURTHER ACTION IS REQUIRED.
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