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 ASAA2016032016022Control Panel · failedMCP PANEL BACKLIGHTING MAKES DIFFICULT TO SEE DIGITS, ESPECIALLY ALTITUDE SETTING. ACFT GROUNDED. R & R DFCS MODE CONTROL PANEL IAW AMM 22-11-34. SYS OPS CHECKS NORMAL IAW SAME, GROUND VERIFICATION SUCCESSFUL. DFCS BITE GROUP NR 32 & 49 AND HGS SENSOR TEST SDR ASAA2016032016021Autoland Sys · unknownAUTOLAND UNSATISFACTORY DUE TO LATERAL OFFSET TO THE RT OF CENTERLINE. ACFT LANDED JUST 35FT RT OF CENTERLINE WITH IN THE TOUCHDOWN ZONE, 1000-2000 FT FROM THRESHOLD. WINDS WERE CALM. ACFT GROUNDED. DFCS FLIGHT FAULT REVIEW LOGGED NO FAULT. ACCOMPLISHED LANSDR ASAA2016031715995Autopilot Sys · malfunctionedON RECALL FLT CONTINUED AND SPEED TRIM FAIL LIGHT ILLUMINATE. AUTOPILOTS A AND B WILL NOT ENGAGE. ACFT GROUNDED. MOVED A/P STABILIZER TRIM CUTOUT SWITCH TO NORMAL. PERFORMED DFCS BITE REF FIM TASK 22-11, TASK 801. TEST PASSED. NO FURTHER FAULTS FOUND.SDR ASAA2016031515947Autoland Sys · malfunctionedFLIGHT CREW REPORTS AUTOLAND UNSUCCESSFUL. ACFT LANDED 30 FT RT OF CENTER LINE AND NO FLARE. FAILS LAND VERIFY BITE GROUP 49. HGS OPS TEST IAW AMM 34-36-00 NORMAL. ACFT GROUNDED. REVIEWED DFCS AND HGS IN-FLIGHT FAULTS. NO RELEVANT FAULTS FOUND EXCEPT ILS ANSDR ASAA2016031415904Control Panel · failedMODE CONTROL PANEL AMBIENT LIGHT SENSOR WILL NOT DIM MCP DISPLAY. ACFT GROUNDED. REPLACED MODE CONTROL PANEL. ALL OPS NORMAL AMM 22-11-34. ACCOMPLISHED DFCS LRU INTERFACE TEST FOR MCP, BITE GROUP NR 32, LAND VERIFY TEST, BITE GROUP 49, AND HGS SENSOR TEST SDR ASAA2016031015884Warning Light · false activationUPON PUSHBACK ON RECALL, SPEED TRIM AND MACH TRIM LIGHTS CAME ON. RETURNED TO GATE. ACFT GROUNDED. CYCLED POWER TO AFCC OPS RESTORED. MACH TRIM & SPEED TRIM CHECKS OK, IAW AMM 22-11-00, PB 201, DFCS BITE TESTS 10,13, AND 14. ACFT DOWNGRADE TO CAT 1 STATUS SDR ASAA2016031015864Indicator · malfunctioned"HDG SEL" INDICATOR LIGHTS DO NOT ILLUMINATE WHEN SELECTED. ACFT GROUNDED. PERFORMED MCP PANEL LIGHTS TEST IAW AMM 22-11-00, TEST GRP 50. NO FAULTS NOTED AT THIS TIME.SDR ASAA2016031015863Control Panel · malfunctionedMCP BLANK ON PREFLIGHT. ACFT GROUNDED. RESET 9 C/B. MCP R2 REF AMM 22-11-34. ACCOMPLISHED MCP INSTALL TEST IAW AMM 22-11-34-740-001. SYS OPS NORMAL. ALL TESTS PASSED. PROBLEM OCCURRED AT POWER TRANSFER. BOTH APU AND GROUND POWER OK.SDR ASAA2016030515747Computer · failedUNCOMMANDED REVERSION TO CWS WITH AUTOPILOT ON AND ACFT LEVEL AT FL340. NO AUDIBLE OR VISUAL WARNING OTHER THAN FMA INDICATING, ALT HOLD AND CWS R. B AUTOPILOT STILL ENGAGED IN "CMD". RE-ENGAGED LNAV AND YNAV WITHOUT INCIDENT. ACFT GROUNDED. PERFORMED DFCSSDR ASAA2016030315746Autoland Sys · malfunctionedAUTOLAND UNSUCCESSFUL: AT 100' AGL ACFT DRIFTED WELL LT OF CENTERLINE AND LANDED OUTSIDE THE TOUCHDOWN ZONE LT. THERE WAS A LT CROSSWIND OF 8 KTS. ACFT GROUNDED. PERFORMED FIM 22-11, TASK 825 - NR 49 BITE LAND VERIFY TEST WITH NO FAULTS. HOUSING SYSTEM, OPSSDR CA160304003Switch · failed(CAN) ON APPROACH, WHEN CREW SELECTED FLAPS TO BE EXTENDED BOTH AUTOPILOT SYS, A AND B DISCONNECT. ACFT IS OPERATING UNDER MEL WITH TROUBLESHOOTING UNDERWAY BY MAINTENANCE PERSONNEL. MORE DETAILS TO FOLLOW WHEN TROUBLESHOOTING IS COMPLETE. UPDATE INFO: MAINTSDR ASAA2016030115711Autopilot Sys · malfunctionedCOUPLED CAT III APPROACH ACFT ROLLED 10 DEGREES LT AT 60 FT, AUTOPILOT WAS DISCONNECTED MANUALLY, NORMAL LANDING. ACFT GROUNDED. DFCS'S SHOW NO RELATED FAULTS ON DAY DISCREPANCY OCCURRED. HGS FFR SHOWED AN ILS ANOMOLY FAULT. PERFORMED FIM 22-11, TASK 825. LASDR ASAA2016022915698Autopilot Sys · malfunctionedAT APPROXIMATELY 20' AGL APPROACH WARNING ILLUMINATED AND BOTH AUTOPILOTS DISCONNECTED. ACFT GROUNDED. REF FIM 22-11, TASK 801, NO CURRENT STATUS FAULTS. LAND VERIFY TEST PASSED REF AMM 22-11-00.SDR SAJFCAL105004Control Panel · malfunctionedAT BUNTA 1224Z FL330 MCP INOPERATIVE, AUTOPILOT INOPERATIVE, REVERT TO MANUAL UNABLE RVSM DES FL270 B4 LEVEL OFF, OPERATIONS NORMAL ACTION TAKEN. REPLACED MCP & PFM INSTALLATION TESTED NORMALLY.SDR CA160219001Clutch · mismanufactured(CAN) AUTOPILOT CLUTCH ASSY ORDERED AND RECEIVED AT ARE FACILITY FOR 1 OF OUR CUSTOMER WITH AN FAA FORM 8130-3 ATTACHED TO IT, STATUS REPAIRED. THE PN ON THE DOCUMENT WAS EFFECTIVE FOR THE ACFT MODEL AND MSN, BUT THE ACTUAL ASSY WAS WRONG ACCORDING TO OUR TECHSDR HALA2016021800051Autopilot Sys · malfunctionedDURING CLIMB WITH LEFT AUTOPILOT IN COMMAND, AUTOPILOT EICAS MESSAGE ILLUMINATED. RACKED LT SAM. GROUND OPS CHECK OK, IAW FIM 22-04, TASK 811. ACCOMPLISHED LAMP MCDP TEST 40. TEST PASS WITH NO FAULTS.SDR CA160215016Actuator · failed(CAN) AN AUTO-PILOT FAILURE MESSAGE WAS OBSERVED BY THE CREW IN FLIGHT. MAINTENANCE FOUND CDS CODE APAU-P, REPLACED THE PITCH ACTUATOR AND COMPLETED SATISFACTORY FUNCTION CHECKS.SDR CALA2016021695106Autoland Sys · malfunctionedAUTO LAND SYS INOPERATIVE DUE TO FAILURE IN AUTOPILOT FLIGHT DIRECTOR COMPUTERS, MODE CONTROL PANEL, AUTOPILOT BACK DRIVE ACTUATORS OR INTERFACING SYSTEMS. STATUS MSG 2713002 LATCHED CL MODE. ACCOMPLISHED FULL CAT 111 AUTO LAND CHECK. PERFORMED AFDC, MCP, BSDR ASAA2016021115419Control Panel · failedWINDOW LIGHTED NUMERALS CONSTANTLY PULSING ON MCP. ACFT GROUNDED. CONFIRMED FAULT. R & R DFCS MCP REF AMM 22-11-34, OPS CHECK NORMAL. ACCOMPLISHED DFCS LRU INTERFACE TEST MCP, GP 32, REF AMM 22-11-34, DFCS LAND VERIFY TEST, GP 49, REF AMM 22-11-00 AND HGS SESDR ASAA2016020515297Display · malfunctionedMCP ALT WINDOW WILL NOT CHANGE. ACFT GROUNDED. AFTER LOSS OF EXT POWER AND RE-ESTABLISHING EXT POWER, DFCS MODE CONTROL PANEL ADJ/TEST NORMAL IAW AMM 22-11-34.SDR ASAA2016013115216Autoland Sys · malfunctionedAUTOLAND UNSUCCESSFUL ACFT QAS LINED UP WITH LT THIRD OF RUNWAY. IT ATTEMPTED TO CORRECT BACK BUT TOUCHED DOWN APPROXIMATELY 30-40 FT LEFT OF CENTERLINE. ACFT GROUNDED. CURRENT STATUS SHOWS NO FAULTS. FLIGHT REVIEW SHOWS NO FAULTS. ACCOMPLISHED LAND VERIFSDR ASAA2016012615026Warning Message · false activationWHILE PERFORMING DFCS BITE, LIBRARY 32, FAULT CODE 22-11126 FOUND. ACFT GROUNDED. ACCOMPLISHED FIM 22-12, TASK 812, NO FAULTS. ACCOMPLISHED LANDING, VERIFY NO FAULTS. GROUND VERIFICATION SUCCESSFUL, IAW AMM 22-00-01-730-801.SDR A6WA201643482Unknown · malfunctionedSHORT ERRATIC UNCOMMANDED YAW MOTION, FOLLOWED BY YAW DAMPER 2 INOPERATIVE STATUS MSG. RE-ENGAGED YAW DAMPER 2 & UNCOMMANDED YAW PERSISTED. DISENGAGED BOTH YAW DAMPERS, THE RE-ENGAGED YAW DAMPER 1 ONLY. NO FURTHER UNCOMMANDED YAW.SDR ASAA2016011814866Autoland Sys · malfunctionedAUTOLAND DURING FLARE ACFT DRIFTED LT OF CENTERLINE RWY 16R WINDS 150 DEGREES, 07 KNOTS. ACFT GROUNDED. ACCOMPLISHED LAND VERIFY TEST NUMEROUS TIMES, TEST PASSED REF AMM 22-11-00. PREVIOUSLY RECORDED MSG NOT OBSERVED.SDR ASAA2016011414805Warning Flag · false activationFLIGHT DIRECTOR FLAG ON CAPTAINS EADI. ACFT GROUNDED. FOUND FCC "A" WOULD NOT ENTER BITE. PERFORMED FIM TASK 22-11, TASK 826. DFCS CURRENT STATUS NORMAL, NO CURRENT FAULTS, NO FLAGS REF AMM 22-11-00-810-801.SDR MASA2016011212671Control Panel · overheatedFLIGHT CONTROL PANEL OVERHEATING WITH FUMES. R & R FLIGHT CONTROL PANEL.SDR DALA2016011900435Control Unit · malfunctionedAT CRUISE ALTITUDE, ACFT PORPOISES UP AND DOWN +/- 300 FPM. MAINTENANCE FOUND LT EPCU WITH EXCESSIVE PLAY CAUSING 2" OF MOVEMENT IN ELEVATOR. R & R EPCU IAW MM. OPERATION AND LEAK CHECKS OK.SDR DALA2016010800099Wire · shortedFLIGHT RETURNED TO DEPARTURE DUE TO SEVERAL LARGE UNCOMMANDED YAW - RUDDER INPUTS REPORTED WHILE CLIMBING THROUGH 16K FT. THE AUTOPILOT DISENGAGED AND THE DFGC SYSTEM CIRCUIT BREAKER C18 OPENED AND WOULD NOT RESET. BOTH MCP AND AUTOTHROTTLE FUNCTIONS WERE LOSDR MASA2015122612658Adc · failedDIVERTED, LOST FLIGHT DIRECTORS IN FLIGHT. REPLACED NR 1 ADC.SDR AALA20151223006Control Panel · faultyAIRCRAFT WAS GNDED. AIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT OVERWEIGHT. DURING CLIMB LG WOULD NOT RETRACT & LNAV WOULD ENGAGE, BUT NOT LOCK. PERFORMED MANUAL EXTENSION SYS ACCESS DOOR SWITCH ADJUSTMENT IAW AMM 32-34-00. PERFORMED GEAR SWINGSDR ASAA2015121414262Control Panel · failedCAPTAINS COURSE SELECTOR STUCK ON 005 AND WILL NOT CHANGE. VOR MODE AND APP MODE ALSO STUCK ON 005 AS DISPLAYED ON EHSI. ACFT GROUNDED. R & R MCP IAW AMM TASK 22-11-34-000-801/22-11-34-400-801. GROUND VERIFICATION TEST OK IAW AMM TASK 22-11-34-740-801.SDR ASAA2015121414261Sensor · failedLAND VERIFY BITE GROUP 49 IAW AMM 22-11-00 3 TIMES, FAILS AUTOTEST LIBRARY TEST 21 EA TIME ANALOG SENSOR A/B, WITH MSG 22-11649, SENSOR FAIL, SUSPECTED LRU: TRANSDUCER 2. ACFT GROUNDED. FFR SHOWS NO FAULTS, ACCOMPLISHED LAND VERIFY TEST SEVERAL TIMES WITH NSDR ASAA2015121214204Sensor · malfunctionedAILERON POSITION SENSOR FOUND OUT OF ADJUSTMENT ON DFCS EXTENDED MAINTENANCE UPGRADE T/C. ACFT GROUNDED. ACCOMPLISHED AILERON POSITION SENSOR ADJUSTMENT REF AMM 22-11-29-820-801. OPS NORMAL. DFCS LRU REPLACEMENT TEST FOR ROLL SENSOR 46, PASSED. ALL DFCS ESDR 2015FA0000639Rudder · malfunctionedDURING CLIMBOUT, WITH YAW DAMPER ENGAGED, THERE WAS A RUDDER TRIM RUNAWAY. PILOTS DECLARED AN EMERGENCY AND DIVERTED.SDR ASAA2015120614131Autopilot Sys · malfunctionedABOUT 1200 AGL WITH BOTH AUTOPILOT A AND B ENGAGED, THE AUTOPILOT DISCONNECTED. ALL PARAMETERS WERE NORMAL. NO APPROACH WARNING BOTH ILS FREQUENCIES WERE TUNED CORRECTED AND HAD GOOD IDENTS. THE HGS WORK NORMAL. ACFT GROUNDED. ACCOMPLISHED DFCS BITE REF FIMSDR ASAA2015120214080Autopilot Sys · malfunctionedFAILED ATTEMPTED AUTOLAND APPROACH. AUTOPILOT DISENGAGED. ACFT GROUNDED. PERFORMED FIM 22-11, TASK 801, FFR SHOWED ON FCC A, LOC BEAM ANOMALY DET NR 22-11367 AND FCC B SHOWED FGN, FCC DROPPED IN APPROXIMATELY 22-11414. REF SAME FIM, CURRENT STATUS TEST GOODSDR ASAA2015113014046Autoland Sys · malfunctionedAUTOLAND/HGS 16L ACFT HAD LT MAIN WHEEL LINED UP WITH RUNWAY EDGE LIGHTS. DISCONNECT THE AUTO PILOT AND HAD TO MAKE A SIGNIFICANT CORRECTION AT 100FT TO LINE UP WITH THE CENTER LINE. IN ACTUAL WEATHER COULD HAVE BEEN A BIG ISSUE. ACFT GROUNDED. PERFORMED DFSDR WX0A2015113000026Autopilot Sys · disengagedIN FLIGHT, AIRCRAFT BANKED HARD TO THE LEFT WITH AUTOPILOT ENGAGED, THEN HARD TO THE RIGHT, FLIGHT DIRECTERS DISENGAGED AND AUTOPILOT DISENGAGED, PERFORMED RTS ON DFGC 1 & 2, GO-REPORTED FROM BOTH. OK FOR CONTINUED SERVICE IAW MM 22-01-05.SDR ASAA2015112914024Control Panel · malfunctionedA/P B WILL NOT ENGAGE. FOUND, ENGAGE INTERLINK, C/B POPPED. ACFT GROUNDED. RESET A/P B SYS ENGAGE INTLK C/B IAW AMM TASK 20-60-01-860-801. PERFORMED DFCS MODE CONTROL PANEL INSTALLATION TEST IAW AMM 22-11-34/501. TEST PASSED.SDR ASAA2015112813956Unknown · unknownAFTER A MOMENTARY PITCH UP, THE A AUTOPILOT WOULD DISENGAGE TRYING TO REACQUIRE ALTITUDE. OCCURRED IN LEVEL FLT, SMOOTH AIR. ACFT GROUNDED.SDR ASAA2015112813976Warning Light · illuminatedDC FAIL LIGHT ILLUMINATES ON & OFF ON MODE SELECT UNIT DURING & AFTER ALIGNMENT. ACFT GROUNDED. NO FAULT CODE ON IRS BITE EVEN WITH DC FAIL LIGHT ON. ACCOMPLISHED FIM 34-21 TASK 842 POWER & CONTINUITY CHECKED NORMAL. R & R IFSAU REF AMM 22-11-37. ACCOMPLISSDR ASAA2015112713958Autopilot Sys · malfunctionedA-AUTOPILOT ENGAGES FOR 2 SECONDS THEN DISENGAGES WITH VISUAL AND AURAL ALERTS. B-AUTOPILOT WORKS FINE. ACFT GROUNDED. ACCOMPLISHED DFCS BITE REF FIM 22-11, TASK 801. NO FAULTS IN CURRENT STATUS FAULT HISTORY FOR LEG 1 LOGGED CHANNEL A ELEVATOR SYNC INV, 4 SDR ASAA2015112413957Control Panel · failedWINDOW ON DFCS MCP HAS LED "DOTS" IN BACKGROUND. NRS ARE READABLE. ACFT GROUNDED. R & R MODE CONTROL PANEL AMM 22-11-34. INSTALLATION TEST PASSED REF AMM 22-11-34-740-801. ACCOMPLISHED ADDITIONAL TESTING REF AMM 22-00-01 DFCS LRU INTERFACE FOR MCP, LAND VESDR 2015FA0000608Pitch Control · malfunctionedAS ACFT APPROACHED, THE ACFT BEGAIN TO LIFT OFF WITHOUT PILOT IN PUT TO CONTROLS. THE GTA 82 ELEVATOR TRIM ADAPTER WENT TO FULL NOSE UP DEFLECTION WITHOUT ANY PILOT INPUT. ACFT NEARLY WENT INTO A STALL, PILOT WAS BARELY ABLE TO MAINTAIN CONTROL OF THE ACFT. SDR A6WA201543244Unknown · malfunctionedUNCOMMANDED YAW MOTION SHORTLY AFTER ENGAGING AUTOPILOT ABOVE 20,000 FT, NOSE SWUNG RIGHT. DISCONNECTED YAW DAMP AUTOPILOT, ACFT SWING BACK TO THE LEFT & IS NO LONGER TRIMMED OUT IN COORDINATED FLIGHT AS IT WAS BEFORE AUTOPILOT WAS ENGAGED. RE-TRIMMED ACFT FSDR ASAA2015111313759Autopilot Sys · disengagedSECOND AUTOPILOT DISENGAGED DURING PRACTICE AUTOLAND PRIOR TO 1500 AGL OTHER AUTOPILOT WAS DISENGAGED MANUALLY AND HAND FLOWN TO LANDING, NO OTHER DEFECTS NOTED. ACFT GROUNDED. ACCOMPLISHED CURRENT STATUS TEST FOR CHANNEL B REF MM 22-11-00, ALL TESTS PASSED.SDR CA151029010Actuator · failed(CAN) REPORTED YAW DAMPER UNCOMMANDED MOVEMENT. OLD P/N 622-9968-001 WAS INSTALLED AND THE SB 670BA-22-007 ADRESSING THIS ISSUE WAS NOT PERFORMED.SDR ASAA2015102713547Autopilot Sys · inoperativeCMD A AUTOPILOT WILL NOT ENGAGE. ACFT GROUNDED. ACCOMPLISHED DFCS BITE FAULT REVIEW. NO FAULTS LOGGED FOR LAST 5 LEGS. REF FIM 22-11, TASK 801. DFCS CURRENT STATUS TEST PASSED. PERFORMED DFCS GROUP 11 AUTOPILOT AND GOUP 47 LRU REPLACEMENT TEST FOR PITCH SDR AALA201510309012Yaw Damper · defectiveNON-COMMANDED RUDDER INPUT WITH AUTOPILOT ON AT FL280. REPLACED NR 2 YAW DAMPER SERVO ACTUATOR. ACCOMPLISHED A SATISFACTORY LEAK & OPERATIONAL CHECK IAW AMM 27-26-51-400-001-A & 22-63-00-710-001-A.SDR ASAA2015102713538Autopilot Sys · malfunctionedND AUTOPILOT WOULD NOT ENGAGE ON AUTOLAND APPROACH SINGLE CHANNEL, REMAINED ILLUMINATED WITH BOTH AUTOPILOT SWITCHES ILLUMINATED. HGS OK. ACFT GROUNDED. FLT FAULT REVIEW SHOWS NO FAULTS ON A OR B AUTOPILOT. REF FIM 22-11, TASK 801. PERFORMED LAND VERIFY TE
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