JASC 2210

Service difficulty reports · 4,019

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.

SDR CA051103005Adapter · faulty(CAN) AUTO PILOT TRIPPED OFF LINE. RED TRIM ANNUNCIATOR ILLUMINATED ON MODE CONTROLLER. FLIGHT DIRECTOR WAS FUNCTIONING NORMAL. ALL ELECTRIC TRIMS FUNCTIONING NORMAL. AUTO PILOT WOULD NOT TEST, THEREFORE NOT ENGAGE. PITCH TRIM ADAPTER FOUND AT FAULT.Oct 29, 2005 · Pilats PC1245SDR DJFA2005155Autopilot Sys · malfunctionedWHEN CREW SELECTED VERTICAL SPEED ON MODE CONTROL PANEL TO BEGIN DESCENT, AC BEGAN STEEP CLIMB, AIRSPEED INDICATOR WAS NEAR BARBER POLE. CONTROL COLUMN YOKE WAS PUSHED FWD TO REDUCE CLIMB. AC FOUGHT CREW BY TRIMMING AC FURTHER NOSE UP. CLIMB WAS REPORTED TOct 24, 2005 · N861CW · Braero BAE125800ASDR PIDA20050179Yaw Damper · malfunctionedYAW DAMPER TRIPS OFF ON GROUND ONLY WHEN WIDE TURNS ARE MADE WITH TILLER OR RUDDER. PLACED ON MEL 22-3-1B.Oct 21, 2005 · N250TR · Boeing 7372K5SDR PIDA20050178Actuator · leakingHYDRAULIC FLUID ON LINES AT AUTO PILOT ACTUATOR -B- IN LEFT WHEEL WELL. REPLACED -B- SYSTEM AUTO PILOT ACTUATOR PER MM 22-11-251.Oct 17, 2005 · N251TR · Boeing 737228SDR SWIA200515681Computer · malfunctionedYAW DAMP 1 INOP STATIS MSG. REPLACED NR 1 AND NR 2 FCC CARDS IAW CRJ 200 MM 22-12-14, OPERATIONAL CHECK GOOD, PN OFF 622-9815-704, SN1 OFF: 10BMP, SN2 OFF: 09RWOct 12, 2005 · N929SW · Cndair CL6002B19SDR PIDA20050175Control Panel · malfunctionedAIRSPEED IN THE IAS/MACH WINDOW IS FROZEN IN PLACE AND CANNOT BE MANUALLY SET. REPLACED MODE CONTROL PANEL PER MM 22-11-01.Oct 11, 2005 · N371PA · Boeing 737306SDR PIDA20050173Yaw Damper · failedYAW DAMPER WILL NOT ENGAGE. PLACED YAW DAMPER ON MEL 22-3-18.Oct 9, 2005 · N250TR · Boeing 7372K5SDR BB05088Module · malfunctionedFLIGHT 43, AMS-PHL - ON CLIMB-OUT FROM AMS, AILERON LOCKOUT AND RUDDER RATIO EICAS MESSAGES DISPLAYED. DIVERTED TO LGW. RESET LEFT AND RIGHT SAM MODULES AND LEFT RUDDER RATIO CHANGER MODULE. NO FURTHER FAULTS NOTED.Oct 9, 2005 · N648US · Boeing 767201SDR PIDA20050170Control Panel · malfunctionedMCP COURSE DISPLAY SKIPS NUMBERS. REPLACED MODE CONTROL PANEL PER MM 22-01-00. GROUND OPS CHECKS GOOD.Oct 8, 2005 · N390WL · Boeing 7373G7SDR HNAA0500087Controller · jammedROLL CONTROL JAMMED 10 MILES OUT ON APPROACH, CREW SPLIT YOKES IAW CHECK LIST AND CAPTAINS SIDE FREED. FIRST OFFICER STAYED JAMMED UNTIL JUST BEFORE TOUCH DOWN. CAPTAIN CONTROLLED AIRCRAFT WITH SPOILERS. INSPECTED ROLL CONTROL FOR JAMMING AND BINDING OPS NOOct 6, 2005 · N935HA · Dhav DHC8102SDR PIDA20050174Actuator · malfunctionedALTITUDE OCCASIONALLY CLIMBS 300 FEET WITH STAB OUT OF TRIM LIGHT (LEAVES FLIGHT DIRECTOR). REPLACED AUTO PILOT STAB TRIM ACTUATOR PER MM 22-11-81. OPS CHECKS GOOD PER MM 22-11-81.Oct 5, 2005 · N371PA · Boeing 737306SDR PIDA20050163Control Panel · malfunctioned"B" AUTO PILOT CMD WILL NOT ENGAGE WITHOUT PAUSING IN CWS AND "A" AUTO PILOT WILL NOT ENGAGE (INTERMITTENT). REPLACED MODE CONTROL PANEL PER MM 22-11-34. BITE TEST ACCOMPLISHED SATISFACTORY.Oct 5, 2005 · N371PA · Boeing 737306SDR Z1RA106192Transducer · intermittentDURING FLIGHT AL-300 DISPLAYS 1E30 CODE INTERMITTENTLY.Sep 26, 2005 · N761AF · Skrsky S76CSDR WRNA200500021Indicator · failedFLIGHT DIRECTOR FAIL FLAG IN VIEW ON CAPT ADI WHEN FLT DIR 1 OR FLT DIR 2 SELECTED. FLT DIR CMD BARS BIAS OUT OF VIEW. F/O ADI GYRO FAILED, UNABLE TO TRANSFER ATTITUDE INFO WITH INSTRUMENT SWITCHING. GYRO FLAG IN VIEW. BOTH LOGIC COMPUTER TRI-FOILS IN VIEWSep 16, 2005 · N820SC · Airbus A300B4203SDR AMCR200500008Switch · separatedDURING CLIMB, CREW COULD NOT ENGAGE AUTOPILOT. DURING HAND FLYING, CREW GOT SEVERAL UNCOMMANDED GO-AROUND COMMANDS IN WHICH COMMAND BARS WOULD POP-UP AND THROTTLES WOULD ADVANCE TO FULL POWER. MX FOUND THE BODY OF GO-AROUND SWITCH HAD SEPARATED WHICH CAUSED Sep 15, 2005 · N522AC · Gulstm GIVSDR VTZA200500180Autopilot Sys · malfunctionedUNCOMMANDED LT ROLL WITH AUTOPILOT ENGAGED. INTERROGATED FCC FOR FAULTS, FOUND NO DEFECTS. PERFORMED YAW DAMP COMMAND AND FEEDBACK TEST W/ NO DEFECTS NOTED REF FIM 22-11-00. PERFORMED AILRON/ELV SERVO SPIN UP TEST, FOUND NO DEFECTS AT THIS TIME REF FIM 22-2Sep 12, 2005 · N623BR · Cndair CL6002B19SDR P5CA0501393Computer · inoperative"A" AUTOPILOT ALT HOLD INOP. "B" AUTOPILOT ON DEFERRAL WILL NOT ENGAGE. REPLACED "A" PITCH COMPUTER PER MM 22-12-01. DMI CONTINUES.Aug 23, 2005 · N355MC · Boeing 747341SDR PIDA20050066Autopilot Sys · malfunctionedCENTER AUTO PILOT PITCHES NOSE DOWN WHEN ENGAGED. PLACED ON MEL 22-10-1.Aug 22, 2005 · N757BJ · Boeing 757236SDR DXTA200500911Warning Light · illuminatedAFTER TAKEOFF RED AP PITCH TRIM FAIL LIGHT CAME ON AND AP KICKED OFF. AIRCRAFT CHECKLIST COMPLETED AND LANDED AS SOON AS PRACTICAL. ITEM IS UNDER INVESTIGATION.Aug 21, 2005 · N140QS · Beech 400ASDR DXTA200500907Circuit Card · malfunctionedDURING T/O ROLL AT 70-80 KIAS OVERSPEED TONE ACTIVATED MOMENTARILY. REMOVED AND REPLACED NR 2 FCC CARD IAW HAWKER 400XP MM CH 22-13-00.Aug 19, 2005 · N108QS · Beech 400ASDR DXTA200500913Autopilot Sys · malfunctionedARRIVING 180 KNOTS, AUTO-PILOT REPEATEDLY CAME OFF-LINE. ELEV FELT HEAVY ON CONTROLS. AT 140 KNOTS, PRIMARY TRIM WOULD NOT WORK. NO CAS MESSAGES RECEIVED EXCEPT WHEN SECONDARY TRIM ARMED. SECONDARY TRIM NOT ATTEMPTED. DOWNLOADED FAULT HISTORY FROM IAC NR 1&Aug 18, 2005 · N913QS · Cessna 750SDR ASMF200508006Computer · failedAIRCRAFT RETURNED OF FLIGHT, BOTH DFGC OUT OF SERVICE. THE DFGC RTC BITE WERE PERFORMED IAW MM 22-01-05, TESTED CORRECT. THE OVERWEIGHT LANDING CHECK WAS PERFORMED IAW MM 05-51-04, ALL CORRECT. DURING OVERNIGHT CHECK, BOTH DFGC TESTS WERE PERFORMED IAW MM 22-0Aug 15, 2005 · N945AS · Doug MD83SDR SWIA200515439Servo · bindingROUGHNESS IN CONTROL YOKE WHEN MOVING AILERONS FROM CENTER TO THE LT. REPLACED AILERON AUTO-PILOT SERVO IAW 22-10-05. OPERATIONAL CHECK GOOD.Aug 15, 2005 · N236SW · Emb EMB120ERSDR PIDA20050064Servo Valve · inoperativeCENTER AUTOPILOT INOP, WILL NOT ENGAGE IN FLIGHT. PLACED ON MEL 22-10-1. 08/21/2005, REPLACED CENTER SYSTEM AILERON SERVO VALVE. OPS CHECKS GOOD PER MM 22-13-04.Aug 14, 2005 · N757BJ · Boeing 757236SDR 08152005CServo · malfunctionedDURING COUPLED ILS APPROACH YELLOW ELV LIGHT ON EADI FOLLOWED BY YOKE VIBRATION AND A STRONG RATTLING SOUNDED UNDER CAPT'S FLOORBOARD. PERFORMED OPERATIONAL CHECK OF A/P SYSTEM. ABLE TO DUPLICATE YOKE VIBRATION WHEN SIMULATING APPROACH. SERVO RATTLES UNDER Aug 10, 2005 · N303CE · Saab 340BSDR SIMA200522007Wire · failedAMA - FLT 3779 - ON LANDING, CREW RECEIVED DUAL PITCH TRIM FAILURE 50 FT ABOVE GROUND. FOUND NR 2 AUTOPILOT DISCONNECT TRIM SWITCH WIRING CAUSED SWITCH TO BIND. REPOSITIONED WIRES AND SWITCH OPERATES CORRECTLY. ALL OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNEAug 4, 2005 · N612AE · Emb EMB145SDR QXEA20051139Mount · malfunctionedAFTER AUTOPILOT DISENGAGED, AILERONS WERE IMMOVEABLE (STUCK) FOR SEVERAL SECONDS. ACCOMPLISHED A UNEVENTFUL LANDING. MAINTENANCE REPLACED THE AILERON SERVO MOUNT. PERFORMED OPERATIONAL CHECKS ON THE AILERON SERVO, SERVO MOUNT, FLIGHT CONTROL COMPUTER, AUTOPILOJul 27, 2005 · N610QX · Cndair CL6002C10SDR 2005FA0001354Drive Assy · stiffTHE PILOT REPORTED THAT THE CONTROLS WERE STIFF IN THE ROLL AXIS. THE AUTOPILOT WAS TURNED OFF AND THE CB WAS CYCLED WITH NO CHANGE IN THE CONDITION. AFTER LANDING, WITHOUT INCIDENT, TECHNICIANS ARRIVED AND TROUBLESHOOT THE A/P SYSTEM. THEY DISCOVERED THE AJul 26, 2005 · N5408G · Cessna 550SDR QXEA20051135Yaw Damper · failedYAW DAMPER FAILED DURING CLIMB, RESET AND FAILED AGAIN WITH 15 SECONDS. RUDDER TRIM EXCESSIVE TO THE RIGHT DURING ALL PHASES OF FLIGHT. MAINTENANCE PERFORMED OPEATIONAL TEST OF THE RUDDER TRIM SYSTEM IAW Q400 AMM 27-22-00-71-801. OPS CHECKED GOOD. REMOVED ANDJul 23, 2005 · N410QX · Bombdr DHC8402SDR SWAA052118Computer · faultyAIR TURNBACK, ELEVATORS FELT BINDING DURING ROTATION. REMOVED AND REPLACED ELEVATOR FEEL COMPUTER PER MM.Jul 20, 2005 · N336SW · Boeing 7373H4SDR QXEA200501127Warning Light · illuminatedSEA FLT 2427 WHEN YD WAS SELECTED ON, LIGHTS CAME ON MOMENTARILY THEN WENT OUT AND -YD NOT CENTERED- WAS ILLUMINATED ON BOTH PFD'S. MAINTENANCE NOTES, FAULT UPON ARRIVAL WITH NR 2 ENGINE STILL RUNNING. NO FAULTS IN CDS. FAULT DOES NOT CLEAR, 20 MINUTES AFTER SJul 19, 2005 · N411QX · Bombdr DHC8402SDR UPS05M44934Computer · inoperativeATB - BOTH AUTO PILOTS FAILED SIMULTANEOUSLY. TRIED NUMEROUS TIMES TO RE-ENGAGE, FINALLY ONE OF THEM WAS BACK ON LINE, AND IT LATER FAILED AGAIN REMOVED AND REPLACED NR 2 FCC, BOTH FCC'S PASSED RTS TEST PER MM 22-01-03-4.Jul 19, 2005 · N273UP · Doug MD11FSDR MASA200500534Computer · malfunctionedASH 7033 ORD - THE CAPTAIN REPORTED AN UNCOMMANDED RUDDER MOVEMENT IN FLIGHT. MX REMOVED AND REPLACED FCC CARDS.Jul 10, 2005 · N75998 · Cndair CL6002B19SDR P5CA0501374Yaw Damper · malfunctionedRUDDER WOULD NOT DEFLECT. REPLACED UPPER AND LOWER YAW DAMPER COMPUTERS PER AMM 22-16-02.Jun 19, 2005 · N920FT · Boeing 747249FSDR WX0500044Controller · failedNR 2 AUTOPILOT INOPERATIVE, NR 2 DFGC FAILED. AIRCRAFT RETURNED TO LAS AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NR 2 DFGC AND PERFORMED RETURN TO SERVICE TEST. SYSTEM OPERATIONALLY CHECKED GOOD IAW AMM 22-01-01. AIRCRAFT RETURNED TO SERVICE.May 21, 2005 · N948MA · Doug DC987SDR DXTA200500734Wire · brokenAFTER TAKEOFF, THE MACH TRIM YAW DAMPER AND AUTO-PILOT WOULD NOT ENGAGE ON THE FGC PANEL. REPAIRED BROKEN WIRES AT LAFGS ANNUNCIATOR TRANSFER BUTTON. CLEANED BUTTON CONTACTS IAW ARKANSAS AERO DWG A1-44-001 REV B AND A1-44-003 REV B. OPERATIONAL CHECK SATISFACMay 21, 2005 · N549QS · Braero HAWKER1000SDR COMA0560313Control Unit · malfunctionedFLIGHT 5651 AUTO PILOT DISCONNECT WARNING AND PITCH DOWN AND LOSS OF 500 FT. REPLACED THE HSTCU.May 20, 2005 · N486CA · Cndair CL6002B19SDR P5CA0501359Control Panel · inoperativeON PRE-FLIGHT CREW REPORTS UNABLE TO ENGAGE EITHER -A- OR -B- AUTOPILOT. REPLACED P10 MODE CONTROL PANEL. OPS NORMAL PER MM 22-11-06.May 19, 2005 · N355MC · Boeing 747341SDR MASA200500362Control Unit · malfunctionedASH 7220 CID TO DEN. THE CREW HAD A MACH TRIM, STAB TRIM AND AUTO PILOT FAIL CAUTION MESSAGES IN FLIGHT. MAINTENANCE RESET THE SSCU'S PER ALL OPERATORS MEMO NR 275. NO FAULTS OR MESSAGES WERE PRESENT AFTER RESET.May 16, 2005 · N515MJ · Cndair CL6002C10SDR XN0A1237Connector · dirtyBOTH YAW DAMPERS WOULDN'T DESIGAGE DURING TAXI. CLEANED AND RESEATED YAW RATE CAIRO CONNECTIONS SYSTEM, OPS CHECK GOOD AT THIS TIME IAW A300 MM 22-21-00. (STATUS:ORIG/CLOSED)May 15, 2005 · N371PC · Airbus A300B4203SDR GTIA050154Push-Pull Rod · disconnectedAFTER INITIAL LEVEL OFF, THE NR 1 ENGINE AT NEAR CLIMB POWER STOPPED RESPONDING TO AUTO-THROTTLE POWER REDUCTION, THROTTLES BECAME SPLIT AND A/T DISCONNECTED. FULL THROTTLE GAVE NO INCREASE IN POWER AND FULL IDLE WOULD DROP NO LOWER THAN 1.64 EPR, ENGINE WAS May 13, 2005 · N836NK · Doug DC983SDR ASMF200505011Relay · failedAIRCRAFT PERFORMED AN UNSCHEDULED LANDING AT GDL AS CONSEQUENCE OF AUTOPILOT WAS OUT OF SERVICE. LEFT PFD INDICATOR WAS REPLACED IAW MM 34-24-00; TESTS WERE PERFORMED IN STP, SHOWING FAILURE CODE A/P HEART BEAT TEST FAILURE AND AIL/MECH TORQ SWITCH FAILURE. May 8, 2005 · N160PL · Doug MD88SDR MASA200500334Circuit Card · malfunctionedTHE AIRCRAFT RETURNED TO THE FIELD DUE TO THE CAPTAINS SIDE PFD BLINKS OFF INTERMITTENTLY, YAW DAMP 1 INOP MESSAGE INTERMITTENT AND CAPTAIN AND F/O'S HDG SPLIT EFIS COMP MON. MAINTENANCE REPLACED THE ENVIRO CONTROL CARD.May 5, 2005 · N75998 · Cndair CL6002B19SDR UPS05544416Yaw Damper · leakingINSPECTION TYPE:N/A ATB - EXCESSIVE RUDDER TRIM REQ FOR LEVEL FLIGHT. T/S IN PROGRESS. FOUND BOTH YAW DAMPNERS LEAKING. ORDERED TWO EACH AND TUBE AND LINK ASSY P/N 251N3058-8. AWAITING PARTS.May 2, 2005 · N421UP · Boeing 75724APFSDR PIDA20050019Coupler · damagedPILOT REPORTED YAW DAMPER HARD TO ENGAGE. REPLACED YAW DAMPER COUPLER PER MM 22-12-32. SYSTEM TESTS NORMAL.Apr 29, 2005 · N370WL · Boeing 7373G7SDR 05FDEA01171Computer · malfunctionedON DEPARTURE FROM MEM NEVER GOT AUTOPILOT ON, OR AUTOTHROTLES ON. HAD TO FLY BELOW RVSM DUE TO NO AUTOPILOT. PERFORMED DETAILED AFS SYSTEM CHECK, ALL TESTS PASSED, CHECKED FCC NR 1 AND FCC NR 2 PROFORMED AUTO FLIGHT SYSTEM TEST. REF MD-11 M/M 22-01-10-5. AApr 28, 2005 · N601FE · Doug MD11SDR UIEA200500057Computer · inoperativeAUTOPILOT WILL NOT ENGAGE. AUTOPILOT PUT AIRPLANE IN A 45 DEGREE BANK LT AND RT. DISENGAGED AUTOPILOT, STABILIZED AIRCRAFT AND RE-ENGAGED AUTOPILOT, AIRCRAFT STARTED ROLLING AGAIN. THE AIRCRAFT DIVERTED. RE-RACKED THE AUTOPILOT ROLL COMPUTER IAW MM, AUTOApr 24, 2005 · N537MC · Boeing 747271CSDR PIDA2005006Computer · failedAUTO FLIGHT CONTROL SYSTEM A FCC DC CIRCUIT BREAKER TRIPPED IN FLIGHT. WILL NOT RESET. RESULTING FLIGHT DIRECTOR FLAG IN VIEW. REPLACED FLIGHT CONTROL COMPUTER. OPS CHECKS GOOD PER MM 22-11-33.Apr 16, 2005 · N737DX · Boeing 737400SDR CA050413003Element · broken(CAN) DURING A SCHEDULED 1200-HOUR CHECK, A FUNCTIONAL TEST OF THE RIGHT THRUST REVERSER AUTO THROTTLE RETARDER WAS CARRIED OUT. THE RIGHT THROTTLE FAILED TO RETURN TO IDLE POSITION WITH THE THRUST REVERSERMANUAL DEPLOYMENT. UPON INVESTIGATION IT WAS DISCOVEREApr 13, 2005 · Cndair CL6012A12SDR MASA200500296Servo · malfunctionedASH FLT 2859 CLT - AIRCRAFT HAD A YAW DAMP FAIL MESSAGE. MAINTENANCE PLACED YAW DAMPER ON MEL AND DOWN GRADED THE AIRCRAFT TO NON RVSM STATUS. MX REPLACED RUDDER SERVO.Apr 11, 2005 · N854MJ · Emb EMB145LR
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