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 03FDEA01893Autopilot Sys · malfunctionedAT ALTITUDE FL280 CREW NOTICED AN UNUSUAL VIBRATION OF AIRCRAFT. ALL ENGINES / INSTRUMENTS INDICATED NORMALLY. ELECTED TO DIVERT TO SDF. VIBRATION / SHUTTER CONTINUED DURING TAXI IN. ACN RELEASED FOR SERVICE PER MEL/CDL: 22-06-A CATEGORY: C EXPIRATION: 18Nov 8, 2003 · N463FE · Boeing 727200SDR COMA0370048Damper · malfunctionedFLIGHT 5666 DURING TAKEOFF ROLL RECEIVED A YAW DAMPER NR 2 MESSAGE. REJECTED TAKEOFF AND AIRCRAFT RETURNED TO THE GATE. CYCLED POWER TO THE LEFT AND RIGHT AUTOMATIC FLIGHT CONTROL SYSTEM.Nov 6, 2003 · N368CA · Cndair CL6002C10SDR SWIA200312604Computer · malfunctionedWHEN AUTO PILOT ENGAGED ON CAPTAIN'S SIDE- YAW DAMPER DISENGAGES. WORKS OK WHEN AUTO PILOT SELECTED TO F/O. REPLACED CAPTAIN'S AUTOPILOT COMPUTER. OPS CHECKED GOOD.Nov 3, 2003 · N291SW · Emb EMB120ERSDR SWIA200312575Control Panel · malfunctionedWITH YAW ENGAGED AND RUDDER IN TRIM, THEN ENGAGED AUTO PILOT AND AIRPLANE YAWED AND BALL JUST WENT .5 SCALE TO LT, HAPPENED ON BOTH SIDES. REMOVED AND REPLACED AUTOPILOT CONTROL PANEL IAW MM 22-10-04. OPS CHECK GOOD.Nov 3, 2003 · N295UX · Emb EMB120ERSDR 2003FA0001161Servo · bindingINVESTIGATED PILOT COMPLAINT OF AILERON CONTROLS BINDING. NOTED BINDING/BANGING TYPE SOUNDS UNDER CENTER CABIN FLOOR. FOUND NOISES AND BINDING NOT PRESENT WITH AILERON SERVO REMOVED FROM CAPSTAN, RETURNED WHEN AILERON SERVO REINSTALLED. ALSO NOTED NOISES/BOct 31, 2003 · N447TF · Beech B300SDR VNAA0310022Control Panel · failedSMOKE IN AIRCRAFT FROM AUTOPILOT CONTROL PANEL. SMOKE CLEARED AFTER AP/YD TURNED OFF. MAINTENANCE INSPECTED AND REPLACED THE AP CONTROL PANEL IN ACCORDANCE WITH THE DORNIER MAINTENANCE MANUAL 21-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS Oct 29, 2003 · N433JS · Dorner DO328100SDR SWIA200312568Computer · malfunctionedRED AP LIGHT ON AFCP KEPT FLASHING WITH ASSOCIATED TRIPLE CHIME IN FLIGHT. REPLACED CAPTAIN'S SIDE AUTOPILOT COMPUTER. OPS CHECK GOOD ON GROUND CHECK.Oct 28, 2003 · N250YV · Emb EMB120ERSDR SWIA200312567Computer · malfunctionedFO SIDE AUTOPILOT CAUSES CONTROL WHEEL TO SHAKE. REMOVED AND REPLACED NR 2 APC COMPUTER WITH A SERVICEABLE UNIT. OPS CHECKS GOOD.Oct 27, 2003 · N217SW · Emb EMB120ERSDR SWIA200312560Actuator · malfunctionedTAXI OUT, YAW DAMPER NR 1 WOULD NOT STAY ENGAGED. REMOVED AND REPLACED NR 1 YAW DAMPER LINEAR ACTUATOR IAW WMM 22-22-01. OPS CHECKS GOOD.Oct 27, 2003 · N437SW · Cndair CL6002B19SDR SWIA200312554Computer · malfunctionedAUTOPILOT FAILED WHEN SELECTED TO CAPTAIN'S SIDE. COMPUTER FLAG SHOWING ON CAPTAIN'S ADI. REPLACED CAPTAIN'S AUTOPILOT COMPUTER. OPS CHECK GOOD PER 22-11-00.Oct 25, 2003 · N393SW · Emb EMB120ERSDR SWIA200312552Control Panel · malfunctionedAUTOPILOT FAILED AND DISCONNECTED, INTERMITTENT CAPT F/D FLAG AND ERRATIC FD MOVEMENT ON BOTH SIDES. REMOVED AND REPLACED APP-65A IAW EMB 120 MM 22-10-04. OPS CHECK GOOD.Oct 24, 2003 · N250YV · Emb EMB120ERSDR 372PA0038Connector · dirtyAUTO PILOT B WILL NOT ENGAGE AND AUTO PILOT A IS INTERMITTENT. REMOVED DIRT FROM AUTO PILOT A AND AUTO PILOT B CONNECTORS. A AND B SYSTEMS TEST OK IAW MM 22-10-00.Oct 24, 2003 · N372PA · Boeing 737306SDR SWIA200312553Computer · malfunctionedFD FLAG ON F/O ADI. CANNOT ENGAGE YAW WITH AP TRANSFER SELECT ON F/O SIDE. REPLACED NR 1 APC-69B AUTOPILOT COMPUTER. OPS CHECK GOOD AT THIS TIME.Oct 23, 2003 · N268UE · Emb EMB120ERSDR 2004F00069Switch · malfunctionedDURING FLIGHT, AIRCRAFT DECLARED EMERGENCY ON DESCENT TO PHX. AUTOPILOT FAILED TO DISCONNECT. AIRCRAFT LANDED AT PHX WITHOUT FURTHER INCIDENT. CLEANED AUTOPILOT DISENGAGE SWITCH ON YOKE AND OPERATIONAL CHECK NORMAL. (M)Oct 17, 2003 · N7639U · Boeing 727222SDR SWIA200312525Damper · malfunctionedYD ONE INOP STATUS MSG APPEARED 4 TIMES IN AIR AND TWICE ON GROUND. YD 1 WOULD RESET AND THEN FAIL REPEATEDLY. REMOVED AND REPLACED NR 1 YAW DAMPER IAW CRJ MM 22-22-01. OPS CHECK GOOD.Oct 17, 2003 · N406SW · Cndair CL6002B19SDR SIMA200328803Control Unit · inoperativeDURNG TAKEOFF AT 800 AGL CREW REPORTED PITCH TRIM ONE INOPERATIVE WITH CAS MESSAGE. WHEN AIRCRAFT WAS LEVELED BACKUP PITCH TRIM BECAME INOPERATIVE WITH NO MESSAGE. COMPLIED WITH APPROPRIATE CHECKLIST AND RECOVERED ALL PITCH TRIMS. MAINTENANCE REMOVED AND REOct 14, 2003 · N614AE · Emb EMB145LRSDR 03287307Warning Light · illuminatedDURING CLIMB THE CREW RECEIVED A FLIGHT CONTROL DISCONNECT MESSAGE. CREW RETURNED TO DEPARTURE FIELD AND LANDED UNEVENTFULLY.Oct 14, 2003 · N307UE · Jetair JETSTM4101SDR SWIA200312516Control Panel · malfunctionedDURING DESCENT YAW DAMPER DISENGAGES, CAPTAIN'S SIDE ONLY, WITH ASSOCIATED AMBER DISENGAGE LIGHT AND AMBER ''R'' LIGHT ON A/P CONTROL PANEL. ATTEMPTED TO RE-ENGAGE, BUT DOES NOT STAY ENGAGED.REPLACED APP65. OPS CHECK GOOD IAW MM 22-10-00. 10/16/03 UPDATE: Oct 11, 2003 · N291SW · Emb EMB120ERSDR BAQA089760Actuator · will not testWOULD NOT TEST AUTOPILOT. THIS UNIT CAUSED A FAILURE IN THE PREFLIGHT TEST OF THE AUTOPILOT. REPLACED WITH SERVICEABLE UNIT.Oct 9, 2003 · N554ME · Urocop EC135T1SDR BAQA089586Actuator · faultyYAW ACTUATOR SAS FAULT. REPLACED WITH SERVICEABLE UNIT.Oct 8, 2003 · N135ME · Urocop EC135P1SDR SWIA200312497Computer · malfunctionedCAPTAIN'S AUTOPILOT DISCONNECTS INFLIGHT, FOLLOWED BY RED COMPUTER FLAG. INSTALLED SERVICEABLE APC-65B IN NR 1 POSITION. OPS CHECK GOOD. PN ON 622-8315-402, S/N ON 3788 OFF 1534.Oct 6, 2003 · N221SW · Emb EMB120ERSDR SWIA200312496Computer · malfunctionedCAPTAIN'S AUTOPILOT AND TRIM FAIL. REPLACED CAPTAIN'S AUTO PILOT COMPUTER. OPS CHECK GOOD.Oct 6, 2003 · N288SW · Emb EMB120ERSDR SWIA200312493Computer · malfunctionedCAPTAIN'S FLIGHT DIRECTOR COMMAND BARS ERRATIC IN ROLL DURING TURNS. BARS JERK +/- 3 DEGREES IN ROLL DURING TURNS. COMMAND BARS ARE STABLE IN STRAIGHT FLIGHT. REPLACED CAPT'S AUTOPILOT COMPUTER APC-65B. OPS CHECK GOOD IAW MM 22-10-00.Oct 5, 2003 · N221SW · Emb EMB120ERSDR 2003UALA00746Autopilot Sys · malfunctionedWITH EITHER AUTO PILOTS ENGAGED AND ATTEMPTING TO ACCELERATE THE AIRCRAFT PITCHES UP. UPDATE DURING BITE CHECK OF THE AUTOPILOT BITE, FOUND FCC-B FAULTED, DADC2 FAULTED. DURING FULL TEST OF AUTOPILOT, OBSERVED FAULT WITH AFAU. REPLACED FCC-B, DADC, AND AFAUOct 5, 2003 · N341UA · Boeing 737322SDR P5CA0300957Control Panel · jammedALTITUDE ALERT CONTROL FROZEN. REMOVED AND REPLACED AUTOPILOT FLT DIRECTOR PANEL.Oct 4, 2003 · N924FT · Boeing 747236BSDR SWIA200312486Computer · malfunctionedF/O AUTO PILOT COMMAND BARS WENT DOWN (PITCH), ALSO ATTITUDE INDICATOR F/O SIDE SHOWED 15 DEGREES CLIMB. A/C FOLLOWED F/O COMMAND BARS AND PITCHED DOWN. DISCONNECTED A/P. REMOVED AND REPLACED NR 2 AUTOPILOT COMPUTER APC 65B. OPS CHECK GOOD.Oct 2, 2003 · N212SW · Emb EMB120ERSDR SWIA200312481Computer · malfunctionedFO'S FLIGHT DIRECTOR ERRATIC. REPLACED FO'S APC-65B AUTOPILOT COMPTUER. OPS CHECK GOOD IAW MM 22-10-00.Sep 30, 2003 · N250YV · Emb EMB120ERSDR 03FDEA01653Computer · inoperativeIMMEDIATELY AFTER TAKEOFF, FUEL AND MISC CUE ALERTS CAME ON. (FUEL ALERT, LEVEL 1 (TANK 3 FWD PUMP OFF). MISC CUE ALERT, LEVEL 1 (NO AUTOLAND). ADDITIONALLY, PFD AUTOPILOT BOX WENT AMBER, WITH (AP OFF) DISPLAYED. NEITHER AP WOULD ENGAGE AT 500 FT AGL, ASep 27, 2003 · N578FE · Doug MD11SDR 219PA0010Computer · malfunctionedROLL CHANNEL WILL NOT ENGAGE ON AUTO PILOT AND HEADING SELECT WILL NOT ENGAGE. REPLACED ROLL CHANNEL & OPS CHECKED GOOD PER MM 22-11-0.Sep 25, 2003 · N219PA · Boeing 737222SDR REXA03005Control Panel · malfunctionedON FINAL APPROACH, A LARGE POPPING NOISE CAME FROM THE FCP PANEL. SHORTLY AFTER IT STARTED TO VENT SMOKE BETWEEN NAV AND ALT BUTTON. CREW DECLARED EMERGENCY, FOLLOWED QRH PROCEDURES, LANDED NO FURTHER INCIDENT. REMOVED AND REPLACED FCP IAW AMM 22-11-07. COSep 23, 2003 · N8694A · Cndair CL6002B19SDR DXTA200300122Bungee Cylinder · loosePITCH VIBRATION IN FLIGHT CONTROLS WITH AUTO PILOT ON, VIBRATION INCREASED AS SPEED INCREASED. NOTICED AT 250 KTS AND 10000FT, VIBRATION ALSO COULD BE HEARD AS LOW FREQUENCY SOUND. TIGHTENED LT ELEVATOR BUNGEE AND ADJUSTED ELEVATOR CABLE TENSION IAW CESSNA 75Sep 19, 2003 · N930QS · Cessna 750SDR CA030922003Control Panel · malfunctioned(CAN) UPON AUTOPILOT DISCONNECT ON APPROACH ELEVATORS WERE STUCK AND HAD TO OVERPOWER TO REGAIN CONTROL.FLT DID NOT ENTER ANY VISIBLE MOISTURE DURING FLT. A/C LANDED NORMALLY. PANEL REPLACED (FCP)AS PER AMM 22-11-07-400-801 AND ALL OPERATES NORMALLY.Sep 18, 2003 · Cndair CL6002B19SDR BAQA089470Computer · inoperativeCOMPUTER UNIT IS INOP. REPLACED WITH SERVICABLE ASSET.Sep 18, 2003 · N5405G · Bolkms BK117B1SDR 219PA0009Computer · malfunctionedAUTO PILOT AILERON WILL NOT ENGAGE. REPLACED ROLL CHANNEL & OPS CHECKED NORMAL PER MM 22-11-0.Sep 18, 2003 · N219PA · Boeing 737222SDR SWIA200312426Computer · malfunctionedCAPTAINS AUTOPILOT PITCH IS ERRATIC IN LEVEL FLIGHT PITCH CHANGED +/- 2 DEGREES. REPLACED CAPT AHC 85. OPS CHECK GOOD.Sep 18, 2003 · N215SW · Emb EMB120ERSDR 219PA0008Limiter · inoperativeAUTOPILOT ROLL CHANNEL WILL NOT ENGAGE. REPLACED AILERON FORCE LIMITER IAW MM 22-12-10. OPS CHECKS OK.Sep 17, 2003 · N219PA · Boeing 737222SDR 2003FA0000934Guide · brokenWHILE CHECKING ELEVATOR TRIM WE FOUND INTERMITENT BINDING OF ELEVATOR TRIM WHEN MANUALLY OPERATING TO NOSE DOWN DIRECTION. BINDING WAS OF SUCH THAT IT WOULD MOMENTARILY HANG BEFORE RELEASING. IT OCCURED AT PRETY MUCH THE SAME POSITION EACH TIME, (WHEN MOVING FSep 16, 2003 · N61HA · Beech 1900DSDR SWIA200312414Computer · malfunctionedF/O'S FLIGHT DIRECTOR WILL NOT CAPTURE GLIDE SLOPE. REPLACED F/O'S AUTOPILOT COMPUTER. SYSTEM TESTS NORMALLY PER MM 22-11-00.Sep 14, 2003 · N215SW · Emb EMB120ERSDR SWIA200312437Computer · malfunctionedFO'S HDG BUG SLEWS ITSELF CLOCKWISE INTERMITTENTLY. SEEMS TO ONLY DO IT WITH AP SELECTOR TO FO'S SIDE WITH OR WITHOUT AP ENGAGED. REMOVED AND REPLACED FO'S AUTOPILOT COMPUTER IAW EMB MM 22-10-00. OPS CHECK GOOD.Sep 12, 2003 · N213SW · Emb EMB120ERSDR DXTA200300115Autopilot Sys · malfunctionedAIRCRAFT EXPERIENCED UNCOMMANDED RIGHT RUDDER INPUT DURING CRUISE WITH AUTOPILOT ON, ALSO DEVELOPED NOTICEABLE PITCH ROLL WITH AUTO PILOT ON. PERFORMED NJA OPERATIONAL CHECK FLIGHT AND COULD NOT DUPLICATE DISCREPANCY, NO FURTHER ACTION REQUIRED.Sep 10, 2003 · N312QS · Cessna 560CESSNASDR BAQA089074Computer · intermittentCOMPUTER INTERMITTENT. ERRATIC ROLL OPERATION. REPLACED WITH SERVICEABLE UNIT.Sep 9, 2003 · N777GS · Beech 100BEECHSDR SWIA200312383Switch · inoperativeFO AUTOPILOT WILL NOT ENGAGE.REPLACED FO AP DISCONNECT SWITCH. SYSTEM OPS CHECK GOOD IAW 22-10-00.Sep 8, 2003 · N234SW · Emb EMB120ERSDR SWIA200312380Power Supply · malfunctionedAUTOPILOT FAILED INFLIGHT WITH YD2 FD2 STATUS MESSAGES DISPLAYED ON ED2. QRH PROC'S FOLLOWED, BUT NO HELP. RETURNED TO DFW. REMOVED AND REPLACED IAPS 2A POWER SUPPLY IAW CL600 MM 22-12-02. OPS CHECKS GOOD.Sep 6, 2003 · N464SW · Cndair CL6002B19SDR 0301696718Computer · inoperativeDURING CLIMB THE LOWER YAW DAMPER LIGHT ILLUMINATED BRIEFLY AND THE AIRCRAFT WAS DIFFICULT TO CONTROL IN HEADING. SLOWED AIRCRAFT TO 270 KNOTS AND TURNED OFF LOWER YAW DAMPER BUT AIRCRAFT WAS STILL DIFFICULT TO CONTROL IN HEADING. AIRCRAFT DECLARED AN EMERGENCSep 4, 2003 · N618US · Boeing 747251FSDR HYI2003F00011Computer · failed5 MINUTES INTO CLIMB, CREW REPORTED SMOKE FROM AVIONICS RACK, RETURNED W/O INCIDENT. MECHANIC FOUND A/P PITCH SERVO HARNESS SHORTED, CAUSING A/P COMPUTER TO FAIL INTERNALLY, (TRANSISTORS OVERHEATED AND BURNED) REPAIRED SHORTED HARNESS. REPAIRED A/P COMPUTER,Sep 3, 2003 · N2714M · Cessna 402CSDR SWIA200312388Computer · malfunctionedFD FLAG CAPT SIDE, FOS FD ERATIC WILL NOT CAPTURE AUTOPILOT, EITHER SIDE. DOES NOT TEST ON GROUND. REPLACED CAPT APC 65B AUTOPILOT COMPUTER. OPS CHECK GOOD IAW MM 22-10-00. PN ON 622-8315-402 SN ON 3332 OFF 131.Sep 3, 2003 · N292UX · Emb EMB120ERSDR BAQA088834Actuator · stuckTAIL ROTOR KICK AND GALVA METER STICKING. REPLACED WITH SERVICEABLE UNIT.Aug 27, 2003 · N915ME · Aerosp AS365N2SDR SWIA200312356Control Panel · malfunctionedF/O AUTOPILOT CAPTURES 400 FT HIGH. INSTALLED SERVICEABLE APP-65 AUTOPILOT CONTROL PANEL. OPS CHECK GOOD. PN: 622-6684-006, SN ON: 2297, SN OFF: 1715.Aug 23, 2003 · N15732 · Emb EMB120ERSDR SWIA200312350Dampener · malfunctionedYAW DAMPNER NR 1 FAILED ON PUSHBACK/WILL NOT STAY ENGAGED. REMOVED AND REPLACED NR 1 YAW DAMPNER WITH A SERVICEABLE UNIT IAW CL600 AMM 22-22-01. OPS CHECK GOOD. S/N OFF: 2762.Aug 23, 2003 · N587SW · Cndair CL6002B19SDR SWIA200312358Control Panel · malfunctionedTHE AUTOPILOT FAILURE WITH AP LIGHT ON FCP AND AUTOPILOT PANEL. THE CAPTAIN'S AP WAS SELECTED. REMOVED AND REPLACED AUTOPILOT CONTROL PANEL APPG5A WITH SERVICEABLE UNIT. AUTOPILOT OPS CHECK GOOD IAW 22-10-00. PN: 622-6284-006.Aug 22, 2003 · N224SW · Emb EMB120ER
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