JASC 2210
Service difficulty reports · 4,014
Reports filed under 2210 · Autopilot 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 = '2210' 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 = '2210' 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 CALA2026102120499Autopilot Sys · malfunctionedBOTH CAPTAIN`S & FIRST OFFICER`S AUTOPILOT P/RST AMBER LIGHT ILLUMINATED INTERMITTENTLY THROUGHOUT THE FLIGHT. AUTOPILOT STAYED CONNECTED. ALSO APPEARED WITH THE AUTOPILOT DISCONNECTED. PERFORMED AUTOPILOT TEST, FAULT STAB POS SEN-2. COMPLIED WITH MEL 2201BSDR AALA202610192500Autopilot Sys · inoperativeAIRCRAFT WAS GROUNDED: -- DECISION WAS MADE TO RETURN TO MIA - EMERGENCY DECLARED; AIRCRAFT LANDED WITHOUT INCIDENT -- FEEL DIFF LIGHT ILLUMINATED AFTER TAKEOFF AND THEN EXTINGUISHED. BOTH AUTOPILOTS WOULD NOT ENGAGE. FOUND A DUAL CHANNEL AUTO STAB TRIM CUT SDR QR9R2026100700001Actuator · failedCYCLIC TRIM FAILED MULTIPLE TIMES WHILE AT A HOVER. REMOVED AND REPLACED DUPLEX TRIM ACTUATOR IAW AMM 22-10-00, 4-8; MOC SUCCESSFULLY COMPLETED.SDR FDEA202609281442Solenoid Valve · malfunctionedDURING TAKEOFF, PF NOTICED AN UNUSUAL AMOUNT OF FORCE TO ROTATE ACFT. DURING CLIMB, HAND FLYING, APPROX 3X AMOUNT OF USUAL FORCE REQUIRED TO MOVE ACFT IN PITCH AXIS. WHEN AP1 IN USE, AP FUNCTIONED NORMAL. ATTEMPT MADE TO SWITCH TO AP2, AP2 WAS NOT AVAIL. SDR SCNA20260928411Director · malfunctionedBOTH FLIGHT DIRECTORS DISAPPEARED ON SHORT FINAL WHILE FLYING AN ILS. PERFORMED DFCS BITE REF FIM 22-11 TASK 801. FOUND FAULT FOR FLIGHT DIRECTOR. PERFORMED DFCS (DIGITAL FLIGHT CONTROL SYSTEM) FLIGHT DIRECTOR TEST. TEST FAILED. REMOVED AND REPLACED MODE CCONSDR QR9R2026091100001Actuator · stickingON LIFTOFF, ACTUATOR CAUTION CAME ON. WHEN TRYING TO BUILD BACK UP, THE YAW CAUTION ON THE PFD WAS ILLUMINATED, HOWEVER, AP1/AP2 TURNED ON AS THEY SHOULD. TROUBLESHOOTING DETECTED THE YAW SEMA TO BE STICKING AND RACHETY CAUSING ACTUATOR CAUTION. REMOVED AND RESDR AJXA2026090300046Yaw Damper · faultedYAW DAMPER OFF, MACH TRIM OFF AT 50 KNOTS / FGC ADC MIS-COMPARE AUTOPILOT DISENGAGEDSDR QR9R2026081300002Actuator · failedYAW ACTUATOR CAUTION ILLUMINATED IN FLIGHT. MALFUNCTION WAS INDICATED ON THE CAD ONLY. LOWER YAW TRIM LIGHT DID NOT ILLUMINATE. DURING TROUBLESHOOTING, FOUND YAW SEMA BAD, ALSO HAD CODE YAWEMA INVAL. REMOVED AND REPLACED SEMA ACTUATOR IAW AMM 67-20-00, 4-14.SDR AALA202608081266Control Panel · faultyAIRCRAFT WAS GROUNDED: "CRUISE FLAPS DISAGREE" STATUS MESSAGE WITH MIC# 9621843 INCIDENT. INTERROGATED CMCF AND FOUND EXISTING FAULT OF THE MCP, MAINTENANCE MESSAGE# 22-14861. EMERGENCY DECLARED AS A PRECAUTION AIRCRAFT LAMNDED WITHOUT INCIDENT. MAINTENANCE ACSDR AALA202607274188Adiru · failedAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED INTO BDA DUE TO THE FLIGHT CREW REPORTING DURING DESCENT THEY LOST AUTOPILOT, AUTO THROTTLE AND CAPTAINS INSTRUMENT PANEL (NOTE: ADIRU #3 WAS ON DEFERRAL DUE TO IT BEING INOPERATIVE). THE AIRCRAFT LANDED SAFELY SDR YENA2026072200608Button · missingFLT 1548, RDU-JFK. (ETOPS) HEADING TRACK/VERTICAL SPEED BUTTON MISSING ( AUTO FLIGHT CONTROL PANEL HDG-V/S TRK-FPA CHANGE OVER PB ) OPENSDR KCSA2026071540Circuit Breaker · trippedAC DIST P6 BREAKER POP INFLIGHT W/ ASSOCIATED EICAS MESSAGES. PERFORMED INSPECTION OF AC DIST P6 BREAKER AND ASSOCIATED WIRING, NO DEFECTS FOUND IAW B747-400 AMM 20-60-03. PERFORMED AUTOLAND UNIQUE GROUND TEST IAW AMM 22-10-00. ALL CHECKS SATISFACTORY, NO DESDR AALA202607172820Proximity Sensor · out of adjustAIRCRAFT WAS GROUNDED: CMD A/B AUTO PILOT INOPERATIVE. MULTIPLE ATTEMPTS MADE TO REENGAGE FAILED. DECESION MADE TO RETURN TO PHX. AIRCRAFT LANDED WITHOUT INCIDENT. REF MIC 0144604, MAINTENANCE ADJUSTED AND TESTED ELEVATOR POSITION SENSOR IAW AMM 22-11-30-820-8SDR AALA202607147233Control Unit · defectiveAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO FLL DUE TO THE FLIGHT CREW REPORTING AN AUTO FLT AP OFF AND AUTO FLT A/THR OFF ECAM MESSAGE AROUND 600FT NAV WENT TO HDG AROUND 400. THE AIRCRAFT LANDED SAFELY AT FLL WITHOUT FURTHERSDR 2026F00142Autopilot Sys · faultedDEPARTED KSGR HEADING TO KACK, APPROX 2 HRS 45 MINS INTO FLT, CAPTAIN REPORTED MULTIPLE EQUIPMENT ISSUES/FAILURES. NR 1 & 2 AHRS HEADING FLAGGED, AHRS 1 ADC INPUT, AUTO PILOT, RUDDER BOOST & MACH TRIM LIGHT CAME ON. NO CIRCUIT BREAKERS POPPED WITH ALL OF THESDR DALA2026062903834Control Panel · odorPASSING THRU APPROX 8000' MSL ON ARRIVAL QUICK SCENT OF BURNING PLASTIC (NOT OVERWHELMING) IN COCKPIT DISSIPATED QUICKLY. AT SAME TIME L AUTOPILOT EICAS AND DISENGAGED. AUTOPILOT REENGAGED UPON COMMAND AND NO FURTHER ISSUES. AS A PRECAUTION, REMOVED & REPLACESDR QR9R2026062400001Actuator · failedFAILED SAS/AP CUT TEST DURING START RUN-UP. BACKUP SAS CAUTION WOULD SHOW BUT NOT AS SAS CAUTION. REMOVED AND REPLACED YAW SEMA ACTUATOR IAW AMM 67-20-00, 4-14.SDR AALA202606223316Fcu · warning messageAIRCRAFT WAS NOT GROUNDED: AN EMERGENCY WAS DECLARED INTO DEN DUE TO REPORTING A FCU 1 FAILURE DURING ARRIVAL SEGMENT ON DESCENT. THE AIRCRAFT LANDED SAFELY AT DEN AND TAXIED TO THE GATE UNDER ITS OWN POWER. MAINTENANCE RESET FCU COMPUTER, PERFORMED ALL REQUISDR AALA202606160597Adiru · fault messageAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO DFW DUE TO THE FLIGHT CREW REPORTING THAT SHORTLY AFTER TAKEOFF THEY GOT ECAMS FOR NAV FM GPS POSITION DISAGREE, IRFAULT, AUTOPILOT 1 AND 2 FAIL, AND AUTO THRUST INOPERATIVE. THE FLISDR DXTA2026061108379Actuator · defectiveON DESCENT RECEIVED AMBER CAS AP TRIM STAB FAIL. RAND QRH. ONCE AP DISCONNECTED HAD PUSHING FORCE (NOSE DOWN) ON CONTROLS. MANUAL TRIM WORKED. LANDED. AP SYSTEM MEL APPLIED ALONG WITH MX REQUIREMENTS. YD MEL 22-10-05 WAS REFERENCED AND IS CONSIDERED INOP. REPSDR DXTA2026060808336Trim System · inoperativeON DEPARTURE WE RECEIVED AP FAIL A CAS MESSAGE. REENGAGED AP AND RECEIVED AP FAIL B CAS MESSAGE ALSO. WE FOUND THE PRIMARY STAB TRIM TO BE INOPERATIVE WITH NO PRIMARY STAB TRIM FAIL CAS MESSAGE. WE USED SECONDARY TRIM AND LANDED WITHOUT ISSUE. REMOVED ELEVATOSDR AALA202606025123Control Panel · inoperativeAIRCRAFT WAS GROUNDED: PASSING 1200FT ON TAKEOFF ALT WINDOW WENT ALL DASHES A/P AT TAKEOFF UNABLE TO RESET. DECESION MADE TO RETURN TO PHL. EMERGENCY DECLARED AND AIRCRAFT LANDED OVERWEIGHT WITHOUT INCIDENT. MAINTENANCE REPLACED MODE CONTROL PANEL PER AMM 22-SDR 2026FA0000315Computer · failedACRFT DEPARTED KVNY HEADING TO KDAL. APPROXIMATELY ONE HOUR INTO THE FLIGHT THE AUTOPILOT DISENGAGED AND WOULD NOT RE ENGAGE. THE CAPTAIN DECIDED TO DIVERT INTO KELP, HOME BASE MAINTENANCE FACILITY. THE AIRCRAFT LANDED SAFELY IN ELP. ATI MAINTENANCE WAS ABLE TSDR AALA202604215384Control Panel · failedAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: DURING INITIAL CLIMB OUT WHEN GIVEN A HIGHER ALTITUDE, MCP ALTITUDE WINDOW STOPPED AT 4100 AND WOULD NOT ALLOW ANY FURTHER ADJUSTMENTS. AIRCRAFT AIR INTERRUPTED BACK TO AND LANDED SAFELY AT IAH. REMOVEDSDR 2026FA0000272Indication Sys · malfunctionedON 4/10/26, N975LV CYO975 WAS EXPERIENCING RNAV ISSUES. THE MAINTENANCE FACILITY IN KFXE REPORTED THE FLIGHT CONTROL COMPUTERS WERE CAUSING THE RNAV ISSUES. BOTH FCCS WERE REPLACED AND AN AUTO PILOT FUNCTIONAL CHECK WAS COMPLETED WITH NO ISSUES REPORTED - ALL SDR 2026FA0000254Flight Dir · defectiveFLIGHT GUIDANCE PANEL ON GOING SAFETY OF FLIGHT ISSUE CONCERNING INADEQUATE DESIGN/DURABILITY OF CERTAIN COMPONENTS. FLIGHT GUIDANCE PANEL(FGP) EQUIPPED AIRCRAFT.OUR AIRCRAFT. OUR ORIGINAL FGP, ELECTRONIC ROTARY HDG,/SPEED/ALT. PRESELECT SWITCHES STARTED HAVISDR CALA2026031314550Switch · failedSTAB OUT OF TRIM CAUTION IN FLIGHT PERFORMED FIM 22-11 TASK D72. MAINTENANCE MESSAGE 22-11830 SHOWS. REF FIM 22-11 TASK C17 FOR MESSAGE 22-11830, PERFORMED LIBRARY TESTS 60.32 AND 60.35. MAINTENANCE MESSAGE 22-11163 SHOWS FOR CHANNEL B ON BOTH TESTS. DURING CHSDR CALA2026022514062Adiru · faultedIN CLIMB AT FL290, AUTOPILOT DISENGAGED. NO MODES WOULD RE ENGAGE ACCOMPLISHED MCDP FCC TEST, TEST 30 & TEST 40. ALL TEST PASS. MCDP FLT FAULT WITH ADIRU LT. REPLACED THE LT AIR DATA INERTIAL REFERENCE UNIT (ADIRU) IAW AMM 34-26-01/401. PERFORMED MCDP TEST 3SDR AALA202602119700Fcu · inoperativeAIRCRAFT WAS GROUNDED: FO BARO REF SET KNOB REVERTS TO STANDARD REGARDLESS OF PUSH/PULL UNABLE TO SET BARO ON FO SIDE. DECESION MADE TO RETURN TO DFW, NO EMERGENCY AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED FCU IAW AMM 22-81-12.SDR UIEA2026020700044Control Panel · faultedMCP ALTITUDE SELECTOR SELECTS ERRONEOUS ALTITUDES PLUS/MINUS 3000 FEET WHEN TURNING. REMOVED AND REPLACED MCP IAW AMM 22-11-02. PERFORMED MCDP GROUND TEST, 30-40 TEST PASS, NO FAULTS NOTED.SDR MISR2026020306754Module · defectiveON CLIMB OUT FULL NOSE DOWN TRIM REQUIRED. AUTOPILOT KICKED OFF. DECISION MADE TO SLOW THE AIRCRAFT BELOW 200 KTS TO MAINTAIN CONTROL AND LESSEN CONTROL INPUTS. LANDED AIRCRAFT UNDER MAX WEIGHT. CORRECTIVE ACTION: DURING ARES DOWNLOAD ANALYSTS DISCOVERED THESDR 2026FA0000063Servo · weakON 1/23/2026 N420KV CYO420 WAS DEPARTING KORL AND WHILE THE AIRCRAFT WAS CLIMBING WITH THE AUTOPILOT ENGAGED, THE CAPTAIN REPORTED THE PITCH CONTROL WAS UNSTABLE. THE CONTROL COLUMN WAS MOVING BACK AND FORTH AND WOULD STOP WHEN AUTOPILOT WAS DISENGAGED. THE TRSDR CALA2026012013112Indicator · faultedON DEPARTURE SPEED TRIM FAIL LIGHT ILLUMINATED TWO TIMES. COULD NOT ENGAGE A/P CMD A OR B. DEBRIEFED CREW, CREW FOUND THE AUTOPILOT STAB TRIM SWITCH IN THE CUTOFF POSITION. THEY STATED THEY MUST OF MISSED IT ON THEIR PREFLIGHT CHECK. BUT THE SPEED TRIM INOP CASDR SCNA20260116029Flight Dir · malfunctionedDURING SHORT FLIGHT WITH ELECTRICAL FUMES AUTOPILOT A WOULD NOT STAY EMGAGED LONGER THAT 2 SECONDS. FLIGHT DIRECTOR WOULD NOT FOLLOW ALT COMMANDS. PERFORMED FIM 22-11 TASK 801 NO DEFECTS NOTED. PERFORMED LAND VERIFY IAW AMM 22-11-00-700-801 NO DEFECTS NOTED OSDR AALA202601085803Computer · faultyAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: CAPTAIN SPEED TAPE AND ALTITUDE TAPE AND VVI BLANKED INFLIGHT WITH ALTITUDE AND SPEED ANNUNCIATED ALSO DISPLAY SOURCE 1 ILLUMINATED INFLIGHT. AIRCRAFT DIVERTED TO AND LANDED SAFELY AT ORD. REMOVED AND RESDR AALA202601089924Computer · faultyAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: CAPTAIN SPEED TAPE AND ALTITUDE TAPE AND VVI BLANKED INFLIGHT WITH ALTITUDE AND SPEED ANNUNCIATED ALSO DISPLAY SOURCE 1 ILLUMINATED INFLIGHT. AIRCRAFT DIVERTED TO AND LANDED SAFELY AT ORD. REMOVED AND RESDR DXTA2026010806462Autopilot Sys · faultyCRUISING AT FL430, AUTOPILOT KICKED OFF AND 4 OR 5 MESSAGES FLASHED WHICH WE WERE NOT ABLE TO COMMIT TO MEMORY. THE ONLY MESSAGE THAT REMAINED WAS SWPS FAULT. CHECKLIST WAS ACCOMPLISHEDSDR 2026FA0000634Servo · failedDURING DESCENT FROM BIG BEAR, THE GARMIN AUTOPILOT ABRUPTLY DISCONNECTED FOLLOWING FAILURE OF THE GSA 28 PITCH SERVO. IMMEDIATELY PRIOR TO THE FAILURE, I OBSERVED A MOMENTARY PITCH-TRIM-DOWN INDICATION. THE AIRCRAFT USES MANUAL PITCH TRIM. UPON SERVO/AUTOPILOTSDR 62MA2025120800797Autopilot Sys · false activationAFTER TAKEOFF MASTER WARNING COME ON, PRIMARY TRIM FAILED. NOTED FLIGHT DIRECTOR WENT DOWN (INDICATOR ERRATIC). ACCOMPLISHED RE RACK OF THE AUTO PILOT COMPUTERS OPS CHECK SUCCESSFUL AFTER THE MX ACTION PER. AMM 22-10-02SDR YENA2025120901182Fcu · failedFLT 2724, LAX-JFK. (ETOPS) ND MAP RANGE ONLY WORKS ON 20 AND 80, EFIS CONTROL PANEL ND RANGE SELECT. REMOVED AND REPLACED FLIGHT CONTROL UNT IAW AMM 22-81-12. OPS CHK GOOD. MX-4 UPDATED. PLACARD REMOVED. MDDR CLEARED.SDR R61A2025120400522Ace · failedAP FAIL IN FLIGHT ON APPROACH. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. PERFORMED OPS CHECK OF AUTOPILOT. PITCH TRIM FAIL IN FLIGHT ON APPROACH. DECLARED EMERGENCY. LANDED WITHOUT INCIDENT. REMOVED AND REPLACED HS-ACE.SDR QXEA2025111799344Autopilot Sys · faultedAUTOPILOT FAILED ON SHORT FINAL WITH AUTOLAND SETUP ON APPROACH. RESULTING IN MISSED APPROACH. LANDING UNEVENTFUL. REMOVED FROM SERVICE. NO FAULTS ON EICAS. INTEROGATED CMC FOUND FAULT CODE 27030348FCS IN HISTORY VIEW. PERFORMED FIM MCN E270027 COMPLETED THROUSDR AALA202511129711Control Unit · failedAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: DURING TAKEOFF ROLL, FIRST OFFICER LOST PITCH AND ROLL GUIDANCE. THEN ON CLIMB OUT, COULD NOT SELECT DIRECT TO A POINT IN LNAV, AND COULD NOT ENGAGE HEADING SELECT. ALSO, UNABLE TO SELECT AUTOPILOT-B ANDSDR QR9R2025101700002Actuator · failedFAILED AUTOPILOT TEST DURING START RUN-UP. REMOVED AND REPLACED PITCH TRIM ACTUATOR IAW AMM 67-14-00, 4-1.SDR CALA2025101510132Autopilot Sys · faultedSTABILIZER OUT OF TRIM LIGHT LIGHT. ON DEBREIF PILOT ON AIR RETURN. AUTOPILOT A, CAUSED OUT OF TRIM & COLLUM BUMP WHEN ENGAGED. PERFORMED TEST & FOUND ELEV SENSOR SUGGESTED REPLACEMENT. AUTOPILOT B IS OPS. PLACED AUTOPILOT A ON MEL IAW 2201A. INSTALLED SDR CALA2025101309974Trim System · no discrepancySPEED TRIM FAILED VERIFIED DISCREPANCY CAPTAIN REPORTED SPEED/TRIM CUTOUT SWITCH WAS IN CUTOUT POSITION. PLACED SPEED/TRIM SW IN NORMAL. PER FIM 22-11 TASK D73 SPEED TRIM FAIL LIGHT ON, PERFORMED THE SPEED/STAB TRIM TEST 60.32, TEST PASSED, NO FAULTS.SDR QR9R2025100200004Actuator · failedPITCH ACTUATOR FAIL ON AUTOPILOT TEST. DURING TROUBLESHOOTING, FOUND THE P2 SEMA HAD A VALID SIGNAL IN BUT NO VALID SIGNAL OUT. REMOVED AND REPLACED SEMA ACTUATOR IAW AMM 67-10-00, 4-8.SDR CALA2025092409220Computer · faultyNEITHER AUTOPILOT WOULD ENGUAGE 15000 FEET DEBRIEFED CREW. PILOT STATED AT 15K FEET NEITHER AUTOPILOT WOULD ENGAGE. AFTER PRESSING RECALL GOT SPEED TRIM LIGHT. RAN DFCS BITE CHECK AND GOT THE FOLLOWING FCC A AND FCC B FLIGHT FAULTS FOR LEG 1. SEE PICS MORE PICSDR QXEA2025091500304Autoland Sys · malfunctionedFLIGHT- 2434. IN CRUISE "AP FAILED" EICAS MSG "AUTOLAND 1 NOT AVAIL" AND PITCH CONTROL DISC". RETURNED TO FIELD AND ACCOMPLISHED UNEVENTFUL LANDING. REMOVED FROM SERVICE. NO TRAX HISTORY. CMC SHOWS FAULT CODE 27030348FCS FOR PITCH CONTROL DISC EICAS MSG.C/W FISDR QR9R2025091000001Actuator · failedWHILE ATTEMPTING TO PICK UP TO HOVER, PITCH ACTUATOR CAUTION APPEARED. ATTEMPTED TWICE, SAME CAUTION APPEARED. A TEST FLIGHT EVAL REVEALED WHEN PICKING A/C UP TO A HOVER, ACTUATOR LIGHT ILLUMINATED ON CAD WITH P ON PFD. REMOVED AND REPLACED SEMA ACTUATOR IAW A
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