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 4070198Servo · overtorquedCOMPLIANCE WITH THE 1000 HOUR/ 12 MONTH KFC-150 AUTOPILOT SERVO CLUTCH TORQUE CHECK( TASK CODE 221009) OF SUBJECT SERVO REVEALED CLUTCH TORQUE TO BE 60 IN/LB, STC NR SA2053CED. SLIP CLUTCH VALUE TABLE SPECIFIES A TORQUE VALUE OF 43 IN/LB PLUS OR MINUS 4 IN/LDec 19, 2002 · N822SA · Cessna 208BSDR SWIA200211601Damper · malfunctionedDURING FLIGHT, RECEIVED A -FLUTTER DAMPER- STATUS MESSAGE FOR THE LEFT AILERON. REMOVED AND REPLACED LEFT AILERON FLUTTER DAMPER IAW CRJ 27-15-05. OPS CHECKS GOOD.Dec 19, 2002 · N426SW · Cndair CL6002B19SDR HEEA082559Amplifier · malfunctionedSCAS AMPLIFIER ROLL TRIPS OFF.Dec 2, 2002 · Bell 214STSDR 159PL0023ComputerRoll channel will not engage. R&R roll channel computer per MM 22-11-161. Ops check good.Dec 1, 2002 · N159PL · Boeing 737242SDR BAQA081536Switch · failedFDSEL SWITCH STICKS. REPLACED WITH SERVICEABLE UNIT.Nov 26, 2002 · N955ME · Bolkms BK117A1SDR 372PA0014ComputerOccasional FCC in-flight faults on FMC Bite. Swapped FCC's for further evaluation. Both FCC's Ops normal per LRU interface Bite checksNov 26, 2002 · N372PA · Boeing 737306SDR 920WA0008PanelAt 12000 feet, autopilot on, in heading select mode, displayed heading changed on its own several times. R&R mode control panel IAW MM 22-11-341. Ops checked normal.Nov 24, 2002 · N920WA · Boeing 737236SDR 2002FA0001337Roll Servo · defectiveSERVO DRIVE MOTOR SEPARATED FROM REDUCTION GEAR ASSEMBLY. OCCURRED IN NORMAL FLIGHT OPERATIONS. SECOND OCCURRENCE IN THIS AIRCRAFT, IDENTICAL FAILURE. WARRANTY SERVO INSTALLED 9/27/2002, FAILED 11/12/2002.Nov 13, 2002 · N36VG · Beech A36SDR C2XA02IA237Circuit Card · malfunctionedTHE CREW NOTED THAT THE AUTOPILOT/YAW DAMPER FAILED. MAINTENANCE REMOVED AND REPLACED THE NR 1 IC-600. PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Nov 10, 2002 · N14933 · Emb EMB145ERSDR SWIA200211479Actuator · malfunctionedYD 1 STATUS MESSAGE COMES ON DURING TAXI. RETURNED TO GATE. REPLACED NR 1 YAW DAMPER LINEAR ACTUATOR WITH A SERVICEABLE UNIT IAW 22-22-01. OPS CHECK GOOD.Nov 8, 2002 · N448SW · Cndair CL6002B19SDR ABXA020307Controller · malfunctionedELEVATOR OSCILLATES VIOLENTLY WHEN AUTO PILOT WAS ENGAGED. COULD NOT DUPLICATE. REPLACED THE AUTO PILOT CONTROLLER IAW DC9 M.M. 22-10-00-5. AUTO PILOT SYSTEM OPS CHECK GOOD.Nov 8, 2002 · N952AX · Doug DC941SDR SWIA200211436Circuit Board · malfunctionedSTAB TRIM CHANNELS 1 AND 2 WILL NOT ENGAGE.REMOVED AND REPLACED NR 1 FCC CARD IAW 22-10-14. OPS CHECK GOOD.PN OFF/ON 622-9815-704 SN OFF 4X1A SN ON337.Nov 4, 2002 · N720SW · Cndair CL6002B19SDR SWIA200211442Computer · malfunctionedYAW DAMPER 1 INOP STATUS MESSAGE RECEIVED ON TAXI OUT. COULD NOT CLEAR THE MESSAGE. REMOVED AND REPLACED FCC CARD 1 IAW 22-12-14. OPS CHECK GOOD.Nov 3, 2002 · N448SW · Cndair CL6002B19SDR SWIA200211420Actuator · malfunctionedYAW DAMPER NR 2 FAILED IN FLIGHT. MESSAGE ON EICAS. REMOVED AND REPLACED NR 2 YAW DAMP LINEAR ACTUATOR IAW CRJ MM 22-22-01. OPS CHECK GOOD.Nov 1, 2002 · N916SW · Cndair CL6002B19SDR AALA20021555Control Panel · malfunctionedMIA - FLT 934 - EN ROUTE GYE-MIA, AT FL310, .78 MACH, RIGHT AUTOPILOT KICKED OFF RESULTING IN TAIL SWING AND RIGHT BANK. CHECKED SYSTEMS AND REENGAGED AUTOPILOT. LANDED AT MIA WITHOUT FURTHER INCIDENT. MAINTENANCE DOWN LOADED DFDR. VERIFIED THAT RIGHT BANKOct 28, 2002 · N41063 · Airbus A300B4605RSDR MV5R055MServo · seizedAILERON PRIMARY AUTO PILOT SERVO SEIZED. FLIGHT CREW APPLIED SUFFICIENT FORCE IN AN ATTEMPT TO FREE AILERON MOVEMENT. CAUSING AILERON CONTROL CABLE TO BECOME DISLODGED FROM FORWARD AILERON CONTROL DRUM. INVESTIGATION OF THE SERVO REVEALED A BEARING FAILURE Oct 24, 2002 · N695GG · Gulstm 695ASDR BAQA081190Head · brokenREMOTE CONTROL HEAD VHF/PRIORITY SWITCH BROKEN.Oct 24, 2002 · N575ME · Urocop EC135T1SDR 2002UALA01559Damper · leakingLANDED UNDER AMBER ALERT DUE TO LOSS OF GREEN HYDRAULIC SYSTEM. NR 1 YAW DAMPER WAS FOUND LEAKING HYDRAULIC FLUID. NEW YAW DAMPER ACTUATOR WAS INSTALLED AND OPERATIONAL CHECK WAS GOOD.Oct 10, 2002 · N448UA · Airbus A320232SDR 2002FA0001223Servo · failedSERVO CAUSED AUTOPILOT MISTRIM CONDITION AND EVENTUALLY DID NOT PERMIT AUTOPILOT TO ENGAGE.Oct 8, 2002 · N83EJ · Israel GALAXYSDR 377PA0008Control Unit · malfunctionedCHANNEL B ON AUTO PILOT INOPERATIVE. AUTO THROTTLES RETARD TO IDLE, WOULD NOT DISPLAY MACH SPEED ON MCP. PERFORMED A/P LAND VERIFY BITE CHECK THROUGH FMC. NO FAULTS INDICATED.Oct 5, 2002 · N377PA · Boeing 7373L9SDR UIEA200200050Module · leakingNR 1 HYDRAULIC LOW QUANTITY LIGHT CAME ON AFTER TAKEOFF. HYDRAULIC QUANTITY DROPPED TO ZERO. APPROXIMATELY 30 SECONDS LATER THE EDP AND ADP PRESSURE LIGHTS BEGAN TO FLASH. SHUT SYSTEM DOWN IAW PROCEDURES. EDP PUMP SWITCH PLACED TO SUPPLY OFF POSITION AT 08Sep 29, 2002 · N512MC · Boeing 747230BSDR HALA0200569Autopilot Sys · malfunctionedFLT 11 - SFO - CLIMBING-OUT OF 9000 FEET FMA BRIEFLY SHOWED ALPHA SPEED AT 250 KTS LEVEL OFF FL360, NR 2 AUTOTHROTTLES DROPPED OFF, NR 1 STILL FUNCTIONED. AT 1 MINUTE LATER, STICK SHAKER OCCURRED, FOLLOWED BY AUTO SLAT EXTENSION AT MACH .81.5. DESCENDED TO FSep 27, 2002 · N128AA · Doug DC1010SDR AUS20021169Damper · failed(AUS) RT YAW DAMPER FAULTY.Sep 18, 2002 · Boeing 767330SDR XNOA01069Circuit Breaker · trippedNR 2 PITCH TRIM TRIPS OFF WON'T RESET. TRANSFERRED TO DMI 2623 IAW MEL 22-11-03. PLACARDS INSTALLED.Sep 18, 2002 · N307FV · Airbus A300B4203SDR SWIA200211215Damper · faultyNR 1 YAW DAMPER WOULD ENGAGE UNTIL RUDDER MOVEMENT WAS INITIATED THEN NR 1 WOULD AGAIN DISCONNECT. REPLACED NR 1 YAW DAMPER LINEAR ACTUATOR IAW MM 22-22-01. OPS CHECK GOOD.Sep 11, 2002 · N439SW · Cndair CL6002B19SDR SWIA200211218Damper · malfunctionedNR 2 STATUS MESSAGE DURING FLIGHT. WOULD NOT RESET. SWAPPED FCC CARDS FROM TOP TO BOTTOM. REPLACED NR 2 YAW DAMPER W/SERVICEABLE UNIT IAW MM 22-22-01. PERFORMED EXTENSIVE FUNCTIONAL CHECKS OF BOTH NR 1 & 2 YAW DAMPER SYSTEMS. OPS CHECK GOOD ON GROUND AT TSep 7, 2002 · N923SW · Cndair CL6002B19SDR DHL2002363526Autopilot Sys · malfunctionedACCEPTANCE FLIGHT/DURING COUPLED APPROACH WITH BOTH AUTOPILOTS ENGAGED IN CMD AND IN LAND MODE AT A PREDETERMINED ALTITUDE GO AROUND WAS SELECTED AND THE PITCH CLIMBOUT DID NOT SEEM TO BE CORRECT TO THE FLIGHT CREW, AS WELL AS THE ALTITUDE ACQUISITION. THE CHSep 5, 2002 · N363DH · Airbus A300B4203SDR SWIA200211189Damper · malfunctionedYAW DAMPER NR 2 INOP. REMOVED AND REPLACED NR 2 YAW DAMPER IAW 22-22-01. REPLACED NR 2 FCC CARD. OPS CHECK GOOD.Sep 1, 2002 · N435SW · Cndair CL6002B19SDR 2002F00969Damper · malfunctionedAMBER YAW DAMP NOT CENTERED MESSAGE ILLUMINATED DURING TAKEOFF. TAKEOFF WAS ABORTED. YAW DAMP NOT CENTERED. CREW REFERENCED AND FOLLOWED APPROVED FLIGHT MANUAL PROCEDURES ON PAGES 3-151/3-152 OF THE AFM. SYSTEM RESET WAS NORMAL. CREW CONTINUED TRIP. (M)Aug 23, 2002 · N5113 · Cessna 750SDR USAASB02158Coupler · faultyENROUTE, CLIMBING THROUGH FL210, AIRCRAFT EXPERIENCED A PULSING LEFT/RIGHT YAWING CONDITION. ONCE AUTOPILOT, AUTOTHROTTLE AND YAW DAMPER WERE OFF, YAWING STOPPED. CREW WAS UNABLE TO DUPLICATE CONDITION. PRIOR FLIGHT OF THIS AIRCRAFT WAS UNEVENTFUL. FLIGHT Aug 20, 2002 · N346US · Boeing 737301SDR QXEA0201110Warning System · activatedSEA- AUTO TRIM FAIL. INFLIGHT FAILURE OF PITCH TRIM. CLEARED CAUTION LIGHT. OPERATIONAL CHECKED GOOD. NO FURTHER DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.Aug 5, 2002 · N406QX · Bombdr DHC8401SDR HEEA080709Amplifier · erraticADI HAD ERRATIC MOVEMENT.Aug 2, 2002 · Bell 412SDR HEEA080706Amplifier · malfunctionedAMPLIFIER ROLLS CHANNEL AND KICKS OFF LINE.Jul 31, 2002 · Bell 214STSDR USAABB02122Throttle · malfunctionedPHL - FLT 11 - APPROXIMATELY THREE HOURS INTO THE FLIGHT, AT FL350, THE AUTO THROTTLES WENT TO IDLE DETENT. MAINTENANCE PERFORMED A FUNCTIONAL CHECK OF THE AUTO THROTTLE SYSTEM. NO FAULTS WERE FOUND. (M)Jul 22, 2002 · N656US · Boeing 7672B7SDR SWIA200211074Control Panel · malfunctionedNR 2 YAW DAMPER INOP. REMOVED AND REPLACED FCP IAW 22-11-07. OPS CHECK GOOD.Jul 19, 2002 · N597SW · Cndair CL6002B19SDR GUUA07270209Switch · dirtyYAW DAMPER DISENGAGES BOTH LEFT AND RIGHT, IN FLIGHTCLEANED CAPTAINS YOKE DISCONNECT SWITCHJul 17, 2002 · N87552 · Beech 1900DSDR CA020712002Servo · worn(CAN) AS PART OF PRE-FLT FUNCTION AUTOPILOT IS ENGAGED & SERVOS ARE MECHANICALLY OVERRIDDEN. IT INITAILLY DISCOVERED BY MAINT PERSONNEL THAT WERE WEAR MARKS ON THE PITCH SERVO CAPSTAN COVER. MAINT TESTING DISCOVERED THAT SLACK IN PRIMARY PITCH CABLE CAUSEDJul 12, 2002 · Dhav DH60GSDR 251TR0003VaneReference DMI #0707002. Auto pilot V/S mode reverts to LVL change uncommanded. Alpha vane replaced. See item #1 log page 09871, test C/W I/A/W ch. 22-11-381, ops chk. good. This clears DMI 0707002. Placard removed.Jul 12, 2002 · N251TR · Boeing 737228SDR GTIA020784Rheostat · failedLAX - FLT 709 - FOUND AUTO PILOT NR 1 AND NR 2 DISCONNECTS DURING RIGHT TURNS. ALSO PULSES IN ROLL. OK STRAIGHT AND LEVEL AND LEFT TURNS. TROUBLESHOT AUTOPILOT SYSTEM. FOUND AILERON SERVO RHEOSTAT BAD. CHECKED WITH METER LEFT SIDE GOOD RIGHT SIDE BAD. REJul 9, 2002 · N827NK · Doug DC983SDR 251TR0001Autopilot SysAuto pilot V/S mode reverts to LVL change mode uncommanded. Deferred per MEL 22-15-8 CTL #0707002 CATCJul 7, 2002 · N251TR · Boeing 737228SDR GTIA020779Servo · noisyACY - RIGHT TURN WHEN AUTO PILOT ENGAGED AILERON SERVO MAKES GROUND NOISE FROM 0-25. REMOVED AND REPLACED AILERON SERVO DRIVE IAW MM 22-10-01. OPS CHECK NORMAL RTS CHECK PERFORMED IAW MM 22-01-05, OPS CHECK NORMAL. (M)Jul 6, 2002 · N827NK · Doug DC983SDR GTIA020777Drive Unit · chatteringFLT 594 - MCO - WITH AUTO PILOT ENGAGED, THE YOLK CHATTERS IN RIGHT TURNS. REMOVED AND REPLACED AILERON SERVO DRIVE. PERFORMED SYSTEM CHECK SYSTEM GROUND CHECKED GOOD. ALL IAW MD80 MM SECTIONS 22-11-01 AND 22-01-05. (M)Jul 4, 2002 · N827NK · Doug DC983SDR HEEA080292Amplifier · malfunctionedAMPLIFIER ASSY ROLL CHANNEL KICKS OFF IN HOVER. COULD NOT ADJUST.Jul 2, 2002 · Bell 214STSDR GTIA020736Control Panel · failedMCO - FLT 506 - INTERMITTENT AUTOTHROTTLE DISCONNECT ON APPROACH. REMOVED AND REPLACED FLIGHT GUIDANCE CONTROL PANEL, SYSTEM OPS CHECKS GOD IAW MD80 MM 22-01-05. (M)Jun 30, 2002 · N803NK · Doug DC982SDR P5CA0200686Autopilot Sys · malfunctionedB-AUTOPILOT WILL NOT ACCEPT STEERING COMMANDS IN HDG OR INS MODE. ALSO INOP IN MANUAL. TRANSFERRED TO DEFERRED MX ITEM.Jun 30, 2002 · N806FT · Boeing 747249FSDR P5CA0200685Wire · broken"A" AUTOPILOT WILL NOT ACCEPT STEERING COMMANDS IN HDG OR INS MODES. ALSO INOP IN MANUAL. TRANSFERRED TO DEFERRED MX ITEM ID #036042 CTR #29299 IAW MEL 02-22-2-1 IN CONSULT W/ MTC & PLACARD INSTALLED. JFK MX FOUND BROKEN WIRE AT PINS 9 & 10 ON CONNECTOR DB193 Jun 30, 2002 · N806FT · Boeing 747249FSDR GTIA020747Controller · failedMCO - FLT 594A - AUTO THROTTLE TURNED OFF ON APPROACH WHEN SPEED WAS CHANGED AUTO PILOT 2. REMOVED AND REPLACED FLIGHT GUIDANCE CONTROLLER, OPS CHECK GOOD AT THIS TIME. (M)Jun 28, 2002 · N803NK · Doug DC982SDR 070201Trim Switch · malfunctionedPILOT REPORTED UNCOMMAND VIOLENT ROLL TO LEFT. CREW LOST 15000 FT OF ALTITUDE BEFORE GAINING CONTROL. CONTINUED TO VAN NUYS & LANDED WITHOUT INCIDENT. GULFSTREAM TECHNICAL OPERATIONS CAME TO OBSERVE TEST IAW IAI REF LETTER DATED 6-26-2002. PERFORMED A OPS CJun 28, 2002 · N118MP · Israel 1124ASDR GTIA020728Control Panel · failedFLT 706 - LGA - IAS/MACH BUTTON WILL NOT SWITCH TO MACH ON DFGS NR 2, OK ON NR 1. REMOVED AND REPLACED FLIGHT GUIDANCE CONTROL PANEL. PERFORMED OPS HECK IAW MM 22-01-05. OPS CHECKS NORMAL. (M)Jun 27, 2002 · N808NK · Doug DC983SDR 2002F00764Dampener · faultyAT CRUISE ALTITUDE THE AIRCRAFT EXPERIENCED FULL LEFT RUDDER DEFLECTION. EMERGENCY PROCEDURES WHERE INITIATED. DURING RECOVERY PROCEDURES ALTITUDE LOSS OF 15,000 FEET. YAW DAMPENER WAS DISABLED AND AIRCRAFT CONTROLS RETURNED TO NORMAL. AIRCRAFT RETURNED TOJun 19, 2002 · N118MP · Israel 1124A
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