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 ASAA2017061021004Pressure Switch · failedAUTOPILOT B WILL NOT ENGAGE IN CMD OR CWS. AUTOPILOT A ENGAGES IN BOTH CMD AND CWS FOR 3-5 SECONDS BEFORE DISENGAGING WITH HORN & LIGHT WORKING. NO OTHER LIGHTS ILLUMINATED. ACFT GROUNDED. DFCS BITE, MAINTENANCE MESSAGE 22-1150, FIM 22-13 TASK 805, B AILERSDR ASAA2017060921006Knob · looseHEADING SELECT KNOB WILL OCCASIONALLY NOT CHANGE DIGITS. MOVING OR PUSHING AND PULLING ON THE SELECTOR KNOB WILL START IT WORKING AGAIN. ACFT GROUNDED. HEADING KNOB ON MCP WAS SLIGHTLY LOOSE. TIGHTENED THE TWO SET SCREWS ON KNOB USING ALLEN WRENCH. KNOB OPS. SDR ASAA2017060921005Autopilot Sys · malfunctionedHEADING BUG STUCK ON 102 HEADING CAN NOT BE MOVED. ACFT GROUNDED. UNABLE TO DUPLICATE, HEADING DISPLAY ON MCP AND ND OPERATE NORMALLY IAW AMM 22-11-34.SDR ASAA2017060821007Control Panel · failedMCP VERTICAL SPEED WINDOW HAS ONE DIGIT SEGMENT PERMANENTLY ILLUMINATED. ACFT GROUNDED. REMOVED & REPLACED THE MCP IAW AMM 22-11-34-000-801, & 22-11-34-400-801. OPS CHECKED NORMAL IAW AMM 22-11-34-740-801. MCP TESTS NORMAL, BITE GROUP 32. LAND VERIFY NORMAL.SDR ASAA2017060720981Warning Light · false activationSPEED TRIM FAIL ANNUNCIATOR ILLUMINATED ON RECALL. EXTINGUISHED WHEN MASTER CAUTION PUSH TO RESET PRESSED. ACFT GROUNDED. ACCOMPLISHED RESET OF POWER. ACCOMPLISHED DFCS BITE GROUP 14 SPEED TRIM TEST. NO CURRENT STATUS FAULTS AND BITE CHECKED GOOD IAW FIM 22-SDR ASAA2017060320942Autoland Sys · malfunctionedWHILE PERFORMING AN AUTOLAND-HGS APPROACH FOR THE APPROACH SURVEY, RECEIVED A APPROACH WARNING BELOW 50 FT. REASON IS UNKNOWN. DISCONNECTED AND LANDED. ACFT GROUNDED. RESET SYSTEM AND RAN LAND VERIFY TEST IAW AMM 22-11-00/201, OPS CHECKED GOOD.SDR ASAA2017053120930Autoland Sys · malfunctionedUNSUCCESSFUL AUTOLAND. ACFT GROUNDED. IAW FIM 22-11, TASK 801 DFCS BITE, NO CURRENT FAULTS. FLIGHT LEG 01 SHOWS FAULTS 22-11210 (FCC-B), 22-11209 (FCC-A). ACCOMPLISHED FIM 22-11 TASK 801 DFCS BITE GROUP NR 20. TESTS PASS, COULD NOT DUPLICATE. ACCOMPLISHED TSDR ASAA2017053020915Circuit Breaker · trippedAFTER TAXIING FOUND AFCS INTERLINK 2 AND AFCS SYS A ENGAGE INTERLINK CIRCUIT BREAKERS TRIPPED. ACFT GROUNDED. ACCOMPLISHED CURRENT STATUS TEST. MAINTENANCE MESSAGE 22-11251 DISPLAYED. CHECKED BOTH CIRCUIT BREAKERS IAW WDM 22-11-12. NO DEFECTS NOTED. RESET BOSDR ASAA2017052720883Warning Message · false activationAUTOPILOT B DISCONNECTED 3 TIMES AT CRUISE. ABLE TO RECONNECT AFTER EACH EVENT. FAULT CODE 221 090 00. ACFT GROUNDED. PERFORMED DFCS BITE IAW FIM 22-11 TASK 801. NO FAULTS. FLT LEG 1 HAS FAULT - MCP DATA INV - MSG 22-11607. PERFORMED FIM 22-11 TASK 817. NSDR ASAA2017052520884Control Panel · failedDURING DESCENT, VERTICAL SPEED WHEEL DID NOT RESPOND TO COMMANDS. ACFT GROUNDED. REMOVED AND REPLACED MCP IAW AMM 22-11-34-000-801 AND 22-11-34-400-801. TESTS OK IAW AMM 22-11-34-740-801. PERFORMED LLM TESTS DFCS REPLACEMENT TEST FOR MCP IAW AMM 22-11-33/401 SDR VGCA20170523001Air Data Module · defectiveNR 2 AUTOPILOT AIR DATA CIRCUIT BREAKER TRIPPED AND HAD A BURNING ODOR.SDR HDNA20172205017Autopilot Sys · malfunctionedWHILE BEING RADAR VECTORED FOR AN APPROACH UNDER IFR CONDITIONS, AUTOPILOT DECOUPLED. ACTIVATED SAS/AP CUT BUTTON AND ATTEMPTED TO CLEAR CAD AND ENGAGE AUTOPILOT WAS UNSUCCESSFUL. AUTOPILOT WORKED IN HEADING MODE, BUT NOT ON ALTITUDE HOLD. P DAMPER REMAINEDSDR ASAA2017052120843Unknown · malfunctionedVERTICAL SPEED FUNCTION OF MCP INOP WHEN A AUTOPILOT IS ENGAGED. ALL OTHER MCP FUNCTIONS OPERATE NORMALLY WITH A AUTOPILOT ENGAGED. ALL FUNCTIONS OPERATE NORMALLY WITH B AUTOPILOT ENGAGED. GROUNDED - YES. PERFORMED DFCS MODE CONTROL PANEL TEST. FOUND NO CURRENSDR ASAA2017051520787Autopilot Sys · malfunctionedENROUTE, AUTOPILOT A DISENGAGED TWICE AT FL340, IN SMOOTH AIR, NO CONTROL FORCE NOTED. AUTOPILOT RE-ENGAGED WITH NO DIFFICULTY EACH TIME. ACFT GROUNDED. DFCS BITE MESSAGE 22-11607 FOR PREVIOUS FLIGHT ON CHANNEL A ONLY. ACCOMPLISHED FIM 22-11 TASK 817. MCP SDR ASAA2017051320722Control Panel · malfunctionedMCP N1 BUTTON DOES NOT ILLUMINATE. ACFT GROUNDED. CONFIRMED N1 BUTTON LIGHT DOES NOT ILLUMINATE WHEN PRESSED. ACCOMPLISHED ALT DEACTIVATION IAW CHAPTER 5, TABLE 3, ITEM 1. REMOVED AND REPLACED MODE CONTROL PANEL IAW AMM 22-11-34-401. ACCOMPLISHED OPS TESTSDR ASAA2017051020710Autothrottle Sys · malfunctionedAUTOTHROTTLE DISENGAGED WHEN TOGA BUTTON DEPRESSED FOR TAKEOFF. ACFT GROUNDED. NO FAULTS LOGGED IN HISTORY. ACCOMPLISHED A/T OPS CHECK IAW MM 22-31-00,TEST PASSED.SDR ASAA2017050520658Control Panel · failedDURING DESCENT, WHEN ENGAGING LEVEL CHANGE MCP SPEED WOULD CHANGE TO RANDOM UNWANTED, UNSPECIFIED SPEEDS REGARDLESS OF DESIRED DESCENT SPEED. ADDITIONALLY, A/C DID NOT HONOR THAT SPEED. AUTOPILOT IGNORED THESE RANDOM SPEEDS AND WOULD NOT CHANGE A/C ATTITUDE TSDR ZDVA20170321003Autopilot Sys · corruptedAIRCRAFT DEPARTED, ENGAGED AUTOPILOT IN CLIMB, EXPERIENCED A RAPID PITCH UP AND LEFT ROLL, AUTOPILOT SELF DISENGAGED, PILOT LEVELED AIRCRAFT AND FOLLOWED CHECKLIST PROCEDURES FOR TROUBLESHOOTING AND VERIFICATION OF ANY OTHER MALFUNCTIONS, DECIDED TO DIVERT FROSDR A6WA2017050544983Autopilot Sys · malfunctionedDURING CLIMB WITH AUTOPILOT ENGAGED AT FL 250, RECEIVED A PRESISTANT UNCOMMANDED YAW. COMPLIED WITH QRH, CONDITION PRESISTED, DIVERTED. YAW BECAME MORE PRONOUCED AT SLOWER AIRSPEEDS.SDR ASAA2017050220614Unknown · malfunctionedAUTOLAND UNSUCCESSFUL. AIRCRAFT ABRUPT FLARE AND DRIFTED LEFT OUTSIDE OF LIMITS OUTLINED IN FLIGHT HANDBOOK. PILOT INTERVENTION REQUIRED. GROUNDED - YES. DFCS NR 1 AND NR 2 DID NOT LOG ANY FAULTS. PERFORMED FIM 22-11 TASK 825. LAND VERIFY TEST NORMAL, REF AMM SDR CALA2017042801140Control Panel · faultyALTITUDE SELECTOR KNOB INOP. UNABLE TO CHANGE ALTITUDE FROM 3190 0. NON-RVSM COMPLIANT FOR FORIEGN AIRSPACE. REPLACED MCP REF IPC 22-11-02-01. MODE CONTROL PANEL GRND TEST PASSED REF AMM 22-10-00. ACFT RETURNED TO CAT-III STATUS REF AMM 22-10-99.SDR ASAA2017042720555Warning Light · illuminatedSTAB OUT OF TRIM LIGHT ON IN DESCENT FL 330 DISENGAGED AP AND HAND FLEW. ACFT GROUNDED. PERFORMED FIM 22-11 TASK 801 DFCS BITE PROCEDURE FAULT HISTORY SORTED BY FLIGHT DECK EFFECT FOUND FAULT CODE 22-11177 PRIMARY STAB TRIM ELEC ACTUATOR. PERFORMED LR TEST FOSDR ASAA2017042420527Control Panel · failedAUTOPILOT B DOES NOT REMAIN ENGAGED. ACFT GROUNDED. ACCOMPLISHED FIM 22-11 817 FOR FAULT CODES PREVIOUSLY LISTED. MCP PASSES DFCS BITE GROUP 32 TEST. RING OUTS PREVIOUSLY ACCOMPLISHED, REPLACED AND TESTED MCP IAW AMM 22-11-34/401, DFCS BITE GROUP 32, LAND VERSDR ASAA2017042220499Unknown · malfunctioned"SPEED TRIM FAIL" LIGHT ILLUMINATED ON RECALL - EXTINGUISHED UPON RESET. GROUNDED - YES. PERFORMED FLIGHT CONTROL SYSTEM BITE PROCEDURE REF AMM 22-11 TASK 801. PASSES ALL TESTS. LAND VERIFY TESTS PASS REF AMM 22-00-01. HGS OPERATIONAL TESTS PASS REF AMM 34-36-SDR ASAA2017042120497Unknown · malfunctionedVERTICAL SPEED LED PANEL INOP MCP MODE CONTROL PANEL. GROUNDED - YES. POWERED DOWN AIRCRAFT, REPOWERED AIRCRAFT, RAN DFGS TEST PER AMM 22-00-01 SYSTEM OP CHECKS GOOD NO HISTORY LAST 60 DAYS NO DEFECTS NOTED AT THIS TIME AIRCRAFT REMAINS HGS/AUTOLAND QUALIFIED SDR SIMA20170421002Servo · malfunctionedAT 35000 FT AND 54 MINUTES IN THE FLIGHT AT CRUISE, THE AIRCRAFT ABRUPTLY PITCHED UP AND AUTOPILOT DISENGAGED STICK SHAKER OCCURED ON PITCH UP AND DURING RECOVERY AUTOPILOT WAS ABLE TO ENGAGE. CMC SHOWS MISCOMPARE CONTROL COLUMN COMAND AND ELEVATOR SERVO IAW SDR ASAA2017041820479Autopilot Sys · malfunctionedNEITHER AUTOPILOT A OR B WILL ENGAGE. ACFT GROUNDED. FFR SHOWS MAINTENANCE MESSAGES 22-11182, 22-11208, 22-11161 ON LEG 1 ONLY. ACCOMPLISHED CHANNEL A SPEED STAB TRIM LIBRARY TEST. NO CURRENT FAULTS NOTED. GROUND VERIFICATION SUCCESSFUL IAW AMM 22-11-00.SDR ASAA2017041220438Computer · failedAUTOPILOT COMMAND A DISCONNECTED AFTER APPROXIMATELY 20 MINUTES AT CRUISE FL 360. WAS ABLE TO REENGAGE. ACFT GROUNDED. FOUND THAT THE MCP WAS FAULTING CODE 22-11606 FOR CHANNEL A. PERFORMED THE RING OUTS THAT ARE CALLED OUT ON FIM 22-11/817 WITH NO NOTED DISCRSDR ASAA2017041120429Control Panel · intermittentAUTOPILOT A DOES NOT ENGAGE IN CMD OR CWS. ACFT GROUNDEDS. DFCS FFR SHOWED 2 FLIGHTS WITH 17 FAULTS OF MCP ELEV/AIL ENGAGE DISAGREE 22-11625 AND 22-11626 FAULTS. MCP WAS SHOWN AT FAULT. DID PASS MCP QUICK TEST 32. REMOVED & REPLACED MCP, IAW AMM 22-11-34. OPSDR CALA2017041000947Warning System · false activationAUTO FLT ''AP OFF'' AND ''A-THR OFF'' DISPLAYED ON UPPER ECAM SCREEN. EMERGENCY DECLARED. SUSPECTED LGCU 1 FAULT PERFORMED BITE TEST ON LGCU1 TEST OK MESSAGE CLEARED.SDR DXTA2017040806392Autopilot Sys · malfunctionedGEA 1 FAIL CAS DISPLAYED. FOLLOWED BY: PRESN AUTO FAIL/OXY LO PRES CAUTIONS. ALSO ENG NO DISPATCH/ADS 1-2 SLIP ADVISORY MESSAGES. LOSS OF #1 ENG OIL PRESS/OIL TEMPERATURE/FUEL FLOW/BATT VOLT/OXYGEN QUANTITY INDICATORS. ALSO THE GEAR INDICATOR TURNED RED ON THESDR ASAA2017040620385Knob · stuckA/S KNOB CONTROLLING A/S IN SPD WINDOW =FROZEN @ 178 KTS. ACFT GROUNDED. REMOVED AND REPLACED MCP, IAW AMM 22-11-34-00-801, & 22-11-34-400-801. PERFORMED OPS CHECKED IAW AMM 22-11-34-740-801.SDR ASAA2017040420360Autopilot Sys · failedAFTER TAKEOFF, FIRST OFFICER`S FLIGHT DIRECT FAIL LIGHT ON PFD ILLUMINATED. AUTOPILOT B WILL NOT ENGAGE. ACFT GROUNDED. VERIFIED DISCREPANCY. DOWN-POWERED AIRCRAFT. RESET ALL ASSOCIATED FCC B CIRCUIT BREAKERS. RACKED FCC B IAW AMM 22-11-33. APPLIED POWER-UPSDR ASAA2017040420359Control Panel · failedCOMMAND B LIGHT ON MCP IS INOPERATIVE. ACFT GROUNDED. REMOVED AND REPLACED MODE CONTROL PANEL IAW AMM 22-11-34-000-801 AND 22-11-34-400-801. ACCOMPLISHED GROUP 32 DFCS LRU INTERFACE TEST FOR MCP AND GROUP 49 LAND VERIFY TEST IAW AMM 22-11-00. PERFORMED HGS SSDR SIMA20170402001Warning Message · false activationDURING APPROACH, AROUND 24,000 FEET, RECEIVED A HDG FLAG ON CAPTAIN`S SIDE FOLLOWED BY IRS NAV MODE FAIL. PROCEEDED TO PERFORM THE QRH. RECOVERED EVERYTHING FOLLOWED BY A SECONDARY FAIL, AP OFF, AT OFF, NO FLIGHT DIRECTOR. CYCLED AC POWER TO RESET SYSTEMS.SDR ASAA2017033120307Control Panel · malfunctionedAUTOPILOT A KICKED OFF TWICE IN SMOOTH AIR DURING CRUISE. BOTH TIMES IT RESET. ACFT GROUNDED. ADJUSTED THE ELEVATOR CONTROL CABLES EA & EB IAW AMM 27-31-00-820-801. CHECKED ADJUSTMENT OF PITCH FORCE TRANSDUCERS, WITHIN LIMITS IAW AMM 27-31-00-820-801 PARA G.SDR QXEA2017032700176Switch · failedLOSS OF ALL FLIGHT DIRECTOR AND AUTOPILOT FUNCTIONS DURING CLIMB OUT THROUGH 6000 FT. FOUND NO FAULTS IN CDS. FOUND THE FIRST OFFICER`S TCS SWITCH TO BE STUCK IN THE ON MODE. REMOVED AND REPLACED THE TCS SWITCH IAW AMM 22-11-51-000/400-801. OP TESTED GOOD. FSDR ASAA2017032420259Control Panel · intermittentMODE CONTROL PANEL BACKGROUND LIGHTING ON CAPTAIN'S SIDE INTERMITTENT. GROUNDED - YES. REPLACED MODE CONTROL PANEL, REF AMM 22-11-34-000-801 AND 22-11-34-400-801. TESTED, REF AMM 22-11-34-740-801. TESTS OK. PERFORMED REQUIRED LWMP TESTS, REF AMM 22-00-01 LWMP SDR SIMA20170324001Autopilot Sys · malfunctionedAUTOPILOT FAILED DURING GO AROUND, WITH UP & DOWN DRAFT OVERSPEED INDICATION FOR ABOUT 3 MINUTES. PERFORMED A PHASE I INSPECTION IAW AMM 05-50-04, SUB TASK 212-002-A. NO DEFECTS NOTEDSDR ASAA2017032020230Autopilot Sys · malfunctionedIN-FLIGHT, AUTOPILOT B DISENGAGED, UNABLE TO REENGAGE. WAS ABLE AFTER 30 SECONDS TO ENGAGE A/P A. ACFT GROUNDED. ACCOMPLISHED DFCS BITE, IAW FIM 22-11 TASK 801. FLIGHT FAULT REVIEW SHOWED MESSAGES 22-11208 AND 22-11607 LOGGED ON BOTH FCC. ACCOMPLISHED STAB TSDR ASAA2017031720196Display · malfunctionedFLIGHT DIRECTOR FLAG ON CAPTAIN'S PRIMARY DISPLAY. ACFT GROUNDED. CYCLED GROUND POWER AND FLIGHT DIRECTOR DISPLAYS NORMALLY. PERFORMED DFCS BITE GROUP 12 FOR FD AND ALL TESTS PASSED IAW FIM 22-11 TASK 801.SDR ASAA2017031620195Unknown · malfunctionedDURING CRUISE FL 330 "B" A/P DISCONNECTED BY ITSELF, NO HYDRAULIC ANOMALIES NOTED OR TURBULENCE. REENGAGED B A/P, WORKED FOR THE REST OF THE FLIGHT. GROUNDED - YES. DFCS GROUP 20 SHOWED TWO AUTOPILOT DISCONNECTS LOGGED BY FCC-B ON LEG 10 - ONE CAUSED BY FAULT SDR ASAA2017031620194Unknown · malfunctionedAUTOPILOT A KICKED OFF MOMENTARILY, TURNED IT BACK ON AND IT WORKED NORMAL. GROUNDED - YES. ACCOMPLISHED FIM TASK 22-11 #001. NO FAULTS, AUTO-PILOT TEST PASSED.SDR FDEA201703150917Autopilot Sys · inoperativeBOTH AUTOPILOTS WOULD NOT ENGAGE AFTER TAKEOFF.SDR ASAA2017031320155Autoland Sys · malfunctionedHGS / AUTOLAND CATIII UNSUCCESSFUL. ACFT GROUNDED. PERFORMED REQUIRED LWMP TESTS IAW AMM 22-00-01. PERFORMED FIM 22-11, TASK 801, BITE 20, AND 22-11-00/200, BITE 49. ALL TESTS OK. PERFORMED HGS SYSTEM TEST IAW SMM 34-36-00. TESTED OK.SDR ASAA2017030420005Control Panel · malfunctionedWITH MAIN PANEL LIGHTS LESS THAN FULL BRIGHT, IAS & MACH DIGITS FLICKER. ACFT GROUNDED. REMOVED & REPLACED THE AUTOPILOT MODE CONTROL PANEL IAW AMM 22-11-34. SYSTEM OPS CHECKED NORMAL, LAND VERIFY & HGS SENSOR TEST IAW AMM 34-36-00 PASSED.SDR FDEA201702280674Computer · failedDURING TAKE OFF ROLL AUTO PILOT DISCONNECTED WITH AURAL HORN & RED ECAM. NO AUTOPILOT ENGAGED AT THE TIME. REPEATED SEVERAL TIMES DURING TAXI BACK TO GATE. CONDUCTED AUTOLAND TEST AND TEST FAILED FOR NR 2 FCC. R & R THE NR 2 FCC AND OPS CHECKED GOOD MSDR ASAA2017022619946Warning Flag · false activationYELLOW FD FLAG ON CAPTAIN'S HSI. ACFT GROUNDED. PERFORMED DFCS CURRENT STATUS ON "A" CHANNEL & NO FAULTS FOUND. FD FLAG EXTINGUISHED AFTER BITE CHECK, IAW AMM 22-11-00-740-801.SDR ASAA2017022019880Autopilot Sys · malfunctionedDURING DESCENT, IN LNAV/VNAV PATH, AIRCRAFT DESCENDED PREMATURELY AT A FIX WITH AN ALTITUDE RESTRICTION OF 14,000', CROSSED THE FIX APPROXIMATELY 150' LOW. THEN AGGRESSIVELY PITCHED NOSE DOWN AND DID NOT CAPTURE THE NEXT ALTITUDE THAT WAS SET IN THE MCP, 13,0SDR T17A201703034019Autopilot Sys · malfunctionedAFTER DEPARTURE AND DURING CLIMB WITH AUTOPILOT ON, CREW EXPERIENCED ROLL TRIM RUNAWAY TO THE RIGHT. DISCONNECTING AUTOPILOT STOPPED FURTHER MOVEMENT. RESET SYSTEM AND OPERATION RETURNED TO NORMAL. MAINTENANCE COULD NOT DUPLICATE ISSUE. MAINTENANCE REPLACED P
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