JASC 2210
Service difficulty reports · 4,016
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 ASAA2014120609882Autoland Sys · unknownPERFORMED HGS/AUTOLAND ACFT PERFORMED NORMALLY ON APPROACH AND LANDING EXEPT LANDED 45 FT LT OF CENTERLINE HGS PERFORMED NORMALLY. ACFT GROUNDED. TROUBLESHOT IAW FIM 22-11, TASK 825. LAND VERIFY TEST PERFORMED IAW AMM TASK 22-11-00-700-801. TEST PASSED. NOSDR SIMA20141206001Switch · malfunctionedON ILS APPROACH AP ON AT LOC CAPTURE AUTO PILOT COMMANDED & UNCOMMANDED TO & GA. FD STILL COMMANDED TO & GA WITH AP DISCONNECTED. ON CLIMB OUT WHEN SPEED MODE SELECTED & UNCOMMANDED FD TO ROL & GA. TRANSFERRED TO NRWC 627-DFW-02156. R & R RT GA SWITCH. OPSDR CA141208003Control Panel · failed(CAN) DUAL YAW DAMPER FAILURE. DIFFICULTY CONTROLLING THE A/C. EMERGENCY DECLARED. REPLACED RELAY K58, K59. REPLACED YAW DAMPER PANEL , REPLACED RELAYS IAW AMM 22-22-07, PANEL IAW AMM 22-22-04 OK FOR SERVICESDR ASAA2014120109839Control Panel · failedAUTOPILOT "A" WILL NOT STAY ENGAGED AT CRUISE ALTITUDE. ACFT GROUNDED. DFCS FLT FAULT REVIEW SHOWS FLTS W/ NUMEROUS MCP DATA INV 22-11607 FAULT W/MCP SUSPECTED LRU. ALSO REF FIM 22-11, TASK 817. R & R MCP REF MM 22-11-34. OPS NORMAL REF SAME.SDR UIEA2014120200624Autopilot Sys · malfunctionedDESCENDING ACFT ABRUPTLY PITCHED UP & STARTED TO CLIMB ON AUTOPILOT. DISCONNECT AUTOPILOT & RE-ENGAGED LATER & OPERATIONS WERE NORMAL. VERIFIED NO CMC ACTIVE FAULTS. PERFORMED AUTO LAND UNIQUE TEST & PASSED IAW AMM 27-00-00.SDR SIMA20141128002Actuator · failedUNCOMMANDED RUDDER MOVEMENTS IN FLIGHT BOTH TO THE LT & RT WITH & WITHOUT YAW DAMPER ENGAGED. TRANSFERRED TO NRWC 524-ABI-01793. R & R NR 1 YAW DAMPER ACTUATOR IAW AMM 22-22-01. SEE NRWC 524-ABI-01793 FOR DETAILS. ACTUATOR, LIN, YAW DAMP PN 822-1308-320 & SDR SIMA20141125010Circuit Card · failedUPON DEPARTURE ALT SPD & HDG SELECTORS BECAME INOPERATIVE. THE SELECTORS REMAINED INOPERATIVE UNTIL SHORT FINAL. DEFERRED IAW MEL 33-02. R & R NR 1 IC 600 IAW AMM 31-42-01. OPERATIONS CHECKED GOOD IAW 31-42-00 & 22-11-00 MEL 22-2 IS RESTORED.SDR O84A2015F00008Actuator · faultyAS AIRCRAFT WAS PICKED UP INTO A HOVER CAD WARNING ACTUATOR APPEARED WITH THE ASSOCIATED Y ON THE PILOTS PRIMARY FLIGHT DISPLAY. AIRCRAFT WAS LANDED, SYSTEM WAS RESET AND PICKED UP INTO A HOVER WITH THE SAME RESULT. AIRCRAFT LANDED, FLIGHT DISCONTINUED AND MSDR VNAA2014112500011Circuit Card · failedCREW REPORTED YAW DAMPER-1 FAIL FD & AUTO PILOT FAIL IN FLT. INTERROGATED MDC AND FCC DIAGNOSTIC, FOUND FCC 1 FAILING INTERMITTENTLY, R & R NR 1 FCC CARD IAW AMM 22-12-14-00-400-801, OPS CHECK GOOD. ALSO, R & R YAW DAMPER NR 1 PUSH BUTTON IAW CMM 22-22-04 FOSDR ASAA2014111709690Autopilot Sys · malfunctionedAUTOPILOT B RANDOMLY DISENGAGES IN FLIGHT. ACFT GROUNDED.SDR ASAA2014110909626Light · inoperativeMCP LIGHTS INOPERATIVE. ACFT GROUNDED. VERIFIED DISCREPANCY. CYCLED POWER TO MCP, PANEL RETURNED TO NORMAL. GROUND VERIFICATION AND LWMP TESTS ARE SUCCESSFUL REF MM 22-11-34 GRP 32, 22-11-0 GRP 49 LAND VERIFY AND HGS SYS AND SENSOR TEST 34-36-0 SSM. ACFT REMASDR ASAA2014110909622Circuit Breaker · trippedAFCS SYS A WARNING LIGHT CIRCUIT BREAKER FOUND EXTENDED. ACFT GROUNDED. RESET CIRCUIT BREAKERS IAW AMM 20-60-01, WDM 22-14-11 AND WDM 22-31-11. CIRCUIT BREAKERS REMAIN SET. ACCOMPLISHED DFCS BITE LIBRARY TEST NR 60 ,CHANNEL A DISENGAGE WARNING. ACCOMPLISHEDSDR SWIA201439887Computer · smokeWHEN FO TOGGLED ON AUTOPILOT, GOT A TRIM FAIL AND AUTOPILOT FAIL ON MAP AND SMOKE OUT OF GLARESHIELD ABOVE FOS FCP. DECLARED EMERGENCY. REPLACED FCP AND AUTOPILOT COMPUTER. PERFORMED OPS CHECK OF AUTOPILOT SYS. TESTED OK. IAW AMM.SDR CALA2014110701430Transmitter · intermittentUNSCHEDULED STAB TRIM EICAS MSG WITH CTR AUTOPILOT ENGAGED SWITCHED TO RT AUTOPILOT CORRECTED ACFT NR FROM 113. ON ARRIVAL LT STCM FAULT BALL LATCHED. ACCOMPLISHED MCDP STAB TRIM TEST 65. ALL OPERATIONS NORMAL IAW AMM 22-04-00-815-825. NO FURTHER FAULTS ONSDR ASAA2014103009543Autopilot Sys · malfunctionedABOUT ONE HOUR INTO CRUISE AT FL 320, AUTOPILOT B ENGAGED, THE AUTOPILOT DISCONNECTED WITHOUT CAUSE. DID NO RECUR AFTER ENGAGED. ACFT GROUNDED. ACCOMPLISHED FLIGHT FAULT REVIEW. ACCOMPLISHED TEST IAW 22-11-34-501 BITE GROUP 32, TEST PASSED. HGS TEST OK, RSDR SWIA201439730Autopilot Sys · malfunctionedWITH AUTO PILOT ON UNCOMMANDED RT ROLL IN HEADING MODE NO PROBLEMS WITH AUTO PILOT OFF. PERFORMED OPS CHECK OF AUTOPILOT SYS IAW AMM. OPS CHECK GOOD.SDR CALA2014102701396Control Panel · malfunctionedMCP ALT SELECTOR WILL NOT SELECT OR HOLD ALT UN SELECTABLE. R & R MCP IAW MM 22-11-02. PERFORM FIM TASK 22-0 3-00 815-829 TEST 4, TEST PASSED. PERFORMED TEST 30 IAW MM 22-00-02-201, NO FAULTS FOUND. ACFT REMAINS FULL CAT CAPABILITY. OK FOR SERVICE. ROTABLSDR CA141022004Module · malfunctioned(CAN) 1) PILOT REPORTED DISCREPANCY. YAW DAMPER DISENGAGED MESSAGE DISPLAYED, TAKEOFF REJECTED. RETURNED TO THE GATE. MAINTENANCE REPLACED INPUT/OUTPUT PROCESSOR NR 1 IAW AMM 31-41-06. YD OPERATIONAL TEST CARRIED OUT IAW AMM 22-11-36. COULD NOT FAULT. SYSTEM SDR ASAA2014101809406Autoland Sys · malfunctionedAUTOPILOT LINED UP SLIGHTLY TO THE LT OF THE LOCALIZER AND FLEW THE ENTIRE APPROACH TO THE LT. AIRPLANE WOULD HAVE LANDED ON LT EDGE OF RUNWAY. DISCONNECTED A/P AND CORRECTED TO CENTERLINE. ACFT GROUNDED. PERFORMED TASK-FIM 22-11, TASK 825. NO FAULTS LOGGSDR WX0A2014102072215Unknown · malfunctionedFLIGHT AUTOMATION FAILURE IN FLIGHT IN BOTH AUTO PILOT 1 & 2 POSITIONS AUTO THROTTLE ALSO FAILED. MAINTENANCE & TROUBLESHOOTING PERFORMED ON WORK ORDER 236488, LP 525986 & LP 525979. PERFORMED RTS OF BOTH AUTO PILOTS 1 & 2 IAW AMM 22-01-05 BOTH CHECKED GOOD.SDR ASAA2014100909336Autoland Sys · no testAUTOLAND EVALUATION UNSUCCESSFUL. HGS WAS SUCCESSFUL. ACFT TRACKED LOCALIZER ACCURATELY UNTIL ABOUT 200' AGL WHEN IT STARTED TO DRIFTING TO THE RIGHT. DISCONNECTED AUTOPILOT AT ABOUT 100' AND CORRECTED. ACFT WOULD HAVE BEEN MORE THAN 35' FROM CENTERLINE. PDSDR SWIA201439399Actuator · failedDURING CLIMBOUT, RECEIVED MULTIPLE AIR DATA HEAT MESSAGES. THE NR 2 YAW DAMPNER KICKED OFFLINE AND THEN ESS TRU 1 DROPPED OFFLINE, ESS TRU 1 CB WAS TRIPPED. RETURN TO FIELD. REPLACED THE NR 2 YAW DAMPNER ACTUATOR. RESET ESS TRU 1 CIRCUIT BREAKER. ALL SYSSDR VNAA2014092700011Circuit Card · malfunctionedCREW REPORTED UNCOMMANDED YAW MOTION IN FLIGHT AND WHEN ACFT YAWS, YAW DAMPER 1 DISCONNECTS. CREW DECLARED AN EMERGENCY, DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, R & R FLIGHT CONTROL COMPUTER (FCC) NR 2 CARD AND PERFORMED CHECKS IAW AMM. ASDR VNAA2014092700010Circuit Card · failedCREW REPORTED UNCOMMANDED YAW IN FLIGHT AND WHEN ACFT YAWS, YAW DAMPER 1 DISCONNECTS. DECLARED AN EMERGENCY, DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND R & R FLIGHT CONTROL COMPUTER (FCC) NR 1 CARD AND PERFORMED CHECKS IAW AMM. ACFT RELESDR BN5A2014092400001Amplifier · faultyEXPERIENCED AN UN-COMMANDED 400 DECENT BY THE AUTOPILOT. PILOTS ADI TUMBLED 15 DEGREES WITH HEADING & NAV MODE UNRESPONSIVE. CREW DESCENDED ACFT TO FL020. CONTINUED FLIGHT WITHOUT AUTOPILOT TO HOME BASE. R & R THE AUTOPILOT AMPLIFIER PN 522-2900-028 SN 2617SDR ASAA2014091909173Sensor · out of adjustELEVATOR NEUTRAL SHIFT SENSOR OUT OF LIMITS. ACFT GROUNDED. ADJUSTED NEUTRAL SHIFT SENSOR IAW MM 22-11-14-820-801. OPS NORMAL, ADDITIONAL TEST IAW BITE GROUP 47, CHECK GOOD.SDR ASAA2014091009098Switch · failedBOTH YOKE AUTOPILOT DISCONNECT SWITCHES DISCONNECT AUTOPILOT BUT DO NOT SILENCE AURAL WARNING OR THE AP/P-RST LIGHTS. AURAL WARNING IS SILENCED WHEN EITHER AP /P -RST SWITCH ON FWD INST PANEL IS PUSHED. ACFT GROUNDED. FOUND CAPTAINS YOKE AUTOPILOT DISENGAGE SDR FDEA201409072503Control Panel · malfunctionedAUTOPILOT NR 1 & 2, AUTO THROTTLES WOULD NOT ENGAGE. NO FLIGHT FAULTS LOGGED FOR THE FCC1 OR FCC2. CHECKING THE FCC1 & FCC2 PREVIOUS FAULTS. BOTH FCC SHOW LEG 1 NO FAULTS, OR FLY INTO IND. LEG 2 FAULTS WERE ELEV FAULT, WHICH EWR RESOLVED. THEN NEXT FAULT SDR USAA2014090800006Switch · faultyTHE AUTO FLIGHT RUDDER TRIM SYS INOPERATIVE AFTER TAKEOFF. FLIGHT RETURNED TO FIELD & LANDED WITHOUT INCIDENT. REPLACED RUDDER TRIM RESET PUSH BUTTON SWITCH IAW AMM 22-62-12-400-001-A.SDR YENA20140901174Fcu · odorCREW DECLARED AN EMERGENCY AND ACFT DIVERTED. SMOKE & STRONG ACRID FUMES FROM FCU DURING CRUISE. ACCOMPLISHED TSM TASK 24-00-00 810-823-A INSPECTED REPORTED SUSPECT AREAS AND FOUND FCU TO HAVE ELECTRICAL BURNING ODOR INTERNALLY. R & R FCU IAW AMM 22-81-12. SDR IPXA2014082784076Autopilot Sys · malfunctionedAUTOPILOT WOULD MAKE ERRATIC PITCH CHANGES DOWN IN CLIMB UP AND IN LEVEL FLIGHT. RETURNED TO DEPARTURE. PERFORMED RTS TEST ON FCC 2IAW AMM 22-00-00-700-801. TEST PASSED.SDR ASAA2014082008901Autopilot Sys · malfunctionedDURING CLIMB OUT AT APPROXIMATLY 12000 FEET, AUTOPILOT A WAS ENGAGED AND IMMEDIATLEY BUMPED AND STARTED TO CLIMB AT ABOUT 2000 FPM. AUTOPILOT WAS DISENGAGED AND SWITCHED TO AUTOPILOT B AND OPERATED NORMALLY. ACFT GROUNDED. OPENSDR ASAA2014081908890Computer · failedDURING CLIMB BETWEEN 12,000 AND 17,000 FT, THE A AUTOPILOT WAS ENGAGED AND IT IMMEDIATELY "PUMPED" THE YOKE ONCE, FELT BY EVERYONE AND THEN IT SEARCHED FOR A VERTICAL SPEED TO MAINTAIN, VARYING BY 2,000 FPM. IT WAS DISCONNECTED AND A 2ND ATTEMPT MADE WITH SAMSDR ASAA2014081808879Control Panel · failedAUTOPILOT B DISENGAGED TWICE DURING LEVEL FLIGHT AT FL380, .80M. NO TURBULENCE. ACFT GROUNDED, DFCS LOGGED MESSAGE 22-111607 MCP DATA INV. R & R MCP IAW MM 22-11-34. OPS CHECK NORMAL.SDR REXA2014081600835Actuator · inoperativeDECLARED EMER FOLLOWED NEW POLICY IN FOM. PROGRESSIVELY GOT WORSE INTO DUTCH ROLL. OSCILLATING BOTH DIRECTIONS, FOLLOWED QRH DISCONNECT YD. HARD PUSH ON RT RUDDER, NEEDED TO COUNTER WITH LT INPUT PRIMARILY, ONCE IT LEVELED DRIFTED TO LT FROM HAVING INPUT TOSDR ASAA2014081508844Control Panel · faultedAUTOPILOT "B" INOPERATIVE IN VERTICAL SPEED MODE. OPERATES NORMALLY IN ALL OTHER MODES. AUTOPILOT "A" OPERATES NORMALLY IN ALL MODES. ACFT GROUNDED. CONFIRMED FAULT, MCP VERTICAL SPEED CH B FAILS MCP INTERACTIVE TESTS MSG 22-11063. ACCOMPLISHED FIM 22-11, SDR SWIA201439100Servo · malfunctionedAT 12,300 FT DESCENDING TO 12,000, ACFT STARTED ON UNCOMMANDED CLIMB. DISCONNECTED AUTOPILOT TO CONTINUE DESCENT. RESET AUTOPILOT WITH NO FURTHER PROBLEMS. IN FCC DIAGNOSTICS FOUND ESVOR AT 1.25VDC ON BOTH LT AND RT. SHOULD BE BELOW +/- .20VDC. NO REPAIR SDR SWAA2014081230780Control Panel · faultyDIVERSION MCP LOCKED UP IN CRUISE. PERFORMED QRH PROCEDURE RESET & MCP UNLOCKED ON THIRD TRY. LOCKED UP ONCE MORE DURING FLIGHT, UNLOCKED ON FIRST TRY. R & R MODE CONTROL PANEL IAW MM.SDR ASAA2014073108728Autopilot Sys · malfunctionedAUTOPILOT "B" DISENGAGED TWICE OVER COURSE OF 90 MINS FOR UNKNOWN REASONS. ACFT GROUNDED. DFCS LOGGED, MCP DATA INV MESSAGE 22-11607. FOLLOWED FIM 22-11, TASK 817, INITIAL EVAL TEST PASSED. NO CURRENT STATUS FAULTS.SDR ASAA2014072808702Computer · failedAFTER TAKEOFF, ATTEMPTED TO ENGAGE B AUTOPILOT AT 1000' AND HEARD A/P DISENGAGE WARNING PLUS A/P DISCONNECT LIGHT THEN AUTOPILOT RE-ENGAGED AND WORKED UNTIL APPROACH AT 2000' AUTOPILOT B DISENGAGED BY ITSELF. BOTH F/D SWITCHES WENT TO "MA", RT WING FELT HEAVYSDR ASAA2014072408677Autoland Sys · malfunctionedIN AUTOLAND, AIRPLANE ATTEMPTED TO LAND 35' OR MORE RT OF CENTERLINE. LEFT MAIN WAS RT OF RWY 34L CENTERLINE CLICKED OFF AUTOPILOT AND LANDED MANUALLY AT APPROX 10' AS AIRPLANE WAS TRACKING FURTHER FROM CENTERLINE. ACFT CRITICAL AREAS WERE CLEAR ON GROUND. SDR ASAA2014072108628Autopilot Sys · malfunctionedAUTOPILOT 2 DISCONNECTED TWO TIMES DURING APPROACH AT 3000FT. PITCH COMMAND FD DROOPED OUT. ACFT GROUNDED.SDR ASAA2014072008613Autoland Sys · malfunctionedAUTOLAND NOT SUCCESSFUL. AT APPROXIMATELY 75 FT, THE ACFT ROLLED TO THE RIGHT. DRIFTING RIGHT, CORRECTED BUT LANDED AWKWARDLY - DRIFTING BACK LEFT SLIGHTLY NOSE HIGH - CRITICAL AREAS PROTECTED. ACFT GROUNDED. NO FAULTS LOGGED IN FFR, DFCS, ACCOMPLISHED LANSDR ASAA2014071908589Autopilot Sys · malfunctionedDURING PRACTICE CAT III AUTOLAND, AUTOPILOT DISCONNECTED AT 2200 FT. ACFT GROUNDED. ACCOMPLISHED DFCS FAULT REVIEW AND LAND VERIFY TEST BITES 20 & 49. NO DEFECTS. ACFT REMAINS CATIIIA AUTOLAND + HGS QUALIFIED. VERIFIED LWMP PLACARD STATUS SCREW REFLECTS SSDR ASAA2014071708588Control Panel · failedAUTOPILOT CLICKED OFF DURING CRUISE FLT, TWICE. ONCE WHILE CMP A ENGAGED AND ONCE WHILE CMP B ENGAGED, ACFT WAS IN TRIM AT DISCONNECT. ACFT GROUNDED. BITE TEST SHOWED MCP REPLACED MCP IAW MM 22-11-34 ETOPS PN 822-1567-102 AS VERIFIED SEAMC.SDR CA140729007Control Panel · failed(CAN) DURING CLIMB OUT WITH AUTOPILOT "A" OR "B" ENGAGED, ENCOUNTERED CONSTANT TRIMMING OF AIRCRAFT NOSE UP AND THEN NOSE DOWN ALMOST CONTINUOUSLY. MAINTENANCE ADVISED A RETURN. DURING RETURN OCCURED AGAIN IN LEVEL FLIGHT AND HELD AT 12000FT. THE MODE CONTROL SDR ASAA2014070608462Control Panel · failedTHE AUTOPILOT SELECTED, DISCONNECTED TWICE DURING THE FLIGHT, ONCE DURING CLIMBOUT AND ONCE IN LEVEL FLIGHT AT 38,000 FT. THE AIR WAS SMOOTH IN BOTH CASES. WHEN THE AUTOPILOT DISCONNECTED IN CRUISE, AUTOTHROTTLES WORKED FINE. ACFT GROUNDED. FCC A & B LOGGESDR SWIA201438579Computer · failedF/O AUTO PILOT WENT INTO DESCENT MODE BY ITSELF. CREW DISENGAGED AND HAND FLEW ACFT. REMOVED AND REPLACED NR 2 AUTOPILOT COMPUTER.SDR ASAA2014070308434Computer · failedONLY "B" AUTOPILOT DISENGAGED TWICE ON THE APPROACH. ACFT GROUNDED. FCC B LOGGED 22-11082 NR 2 SMYD DATA INVALID. ACCOMPLISHED FIM 22-15, TASK 801. WIRING CHECKS BETWEEN FCC B AND NR 2 SMYD GOOD. REPLACED FCCB REF MM 22-11-33, OPS CHECK NORMAL. REPLACED SDR CA140707007Autopilot Sys · failed(CAN) DURING DESCENT, THE ACFT AGGRESSIVELY ROLLED UNCOMMANDED TO THE RT. THE AUTOPILOT WAS AUTOMATICALLY DISENGAGED, NOT BY THE PF AND THE PF WAS ABLE TO REGAIN CONTROL OF THE ACFT. "YD NOT CENTERED" AND "AP DISENGAGED" MESSAGES APPEARED ON THE PFD. ONCE T
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