JASC 2210
Service difficulty reports · 4,017
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 DXTA2010100104255Servo · failedFLASH OF RUDDER BOOST FAIL ANNUNCIATOR AND YAW DAMP KICKED OFF SHORTLY AFTER TAKEOFF. 600-800 FT. TWICE DURING DESCENT, AUTOPILOT AND YAW DAMP KICKED OFF WITH GA INDICATIONS ON PFD. 12,000-11,000FT AND 9,000-8,000FT. TWICE RUDDER BOOST FAIL AND YAW DAMP KICSDR FDEA201009213592Control Unit · failedON APP, AT 8,000' F/O WAS FLYING WE WERE CLEARED FOR THE ILS 25L APP. CAT3 LOX SO SECOND A/P WAS ENGAGED AFTER LAND WAS SELECTED. AFTER G/S & LOC CAPTURE AUTO PILOTS DISCONNECTED AND ALL FMA'S WENT BLANK AND ILS INFO. ATTEMPTED AGAIN WITH SAME RESULT. THEN SDR MYWA100107Autopilot Sys · malfunctionedETOPS SIGNIFICANT SYSTEM: AUTOPILOT "A" DOES NOT ENGAGE WHEN CMD IS PUSHED. LIGHT DOES NOT ILLUMINATE AND STATUS DOES NOT SHOW ON FMAP.SDR F3LA2010090100500Pitch Control · malfunctionedPILOT REPORTED, ACFT PITCH WILL NOT STABLE WHILE HAND FLYING, UNCOMMANDED INCREASE IN PITCH UP. MX PERFORMED BITE TEST OF THE EFCS IAW AMM 27-96-00-740-001 WITH NO DEFECTS NOTED. PERFORMED OPS TEST OF THE AFS IAW AMM 22-96-00-710-001 WITH NO DEFECTS NOTED.SDR CA100916010Computer · malfunctionedAN ANOMOLY EXISTS IN THE AUTOPILOT FUNCTION OF THE APS-65H COMPUTER PN 622-9724-140 (COMPUTER MOD FROM A -130 TO ACCOMODATE THE INSTALLATION OF THE AHRS1000A SYS). WHEN THE ACFT IS CONFIGURED IN CLIMB MODE, AND THE PRE-SELECTOR SET TO A HIGHER ALTITUDE (SO THSDR UALA2010091003361Control Panel · faultyFMC FAILURE, FLIGHT DIVERTED. UPON INVEST FOUND HALF OF MCP SWITCH LIGHTS INOP INCLUDING ALL AUTOPILOT LEFT AND CENTER LIGHTS.SUSPECT LEFT SIDE OF MCP DOWN. RESET MCP CBS AND FUNCTIONS RESTORED. NOW ABLE TO ENGAGE ALL AUTOPILOTS NORMALLY. REPLACED MCP PER MM.SDR MASA2010090800965Yaw Damper · malfunctionedEXCESSIVE RUDDER BUMP IN CRUISE FLT. MX R2 YAW DAMP ACTUATOR NR 1.SDR IPXA10M62143Computer · faultyATB - BOTH AUTO PILOT FAIL TO ENGAGE. RECYCLE CBS NO HELP. FOUND FCC 1 CURRENT FAULT IRU-1, IRU-2, IRU-3, AND FCC-1. ALSO FCC-2 CURRENT FAULT IRU-1, IRU-2, IRU-3, AND FCC-2. PERFORMED FCC-1 AND FCC-2 AFS RTS TEST AND AUTOLAND TEST. ALL TEST PASSED IAW AMM SDR CA100820008Computer · failed(CAN) PILOT REPORTED AP COMPUTER U/S. REMOVED S-TEC 55X AP COMPUTER FROM AIRCRAFT, FOUND PIN 34 BURNED OFF COMPUTER AND AIRCRAFT CONNECTOR P551 HAD MINOR DAMAGE. REPLACE AIRCRAFT 50 PIN CONNECTOR, PINS 34 AND 35. S-TEC 55X COMPUTER WAS REPAIRED BY S-TEC: MIDSDR FDEA201008123001Autothrottle Sys · malfunctionedIN PROFILE WITH BLUE SPEED LINE AT 290 THROTTLE WENT TO IDLE WOULD NOT HONOR SELECTED SPEED. IN LEVEL CHANGE NO PROBLEMS. AT 10000 FT PROFILE SELECTED SPEED BUG WENT TO 126 & THROTTLE TO IDLE. NO PROBLEM IN LEVEL CHANGE. CATEGORY: C EXPIRATION: 22AUG10 "MESDR ASAA1058114Flight Dir · malfunctionedFD (FLIGHT DIRECTOR) FAILURE FLAG ON PFD ON NR 1 SIDE. POWERED DOWN AIRCRAFT AND RESTORED POWER. FAULT CLEARED. PERFORMED OPS TEST REF AMM 22 11 00 740 801 DFCS OPS TEST. TEST SUCCESSFULLY PASSED.SDR VNAA2010072800012Unknown · malfunctionedCREW REPORTED AFTER ENGAGING AUTOPILOT THE AIRCRAFT ROLLS TO RIGHT. AIRCRAFT RETURNED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE CHECKED THE AUTOPILOT AND AILERON CONTROL SYSTEMS USING AIRCRAFT MAINTENANCE MANUAL. NO DEFECTS WERE NOTED AND AIRCRAFT WASSDR RU3A1018Unknown · malfunctionedTWO UNCOMMANDED ABRUPT RIGHT RUDDER INPUTS. AUTOPILOT ON. YAW DAMP ON. AIRCRAFT CLIMBING THROUGH 8000 FEET AT 250 KNOTS. SECOND EVENT 11000 FEET AT 250 KNOTS. NO SERVO MONITOR LIGHT ILLUMINATED. NO INDICATION OF JAM RUDDER. ALL THREE HYDRAULIC SYSTEM PRESDR ASAA1058097Unknown · malfunctionedRECEIVED "APPROACH WARNING" AT 150 FEET AGL WITH AUTO PILOT DISCONNECT AIRBORNE WINDS INDICATED APX, 10 KT X WIND IN CONJUNCTION WITH LIGHT TURB WAS NOT IDEAL CONDITIONS FOR APPROACH HOWEVER WITHIN TOLERANCE. DFCS FFR SHOW CH A AND CH B + FGN FCC DROPPED IN ASDR UALA2010072102611Control Panel · faultyVERTICAL SPEED WINDOW DOES NOT DISPLAY THE PLUS OR MINUS SIGN. REPLACED AUTOPILOT MODE CONTROL PANEL IAW MM, GROUND CHECKS NORMAL. ACP'D CAT III TEST IAW MM. ACFT RETURNED TO CAT III STATUS.SDR UALA2010071602554Control Panel · faultyC AUTOPILOT CMD LIGHT INOP. BACK LIGHTING FOR CMD INDICATION INOP. LIGHT BAR OPERATES NORMALLY. AIRCRAFT WILL REQUIRE CAT III CK AFTER RELAMPING. REPLACED AUTOPILOT MODE CONTROL PANEL (RELAMP NO HELP). ACP MCDP TESTS 4,30,40 & CAT 3 TESTS MM. ALL TESTS OKAY.SDR N6WA20100710ATrim System · malfunctionedSTAB TRIM RUNAWAY IN FLIGHT. DEFERED AUTOPILOT ON DMI 16728 CAT B APPROVED.SDR UALA2010070602402Control Panel · failedTHE MCP AIRSPEED INDICATOR, MCP HEADING SELECTOR & ALT SELECT KNOB ARE ALL INOP. REPLACED MODE CONTROL PANEL, OPS CHECK OKAY.SDR ASAA1058017Indicator · warning lightPRIOR TO PUSHBACK F/O FD FLAG CAME ON. CYCLED POWER F/O FD FLAG RESOLVED, OPS NORMAL.SDR 2011F00133Autopilot Sys · inoperativeDURING INSPECTION AUTOPILOT B WAS FOUND NOT ENGAGING IN ANY MODE. ALL RELEVANT LRU'S REPLACED BUT DEFECT PERSISTED.SDR ASAA1057978Unknown · malfunctionedDURING AUTO LAND AIRCRAFT TOUCHED DOWN 45 50 FT LEFT OF CENTERLINE. (NOTE) ILS CRITICAL ZONE WAS NOT PROTECTED. ACCOMPLISHED FIM TASK 22 11 00 810 825. LAND VERIFY TEST PER AMM TASK 22 11 00 700 801, OPS CHECK GOOD.SDR QXEA2010062100360Actuator · malfunctionedDURING CRUISE FLIGHT WITH AUTO PILOT ENGAGED, ACFT ROLLS LT AND RT APPROX EVERY 30-45 SECOND , ATTEMPTING TO MAINTAIN CRUISE. WHEN AUTO PILOT IS DISENGAGED, ACFT CONTINUES TO ROLL UNCOMMANDED MAINLY TO THE LT, APPROX EVERY 30-45 SECONDS. R & R ROLL ACTUATOR SDR UALA2010061402076Computer · faultyAUTOPILOT DISC LIGHT ON & EICAS MSG 'AUTOPILOT DISC' DISPLAYED WITH 2 AUTOPILOT SYS ENGAGED IN COMMAND (1=L, 2=C, 3=R). CREW COMMENTS: CTR AP INOP IN CRUISE WOULD NOT RESET LT AND RT AP OK: MCDP STORED FAULTS SHOWS NO INFC FCC CTR, CONFIRMED BY TEST. FCC C RSDR CA100605001Control Panel · failedCREW REPORTED UNABLE TO ENGAGE THE AUTO PILOT AND MODE CONTROL PANEL INTERMITTENTLY FAILS. CREW RETURNED TO BASE, MODE CONTROL PANEL REPLACED AND GROUND CHECKED SERVICEABLE IAW MM AND ACFT RELEASED.SDR UALA2010052801852Adc · failedAIRCRAFT HAS PITCH OSCILLATION (PORPOISES) WITH ANY AUTOPILOT IN COMMAND AND (V-S, ALT HOLD, VNAV, FLCH) MODE SELECTED. REPLACED LOWER RT ADC. PERFORMED THE FOLLOWING: HOOKED UP AIR DATA TESTER TO LT & RT ADC'S. APPLIED PRESSURE FOR 5000 FT & 250 KTS, THEN 15SDR ASAA1057875Unknown · malfunctionedA/C LANDED COMPLETE LEFT OF CENTERLINE. AUTO THROTTLE STARTED RETARDING AT 30 FT AGL. ACCOMPLISHED FIM TASK 22 11 825. NO FAULT HISTORY AND LAND VERIFY TEST GOOD.SDR ASAA1057831Unknown · malfunctionedHGS AIII/AUTOLAND UNSUCCESSFUL ON SEA RWY 16C. HAD HUD APPROACH WARNING AT 100FT. AIRCRAFT WENT SLIGHTLY BELOW GLIDESLOPE AND IN VFR CONDITIONS DID A NICE DID A NICE TOUCHDOWN AT 900' ON CENTERLINE. GROUNDED YES. NO FAULTS LOGGED IN DFCS ACCOMPLISHED LAND SDR 2010FA0000469Servo · out of toleranceRUDDER AUTO PILOT SERVO MOUNT SLIP CLUTCH COULD NOT BE ADJUSTED TO AMM LIMITS.SDR QXEA2010051100300Servo · bindingON SHORT FINAL, AT 500 AGL, HARD RT UNCOMMANDED V ROLL REQUIRING PILOT TO OVER POWER WITH HIGH CONTROL PRESSURE. AILERON TRIM INDICATOR ALWAYS NEUTRAL. AUTOPILOT OFF AT THE TIME, ACFT BEING HAND FLOWN. LANDING UNEVENTFUL. PERFORMED GVI OF ROLL CONTROL SYS/CABSDR UALA2010043001454Control Panel · faultyRIGHT A-T ARM SWITCH HAS FALLEN OFF. PANEL OUT OF TOLERANCE. R & R MODE CONTROL PANEL. OPS GOOD.SDR FDKA2010042800092Unknown · malfunctionedACFT ROLLED LEFT WITH AUTOPILOT FAIL A6. OPS CHECK SEVERAL TIMES, NO DEFECT NOTED.SDR A6WA201040304Unknown · malfunctionedWHILE WAITING TO CAPTURE GLIDE SLOPE, AP PITCHED UP 15 DEGREES, TURNED OFF AUTO PILOT AND RETUREND TO NORMAL FLIGHT. REENGAGED AP AND AP FUNCTIONED NORMALLY. PERFORMED ELEVATOR SERVO SPIN TEST IAW AMM 22-11-00. SERVO SPIN TEST GOOD AT THIS TIME, AUTOPILOT RSDR V2JA149Controller · failedDURING CLIMBOUT, AUTOPILOT CONTROLLER FAILED WITH ODOR IN COCKPIT.SDR 2010FA0000458Lever · bindingAT START OF APPROACH, DISENGAGED AUTO-PILOT BUT FOUND CONTROLS AND TRIM STIFF OR JAMMED. COMMANDED AUTO-PILOT DISCONNECT AGAIN BUT NO CHANGE. TRIED ELECTRIC TRIM ALSO BUT WITHOUT CHANGE AND GOT NO TRIM MOTION. THEN SAW THAT AUTO-PILOT ENGAGE LEVER HAD NOT MSDR FDKA2010032500048Switch · unknownRUDDER PEDALS WILL NOT MOVE. DIS-ENGAGED YAW DAMPER SWITCH, OPS CHECK GOOD.SDR ASAA1057555Autoland Sys · malfunctionedAPP SURVEY AUTO LAND UNSUCCESSFUL. PERFORMED AUTO LAND VERIFY TEST PER MM 22 03 10/101. ALL TESTS PASSED. A/C REMAINS CAT IIIA AUTO LAND QUALIFIED.SDR ASAA1057533Autopilot Sys · malfunctionedAUTOLAND PERFORMED 'FLARE' NOT ANNUNCIATED AT 500 AFL. AUTOPILOTS DID NOT DISENGAGE AT 350 FEET. FLARE WAS ANNUNCIATED AT APPROX 100 FEET AND ACFT FLARED PROPERLY. FLT FAULT REVIEW / CURRENT STATUS LOGGED NO FAULTS. REF FIM TASK 22 11 TASK 801. LAND VERIFSDR ASAA1057509Actuator · malfunctionedTHE "A" AUTOPILOT DISENGAGES WHEN SELECTED IN COMMAND MODE (FAULT CODE 221-080-00). ACFT GROUNDED. REPLACED AUTOPILOT ELEVATOR ACTUATOR 'A' (M1020) IAW AMM 22-11-26 PAGE BLOCK 401. ACCOMPLISHED LEAKS CHECK AND AUTOPILOT ELEVATOR ACTUATOR TEST ARE GOOD.SDR ASAA1057479Sensor · faultyAUTOPILOT ELEVATOR POSITION SENSOR AND NEUTRAL SHIFT SENSORS REQUIRE ADJUSTMENT. ADJUSTED ELEVATOR POSITION SENSOR REF MM 22 11 30 AND NSS REF MM 22 11 14. GROUND FUNCTIONAL TEST GOOD REF MM 22 11 00. BITE TEST GROUP 47 GOOD. PITCH SENS LRU REPLACEMENT TESSDR HALA2010022300074Autopilot Sys · malfunctionedETOPS SIGNIFICANT SYSTEM, ATTEMPTED AUTO LAND IN PDX ILS 10R AFTER GS INTERCEPT AIRCRAFT STARTED PITCHING SMALL AT FIRST THEN LARGER AMBER LINE APPEARED THROUGH GLIDE SLOP WINDOW ON THE FMA AUTOPILOT DISCONNECTED. T/S PER FIM 22-00-02-1 FAULT ISOLATION LAST FSDR SROM20100001Autopilot Sys · disconnectedSPEED TRIM FAIL LIGHT ILLUMINATED AND YAW DAMPER WON'T ENGAGE DURING TAKEOFF. MADE UNEVENTFUL RETURN TO DEPARTURE AIRPORT. PERFORMED YAW DAMPER SYS TEST IAW AMM 22-23-00, NO DEFECTS NOTED. PERFORMED DFCS BITE PROCEDURE AND DFCS ADJUSTMENT/TEST IAW AMM 22-11-SDR ASAA1057375Unknown · malfunctionedDURING 30 DAY EVAL AUTOLAND WAS UNUSUALLY FAR TO THE LEFT OF CENTERLINE, ABOUT HALF WAY BETWEEN CENTERLINE AND RUNWAY EDGE. SLIGHT TAILWIND (040/6) AND GROUND CONTROLLER VERIFIED PROTECTED AREA WAS CLEAR. AUTOTHROTTLES SEEMED TO LAG TO IDLE AND A/C "HUNTED" SDR HDNA201002120001Software · defectiveAFTER DEPARTURE, WITH THE AUTO PILOT COUPLED AND CLIMBING THRU 1500 FT. IN A LEFT TURN, THE YAW DAMP HAD A HARD OVER TO THE LEFT AND DISENGAGED THE AUTO PILOT. THE AUTO PILOT AND YAW DAMP FAILED TO RE-ENGAGE. THE AIRCRAFT LANDED WITHOUT INCIDENT. AFTER LENGSDR USAA20100211BB007Unknown · malfunctionedGIG FLT 801 EN ROUTE GIG TO CLT. ON TAKEOFF, MAP DID NOT REALIGN. NO AUTO THROTTLES. NO VNAV. NO LNAV. CENTER AUTOPILOT WOULD NOT ENGAGE. NO NAV UPDATES. EMER EXIT LIGHTS ILLUMINATED IN CABIN IN ARMED MODE. COULD NOT CONTROL CABIN OR COCKPIT TEMP. ASDR ASAA1057333Unknown · malfunctionedDURING AUTOPILOT APPROACH BOTH AUTOPILOTS ENGAGED BUT "SINGLE CHANNEL" ANNUNCIATED ON BOTH EADI'S. COULD NOT DUPLICATE. DFCS FAULT REVIEW LOGGED FCC "A" DROPPED IN APP FAULT NR 22 11414 FOR RELATED FLT LEG ONCE. PERFORMED DFCS CURRENT STATUS CK LRU FCC TEST SDR MYWA100037Servo · inoperativeETOPS SIGNIFICANT SYSTEM - AUTOPILOT COMMAND A AND B WILL NOT HOLD ALTITUDE OR SPEED COMMAND.SDR MYWA100038Unknown · malfunctionedETOPS SIGNIFICANT SYSTEM - SPEED TRIM FAIL LIGHT ILLUMINATED SEVERAL TIMES IN FLIGHT.SDR MYWA100036Autopilot Sys · malfunctionedETOPS SIGNIFICANT SYSTEM - AUTOPILOT COMMAND A AND B WILL NOT HOLD ALTITUDE OR SPEED COMMAND.SDR IPXA10158259Computer · faultedEMERGENCY DECLARED - WHILE IN CRUISE, NAV MODE FAILED SEVERAL TIMES REVERTING TO HDG MODE. T/S IN REF TO TSM 2-10-00 AND AMM 22-40-00-05, FOUND FCU FAULTED, REMOVED AND REPLACED FCU IN REF TO AMM 22-15-12-04 AND TESTED IN REF TO 22-00-00 P BLOCK 501 AND 22-40-SDR SWIA201023501Servo · malfunctionedFLT 6488 - RUDDER TRIM FROZE ON DESCENT, PEDALS WORKED NORMAL. REPLACED RUDDER AUTOPILOT SERVO AND RUDDER TRIM ACTUATOR.
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