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 ASAA0954633Autoland Sys · malfunctionedCAT III APPROACH AND AUTOLAND. AIRCRAFT LANDED OUT OF LIMITS TO LEFT SIDE OF RUNWAY. GP NR 20 FFR OF DFCS A & B & HGS SHOWS NO FAULTS LAST FLT. GP NR 49 LAND VERIFY OF DFCS PASSES. HGS SYS TEST PASSES REF MM 34 36 00. A/C REMAINS CAT IIIA AUTOLAND & HGS QSDR V2JA132Autopilot Sys · malfunctionedAT FL300 CREW BEGAN TO NOTICE SMOKE COMING FROM INSTRUMENT PANEL.SDR SWIA200921050Servo · out of adjustFLT 5912 - HEAVY CONTROL FORCES ON ELEVATOR ON LANDING FLARE AND ON TAXI IN. ADJUSTED ELEVATOR SLIP CLUTCH AND REPLACED ELEVATOR SERVO.SDR UALA2009031000284Servo · unreliable2 YAW DAMPER DISPLAYED ON EICAS & YAW DAMP INOP LIGHT ON (1=L, 2=R). CREW COMMENTS: R YAW KICKED OFF. REPLACED YAW DAMPER SERVO RT. OPS CHECK GOOD.SDR UALA2009012600284Servo · unreliableTWO YAW DAMPER DISPLAYED ON EICAS & YAW DAMP INOP LIGHT ON (1=L, 2=R). CREW COMMENTS: R YAW KICKED OFF. REPLACED YAW DAMPER SERVO RT. OPS CHECK GOOD.SDR ASAA0954298Unknown · malfunctionedHGS/AUTOLAND 30 DAY CHECK UNSUCCESSFUL. ALL SYSTEMS ON HGS AND A/L WORKED NORMALLY EXCEPT ACFT FLARED AND TOUCHED DOWN 55 FEET LT OF CENTERLINE. WINDS WERE CALLED AT 12KTS LT CROSSWIND. GROUNDED YES. CHECKED. NO HISTORY. FFR GP NR 2O SHOWS NO FAULTS "A" OSDR ASAA0954297Autopilot Sys · malfunctionedDURING THE FLARE THE APCH WARNING CAME ON BOTH THE FO'S PANEL LIGHTS AND THE CAPT'S HUD. THE RWY EDGE LINES ON THE HUD DID NOT ALIGN WITH THE RWY EDGE AND THE A/C VEERED OFF SHARPLY TO THE LT DISCONNECTED THE A/P AND LANDED MANUALLY. GROUNDED YES. DFCS LOGGSDR ASAA0954261Unknown · malfunctionedAUTOLANDED ON RWY 16R. ALL GOOD UNTIL FLARE ACFT DRIFTED TO THE LT AND TOUCHED DOWN APPROX 35' LT OF CENTERLINE WINDS CALM. GROUNDED YES. REF FIM 22 11 TASK 801 AND 22 11 TASK 825. NO FAULTS LOGGED ON EITHER FCC LAST FLT. LAND VERIFY CHK NR 49 BITE REF. 22SDR ASAA0954246Computer · faultedSINGLE CHANNEL "SPEED TRIM FAIL" ON APPROACH. GROUNDED YES. FOUND DUAL CHANNEL FAULT. WOULD NOT RESET. RE RACKED FCC NR 1 AND NR 2. OPS CK NORMAL PER FIM TASK 22 11 TASK 801.SDR HALA2009011700026Computer · failedETOPS SIGNIFICANT SYSTEM, ATB, LEFT FMC FAIL LIGHT EICAS MSG ILLUMINATED APPROX 1 HR INTO FLIGHT. AUTOPILOT, AUTOTHROTTLES DISENGAGED 15 MIN LATER. RT FMC EICAS FAIL LIGHT ILLUMINATED. REMOVED AND REPLACED TMC PER AMM 22-31-01. REMOVED AND REPLACED CENTER SDR ASAA0954245Autoland Sys · malfunctionedAUTOLAND PERFORMED ON RWY 16R. ACFT LANDED APPROXIMATELY 30 FT LT OF CENTERLINE. GROUNDED YES. PERFORMED FIM 22 11 TASK 825 LAND VERIFY TEST AMM TASK 22 11 00 700 801 ACCOMPLISHED WITH NO DISCREP. OPS CHK GOOD. ACFT APPROACH SURVEY COMPLETED ON D/P 664601SDR 2009FA0000424Bearing · damagedPILOT REPORTED PITCH OSCILLATIONS WITH AUTOPILOT ENGAGED. AUTOPILOT WAS DISENGAGED MANUALLY, AND ACFT WAS HAND FLOWN TO DESTINATION. AUTOPILOT COMPUTER, PITCH SERVO, AND FLIGHT COMMAND INDICATOR REMOVED AND SENT OUT FOR BENCH TEST. FLIGHT COMMAND INDICATOR SDR AALA2009010700153Accelerometer · failedORD INFLIGHT - AFTER TAKEOFF CREW REPORTED AUTO THROTTLE AND AUTO PILOT WERE INOPERATIVE. CAPTAIN ELECTED TO RETURN TO ORD. LANDED ORD WITHOUT INCIDENT. REPLACED BOTH ACCELEROMETERS. SYSTEM GROUND CHECKED NORMAL OPERATION.SDR FDEA200901060046Computer · malfunctionedAT FL320 APPROX 40 MIN INTO FLT A/P 2 EXECUTED A SLOW UNCOMMANDED CLIMB TO FL 325. PRIOR TO PUSHBACK HAD LVL 2 FCC 2A & 2B DATA FAULT. STN MX RESET C/BS & ALERTS WENT AWAY. SWITCHED TO A/P 1 FOR REMAINDER OF FLT WITH NO FURTHER PROBLEMS. ADDITIONAL INFO ONSDR DXTA2009010303463Control Unit · inoperativeDURING CRUISE AP A FAIL CAS MESSAGE POSTED FOLLOWED 30 SECONDS LATER BY AP B FAIL CAS MESSAGE. BOTH MESSAGE REMAINED ON THE RESET OF THE FLIGHT REVIEWED CDMS FAULTS, FOUND PITCH TRIM FAULT ON LAST FLIGHT. REMOVED AND REPLACED HORIZONTAL STAB TRIM CONTROL UNISDR DXTA200901033462Control Unit · inoperativeDURING CRUISE, AP A FAIL CAS MESSAGE POSTED FOLLOWED 30 SECONDS LATER BY AP B FAIL CAS MESSAGE. BOTH MESSAGES REMAINED ON THE RESET OF THE FLIGHT REPEAT WRITE-UP. REVIEWED CDMS FAULTS, FOUND PITCH TRIM FAULT ON LAST FLIGHT. REMOVED AND REPLACED HORIZ STAB SDR ASAA0954130Sensor · out of adjustAUTOLAND APP TO 7L: ACFT LANDED APPROX 55 FT LT OF CENTERLINE. CALM WINDS. GROUNDED YES. FOUND SPOILER 9 POSITION SENSOR OUT OF ADJUSTMENT AND ADJUSTED SENSOR REF MM 22-11-27. OPS NML IAW SAME. ILS SYS OPS NML REF MM 34-31-00. LAND VERIFY TEST NML REF MM 22-11SDR HNAA2009010300375Resistor · blownRAMP PEOPLE ADVISED THAT POWER ON ACFT FLUCTUATED WHILE CLEANING ACFT AND THERE WAS BURNING SMELL. CONTRACT MX CONFIRMS SMELL IS FROM LT AUTOPILOT DISENGAGE LT AND AUTOPILOT DISENGAGE LT CIRCUIT BREAKER POPPED. FOUND RESISTOR ON AUTO PILOT DISENGAGE BOARD BLOWSDR HALA2009010300001Autopilot Sys · malfunctionedOPEN - ETOPS SIGNIFICANT SYSTEM - ATB: UNABLE TO SELECT RT AUTO PILOT, WHEN SELECTOR VNAV FAILURE WAS INDICATED IN FMA AND AUTO PILOT WOULD NOT ENGAGE. FERRIED ACFT TO PAE FIELD. REPAIR IN WORK.SDR DXTA2009010503462Autopilot Sys · malfunctionedDURING CRUISE AP A FAIL CAS MSG POSTED FOLLOWED 30 SECONDS LATER BY AP B FAIL CAS MSG.SDR QXEA2009010500001Yaw Damper · unknownACFT WAS EXPERIENCING A SLIGHT NOSE LT NOSE RT OSCILLATION DURING CLIMB AND CRUISE. PFCS SHOWED MINOR OSCILLATIONS OF RUDDER ALSO. TURNING OFF YAW DAMPER, RIGHT TO LEFT MOVEMENT OF ACFT STOPPED . PERFORMED OPS TESTS OF THE YAW DAMPER ACTUATOR IAW AMM TASK 2SDR DXTA200901020345AAutopilot Sys · oscillatesDURING DESCENT, AUTOPILOT BEGAN TO OSCILLATE.SDR DXTA2008122303420Autopilot Sys · malfunctionedWHILE ADVANCING THROTTLES ON APPROACH AUTOPILOT KICKS OFF, FLIGHT DIRECTOR REVERTS TO GO AROUND MODE.SDR DXTA2008122003418Actuator · lack of lube22-1 AUTO PILOT DISENGAGED 5 SECONDS AFTER SELECTING FLAPS TO 15 DEGREES. AUTO PILOT FAIL AMBER LIGHT SHOWED ON PFD'S. SEEMED LIKE AUTO PILOT TRIM COULD NOT KEEP UP. LUBRICATED ELEVATOR TRIM ACTUATORS AND COMPLIED WITH A SATISFACTORY OPS CHECK OF THE ELEVATORSDR DXTA2008122008034Autopilot Sys · failedAUTO PILOT DISENGAGED 5 SECONDS AFTER SELECTING FLAPS TO 15 DEGREES. AUTO PILOT FAIL AMBER LIGHT SHOWED ON PFD'S. SEEMED LIKE AUTO PILOT TRIM COULD NOT KEEP UP. LUBRICATED ELEVATOR TRIM ACTUATORS AND COMPLIED WITH A SATISFACTORY OPS CHECK OF THE ELEVATOR TSDR DXTA2008122203414Autopilot Sys · malfunctionedON DESCENT THE RUDDER BOOST FAILED. AUTO PILOT DISCONNECTED & COPILOTS FD FAILED.SDR UALA2008121906920Computer · failedAUTOPILOT FAILURE. FLT DIVERTED. SUPPLEMENTAL DATA UPDATE FOUND MULTIPLE INFC FAULTS AND CENTER FCC FAILED. CTR FCC PULLED DOWN INTERCONNECT BUS. REPLACED CENTER FLIGHT CONTROL COMPUTER AND CHECKS OK.SDR DXTA2008121603404Autopilot Sys · inoperativeAUTOPILOT INOP. REMOVED AND REPLACED BOTH FCC CARDS. COMPLIED WITH AN AUTOPILOT FUNCTIONAL CHECK IAW THE AMM 22-100 WITH NO DISCREPANCIES NOTED. 2ND CARD REPLACED WAS AS FOLLOWS: LIGHT CONTROL COMPUTER 822-0327-508 SN FX9H HRS 5.4 CYCLES 7.0.SDR DXTA2008121503403Autopilot Sys · unknownAFTER DEPARTING, THE AP FAIL B MESSAGE FLICKERED THEN ILLUMINATED SOLID. TROUBLESHOT AUTOPILOT SYS USING DIAGNOSTIC MX SYS. NO FAULTS FOUND SYSTEM CHECKS GOOD IAW MM 45-40-00.SDR DXTA2008121603403Autopilot Sys · malfunctionedAFTER DEPARTING CMH THE AP FAIL B MSG FLICKERED THEN ILLUMINATED SOLID.SDR HALA2008121300889Computer · malfunctionedETOPS SIGNIFICANT SYSTEM - ATB - VNAV/LNAV WOULD NOT ENGAGE WITH CENTER AUTOPILOT ENGAGED. CAPTAIN SPEED LIMIT INOP DISPLAYED ON CAPTAINS ADI. REPLACED NR 1 FMC. GND OPS CHK OK AMM 34-61-02. ACCOMPLISHED MCDP TEST 30 TEST PASS A/C OK TO REMAIN AT LMP STATUSDR A6WA200840640Autopilot Sys · malfunctionedAFTER TAKEOFF FROM WET RUNWAY, CLIMBED TO FL320 IN RAIN/SNOW. TEMP -48`C IN CRUISE. WHILE MAKING LT TURN, WITH AP, RECEIVED LT WING DOWN AUTOPILOT TRIM CAUTION MSG MOMENTARILY. PERFORMED VISUAL INSP AILERON SYS FROM BULKHEAD TO AILERONS WHILE OPERATING THE SDR IXXA080036OComputer · defectiveDURING CLIMB-OUT OF KTOL WITH RUDDER POWER ON, YAW DAMPER ON AND AUTO PILOT ON THE RUDDER HAD A LEFT RUDDER INPUT. THE CREW TURNED THE AUTO PILOT OFF AND THE CONDITION REMAINED, TURNED THE YAW DAMPER OFF AND NO CHANGE. THE LEFT INPUT WENT AWAY ONLY WHEN RUDDSDR UALA2008120106689Fcu · faultyAUTOPILOT ISSUES. FLIGHT DIVERTED. AUTO FLT 'FCU 1+2 FAULT' DISPLAYED ON UPPER ECAM SCREEN. CYCLED CB B5 AND M21 AND FCU CHANNEL 1 RECOVERED BUT FCU CHANNEL 2 REMAINED INOP. REPLACED FCU.SDR QMLA1127200808055Actuator · inoperativeON SHORT FINAL AT STOUGHTON HOSPITAL HELIPAD CAUTION LIGHT ILLUM AND CAD INDICATED YAW SAS AND ACTUATION LIGHTS WITH A CORRESPONDING AMBER "Y" ON THE PFD. INITIATED A GO AROUND. AS POWER WAS APPLIED THE MASTER WARNING PANEL ILLUMINATED AND THE AP A. TRIM LIGHTSDR ASAA0853886Control Panel · burnedDIGITAL COURSE WINDOW (CAPT'S) HAS A BURN SPECK IN IT. VERIFIED BURN SPECK ON CAPTS COURSE WINDOW. REPLACEMENT MODE CONTROL PANEL P/N VERIFIED BY SEAMC ROB. REMOVED AND REPLACED MCP REF AMM 22 11 34/401. ACCOMPLISHED LRU PELACEMENT TEST GRP NR 32 LAND VERISDR SWIA200820511Actuator · bindingFLT 2626 - AILERON CONTROL EXTREMELY DIFFICULT TO MOVE. REPLACED AILERON SERVO ACTUATOR, PN 622-4404-101, SN ON 1284, SN OFF HX6P.SDR DL738081540Accessory Unit · failedF/O FLT DIR WOULD NOT DISPLAY PITCH BAR EVEN W/CA SIDE INFO CA'S OK. FOUND C/B AFCS SYS B SNSR EXC AC BREAKER POPPED. RESET C/B PERFORMED TEST PER MM ON IFSAU. ACC TEST NORMAL REPLACED INTEGRATED FLT SYS ACC UNIT SYSTEM TEST NORMAL AS PRECAUTIONARY MEASURE SDR CA081117005Circuit Board · intermittent(CAN) ACFT IN NORMAL CLIMB CONFIGURATION WITH FCS DISPLAYING CLIMB (GREEN) AND ALT ARM (WHITE.) THE VERTICAL MODE DISPLAY MAY THEN CHANGE TO ALT (GREEN) EVEN THOUGH THE TARGET ALTITUDE IS SEVERAL THOUSAND FT ABOVE (E.G. WITH THE ALT SELECT SET FOR 20,000 FEET,SDR DXTA2008111003342Computer · malfunctionedFL390 AP/FAIL, ATT FAIL, HDG FAIL COPILOTS SIDE STBY HSI FAIL. YAW DAMP WOULD NOT RE-ENGAGE. WHEN PUSHING TCS BUTTON FOR FLIGHT DIRECTOR AP FAIL LIGHT WOULD ILLUMINATE AND COULD BE EXTINGUISHED BY PRESSING AP DISCONNECT BUTTON. REMOVED AND REPLACED NR 2 AHRSDR 08FDEA04699Warning Light · false activationAT 250' ON AN ACTUAL CAT3 APPROACH GOT RED AUTOLAND FLASHING LIGHT ALL PARAMETERS APPEARED NORMAL. EXECUTED A GO AROUND. PERFORMED A FAULT ISOLATION PROCEDURE AND A AFS LAND TEST PER AMM 22-42-00-0. NO FAULTS WERE RECORDED ON DISPLAY OR TRIFOLD FAILURE RESDR DXTA2008110403335Autopilot Sys · malfunctionedAUTOPILOT CAME OFF 3 TIMES INFLIGHT. IT KICKED OFF TWICE ON CLIMB OUT AND ONCE AT LEVEL OFF. NO TRIM MISCOMPARE OR HEAVY CONTROL FORCES, NO ANNUNCIATORS. RAN DIAGNOSTIC CHECK IAW MM 34-60-00. NO CURRENT AUTOPILOT FAULTS NOTED. AUTOPILOT SYS OPS CHECK GOOD ISDR QMLA1101200808048Computer · intermittentPILOT REPORT - DURING A FLIGHT TO SAINT FRANCIS HOSPITAL, THE AIRCRAFT BEGAN TO HAVE VERY STRONG UNCOMMANDED YAW INPUTS. THE PILOT DISENGAGED THE YAW CSAS BUT STILL FELT WHAT HE THOUGHT WAS UNCOMMANDED YAW INPUTS. BOTH ENGINES INDICATED NORMAL. THE PILOT THSDR UALA2008112006574Relay · faultyNO LAND 3 DEGRADATION IN AUTOLAND SYS PRIOR TO APPROACH (BEFORE LAND 3 AUTOLAND STATUS ANNUNCIATION). AUTOLAND SYS IS NO LONGER FAIL-OPERATIONAL. ADVISORY MSG01- ACTIVE CRUISE MODE DEPENDENT; BUS ISOLATION IS NOT AVAILABLE. DB- AUTOPILOT FLIGHT DIRECTOR COMPUSDR 2008FA0000727Autopilot Sys · unknownFLIGHT FROM SDL TO TUL, DIVERT TO ABQ. AUTOPILOT DISENGAGED VIOLENTLY AT 410 AND YD OFF. REFER TO QRH RESET CB. AUTOPILOT BACK ON AT 390. 40 SECONDS LATER, AUTOPILOT AND YD DISENGAGED. UNABLE TO RESET CB. FL 370 AUTOPILOT BACK ON AND 30 SECONDS LATER DISESDR DXTA2008102003310Autopilot Sys · malfunctionedAT 14000FT AND AT 280 KTS WITH AP/FD SELECTED TO LEFT SIDE, RIGHT SIDE ONLY AP PITCH TRIM FAIL LIGHT CAME ON.SDR DXTA200810173310Controller · inoperativeAT 14000' AND AT 280 KTS WITH AP/FD SELECTED TO LEFT SIDE, RIGHT SIDE ONLY AP PITCH TRIM FAIL LIGHT CAME ON. DISENGAGED AP, NO TRIMMING WAS REQUIRED, AND LIGHT WENT OUT. RE-ENGAGED AP AND SAME THING HAPPENED. REMOVED NR 2 FCC-4007, INSTALLED OVERHAULED FCC-4SDR DXTA2008101703308Autopilot Sys · malfunctionedAUTOPILOT DISCONNECTED 6 TIMES IN 30 MINUTES.SDR UIEA200800336Computer · failedWHEN "A" AUTOPILOT ENGAGED AIRCRAFT STARTED UNCOMMANDED LEFT ROLL. DISENGAGED "A". "B" WOULD NOT ENGAGE. CYCLED YOKE SWITCHES AND YOKES NEITHER WOULD ENGAGE. FINALLY GOT "B" TO ENGAGE BUT IT WOULD NOT FOLOW ANY COMMANDS. REPLACED "A" CHANNEL CCA IAW 22-13-02. SDR UIEA200800332Autopilot Sys · malfunctionedAIR TURNBACK, WHEN A/P "A" IS ENGAGED THE AIRCRAFT STARTED UNCOMMANDED LEFT ROLL. DISENGAGED "A" A/P. "B" A/P WOULD NOT ENGAGE. CYCLED YOKE SWITCH NIETHER "A" OR "B" A/P WOULD ENGAGE. FINALLY GOT "B" TO ENGAGE BUT IT WOULD NOT FOLLOW ANY MODE CONTROL PANEL
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