JASC 2200
Service difficulty reports · 568
Reports filed under 2200 · Auto Flight 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 = '2200' 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 = '2200' 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 WVBA2003004Autopilot Sys · malfunctionedIN THE SUPPLIED DOCUMENTATION FROM S-TEC WE HAVE BEEN ABLE TO FIND ANY INFORMATION ABOUT AUTOPILOT LOSS-IN-TURN AND OTHER CRITICAL LIMITS. THIS SEVERELY HAMPERS OUR ABILITY TO DETERMINE WHETHER OR NOT OUR AUTOPILOT IS OPERATING IN A CORRECT FASHION.SDR 03FDEA02208Coupler · failedLOWER YAW DAMPER RUNAWAY - LT AND RT AFTER TAKEOFF - LYD SWITCH TURNED OFF. REMOVED AND REPLACED LOWER YAW DAMP COUPLER IAW 727-100 MM CH 22-11-131-4. OPS CHECKS NORMAL ON GROUND. A/C OK FOR SERVICE.SDR CA031216004Control Unit · jammed(CAN) ON FLT, AUTO-PILOT WAS UNABLE TO CHANGE AC DIRECTION, AUTO-PILOT WAS DISCONNECTED AND CREW DISCOVER THAT THEY WERE UNABLE TO MOVE AILERON CONTROL WHEEL. THEY MOVED TRIM AND SUDDENLY AILERON CONTROL WHEEL TURNED, CONTROL WHEEL DID NOT JAM AGAIN. AFTER ASDR 0301731232Autothrottle Sys · malfunctionedDURING TAKE-OFF ROLL THE CREW OBSERVED THE NR 1 ENGINE EXCEED LIMITS FOR N1, N2 AND EGT. THE NR 3 ENGINE ALSO EXCEEDED THE N2 LIMIT. THE TAKE-OFF WAS ABORTED AT 115KTS AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED THE NR 1 AND 3 ENGINES PER THE SDR USAASB03147Control Panel · inoperativeTHE MODE CONTROL PANEL BECAME INOPERATIVE. CREW WAS UNABLE TO ACTIVATE FLIGHT DIRECTORS. FLIGHT DIVERTED TO CAE AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE MODE CONTROL PANEL. FUNCTIONAL CHECK NORMAL PER MM. (M)SDR HEEA088221Tarsyn · failedNR 2 HELIPILOT FAILED IN FLIGHT, THE COPILOT ATTITUDE INDICATOR FAILED AND THE CIRCUIT BREAKER POPPED. SMELLED BURNING WIRE. MAINTENANCE FOUND WIRING TO COPILOT TARSYN UNIT CHAFED IN THE AVIONICS COMPARTMENT WHERE THE TARSYN UNIT MOUNTS. REPLACED TARSYN UNISDR I05R088213Gyro · malfunctionedAIRCRAFT HAD A PROBLEM WITH THE GYRO CAUTION LIGHT. REPLACED PART.SDR HEEA084905Bearing · wornNR 1 YAW ACTUATOR ROD END HAS A WORN BEARING. SCRAPPED DUE TO CORROSION.SDR 252TR0003CouplerYaw damper inop. Removed and replaced yaw damper coupler IAW MM 22-11-141. Ops. check good IAW MM 22-12-01.SDR HEEA080410Damper · leakingPEDAL DAMPER LEAKING. TO BE SENT TO VENDOR FOR REPAIR.SDR HEEA080135Tarsyn · malfunctionedTARSYN 333 CAUSES YAW CHANNEL TO KICK. REPLACED WITH SERVICEABLE PART.SDR HEEA079958Brake · malfunctionedAUTOPILOT WOULD DROP OFF LINE AND SOMETIMES WOULD NOT PASS THE PRE-FLIGHT TEST DUE TO THE LINEAR PITCH ACTUATOR BRAKE NOT WORKING PROPERLY. WOULD NOT LOCK UNTIL TAPPED OR BUMPED.SDR HEEA079390Tarsyn · malfunctionedTARSYN333 MALFUNCTIONS, PILOT`S ATTITUDE SYSTEM CIRCUIT BREAKER POPPING. REPLACED WITH SERVICEABLE UNIT.SDR VNAA0205016Control Unit · failedDURING TAKE OFF, THE CREW RECEIVED A FLIGHT GUIDANCE COMPUTER FAIL CAS MESSAGE AND ABORTED TAKE OFF. THE AIRCRAFT RETURNED TO THE GATE AND MAINTENANCE CONTROL DEFERRED THE FLIGHT GUIDANCE COMPUTER AND THE FLIGHT THEN CONTINUED ON TO RDU.SDR HEEA079096Amplifier · will not testELEVATOR AMPLIFIER WILL NOT MONITOR TEST.SDR HEEA079086Amplifier · malfunctionedELEVATOR AMPLIFIER COULD NOT ALIGN AMP TO STAY ENGAGED WITH OTHER SYSTEM.SDR HEEA079085Amplifier · malfunctionedELEVATOR AMPLIFIER DRIVES ACTUATOR WITH NO A/S SIGNAL.SDR CA020502014Asymmetry Switch · failed(CAN) AT 400 FEET AFTER TAKEOFF CREW REPORTED AN AILERON LOCKOUT MESSAGE, RUDDER RATIO MESSAGE AND NONE OF THE 3 AUTOPILOTS COULD BE ENGAGED. AIRCRAFT RETURNED TO AIRPORT.BOTH LT AND RT STABILIZER TRIM/ELEVATOR ASYMMETRY MODULES (SAM) REPLACED AS PER AMM 27-09SDR MEX2002051Control Unit · failedFLT 608 - MEX-DFW - AIRCRAFT STOPPED OVER IN MTY AS CONSEQUENCES OF AUTOMATIC THROTTLES, AUTO PILOT AND FLIGHT DIRECTORS FAIL, REPORTS ARE DEFERRABLES, HOWEVER PILOT ASKED THEIR CORRECTION. BOTH DFGC WERE REPLACED IAW MM 22-01-01. (M)SDR HEEA077842Amplifier · failedPITCH LIGHT INOP. WON'T MONITOR TEST. AUTOFLIGHT AMPLIFIER FAILED.SDR 2002F00245Limiter · defectiveATL - AUTO PILOT WILL NOT ENGAGE. REMOVED AND REPLACED AILERON FORCE LIMITER AND OPERATION CHECKED NORMAL PER MM 22-11-13. (M)SDR 2002F00247Accessory Unit · defectiveATL - UNABLE TO ENGAGE EITHER A/B AUTO PILOT SYSTEM IN ANY MODE. REMOVED AND REPLACED AUTO PILOT ACCESSORY UNIT. PERFORMED AFDS TEST BY CDU PER MM 22-11-01. (M)SDR 2002F00249Accessory Unit · malfunctionedDURING DESCENT AUTOPILOT 'A' DISENGAGED, WITH AIRCRAFT IN TRIM. UNABLE TO ENGAGE EITHER A OR B AUTOPILOT IN ANY MODE. REPLACED AUTO-PILOT ACCY UNIT. OPS CHECK NORMAL. (M)SDR HEEA077680Amplifier · malfunctionedAMPLIFIER CAUSING PITCH AXIS TO KICK.SDR HEEA077679Amplifier · malfunctionedCAUSES ELEVATOR LIGHT TO STAY ON.SDR HEEA077678Amplifier · will not testWON'T MONITOR TEST. STICK WANDERS. DIFFICULT TO ADJUST R91 ON BOARD 11 & 9.SDR HEEA077002Pin · looseCOPILOT THROTTLE WOULD NOT CONTROL THE NR 2 ENGINE. MAINTENANCE FOUND PIN CONNECTING COPILOT THROTTLE GRIP TO SHAFT IN COLLECTIVE STICK TO HAD BACKED OUT. REINSTALLED PIN.SDR HEEA076463Tarsyn · malfunctionedCOMPASS CONTROL PANEL NEEDLE FLIPPING CONSTANTLY. PENDING VENDOR REPAIR.SDR WVBA2001050Computer · failedTHIS PITCH COMPUTER WAS A FACTORY REPAIR WHICH UPON RETURN FAILED IN THE SAME MANNER. WHEN INSTALLED THE AIRCRAFT WOULD PITCH UP AND DOWN 5 DEGREES WHILE THE AUTOPILOT WAS ENGAGED FOR CRUISE. THIS AUTOPILOT SYSTEM SEEMS TO BE PARTICULARLY SENSITIVE TO ANY AFSDR WVBA2001048Computer · inoperativePILOT REPORTED AIRCRAFT PORPOISES 5 DEGREES UP AND DOWN IN CRUISE. AUTOPILOT PITCH COMPUTER REMOVED AND REPLACED WITH LOANER UNIT. THIS PROBLEM HAS OCCURRED IN THE PAST IT IS SUSPECTED THAT THE SERVO DRIVE SPEED IS TOO SLOW. SUGEST ADJUSTING THE SPEED AND PSDR HEEA075945Tarsyn · malfunctionedPILOTS ADI BEGAN TUMBLING IN LEVEL FLIGHT. REPLACED WITH SERVICEABLE PART.SDR COMA0160628Pcu · faultyFLIGHT #5800. DESTINATION CVG, DURING CRUISE FLIGHT THE AUTO PILOT FAILED @ FL28. EXCESSIVE INPUT FORCE WAS REQUIRED FOR AILERON CONTROL, FLIGHT WAS DIVERTED TO IAD AND LANDED SAFELY.REPLACED THE LEFT INBOARD AILERON POWER CONTROL UNIT.SDR COMA0160626Servo · faultyFLIGHT #5800. DESTINATION CVG, DURING CRUISE FLIGHT THE AUTO PILOT FAILED @ FL28. EXCESSIVE INPUT FORCE WAS REQUIRED FOR AILERON CONTROL, FLIGHT WAS DIVERTED TO IAD AND LANDED SAFELY.REPLACED THE PRIMARY AILERON SERVO (SVO-85A).SDR COMA0160625Mount · faultyFLIGHT #5800. DESTINATION CVG. DURING CRUISE FLIGHT THE AUTO PILOT FAILED @ FL28. EXCESSIVE INPUT FORCE WAS REQUIRED FOR AILERON CONTROL, FLIGHT WAS DIVERTED TO IAD AND LANDED SAFELY.REPLACED THE PRIMARY AILERON SERVO MOUNT (SMT-87A).SDR HALA0100166ComputerATB - FLT 22 - DURING CLIMB-OUT AT 225 KTS WHEN RETRACTION SLATS, STICK SHAKER ACTIVATED. WE RE-EXTENDED THE SLATS AND STICK SHAKER STOPPED. NOTE SLAT RESET LIGHT STAYED ON. FOUND NR 2 AOA AND A/T S/C COMPUTER FAIL. REMOVED AND REPLACED NR 2 AOA AND A/T S/SDR GTIA010528ComputerDTW - FLT 9951 - AUTO PILOT VERTICAL SPPED WHEN COMMANDED UP OR DOWN THERE IS NO CONTROL UP TO 1500 FT PER MIN GOES DIRECTLY TO 1500 FT PER MINUTE. REMOVED AND REPLACED PITCH AXIS COMPUTER, OPS CHECKED GOOD PER DC9 MM 22-13-01. NO OTHER DISCREPANCIES NOTED. SDR DHL2001363004Computer · failedAUTOPILOTS NR 1 AND NR 2 TRIPPED OFF REPEATEDLY DURING APPROACH. AFCS SHOWS BOTH LOGIC MONITOR COMPUTERS TRIPPED. RESET AFCS AND RESEATED BOTH LOGIC MONITOR COMPUTERS AND OPS CHECK BOTH AUTOPILOT PER 22-10-00 GOOD. STATUS-CLOSED.SDR DHL2001363003Computer · malfunctionedAUTOPILOT NR 1 WILL NOT ALLOW CWS ROLL COMMAND IN CMD OR MAN MODE. SWAPPED A/P LONG COMPUTERS IAW MM 22-12-34 FOR TROUBLESHOOTING PURPOSES. OPS CHECKED NR 1 SYS IAW MM 22-11-00. NO DEFECTS NOTED. STATUS CLOSED.SDR CA010130007Computer · failed(CAN) IN THE CLIMB, SHORTLY AFTER ENGAGING AUTOPILOT, AUTOPILOT DISENGAGED FOR NO APPARENT REASON. AFTER A SUCCESSFUL RETEST, REENGAGING IS POSSIBLE WITH NO FURTHER PROBLEMS. THIS PROBLEM HAS OCCURRED IN THE RECENT PAST.THE AUTOFLIGHT COMPUTER WAS REPLACED FORSDR 20010124SG003Computer · malfunctionedAUTO PILOT PORPOISES IN CRUISE MODE ''A'' CONTINUOUSLY TRIMS STAB UP AND DOWN. REMOVED AND REPLACED AUTO PILOT PITCH COMPUTER. OPS CHECK OK IAW MM 22-11-12. (M)SDR 20001227SH019Control Unit · smokePTY - FLT 622 - DURING CRUISE, COCKPIT CREW OBSERVED SMOKE COMING FROM THE FLIGHT CONTROL UNIT. AIRCRAFT RETURNED TO PANAMA STATION FOR MAINTENANCE. AFTER AN UNEVENTFUL LANDING AT PTY STATION, MAINTENANCE TECHS PERFORMED AN INSPECTION OF THE FCU SYSTEM, THE SDR 20001129SH017Bolt · wornUPPER AND LOWER BOLTS THAT ATTACH BOTH THE MAIN ELEVATOR CABLES AND AUTOPILOT BRIDLE CABLES. (X)SDR AALA20001608Pcu · defectiveMIA - FLT 331 - ON CLIMB-OUT MIA AT 6500 FEET WITH CLIMB POWER SET, AND 250 KNOTS AIRCRAFT YAWED RIGHT AND DID NOT RESPOND TO YOKE IMPUTS. AS WINGS WERE LEVELED AIRCRAFT PORPOISED VIOLENTLY FOR APPROX 5 SECONDS. DECLARED EMERGENCY AND RETURNED MIA WITHOUT INSDR COMA0060771Afcs · malfunctionedUNCOMMANDED YAW DURING FLIGHT, A/P ON OR OFF. COULD NOT DUPLICATE. INSPECTED FLIGHT CONTROLS. NO FAULTS FOUND.SDR 20000627SH004Harness · failedSMOKE ODOR IN COCKPIT. AUTOPILOT DISENGAGED, WOULD NOT RE-ENGAGE. FOUND SHORTED TRANSISITOR , LIFTED TRACES IN SERVO ENGAGE CIRCUIT OF AUTOPILOT COMPUTER. TRANSISTOR FAILURE CAUSED BY SHORT IN SERVO ENGAGE WIRING IN ACFT HARNESS. CHAFED WIRE LOCATED 3 INCHSDR TWAA0009301Afcs · malfunctionedCREW REPORTED UNCOMMANDED PITCH CHANGES IN FLIGHT WITH AUTOPILOT NOT ENGAGED. CHECK-C 12-23-99 MCI.SDR 2000UALA00245Probe · failedBOTH AUTOPILOTS AND AUTO THROTTLE FAILED DURING CLIMB. FLIGHT DIVERTED TO DEN. *S/D* TOTAL AIR TEMPERATURE (TAT) PROBE FIN NR 11FP1 WAS REPLACED. OPERATIONAL TEST AND AUTOLAND TEST PASSED SATISFACTORILY.SDR TSAA0022120Connector · contaminatedFLT 87-KOA-HNL-AT FL190, A/C STARTED ROLLING AND YAWING INCREASING IN RATE. DISENGAGED AUTOPILOT, ROLL AND YAW INCREASED. YAW DAMPER DISENGAGED, PILOT CONTROLLED ROLL AND A/C STABILIZED. DECLARED EMERG, FOUND YAW DAMPER C/B TRIPPED DUE TO COFFEE SPILLAGE ON YASDR DLM88000615Afcs · failedAFTER TAKEOFF, F/O AIRSPEED FAILED, CAPT AND F/O MAP FAILED. ATS AND AUTO PILOT DISCONNECTED. REPLACED NUMBER 2 CADC.SDR 20000622SH015Accelerometer · faultyACCELERATION SWITCH - WHEN SUBJECTED TO VIBRATION (ENGINE AT HIGH POWER OR IN FLIGHT), SERVOS ENGAGE, BUT WILL NOT DRIVE, COMMAND BARS FUNCTION PROPER. AP LIGHT VARIES FROM FULL BRIGHTNESS TO HALF BRIGHT AT A CONSTANT RATE. REPLACED ACCELERATION SWITCH AGAIN
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