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 ASAA2015102313516Autoland Sys · unknownDURING HGS AIII AUTOLAND APPROACH. ACFT BEGAN SIGNIFICANT LT DRIFT AT 100'. DRIFT CONTINUED BELOW 50 WITH NO CORRECTION. DISCONNECTED AND LANDED MANUALLY. HGS APPEARED TO BE OK. ACFT GROUNDED. DFCS CURRENT STATUS - NO FAULTS AND FAULT HISTORY, NO FAULTS,SDR ASAA2015101713514Autopilot Sys · malfunctionedB-AUTOPILOT AND B-CWS INOP. ACFT GROUNDED. ACCOMPLISHED DFCS BITE REF FIM 22-11, TASK 801. FAULT REVIEW FOR LAST LEG LOGGED CHANNEL B, A/P DISC SW INPUT INV FAULT MSG 22-11282. PERFORMED AUTOPILOT LRU TEST GROUP 11, 20 AND DFCS GROUP NR 49 LAND VERIFY TEST SDR ASAA2015101313489Control Panel · inoperativeREPORTED F/O'S MCP COURSE WINDOW IS BLANK. ACFT GROUNDED. REPLACED MODE CONTROL PANEL. OPS GOOD. GROUND VERIFICATION SUCCESSFUL. REF AMM 22-11-34. ACCOMPLISHED DFCS BITE 32 DFCS LRU INTERFACE TEST FOR MCP, 49 LAND VERIFY TEST, AND HGS SENSOR DATA TEST FOR SDR FDEA201510113166Autothrottle Sys · malfunctionedREJECTED TAKEOFF AT 80 KTS. ONCE TAKEOFF POWER WAS SET, APPROACHING 80 KTS. THE AUTO THROTTLES PULLED BACK, NR 3 THROTTLE APPROX TWO KNOB WIDTHS. ENG FAIL LIGHT ILLUMINATED. PER CONVERSATION WITH FLIGHT CREW, ALL OTHER ENG INDICATIONS WERE NORMAL, BEFORE &SDR ASAA2015101013421Computer · malfunctionedWHEN LOWER CRUISE ALTITUDE IS SET IN ALTITUDE ALERTER WHILE ON VNAV & ALTITUDE INTERVENTION BUTTON PRESSED, NEW MCP ALTITUDE DOES NOT DISPLAY IN FMC CRUISE PAGE AND FMA ANNUNCIATION ON LEVEL OFF AT NEW CRUISE ALTITUDE CHANGES TO ALT HOLD. ACFT GROUNDED. DFCSSDR A6WA201543117Status Message · activatedDURING CLIMB, WE EXPERIENCED A VERY SLIGHT YAW MOTION, A YAW YD1 INOPERATIVE STATUS MSG APPEARED SHORTLY THEREAFTER.SDR ASAA2015092713230Control Panel · failedAUTOPILOT KICKED OFF FOR NO APPARENT REASON AT CRUISE, IN AUTO "A", AUTO "B" WORKED REST OF THE TRIP. ACFT GROUNDED. REPLACED MCP. OPS NORMAL REF 22-11-34, INSTALL TEST.SDR ASAA2015092513193Warning Light · false activationDURING CLIMBOUT VNAV COMMANDED 210K INSTEAD OF CLIMB PROGRAMED. ACFT GROUNDED. A/P A & B CHANNELS SHOW NO FAILURES IN CURRENT STATUS. FLT FAULT REVIEW SHOWS NO FAILURES. HAS NO RECENT HISTORY, 30 DAYS. ACFT REMAINS CAT I. STATUS PLACARD REFLECTS SAME.SDR WX0A2015091872864Autopilot Sys · malfunctionedAFTER DEPARTURE, ACFT WAS CLIMBING & ACCELERATING THRU 1300 MSL & 180 KNOTA. NO PRIMARY OR SECONDARY TRIM WAS AVAILABLE. ALL CB WERE IN, QRH WAS REF. ACFT WAS LEVELED AT 5000 MSL & SLOWED TO 210 KNOTS. SPEED CONTROL KNOB WAS NOT FUNCTIONING & WOULD NOT CONSDR A6WA201543050Unknown · malfunctionedRECEIVED FLAPS DEGRADED MSG IN CRUISE. PITCH OSCILLATION IN CRUISE WITH AUTO PILOT ON, PITCH OSCILLATION STOPPED WITH AUTO PILOT OFF. DURING PITCH OSCILLATION THE FLAPS INDICATED UNCOMMANDED MOVEMENT FROM 0-8 DEGREES, THEN BACK, THEN 0-2 DEGREES, THIS STOPPESDR DXTA2015091406084Spring · wornUNCOMMANDED AUTOPILOT DISCONNECT AT FL410. AILERONS WERE STIFF UNTIL REACHING FL270. REMOVED AND REPLACED A WORN AILERON FEEL SPRING. PERFORMED SATISFACTORY OPS CHECKS WITH NO DEFECTS NOTED. WORK DONE IAW AMM 27-10-35.SDR A6WA201543043Yaw Damper · faultyFLIGHT 3846 ON CLIMB OUT, RT RUDDER TRAVELING TO THE LT & NOSE KICKING TO THE RT, FELT & SAW INDICATION ON ED2. HAPPENED ON CLIMB OUT, CRUISE & DESCENT, NO MSGS OBSERVED. R & R NR 1 & NR 2 YAW DAMP ACTUATORS.SDR FDEA201509072811Accelerometer · failedON LANDING TOUCHDOWN, AUTO BRAKES & AUTO SPOILERS KICKED OFF. SPOILERS WOULD NOT MOVE TO GND SPOILER POSITION. R & R LINEAR ACCELEROMETER UNIT IAW AMM 22-11-01-2. CHECKED GOOD, NO FAULT BALL & OK FOR SERVICE.SDR A6WA201543016Actuator · malfunctionedFLIGHT 3817, AT 25,000 FT YAW DAMP 1 STATUS MSG AFTER UNCOMMANDED YAW MOTION. R & R YAW DAMP 1 ACTUATOR IAW AMM 22-22-01. OPERATIONS CHECKED GOOD. SN OFF 3598 & SN ON 661 JC.SDR ASAA2015082712946Indicator · inoperativeF/O'S COURSE INDICATOR WINDOW ON MCP IS BLANK. ACFT GROUNDED. OPENSDR CA150828006Actuator · malfunctioned(CAN) ON SHORT WHEN THE CREW DISENGAGED THE AUTO PILOT - THE CONTROL COLUMN FELT VERY HEAVY IN ALL FOUR DIRECTIONS. AFTER LANDING WITHOUT INCIDENT, TROUBLESHOOTING REVEALED AUTOPILOT ROLL ACTUATOR AT FAULT (NOT DISCONNECTING). NO EMERGENCY WAS DECLARED. ROLL SDR ASAA2015081812923Autopilot Sys · unknownWHILE IN THE FOLOWING MODE; LNAV, MCP SPEED, ALT HOLD, LEVEL AT FL390, F/E IAS/MACH WINDOW OPEN WITH .79 MACH COMMANDED ON A/T, THE COMMANDED SPEED CHANGED FROM .79 TO .80 ON MORE THAN 1 OCCASION AUTONOMOUSLY. NO KNOBS WERE TURNED OR TOUCHED, NOR BUTTONS PUSHSDR ANCF2015080201Warning System · false activationDURING ENG START AUTO FLIGHT YAW DAMPER SYS FAULT MSG ON ECAM. IAW AMM TASK 22-91-00-710 -001 & AMM 22-96-710-001-A THE AFS GND SCAN & TEST WAS PERFORMED. TESTED SATISFACTORY.SDR ASAA2015080212679Computer · failedAFTER START, THE L NAV WOULD NOT ENGAGE AND THE AUTO THROTTLES WOULD NOT ARM AND ON MASTER CAUTION RECALL THE SPEED TRIM AND MACH TRIM LIGHTS ILLUMINATED. ACFT GROUNDED. FFR REVEALS MULTIPLY FCC "A" FAULTS. REPLACED FCC "A" IAW MM 22-11-33. GROUND VERIFICATSDR SIMA20150731001Yaw Damper · failedCLIMBING THROUGH FL200, PLANE MADE A YAW TO THE RIGHT SEVERAL TIMES. TURNED OFF THE AUTOPILOT & TRIMMED THE AIRCRAFT, THEN TURNED ON THE AUTOPILOT. AIRCRAFT BEGAN YAWING TO THE LEFT. CHECKED AOM-1 FOR GUIDANCE, THEN DECLARED THE EMERGENCY & RETURNED. YAWINSDR ASAA2015072512586Control Panel · burnedALTITUDE WINDOW ON MCP HAS SIGNIFICANT BURN IN. TOUGH TO SEE SELECTED ALTITUDE. ACFT GROUNDED. REPLACED DFCS MODE CONTROL PANEL IAW AMM 22-11-34/401. MODE CONTROL PANEL INSTALLATION TESTS PASSED.SDR ASAA2015071912497Autoland Sys · no testHGS AND AUTOLAND NOT SUCCESSFUL. ACFT GROUNDED. ACCOMPLISHED LAND VERIFY TEST IAW 22-11-00/201. FAULT REVIEW IAW FIM 22-11 TASK 801. LIBRARY TESTS NR 20, 49, 47, 46, 60, 32. NO FAULTS NOTED, PASSES ALL TESTS. NON REPETITIVE FAULT.SDR ASAA2015071812521Light · inoperativeV NAV LIGHT DOES NOT LIGHT UP. ACFT GROUNDED. DFCS LIBRARY TEST NR 50 SHOWED ALL MCP SWITCH LIGHTS TO BE INOPERATIVE. SUSPECT INTERNAL MCP FAULT. R & R AND TESTED DFCS MODE CONTROL PANEL IAW MM 22-11-34-004-004, MM 22-11-34-404-003. PERFORMED DFCS GROUP NRSDR ASAA2015071812466Autoland Sys · no testAUTOLAND, HGS CAT 3 EVAL UNSATISFACTORY. WING ROCK AND APPROACH WARN ENCOUNTERED IN FLARE. DISCONNECTED AUTOPILOT, LANDED MANUALLY. ACFT GROUNDED. HGS SHOWS ROLLOUT CAUTION RADIO ALTIMETER 2. DFCS BITE SHOWS NO FAULTS LAST 10 LEGS. ACCOMPLISHED HGS OPS TSDR WX0A2015071572732Control Panel · faultyWHEN ENGAGING THE AUTOPILOT USING EITHER DFGC 1 OR 2, ACFT PITCHES UP & DOWN ABRUPTLY BEFORE STABILIZING. R & R FLIGHT CONTROL PANEL IAW AMM 22-01-02, TEST GOOD. PERFORMED RTS TEST, GO ON BOTH 1 & 2, RTS TESTED GOOD IAW AMM 22-01-05.SDR N6WA2015070805Warning Flag · false activationLOW SPEED, ABORTED TAKEOFF DUE TO FLIGHT DIRECTOR FLAG. FLIGHT DIRECTOR FAULT PREVIOUSLY DEFERRED IAW MEL 22-10-01, 22-10-02B & 22-11-03. ABORTED TAKEOFF INSPECTION IAW AMM 05-51-27. FOUND NOT REQUIRED.SDR ASAA2015070512336Warning Light · false activationF/O AMBER SPEED LIMIT FAULT ON PFD, ILLUMINATED ALONG WITH MAXIMUM OPERATING SPEED BAR REMOVED, PITCH BAR ON FD FAILED WHEN THE SPEED LIMIT FAULT OCCURES. FAULT FLASHED ON AND OFF FOR 5 MIN. THEN RETURNED TO NORMAL. FLT CONDITIONS IN CLIMB FROM 380-390. ACFSDR ASAA2015070212306Autoland Sys · malfunctionedPRACTICE AUTOLAND FAILED WITH THE FOLLOWING INDICATIONS INITIAL FLAIR ABOUT AT 30' CAUSED HIGHER THAN NORMAL FLAIR ALTITUDE AND HIGHER THAN NORMAL PITCH AT TOUCHDOWN. DURING EXTENDED FLAIR THE ACFT DRIFTED FROM 15' LT OF CENTER TO 35' RT OF CENTER. PROTECTEDSDR ASAA2015062512224Autoland Sys · failedCAT III AUTOLAND UNSUCCESSFUL. APPROACH WARNING IN FLARE. F/O NOTED, LOCATED TRACKED 3/4 DOT LEFT, ACFT WAS LT OF CENTERLINE CORRECTING WHEN 3/4 APR WARN APPEARED. RW 24R. ACFT GROUNDED. REPLACED NR 2 FCC. TESTS GOOD IAW PART 2, 22-11-33/401, LIBRARY NSDR CA150630001Actuator · failed(CAN) FLYING THRU AT APPROX FLIGHT LEVEL 190 YAW DAMP 2 KICKED OFF LINE & WOULD NOT RESET. RUDDER OSCILLATION WAS ALSO REPORTED. ACFT WAS PRE SB 601R-22-017A, SB 601R-22-017A PERFORMED & YAW DAMPER ACTUATOR REPLACED.SDR CA150622001Unknown · malfunctioned(CAN) ATC CLEARED FLIGHT TO CLIMB FROM FL 370 TO FL 380. DURING CLIMB, CREW HAD AN UN-COMMANDED SPEED CHANGE FROM .77 TO .64. SELECTED MANAGED SPEED & INPUT .77. RESOLUTION IAW COMMENTS IN TROUBLESHOOTING DVDR DATA & HISTORY DATA LOAD, NO FAULTS. DATA SENTSDR ASAA2015062012133Autoland Sys · failedAUTOLAND FAIL, DOVE BELOW GLIDESLOPE AT 200AGL. ACFT GROUNDED.SDR ASAA2015061612110Warning Light · false activationF/O FLIGHT DIRECTOR INOPERATIVE. SPEED TRIM FAIL LIGHT CAME ON WITH MASTER CAUTION RECALL AND GOES OUT WITH THE RESET. ACFT GROUNDED. RESET POWER FOR FCC B ACCOMPLISHED DFCS BITE FD TEST, NO FAULTS, REF FIM TASK 22-11, TASK 801.SDR CA150611004Yaw Damper · failed(CAN) DURING FLIGHT, APPROX 200 NM SOUTH OF STATION, THE CREW HAD A GREEN SYS HYD SYS FAILURE. THE CREW ELECTED TO RETURN. PAN PAN DECLARED. THE FAILURE RESULTED IN THE CREW NEEDING TO PERFORM AN ALTERNATE GEAR SELECTION. FLIGHT LANDED WITHOUT FURTHER INCISDR FDEA201506111766Warning Message · illuminatedON DES, ON MAGENTA LINE, SPEED BRAKES MID, A/C DID UNCOMMAMDED RT ROLL 35DEG BANK. A/P DISCONNECTED NOOTHER PROB. PERFORMED AUTOPILOT FLIGHT DIRECTOR SYSTEM. GROUND TEST PER AMM 22-11-00-5, TEST PASSED. PERFORMED PRIMARY FLIGHT CONTROL SYSTEM LEFT AND RSDR ASAA2015061012054Autoland Sys · malfunctionedAUTOLAND NOT SUCCESSFUL ACFT LINED UP 20 FT RT OF CENTERLINE. ACFT GROUNDED. FLT FAULT REVIEW SHOWS NO FAULTS LAST FLT OR CURRENT STATUS REF FIM 22-11, TASK 801. PERFORMED LAND VERIFY TEST REF MM 22-11-00/201 ALL TESTS PASSED ACFT REMAINS CAT IIIA AUTOLAND & SDR ASAA2015061012053Autoland Sys · malfunctionedUNSUCCESSFUL AUTOLAND, JUST AFTER TOUCHDOWN THE AIRPLANE KEPT PITCHING UP, FLARE WAS EXCESSIVE. ACFT GROUNDED. PERFORMED FIM 22-11, TASK 801 FOR FAULT CODE 221, 7500, 00 INCORRECT FLARE ON MULTI-CHANNEL APPROACH. NO FAULTS LOGGED ON EITHER DFGC FFR ON DAY DSDR RU3A20150610012Monitor · unserviceableMASTER WARNING LIGHT ILLUMINATED WITH AN ASSOCIATED, AUTOPILOT DISCONNECT, RED SEGMENT LIGHT. THERE WAS NO ACTUAL DISCONNECTING OF THE AUTOPILOT & THERE WAS NO AUDIBLE WARNING ASSOCIATED WITH A DISCONNECTING AUTOPILOT. R & R NR 1 AUTOPILOT MONITOR.SDR ASAA2015060912038Autoland Sys · malfunctionedAUTOLAND UNSUCCESSFUL. ACFT DRIFTED TO THE LT OF CENTER AT 100' AS 5 KNOT CROSSWIND DIED OFF TO ZERO AIII APP WARNING CAME ON AT 50 AGL. ILS CRITICAL AREA WAS CLEAR. ACFT GROUNDED. FAULT REVIEW SHOS NO FAULTS REF FIM 22-11 TASK 801. PERFORMED LAND VERIFY TESSDR 5APR20150604125Autopilot Sys · faultyON DESCENT, THE FLIGHT CREW REPORTED: AUTOPILOT DISCONNECTED IN FLIGHT FOLLOWED BY ELECTRICAL ODOR AND SMOKE IN COCKPIT". THE CREW DECLARED AN EMERGENCY, THE ACFT LANDED SAFELY WITHOUT INCIDENT. DURING TROUBLESHOOTING,THE AUTO PILOT MODE CONTROLLER WAS FOUNDSDR CA150604019Control Panel · malfunctioned(CAN) ON 03-JUNE-2015, THE ACFT FLIGHT CREW REPORTED TO MAINTENANCE THAT WHILE ON-GROUND, DURING TAXI, AFTER AN UNEVENTFUL FLIGHT, THE YAW DAMPER NR 2 DISENGAGED AS INDICATED BY THE EICAS STATUS MESSAGE YD 2 INOPERATIVE. ATTEMPTS TO RE-ENGAGE THE YAW DAMPER NSDR ASAA2015060211951Control Panel · dimHEADING DISPLAY WINDOW ON MCP IS VERY DIM. ACFT GROUNDED. REPLACED AND TESTED MODE CONTROL PANEL REF MM 22-11-34. OPS NORMAL. PERFORMED DFCS GROUP 32, DFCS LRU INTERFACE TEST FOR MCP REF MM 22-11-34/501, DFCS GROUP NR 49, LAND VERIFY TEST, REF MM 22-11-00/SDR AALA201506049003Fcu · malfunctionedAIRCRAFT IN LANDING CONFIGURATION CONDUCTING ILS APPROACH. LOCALIZER & GLIDE SLOPE CAPTURED. SET MISSED APPROACH ALTITUDE IN MCP WITH AUTO THRUST IN CLIMB DETENT. THRUST WENT TO OPEN CLIMB UNCOMMANDED & ACFT BEGAN CLIMB TO MCP SELECTED ALTITUDE OF 5,000 FT.SDR ASAA2015052611864Control Panel · failedMCP COURSE INDICATOR ON COPILOT SIDE HAS DIGIT LINE INDICATOR LINE BURNED OUT. ACFT GROUNDED. R & R DFCS MODE CONTROL PANEL IAW AMM 22-11-34-000-801 AND 22-11-34-400-801, OPS CHECKED GOOD. GROUND FUNCTIONAL CHECKED GOOD IAW AMM 22-11-34-740-801. BITE GROUP NSDR ASAA2015052511846Autoland Sys · malfunctionedDURING AUTOLAND, ACFT LANDED APPROXIMATLY 40' RT OF CENTERLINE AND APPEARED TO HAVE MUCH HIGHER THAN NORMAL FLARE, NOSE HIGH ATTITUDE, WINDS 170/8, LANDED 16R. ACFT GROUNDED. REF FIM 22-11, TASK 825, PERFORMED LAND VERIFY BITE NR 49 - GOOD. NO HISTORY LAST 3SDR ASAA2015051811767Control Panel · failedMCP ALT WINDOW FREEZES. WILL NOT ALLOW YOU TO RESET THE ALT. ACFT GROUNDED. REPLACED MCP REF MM 22-11-34-400-801. MCP INSTALLATION TEST OK. REF MM 22-11-34-740-801. ETOPS GROUND VERIFICATION COMPLETED BY ALSO DOING THE MCP FULL EXTENDED MAINT TESTS. ALL TESTSDR ASAA2015051811766Display · malfunctionedMCP ALTITUDE WINDOW FREEZES UP WILL NOT LET PILOT SELECT DIFFERENT ALTITUDE INTERMITTENTLY. ACFT GROUNDED. ACCOMPLISHED FIM TASK 22-11, TASK 803, MODE CONTROL PANEL TEST PASSED NO FAULTS NOTED.SDR A6WA201542652Autopilot Sys · malfunctionedFLIGHT NUMBER 3753. AUTOPILOT ENGAGED RECEIVED A LT WING DOWN CAUTION, DISCONNECTED AUTOPILOT. AILERON CONTROL WAS HEAVY IN BOTH DIRECTIONS. COMPLIED WITH AUTO PILOT TRIM QRH & AILERON
JAMBED QRH SUSPECTED ICE & FREED JAMB. INSPECTED TED VISIBLE CONTROL CASDR AALA20150420008Control Panel · faultyAIR INTERRUPT, RETURNED & EMER DECLARED. LANDING UNEVENTFUL & ACFT OVERWEIGHT. ALL THREE AUTOPILOTS FAILED ALONG WITH RT FMC. ACCOMPLISHED FMC BITE IAW FIM 34-61-00, AUTO FLIGHT BITE IAW FIM 22-02 TASK 815-818, BPCU BITE IAW FIM 24-20 TASK 815-801 & EEC BITSDR P5CA2015041600022Switch · malfunctionedEXITING RUNWAY, ALL 4 THROTTLES ADVANCED TO FULL POWER, UNCOMMANDED, NO PREV HISTORY NOTED, MSG 22466, GO ARROUND SWITCHES CYCLED, AND FCC LCR GROUND TEST PASSED IAW MM 22-10-00, REF LOG PAGE 700573, ITEM 12, GO ARROUND SWITCH IS REPLACED AS PRECAUTIONARY.
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