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 TAMF20260913061Aoa · out of limitsAIRCRAFT EXPERIENCED AN ECAM NAV AOA EXCEEDED MESSAGE ASSOCIATED WITH TURBULENCE. AIRBUS CONFIRMED LOADS EXCEEDING THE AIRCRAFT DESIGN ENVELOPE. REQUIRED INSPECTIONS WERE PERFORMED AND AIRBUS AUTHORIZED AIRCRAFT RELEASE THROUGH RDAF 81873879/017/2026 ISSUE ASDR SWIA2026081276841Aoa · faultedIMMEDIATELY AFTER TAKEOFF GOT A STICK SHAKER WITH CONTINUOUS IGNITION WITH STALL LIGHT FLASHING. FOS SIDE AIRSPEED TAPE HAD RED BARBER POLE FROM BOTTOM HIGHER THAN NORMAL. ALSO GOT AUDIO WARBLER. NEVER GOT STICK PUSHER. DURING FLIGHT HIGH AIRSPEED BARBER PSDR DALA2026080404491Aoa · failedATO- APPROX 30KTS DUE TO STICK PUSHER FAIL AND DISARM SPOILERS ANNUNCIATION WITH ASSOCIATED MASTER CAUTION. REPLACED NR 2 AOA SENSOR. ALL OPS CHECK GOOD. (6787252) AIRCRAFT WAS GROUNDED.SDR VNAA2026072821502Aoa · faultedFLAP FAIL IN FLIGHT QRH C/W SPEED TAPE STAYED AT 230 KTS WITH FLAPS INDICATING AT 0. REMOVED AND REPLACED RH AOA VANE IAW AMM 27-35-05-000/400-801-A01. OPS CHECKED GOOD IAW AMM 27-35-05-710-801-A01. PERFORMED MDC TEST OF SFECUS, BOTH PASSED.SDR G1IA20260725114Computer · failedPUSHER/SHAKER MALFUNCTION. CAWS PUSHER ADVISORY, AUDIO AND SHAKER ACTIVATED UPON TAKEOFF WITH AOA INDICATING "SLOW DIAMOND." PUSHER DID NOT ACTIVATE. ALL PERFORMANCE AND PROFILE NORMAL. FAULT CONTINUED UNTIL LANDING. PILOT ATTEMPTED PUSHER TEST IN FLIGHT AND PSDR N6WA2026072004Computer · faultedSTALL FAIL CAUTION MESSAGE IN FLIGHT. R & R STALL PROTECTION COMPUTER IAW AMM 27-35-01. OPS CHECKED GOOD, NO CURRENT FAULTS AT THIS TIME.SDR AALA202606098221Aoa · inoperativeAIRCRAFT WAS GROUNDED: CAPTAINS AIRSPEED SPEED LIMIT FLAG INTERMITTENTLY WITH INTERMITTENT LOSS OF FLIGHT DIRECTOR PITCH INDICATION. DECESION MADE TO RETURN TO CVG, EMERGENCY DECLARED AND LANDED OVERWEIGHT WITHOUT INCIDENT.SDR HNAA2026052600433Aoa · abnormalSPS ADVANCED DURING TAKE-OFF ROLL AT 80KTS ON CA AIRSPEED INDICATOR, FO AIRSPEED INDICATOR SHOWED 60KTS. CHECK EICAS MESSAGE WOULD POP UP INTERMITTENTLY ON TAXI OUT. R & R #100 AOA VANE IRW AMM 27-36-01. OPS CHECK GOOD, ACFT OK FOR SERVICE.SDR FXTA20260519001Transducer · false indicationSTALL WARNING HORN GOES OFF INTERMITTENTLY AS HIGH AS 140 KTSSDR 2026FA0000426Stall Warning · false indicationAT 190 KNOTS ASKED FOR CLEAN WING AUTO PILOT ON. SHORTLY AFTER THAT SELECTION AND CLOSE TO 200 KNOTS INDICATED AIRSPEED THE STICK SHAKER WENT OFF ALONG WITH THE AURAL WARNING "STALL, STALL, STALL" WE LEVELED OFF AT AROUND 3700 FEET MSL AND CONFIRMED THE AUTOPISDR DALA2026052403140Aoa · damagedLIGHTENING STRIKE ON ANGLE OF ATTACK (3FP3) BTW FR23 TO FR24 AT STR26L FWD FUSELAGE. REPLACED ANGLE OF ATTACK (3FP3) BTW FR23 TO FR24 AT STR26L FWD FUSELAGE AS PER A320 FAM AMM 34-11-19-000-001-A AND AS PER A320FAM AMM 34-11-19-400-001-A. TEST ARE GOOD. (LP: SDR SIMA20260503001Disconnect Unit · failedAOA PITCH TRIM DISCONNECT. FELT SPRING AND HEARD SPRINGS POP FOLLOWED BY AOA LIMIT FAIL CAUTION MESSAGE.EMERGENCY DECLARED. LANDED NO ISSUES. RAR CONTROL COLUMN DISCONNECT DEVICE IAW AMM 27-11-01. OPS CHECK GOOD.SDR CALA2026050415941Aoa · failedL AOA PROBE EICAS MESSAGE RIGHT AFTER TAKEOFF DEBRIEFED FLT CREW UPON ARRIVAL. THEY NOTED THAT THE L AOA LIGHT AND EICAS MSG REMAINED ON FROM TAKEOFF UNTIL APPROACH WHEN BOTH THE LIGHT AND EICAS MSG BOTH WENT OUT. THEY WERE IN KNOWN ICING CONDITIONS WHICH WARSDR Q5QA20260421002Aoa · failedTHE PILOT REPORTED THAT AFTER DEPARTURE HE RECEIVED A SLOW SPEED INDICATION WITH AN ACCOMPANYING STICK SHAKER AND ORAL WARNING EVEN THOUGH HE WAS WELL ABOVE THE STALL SPEED FOR HIS CONFIGURATION, THE PILOT RETURNED THE AIRCRAFT TO HIS DEPARTURE POINT AND LANDESDR CALA2026040715157Computer · faultedAUTO SLAT FAIL INTERMITTENT IN FLIGHT, PERFORMED FIM 27-32, TASK 801. NR 2 SMYD FAULT 27-32005. REF FIM 27-32 TASK 812. NEED TO REPLACE NR 2 SMYD, NO TROUBLE FOUND FOR AUTO SLAT FAIL LIGHT ON. REMOVED AND REPLACED SMYD IAW AMM 27-32-42. FOUND IN NR 2 POS. SDR IPXA2026030497959Aoa · faultedATB, ON CLIMBOUT CAPT SIDE AIRSPEED WAS ABOVE CLEAN MAN BUT EICAS SHOWED AIRSPEED LOW F/O SIDE NORMAL. GOT STICK SHAKER WITH NORMAL AIRSPEED BOTH F/D VERTICAL GUIDANCE WENT AWAY. ONCE LEVELED OFF A/C WAS€¦. REMOVED AND REPLACED LEFT AOA SENSOR IAW AMM 34-12-0SDR CALA2026022314017Aoa · damagedLIGHTNING STRIKE ON CLIMB. AIR SPEED DISAGRE E . AOA DISAGREE. CONTIN OUS STICK SHAKER. PERFORMED PHASE 1 INSPECTION REF MM 05-51-19-210-804, FOUND DAMAGE ON NOSE RADOME, LEFT SIDE STATIC STRIP WITH AFT SECTION MISSING 3.5". ALSO FOUND EVIDENCE ON AOA AND ON SDR AALA202603066718Aoa · faultedAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS NOT DECLARED DUE TO: CAPTAINS PRIMARY FLIGHT DISPLAY (PFD) FLASHED INTERMITTENTLY SHORTLY AFTER TAKEOFF. BOTH AMBER SPEED AND ALTITUDE DISPLAYED ON CAPTAINS PFD. AIRCRAFT AIR INTERRUPTED BACK TO AND LANDED SAFELY AT DEN.SDR DXTA2026010806473Transmitter · faultyREPEAT WRITE-UP: NR 2 PFD DISPLAYED ERRATIC AOA INDICATIONS. ON TAKE-OFF AND INITIAL CLIMB OUT THE AOA WOULD DISPLAY RED AT 1.0 (FULL SCALE) AND THE LOW SPEED TAPE WOULD COME ALL THE WAY UP AND DISPLAY THE AIRSPEED RED. THIS ACTIVITY TAPERED OFF AND STOPPED SDR DALA2025122309337Aoa · faultedRTO- APPROX. 85 KNOTS DUE TO AIRSPEED SPLIT. PRESSURIZED CAPTAIN'S AND FIRST OFFICER'S PITOT SYSTEM. FOUND 1 KNOT DISAGREEMENT. REPLACED LEFT AND RIGHT AOA SENSORS. AIRSPEEDS AGREE. AIRCRAFT RETURNED TO SERVICE. (LP 7933092)SDR AALA202511106585Aoa · failedAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS NOT DECLARED DUE TO: SPEED LIMIT FLAG APPEARS INTERMITTENTLY ON CAPTAIN'S PFD. WHEN THE FLAG APPEARS THE MIN MANEUVERING AMBER BAR DISAPPEARS AS WELL AS THE VERTICAL PORTION OF THE CAPTAIN'S FLIGHT DIRECTOR, WHICH THEN DSDR 2025FA0000731Stall Warning · inaccurateSTALL WARNING SOUNDS AT TOO HIGH OF AIRSPEED. MAINTENANCE MANUAL PROVIDES NO PROCEDURES FOR ADJUSTMENT OF ELECTRICAL STALL WARNING SYSTEM. MULTIPLE ADJUSTMENTS HAVE BEEN MADE TO THE COMPONENT AND HAS NOT FUNCTIONED PROPERLY PER THE POH.SDR CALA2025101710233Aoa · faultedINT STICK SHAKER ON CA SIDE IN FLIGHT CREW REPORTS STALL WARNING OCCURRED AT 18000FT THROUGH 26000 FT. STICK SHAKER CAME ON INTERMITTENT 4 TIMES AT TEN SECOND INTERVALS. AIRSPEED WAS NORMAL, BUT DID NOTE HIGH SPEED AND LOW SPEED AWARENESS INDICATIONS ON TAPE. SDR KY7A2025091600038Stick Pusher · malfunctionedSTICK PUSHER MOMENTARILY ENGAGED ON FINAL AT ABOUT 1,200 FT. AGL. FLAPS WERE FULL AND LANDING GEAR DOWN ON 09/15/2025 08:06PMSDR CALA2025071706674Aoa · faultedSPD LIM FLAG CAPT PFD NO VERTICAL FD GUIDANCE INTMT STICK SHAKER CA SIDE. REMOVED AND REPLACED CAPT AOA SENSOR REF AMM 34-21-05 OPS CHECK GOOD.SDR JJBA20250728096Cable · out of limitsSTICK PUSHER CABLE CHAFED OUT OF LIMIT. STICK PUSHER ACTUATOR REMOVED. STICK PUSHER ACTUATOR INSTALLED.SDR CALA2025070206155Computer · faultedYAW DAMPENER SWITCH TRIPPED OFF IN FLIGHT ABLE 2 RESET PILOTS STATED YAW DAMPENER SWITCH TRIPPED OFF ONCE DURING THEIR FLIGHT AND WAS ABLE TO RESET SUCCESSFULLY, PILOTS SAID IT TRIPPED ONCE ON THE CREW PRIOR TO THEM AS WELL AND DIDNT FEEL COMFORTABLE FLYING INSDR DXTA2025050703399Stick Shaker · faultedSTALL CHECK: DURING PREFLIGHT SPS SYSTEM CHECK, WITH LEFT AND RIGHT TEST SWITCHES IN TEST, STICK SHAKER ACTIVATED BUT WE HEARD, AND CO-PILOT FELT, A TAPPING/BANGING UNDER HIS RIGHT FOOT. ADDITIONALLY, THE PUSHER FAILED TO ACTIVATE. WE TESTED A SECOND TIME SDR CALA2025042504219Aoa · faultedGRAPHIC DISPLAY OF VLS ON ND IS 5 KNOTS HIGHER THAN FMGC. ND SHO WS VLS SAME AS APP SPEED CREW STATED DISCREPANCY WAS VISIBLE IN BOTH PFDS. FOLLOWED TSM 22-66-00-810-889-A LAST LEG CLASS 3 FAULTS DISPLAYS AOA SENSOR1 ( 3FP1 )", ADR1 TEST SHOWS MSG AOA SENSORSDR CALA2025040903665Aoa · faultedSPD LIM ON CA PFD W/ INTRMTNT VERT FD CMD BAR INTRMTNT STICK SHA KER AND SPEED TAPES REF L/P 4414719 FOR PART REPLACEMENT REMOVED AND REPLACED CAP AOA SENSOR REF AMM 34-21-05. OPS CHECK GOOD. ALL TESTS PASSED.ROTABLE PARTS CHG:TT # 1915849 SN OFF 2217 PN OFF 2SDR IPXA2025040275223Stick Shaker · inoperative**ATB** CAPT/S STICK SHAKER, PLI SHOWING STALL FO STICK SHAKER PLI NORMAL. REMOVED AND REPLACED #1 AOA VANE PER AMM 27-35-02. OPS CHECK NORMAL.SDR SWIA202503210017Aoa · failedAOA LIMIT FAIL, AT FAIL, AP FAIL, AT 34000 FT, STICKER AND LOW SPEED QUE SHOOTING UP. AIRSPEED WAS NOT SLOW, INDICATING PROPERLY. (FLIGHT 5916 - FILED CLOSED) MAR 19, 2025 STATION: LAS--SEE EAML 1561087 & 1561088 & 1561111 & 1561118. SEE EAML 1561878 FOSDR 4DPA2025022800001Computer · failedCREW REPORTED SPS ADV EICAS MESSAGE ELECTED TO RETURN TO DAL. CORR ACTION- MX REPLACED STALL PROTECTION COMPUTER ALL OPS CHECKS C/W GOOD.SDR 6CBA2025022025001Aoa · faultedTHE FLIGHT CREW WERE DEPARTING CYTZ FOR KBED. THE CREW REPORTED "STICK SHAKER ACTIVATED IMMEDIATELY AFTER TAKEOFF ALONG WITH AURAL "STALL" CALLOUT. CREW RETURNED TO DEPARTURE AIRPORT AND SHAKER STAYED ON UNTIL TOUCHDOWN." THE CREW DECLARED AN EMERGENCY AND DIVSDR CALA2025021402328Aoa · faultedAFTER TAKEOFF CA FLT DIRECTOR HAD SPD LIM AND THEN GOT STICK SHA KER AT FL250 T/S PER FIM 27-32 TASK 831, SMYD 1 EXISTING FAULT SHOWS " AOA SIG ERROR" MSG: 27-31004. REMOVED AND REPLACED CAPT AOA SENSOR REF AMM 34-21-05. OPS CHECK GOOD PARTS USED: 29-3412-9-0SDR DALA2025012800661Aoa · faultedSHIP 3410 - ATB - DUE TO CAPTAINS AOA SENSOR FAULT AND AIRCRAFT FLIGHT PROTECTION DOWNGRADING TO ALTN LAW. CORRECTIVE ACTION: REPLACED CAPTAINS AOA. OK FOR SERVICE. (6949080)SDR CALA2025010601787Aoa · faultedSPD LIM FLAG INTERMITTENT ON CA PFD PREFORMED A SELF TEST ON SYMD 1; LRU PASSED. INTERROGATED LRU FOR HISTORY & EXISTED FAULTS, IT SHOWED AOA SIG ERROR, FMC INACTIVE. SEE PIC FOR ADDTIONAL INFO. REF FIM 27-32 TASK 801; 27-32 TASK 831. ACP SMYD 1 BITE CHK SHOSDR CALA2024122001586Aoa · brokenINTERMIT SPD LIM IND ON CA AIRSPEED INTMT SLOW SPD TAPE INTM CA STICK SHAKERFLAGGED AS SDR CAPT STCK SHAKER AND SPD LIM FLAG STARTED ON CLIMB OUT AND CAPT SPEED TAPE FLUXING ABOUT 10000 FT WOULD GO IN AND OUT REMAINDER OF FLIGHT RETURN TO FIELD. AIR SPEED IND SDR DALA2024121111654Aoa · faultedSHIP 1815 -DIV- TO CDG. LOSS OF A/T, LNAV AND VNAV. V/S AND HDG SEL FUNCTIONAL. CORRECTIVE ACTION: C/W OVERWEIGHT LANDING INSP. REPLACED AOA SENSOR. PERFORMED TAT TEST. OK FOR SERVICE. (5789234)SDR FDEA202412091788Aoa · failedPASSING FL 200 THE ALT DISAGREE EICAS MESSAGE ALONG WITH THE AURAL ALERT ACTIVATED MOMENTARILY AND THE AGAIN PASSING FL 220. FOLLOWED QRH. EICAS MESSAGE EXTINGUISHED. THE CAPTAINS ALTIMETER WAS 200 FEET DIFFERENT FROM THE F/O AND THE STANDBY ALTIMETERS. SDR DALA2024120311397Transducer · shortedSHIP 9550 -ATB/DE- THE FLIGHT CREW RETURNED THE AIRCRAFT TO CAE AND DECLARED AN EMERGENCY DUE TO "STICK PUSHER FAIL" MESSAGE WITH AN ASSOCIATED STALL WARNING LIGHT. CORRECTIVE ACTION: MAINTENANCE FOUND THAT THE CAPTAINS CONTROL WHEEL FORCE TRANSDUCER (T2-6080)SDR HALA20241025060Stick Shaker · warning messageABORTED TO @ 30-40 KTS PSEU AND STICK PUSHER FAIL MSG. PERFORMED SLAT DISAGREE BITE PER FIM 27-80 TASK 803. COULD NOT DUPLICATE FAULT. OK TO CONTINUESDR FDEA202409051239Aoa · failedON ARRIVAL, FOUND WHEN STANDBY POWER SWITCH IS PLACED TO BATTERY, LOST ALTITUDE, SPEED & VERTICAL SPEED INFO & SCALE ON CAPT PFD & TAS ON CAPT ND. 1ST OFFICER WORKING. WARNING ELEX & GND PROX SYS STATUS MESSAGE FAULT PRESENT. INTERMITENT. T-SHOOTING FOUND SWSDR CALA2024090300531Stick Shaker · malfunctionedMOMENTARY /ONE SECOND/ ACTIVATION OF CAPTS STIC K SHAKER AFTER L IFTOFF. APPROX 75-100 AGL ON INVESTIGATION FOUND DRIVER CARD 10 FAULTING ON PSEU. FAULT ERASED, PSEU TEST CARRIED OUT IAW AMM 33-09-04-704-013, NOW NO FAULTS EXIST. L AND R STALL WARNING TEST CARSDR CALA2025091008753Aoa · faultyEG HAS BEEN NOTIFIED BY THE FAA THAT THIS AIRCAFT IS REPORTING HIGHER THAN EXPECTED RVSM ALTITUDES EG IS REQUESTING TO ACCOMPLIS H (ASE) ALTIMETRY SYSTEM ERROR CHK. 1. PERFORM AIRBUS SRM 51-11 -00 SECTION 4,A AND SRM 53-00-11 SECTION 4.B SKIN WAVINESS. 2. PERFSDR HNAA2024081900703Warning System · faultedSTALL PRTOECTION TEST PERFORMED DURING PREFLIGHT WITH NO ISSUES. PRIOR TO 60KNOTTS ON T/O SPS FAIL EICAS MESSAGE APPEARED. NOTED STRONG CROSSWINDS AND NO CMC MESSAGES. PERFROMED TEST AGAIN WITH NO ISSUESSDR 2024F00189Aoa · failedQRF CBB/TJA LEG DUE TO SPPED LIMIT YELLOW FLAG ON PFD PILOT SIDE, STICK SHAKER DURING FLIGHT. CORRECTIVE ACTION: HAS BEEN PERFORMED FIM PROCEDURES 27-32 TASK 809 AND REPLACED LEFT AOA VANE IAW AMM 34-21-05-000-801 SYSTEM OK.SDR CALA2024080600375Aoa · faultyIAS DISAGREE MESSAGE SHOWS ON AIRPSEED DISPLAY CAPTAIN'S IAS DISAGREE CAME ON AT TOPOF DESCENTFL370 CHECKLIST RAN FO SIDE RELIABLE CAPT SIDE BAD. REPLACED CAPT AOA SENSOR PER MM 34-21-05-401, OPS CK OK PER MM 34-21-05-501 AND REPLACED CAPT PITOT ADM PER MM SDR QMLA2024080220095Aoa · faultedIMMEDIATELY AFTER TAKEOFF THE STICK SHAKER ACTIVATED CONTINUOUSLY WITH THE PUSHER CAWS LIGHT ILLUMINATED. RETURNED TO AIRPORT FOR LANDING.SDR HNAA2024060700488Computer · faultedSPS 2 INOP DISPLAYED IN FLT FACT 06JUN24 20:04 PHL REMOVED AND REPLACED STALL PROTECT COMPUTER IAW AMM 27-36-02. PREFORMED OPS CHECK IAW AMM 27-36-00. OPS CHECK GOOD. A/C OK FOR SERVICE.
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