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 ASAA2016062917201Indicator · malfunctionedON TAKEOFF IAS/MACH WINDOW WOULD NOT CHANGE WHEN SPEED WINDOW DIAL WAS TURNED. TRIED LEVEL CHANGE, VERTICAL SPEED, AND SPEED INTERVENTION. VNAV MODE WORKED FINE. AT APPROX. 10,000' THE IAS/MACH SELECTOR WORKED NORMALLY IN ALL MODES. ALL IAS/MACH MODES WORKED NSDR ASAA2016062817192Unknown · unknownON APPROACH, AIRSPEED BUG BECAME UNRESPONSIVE TO MCP PANEL INPUT. TURNED OFF FLIGHT DIRECTORS AND REGAINED AIRSPEED BUG FUNCTION. ACFT GROUNDED. COULD NOT DUPLICATE, NO LOGGED FAULTS, SYSTEM TESTS GOOD IAW AMM 22-00-01-730-801.SDR ASAA2016062817191Autopilot Sys · malfunctionedAUTOPILOTS A & B WILL NOT ENGAGE. ACFT GROUNDED. DFCS CURRENT STATUS TEST SHOWED NO FAULTS. FLIGHT FAULT REVIEW SHOWS NO FAULTS. SHOOK OUT FLIGHT CONTROLS AND RAN LAND VERIFY TEST 3 SEPARATE TIMES WITH NO DISCREPANCIES NOTED. AUTOPILOT SYS ENGAGES AND OPSSDR ASAA2016062717183Warning System · false activationAFTER POWER INTERRUPTION, F/O'S PFD DISPLAYS FD AMBER WARNING, ALSO, F/O'S FD SWITCH TURNED TO ON, THERE'S NO FD OR MA ON F/O'S SIDE. ACFT GROUNDED. CYCLED POWER, OPS NORMAL, DUE TO WEAK GPU, ACCOMPLISHED DFCS BITE NO FAULTS NOTED, REF FIM 22-11, TASK 801, ESDR HALA2016062500256Control Panel · malfunctionedETOPS SIGNIFICANT SYSTEM, ALT CONTROL ON MCP GOES FROM 900 TO 10000 WITH NOTHING IN BETWEEN. RESET MCP PANEL. PERFORMED MCDP GROUND TEST 04 AND TEST 30. ALL TEST PASSED. LMPS STATUS TO REMAIN IN LAND 3 MODE.SDR ASAA2016062017098Control Panel · failedCLICKING NOSE HEARD FROM AROUND MCP SEEMED TO ONLY MAKE NOSE WHILE IN CLOUDS WE WERE AT FL360, -45 DEGREES CELSIUS. ACFT GROUNDED. REPLACED MCP PANEL IAW AMM 22-11-34-401, RAN LAND VERIFY TEST IAW AMM 21-11-00-201 AND HGS IAW AMM 34-36-00. ACFT REMAINS HGS ASDR A6WA201644017Status Message · activatedRECEIVED SMALL UN-COMMANDED YAW AND YAW DAMP 2 INOPERATIVE STATUS MESSAGE CLIMBING THRU FL 230.SDR A6WA201644016Yaw Damper · disengagedDURING FINAL DESCENT RECEIVED YAW DAMP 2 STATUS MESSAGE APPEARED, AND YAW DAMP 2 DIS-ENGAGED, UPON RE-ENGAGEMENT, ACFT UN-COMMANDED YAWED RT APPROXIMATELY 10 DEGREES. COMPLIED WITH QRH, DISCONNECTED YAW DAMPER FOR REMAINDER OF LIGHT.SDR ASAA2016061116998Light · inoperativeHDG SELECT, SWITCH LIGHTS OUT, MODE DOES SELECT AND SHOW ON THE FMA. ACFT GROUNDED. UNABLE TO DUPLICATE DEFECT, HDG SELECT SWITCH LIGHT OPS NORMAL WITH LIGHTS SWITCH IN TEST AND DFCS BITE, REF AMM 22-11-00.SDR ASAA2016061116997Computer · failedON RECALL FLIGHT, CONTINUE LIGHT ILLUMINATED, SPEED TRIM FAIL LIGHT ILLUMINATED BOTH EXTINGUISHED ON RESET. ACFT GROUNDED. ACCOMPLISHED FIM 22-11, TASK 801 DFCS BITE, CURRENT STATUS PASS. FLIGHT FAULT AND FDE FAULT 22-1186. R & R FCC A IAW AMM 22-11-33, OPSSDR ASAA2016060916996Warning Message · false activationSPEED TRIM MASTER CAUTION ILLUMINATED ON RECALL DURING DESCENT CHECK. ACFT GROUNDED. FFR, SPEED TRIM, SHOWS 1 RELEVANT FAULT, AUTO STABILIZER TRIM CUTOUT, MESSAGE 22-1182. DFCS BITE GROUP 32.00 SPEED/TRIM PASSES NORMALLY. ETOPS GROUND VERIFICATION SUCCESSFSDR ASAA2016060616956Autoland Sys · malfunctionedFAILED AUTOLAND, DOVE TO RUNWAY AT 50', DID NOT FLARE. ACFT GROUNDED. IAW FIM 22-11 TASK 801, NO FAULTS LOGGED LAST 5 LEGS DFCS A & B. LAND VERIFY TEST PASSED, REF AMM 22-11-00. ALL TESTS FOR INBOUND FMS CONDITION RELATED TO AUTOLAND PASSED, REF LWMP CHECKLISDR 9JLA201609308425Button · disengagedSHORTLY AFTER T/O FOR A REPOSITION FLT FROM SDL TO LAS, EXPERIENCED A FAULT WITH THE FLT DIR CONTROLLER IN THE VERTICAL MODE ON BOTH PILOTS A COPILOTS CONTROLLERS. CREW REPORTED, WERE UNABLE TO ENGAGE EITHER V/S OR F/C MODES ON EITHER SIDE. CREW INDICATED THSDR ASAA2016060216935Circuit Breaker · trippedCIRCUIT BREAKER P6-2 A2 AFCS INTERLINK IS TRIPPED. ACFT GROUNDED. RESET CIRCUIT BREAKER IAW AMM 20-60-01 AND WDM 22-11-12 ACCOMPLISHED DFCS LIBRARY TEST 32 TEST PASSED AND CIRCUIT BREAKER REMAINED SET.SDR ASAA2016052816867Autopilot Sys · malfunctionedJUST AFTER TOC A/P A DISCONNECTED. CAPTAIN HAPPENED TO OBSERVE A BRIEF FLICKER OF THE SOURCE OFF LIGHT ILLUMINATED FOR GENERATOR 2. MASTER CAUTION DID NOT ILLUMINATE. RECALL WAS CLEAR. RE-ENGAGED A/P A AND CONTINUED WITH OUT INCIDENT. ACFT GROUNDED. ACCOMPLISSDR ASAA2016052516847Control Panel · failedMC PANEL, F/O'S COURSE DIGITAL READOUT FIRST DIGIT SHOWS SEGMENTS OF OTHER NUMBERS WHEN ON 1 & 3. ACFT GROUNDED. REMOVED, REPLACED, AND TESTED DFCS MODE CONTROL PANEL IAW AMM 22-11-34-400-801, TEST PASSED. ALSO ACCOMPLISHED DFCS LRU REPLACEMENT TEST FOR MCP SDR ASAA2016052216821Actuator · failedLAND VERIFY TEST FAILS, MESSAGES 22-11145 AND 22-11146 RAIL POSITION SENSOR 1-2 FAIL ON 60.35 DUAL PORTION OF TEST. ACFT GROUNDED. ACCOMPLISHED A/P AILERON ACTUATOR ADJUSTMENT/TEST, REF AMM 22-11-25-820-801/710-801 AND ADDITIONAL TESTS REF AMM 22-11-25/501 BSDR ASAA2016051716769Transmitter · out of adjustWHILE PERFORMING TC 78222000, FOUND AILERON POSITION SENSOR OUT OF ADJUSTMENT. ACFT GROUNDED. ADJUSTED THE AILERON POSITION SENSOR IAW AMM 22-11-29-820-801, OPS CHECKS GOOD. ACCOMPLISHED ADDITIONAL LWMP TEST, DFCS LRU REPLACEMENT TEST, REF AMM 22-11-29/501 BSDR ASAA2016051316709Control Panel · failedALTITUDE ALERT KNOB WILL NOT SET ON MCP PANEL. ACFT GROUNDED. REPLACED MCP IAW AMM 22-11-34. GROUND VERIFICATION TEST PASSED.SDR 2016FA0000237Actuator · brokenDIRECT DRIVE AILERON AUTOPILOT ACTUATOR, ARC PA495A-1, WAS BROKEN INSIDE MOTOR HOUSING CAUSING THE AILERON CONTROLS TO HANG UP.SDR ASAA2016051116694Warning Light · false activationAUTOPILOT, AUTOTHROTTLE, FMC TEST LIGHTS DO NOT ANNUNCIATE UPON TEST OF CAPTAINS PANEL AND F/O PANEL. ACFT GROUNDED. FOUND "WARN LIGHT, BATTERY, CB OUT ON P18-1 D1. INSPECTED AREA BEHIND CB IN P18-1, PANEL, NO DISCREPANCIES FOUND. RESET CB, REF AMM 20-60-01.SDR ASAA2016050816656Warning Flag · false activationDURING PREFLIGHT AMBER "FD" ANNUNCIATION ON FO DISPLAY. ACFT GROUNDED. "FD" FLAG APPEARED AFTER GROUND POWER DROPPED OFFLINE. CYCLED POWER & "FD" FLAG EXTINGUISHED. PERFORMED CURRENT STATUS TEST FOR "B" A/P & AUTO TEST PASSED. FLIGHT DIRECTOR LIBRARY TEST SDR ASAA2016042916575Autoland Sys · malfunctionedHGS AIII & AUTOLAND UNSUCCESSFUL. ACFT TOO FAR LT OF PRODECTED LOCALIZER CENTERLINE ALSO FLAIR RATE SEEMED LATE AND SLOW. NO FAILURES ANNUNCIATED. PERFORMANCE OF AUTOLAND UNSUCCESSFUL. RT MLG WAS WELL LT OF CENTERLINE. ACFT LANDED TOO FAR LT OF CENTERLINESDR ASAA2016042716581Control Panel · failedONE BULB INOPERATIVE IN AUTOPILOT A "CMD" BUTTON. ACFT GROUNDED. REPLACED DFCS MCP IAW AMM 22-11-34-400-801 OPENED. OPS CK OK IAW AMM 22-11-34-740-801. PERFORMED TESTS FOR MCP REPLACEMENT IAW AMM 22-00-01-730-801. ACCOMPLISHED BITE GROUP NR 32 AND 49 LANDSDR ASAA2016042716546Pressure Switch · failedWHILE ON, A-A/P, SELECTED B-A/P. AFTER A FEW SECONDS B-A/P DISENGAGED. THEN A-A/P WOULD NOT ENGAGE. B-A/P WILL ENGAGE BUT DISENGAGE AFTER A FEW SECONDS. NO OTHER SYS PROBLEMS NOTED. ACFT GROUNDED. FAULT REVIEW LAST LEG, BOTH FCC A & B LOGGED SEVERAL ELEVASDR ASAA2016041716433Pressure Switch · failedA-AUTOPILOT WILL ONLY ENGAGE FOR ABOUT 5 SECONDS. IT APPEARS THAT THE ASSOCIATED AUTOPILOT TRIM IS NOT WORKING. B-AUTOPILOT WORKS NORMALLY. ACFT GROUNDED. DFCS BITE T/S INDICATED HYDRAULIC PRESSURE SWITCH -1 FAILURE. R & R SAME. OPS GOOD, REF AMM 22-11-40.SDR ASAA2016041716432Indicator · malfunctionedLNAV, VNAV TEMPORALLY BUMPED OFF PRIOR TO TOP OF DESCENT. OBSERVED VTK & CWS ROLL MESSAGES ON FO SIDE. B AUTOPILOT WAS BEING USED. ACFT GROUNDED. ACCOMPLISHED FLT FAULT REVIEW DFCS IAW FIM 22-11, TASK 801, LAST LEG FAULTS ON B SIDE: 22-11006, 22-11822 AND 2SDR ASAA2016041516425Warning Message · activatedWHILE PERFORMING NR 49 LAND VERIFY BITE STEP 49.35, FAILS FCC A AND FCC B FOR AILERON POSITION SENSOR NR 1 AND AILERON POSITION SENSOR NR 2, FAULT MAINTENANCE MESSAGES 22-11145 & 22-11146. ACFT GROUNDED. PERFORMED BITES 49.35 AND 60.35 NUMEROUS TIMES. NO HESDR ASAA2016041416424Antenna · failedCAPTAIN LOST F/D AND A/P DISENGAGED AT G/S CAPTURE. ACFT GROUNDED. COMPLIED WITH ALL SPECIAL MAINT PROCEDURES, NO DEFECTS NOTED FROM MAINTENANCE PROCEDURES. DFCS FAULT REVIEW SHOWED NUMEROUS RAD ALT 1 FAULTS. REMOVED & REPLACED, AND TESTED NR 1 RAD ALT RXSDR ASAA2016041116349Autoland Sys · malfunctionedUNSATISFACTORY AUTOLAND, HGS APPROACH. ACFT FAR RT OF CENTERLINE AT 1300FT ON RWY 16R. ACFT GROUNDED. PERFORMED FIM 22-11, TASK 825. PERFORMED LAND VERIFY TEST BITE NR 49, AMM 22-11-00 WITH A TEST PASS.SDR ASAA2016041016336Autoland Sys · malfunctionedUNSUCCESSFUL AUTOLAND, LANDED TOO FAR RIGHT. DISCONNECTED MANUALLY, CONTINUED APPROACH. ACFT GROUNDED. ACCOMPLISHED INSTALLATION TEST AND ADDITIONAL MINIMUM TEST IAW LWMP SYS TABLE FOR ILS SYTEM, LAND VERIFY BITE GROUP 49 AND HGS SYS TEST, ALL TESTS PASS,SDR ASAA2016040516248Autopilot Sys · malfunctioned"A" AUTOPILOT DISENGAGED TWICE DURING FLIGHT AT CRUISE ALTITUDE. USED "B" A/P FOR REMAINDER, NO ISSUES. ACFT GROUNDED. FFR SHOWED 2 FAULTS FOR MCP. ACCOMPLISHED DFCS LRU INTERFACE TEST FOR MCP, BITE GROUP NR 32, LAND VERIFY, BITE GROUP NR 49, AND HGS SENSORSDR ASAA2016040416237Autopilot Sys · malfunctionedAFTER SWITCHING FROM AUTOPILOT A TO B, AUTOPILOT B DISENGAGED AFTER 5 SECONDS. NEITHER AUTOPILOT WOULD RE-ENGAGE IN CMD OR CWS AFTER AUTOPILOT A & B INOPERATIVE. ACFT GROUNDED. PERFORMED DFCS BITE PROCEDURE IAW FIM 22-11-TASK 801, FOUND FAULT CODE 22-11127, CHSDR ASAA2016040316223Control Panel · failedDURING TAXI OUT F/O'S COURSE INDICATION BLANK. ACFT GROUNDED. R & R DFCS MODE CONTROL PANEL IAW AMM 22-11-34-000-801 AND 22-11-34-400-801. ACCOMPLISHED MCP INSTALLATION TEST IAW AMM 22-11-34-740-801. PERFORMED DFCS GROUP NR 32 LRU INTERFACE TEST FOR MCP ANSDR ASAA2016040216195Warning Flag · false activationDURING PRE-FLIGHT BOTH FLIGHT DIRECTOR FLAGS IN VIEW. IAS/MACH WINDOW IN MCP CLOSED. ALTITUDE WINDOW IN MCP INDICATED 50000 & UNABLE TO MOVE. ACFT GROUNDED. CYCLED POWER TO ACFT. MCP & D/D OPS RESTORED. OPS CHECK NORMAL, REF AMM 22-11-33. BITE TEST NR 35SDR ASAA2016040116194Knob · intermittentF/O'S COURSE SELECT KNOB INTERMITTANTLY INOPERATIVE. ACFT GROUNDED. COULD NOT DUPLICATE, SYS TESTS GOOD IAW AMM 22-00-01-730-801. ACFT REMAINS CAT III A A/L & HGS QUALIFIED. STATUS IND REFLECTS SAME.SDR O2JA20160401001Position Sensor · defectiveWHEN THE AUTOPILOT IS ENGAGED IN THE SPEED, ALTITUDE OR NAV MODE THE ACFT NOSE PITCHED UP IN ATTITUDE WITH NO MANUAL INPUT OR CONTROLLED COMMAND GIVEN FOR NOSE UP. THE AUTOPILOT NOSE PITCH UP IN ATTITUDE OCCURRED FOUR TIMES AT FLIGHT LEVEL 8,000 FEET, 21,000 SDR WX0A2016040173125Software · faultyWHEN IN NAVIGATION MODE, ACFT IS BANKING 30 DEGREES PLUS AT HIGH ALTITUDES. DURING LEVEL TURNS, IT IS LOSING UP TO 75 FEET OF ALTITUDE. PERFORMED FLIGHT FAULT REVIEW OF DFGC 1 & 2 FOUND MULTIPLE FAULTS FOR PMS & FMS NAVIGATION DATA IAW AMM 22-01-05. RE-LOADSDR WX0A2016040173124Unknown · not reportedON CLIMB OUT, PLATFORM 1 DATA FAIL, FIRST OFFICERS ATTITUDE INDICATOR WAS NOT STABLE & WAS ERRATIC. AUTOPILOT & AUTO THROTTLE DISENGAGED, THEN RE-ENGAGED. PROBLEM REPEATED, SWITCHED AUTOPILOT TO NR 1. FIRST OFFICERS ATTITUDE INDICATOR STILL INTERMITTENTLY ESDR WX0A2016040173122Unknown · not reportedON CLIMB OUT WITH DFGS SWITCH ON NR 1 POSITION FLIGHT & DIRECTOR FAILED ON NR 1 SIDE WITH A BLANK FMA DISPLAY AUTOPILOT & AUTO THROTTLE FAIL. RAN QHR 31.3 & 31.8, LOST NR 2 FMA & FLIGHT DIRECTOR WHEN DFGS SWITCHED TO NR 2. FMA & FLIGHT DIRECTOR RETURNED AT 1SDR ASAA2016032916144Circuit Breaker · trippedAFCS INTERLINK NR 2 CIRCUIT BREAKER TRIPPED. P6-2-A2, AFCS ENGAGE INTERLINK CIRCUIT BREAKER TRIPPED, P18-1-D3. ACFT GROUNDED. PERFORMED GVI OF AREA BEHIND P6-2 AND P18-1, RESET CIRCUIT BREAKERS IAW AMM 20-60-01-860-801. ACCOMPLISHED FIM 22-13/821, MAINTENANCSDR WX0A073118Unknown · not reportedON DESCENT WHILE SELECTING DFGC 2, THE ATTITUDE SELECTOR WENT BLANK, IT ILLUMINATED. WHEN IT WENT BLANK, THE AUTO PILOT & AUTO THROTTLES KICKED OFF & THE FIRST OFFICER LOST THE FLIGHT DIRECTOR, WHEN IT CAME BACK ON WE WERE ABLE TO RESELECT ALL MODES. HOWEVERSDR AALA20160328003Switch · malfunctionedAIRCRAFT WAS NOT GNDED. AIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT WAS OVERWEIGHT. DURING CLIMB BOTH AUTOPILOTS WOULD NOT ENGAGE. CYCLED AUTOPILOT STABILIZER TRIM CUT OUT SWITCHES & ACCOMPLISHED CHECK OUT IAW AMM 22-11-00. ALL CHECKED OK.SDR ASAA2016032716110Transceiver · failedON ILS APPROACH AUTO PILOT B UNCOMMANDED DISCONNECT. ACFT GROUNDED. DFCS FFR SHOWS FLIGHT 8, A/P DISCONNECT DUE TO RAD ALT-2 INV HGS SHOWS NUMEROUS RECENT AND AFTER FLIGHT 8 RAD ALT-2 INVALID. R & R NR 2 RAD ALT RECEIVER/TRANSMITTER REF AMM 34-33-21, OPS NORSDR ASAA2016032516088Transmitter · failedAUTOPILOT "A" BEGAN OSCILLATING UP AND DOWN 30' AT CRUISE. FL360 SAT-53C 265 KTS .798 MACH. TRIM WHEEL MOVED CONTINUOUSLY FORWARD AND AFT. SELECTED AUTOPILOT B AND OSCILLATING STOPPED. RE-SELECTED AUTOPILOT A AND OSCILLATIONS CONTINUED. SWITCHED BACK TO AUTSDR ASAA2016032416087Control Panel · failedLEFT SIDE OF MCP PANEL BACKLIGHTING INOPERATIVE. ACFT GROUNDED. VERIFIED, ADJUSTING FACE PLATE DID NOT FIX ISSUE. R & R MODE CONTROL PANEL REF AMM 22-11-34. INSTALLATION TEST PASSED. ACCOMPLISHED ADDITIONAL TESTING DFCS LRU INTERFACE TEST FOR MCP NR 32, LSDR VNAA2016032100027Computer · intermittentCREW REPORTED INTERMITTENT AUTOPILOT DISCONNECTS AT FL 310. THE CREW DECLARED AN EMERGENCY, DIVERTED TO NEAREST FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R THE ATTITUDE HEADING COMPUTER NR 2, AND PERFORMED CHECKS IAW THE AMM. THE ACFT WSDR ASAA2016032016032Autoland Sys · malfunctionedREQUESTED AUTOLAND HGS APPROACH UNSUCCESSFUL, AUTOPILOT DISENGAGED AT 5 FT APPROXIMATELY. ACFT GROUNDED. ACCOMPLISHED FAULT REVIEW IAW FIM 22-11, TASK 801, GP 20, NO FAULTS LOGGED. ALSO ACCOMPLISHED DFCS LAND VERIFY TEST, GP 49, IAW AMM 22-11-00/201 AND HSDR ASAA2016032016033Warning Light · false activationAFTER ENGINE START ON RECALL, MACH TRIM FAIL LIGHT ILLUMINATED, RESETS WITH MASTER CAUTION RESET. ACFT GROUNDED. PERFORMED MACH TRIM DFCS BITE TESTS 20.33 LRU TESTS, EXT MAINT MACH TRIM BITE 60.33, CURRENT STATUS BITE 10.00 AND MACH TRIM BITE 13.00 NUMEROUS SDR ASAA2016032016023Autopilot Sys · unknownON APPROACH INTERCEPTING LOC AND GS, ACFT STOPPED AUTO TRIMMING WITH AUTOPILOT ENGAGED. ACFT PITCHED UP. DISCONNECTED THE AUTOPILOT AND AUTOTHROTTLES WHEN STABILIZER OUT TRIM LIGHT ILLUMINATED. TOOK APPROXIMATELY 5 FULL ROTATIONS OF THE TRIM WHEEL TO RE-TRI
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