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 DXTA200702345Servo · inoperativeBOTH AUTOPILOTS FAILED IN FLIGHT AND WOULD NOT RE-ENGAGE. REMOVED AND REPLACED ELEVATOR SERVO, PERFORMED FUNCTIONAL TEST OF FLIGHT GUIDANCE / AUTO PILOT SYSTEMS WITH NO DISCREPANCIES NOTED. WORK PERFORMED IAW HAWKER SPZ-8000 M.M. 22-14-00SDR DJFA2007077Computer · failedTRIP NR 1204871- CREW REPORTED A PITCH TRIM FAILURE. CREW PERFORMED EMERGENCY PROCEDURES AND CONTINUED TO DESTINATION. MAINTENANCE DISCOVERED THE AUTOPILOT COMPUTER MALFUNCTIONED. THE COMPUTER WAS REPLACED.SDR DXTA200702339Autopilot Sys · malfunctionedWITH AUTOPILOT CONNECTED RED (AP PITCH TRIM FAIL) ANNUNICTOR ILLUMINATED. WITH AP ON WE HEARD AN INTERMITTENT CLICK ( LIKE WHEN A CB POPS) BUT ALL CB'S ARE IN. [07-23-07] COMPLETED COMPLETE TRIM SYSTEM OPERATIONAL CHECK IN NORMAL EMERGENCY AND AUTO-PILOT. SDR DXTA200702336Autopilot Sys · malfunctionedDURING LEVEL FLIGHT AT FL340 ON THE LT AUTOPILOT, THE AIRCRAFT STARTED A STEEP CLIMB WITH NO INPUTS REQUESTED. AFTER RECOVERING AND SWITCHING TO THE RT AUTOPILOT (WHICH WORKED FINE AND NORMALLY) THE COMMAND BARS ON THE LT SIDE MADE ERRATIC MOVES UP AND DOWN. SDR AMTA200700335Pitch Control · out of rigEITHER AUTOPILOT WHEN ENGAGED AC INITALLY PITCHED THEN TRIMS NOSE DOWN UNTIL REACHING A/P LIMIT AND BEGINS UNDEMANDED DESCENT. RIGGED MECH PITCH FEEL/ TRIM ASSY IAW MM 27-41-17. (INPUT AND SERIES TRIM PUSH RODS WERE OFF) CKD RIG OF A/P STAB SERVO IAW MM 22-1SDR AMTA200700333Feel Unit · out of rigIN FLIGHT ABOVE 20,000 FT, WHEN AUTOPILOT ENGAGED PITCH TRIM MOVES FULL NOSE DOWN AND AC LEAVES ASSIGNED TRIM MOVES FULL NOSE DOWN AND AC LEAVES ASSIGNED ALTITUDE. AP LIMIT FLAG DISPLAYS. RIGGED MECHANICAL PITCH FEEL IAW MM 27-41-17. OPS CHECK NORMAL. (K)SDR SWIA200718480Autopilot Sys · malfunctionedFLT 3900 - PRE-SELECTED ALTITUDE CHANGES SPONTANEOUSLY AFTER BEING SET CAUSING THE AUTOPILOT TO OVERSHOOT ASSIGNED ALTITUDES. FCC DIAGNOSTICS HAD NO FAULTS LOGGED. ALTITUDE SELECT FUNCTIONS NORMALLY. NO DISCREPANCY NOTED.SDR DXTA200702329Controller · inoperativeIN CRUISE ALTITUDE OF FL200 MACH NR APPEARED. SELECTED C/O BUTTON ON AUTOPILOT PANEL AND THE BUTTON REMAINED IN THE DEPRESSED POSITION. NO OTHER MODES WERE ALLOWED TO BE SELECTED AND AUTO PILOT WOULD NOT RE ENGAGE. REMOVED AND REPLACED FLIGHT CONTROLLER GC-SDR DXTA200702325Roll Servo · inoperativeAT CRUISE FL 450 WOULD FAIL TRANSFER TO FGB-B AND RESET WITHIN 30 SECONDS THEN FGC B WOULD FAIL TRANSFER TO FGC-A THEN RESET WITHIN 30 SECONDS. THE AUTOPILOT WOULD DISCONNECT SOMETIMES. GAINED ACCESS TO IMT PAGE. INSPECTED AND FOUND FAULT CODE NR 1250 IAC/AISDR DXTA200702324Vertical Gyro · faultyAUTOPILOT MALFUNCTION - LEVEL AT 41000 MSL, THE AUTOPILOT AGGRESSIVELY PITCHED UP TO OVER 1000 FPM. THE AUTOPILOT WAS DISCONNECTED. AFTER 1 MINUTE, THE AUTOPILOT WAS RECONNECTED AND PROBLEM REOCURRED. REMOVED FAULTY LT SIDE PITOT STATIC PORT HOSE AND NR 1 SDR FDKA200706298Warning System · malfunctionedFDM 6152 FLL (1250 PHX LCL). YAW DAMPER FAIL MESSAGE. MOC RESET WITH THE CREW AND OPS CHECKED.SDR 2007UALA02143Computer · no testNO LAND THREE DISPLAYED NO MALFUNCTION NOTED. [07-20-07] MCDP CODE "SLAT SW-FCC L", ACP MM 22-00-03 & CAT III CHK PER MM 22-10-00, THRUST MANAGEMENT COMPUTER FAILED TEST. RPL TMC PER MM 22-31-01, OP CK GOOD. AC REMAINS IN CAT III STATUS .SDR FDKA200706286Autopilot Sys · malfunctionedFDM 6159 ATL-GPT (1105 PHX LCL). CREW RETURNED TO THE GATE DUE TO AUTO PILOT/ YAW DAMP FAIL MESSAGE. MX RESET, OPS CHECKED NORMAL.SDR FDKA200706284Autopilot Sys · malfunctionedFDM 6203 ATL-CAE (0443 PHX LCL). AUTO PILOT FAIL MESSAGE. MX RESET THE AUTO PILOT AND OPS CHECK NORMAL ON THE GROUND.SDR DXTA200702275Roll Servo · inoperativeDURING DESCENT FROM CRUISE AUTOPILOT ROCKS WINGS BACK AND FORTH BETWEEN FL410 AND FL360 WITH A/P DISCONNECTED AIRCRAFT FLIES LEVEL WITH NO ROLL. REMOVED AND REPLACED THE ALLERON SERVO MOTOR WITH A MODIFIED SERVO MOTOR IAW CESSNA CITATION 750 AMM 22-10-01. OPESDR 2007UALA01853Autopilot Sys · failedCENTER & RIGHT AUTOPILOTS FAILED CAUSING A DIVERSION. [07-31-07] RE-ALIGNED RT FCC. STILL HAD PROBLEM. REPLACED LEFT ELEVATOR SERVO VALVE ASSY. RELOADED NAV DATABASE. TESTS OK.SDR R61A20070011Power Supply · burnedAUTO PILOT/AUTO THROTTLE DISENGAGED, FOLLOWED BY MAU 3 FAIL INDICATION, THEN CREW HAD SMOKE ODOR AND AFT CARGO SMOKE ALONG WITH WARNING. CREW DIVERTED AND FOLLOWED QRH PROCEDURES, INDICATION WENT AWAY AND LANDED WITHOUT INCIDENT. MAINTENANCE WAS DIPATCHED TOSDR NWAA071863251Computer · malfunctionedIN CRUISE AT FL300, HAD HARD RUDDER KICK (NOTED AS 5-7 DEGREE HEADING DEFLECTION), THEN SMELLED BURNING ELECTRICAL ODOR. FAC 1 FAULT ILLUMINATED. DID NOT RESET FAC. DIVERTED TO LAS. YAW DAMPER 1, RUDDER TRIM 1, RUDDER TRAVEL LIMITER 1, ON ECAM. AIRCRAFT LSDR DL76L070484Actuator · leakingCENTER HYD LOW LEAK TRACED TO LT YAW DAMPER SERVO ACTUATOR P/N REQUIRED 1536600-7, LEAY SERVO S/N 1979. A/C DISP IAW MEL 22-21-01 CAT C. C HYD SYSTEM SERVICED TO FULL WITH 6 GALLONS. REMOVED AND REPLACED LEFT YAW DAMPER SERVO PER AMM 21-21-02 MANF PN 154050SDR CA070504009Computer · malfunctioned(CAN) FLIGHT DIRECTOR CB TRIPPED AND WILL NOT RESET. (TC NR 20070504009)SDR QXEA200700715Computer · inoperativePDX - ON FLIGHT 2211, ON CLIMB-OUT FO WAS HAND FLYING THE AIRCRAFT WHEN THE AUTOPILOT ENGAGED AND TURNED TO THE RIGHT. THE FO HIT THE DISENGAGE BUTTON ON THE YOKE AND THE AUTOPILOT DISENGAGED AND FLEW NORMALLY. AFTER THAT, THE FO WAS STARTING A SHALLOW RIGHTSDR FDKA200704175Dau · malfunctionedFDM 5975 ATL-BMI (0948 PHX LCL). AUTO FAIL AND RUDDER SYSTEM 1 AND 2 INOPERATIVE. MX RE-RACKED IC 600 AND DAU 1 AND OPS CHECKED GOOD.SDR DXTA200702130Roll Servo · inoperativeAILERON OSCILLATION BACK AND FORTH DURING CRUISE, WORSENING DURING DESENT WITH AUTOPILOT ON. SWITCHING FGC HAD NO EFFECT. REMOVED AND INSTALLED A NEW POWER SERVO. OPS CHECKS GOOD AT THIS TIME. ALL WORK DONE IAW MM CHAPTER 22-10-01.SDR 2007UALA01273Autopilot Sys · malfunctionedWITH CENTRE AUTO-PILOT IN CMD IN CLEAR AND SMOOTH AIR AIRCRAFT ABRUPTLY PITCHED NOSE DOWN, A-C LOST 30 FEET AND IMMEDIATELY HARSHLY PITCHED UP THEN BEGAN TO PORPOISE. [SUP 05-18-07] REPLACED CTR FLIGHT CONTROL COMPUTER. REF SMC3, NEEDS CAT 3. PERFORMED CASDR NSVA20070098Switch · lack of lubeYAW DAMPER BUTTON STUCK IN ENGAGED POSITION. LUBED AND FREED STUCK SWITCH, SYSTEM OPS CHECK GOOD AT THIS TIME.SDR DXTA200702092Indicator · out of rigDURING TAXI, YD NOT CENTERED AND FGC, B FAIL CAS MESSAGE CAME ON INTERMITTENT. IN FLIGHT DURING TURBULENCE THE YD NOT CENTER CAS MESSAGE CAME ON INTERMITTENT. [SUP 4-19-07] FOUND TRIM SWITCH INDICATOR OUT OF RIG. RIGGED IAW CE-750 M.M. 27-14-00. ALSO, ADJUSDR SWIA200718093Computer · malfunctionedAUTOPILOT PITCHES AIRCRAFT UP AND DOWN. REPLACED NR 1 AUTOPILOT COMPUTER IAW MM 22-00-00, P/N - 622-8315-102 S/N OFF - 1303.SDR SWIA200718089Computer · malfunctionedWITH AUTOPILOT ENGAGED, AIRCRAFT PITCHED NOSE UP THEN NOSE DOWN. REPLACED NR 2 AUTOPILOT COMPUTER.SDR DXTA200702020Trim System · unknownDURING CLIMB WITH THE AUTOPILOT ENGAGED THE AUTOPILOT DISENGAGED ALONG WITH ILLUMINATION OF THE A/P PITCH TRIM CAUTION MESSAGE 3 TIMES AFTER THE THIRD FAILURE THE PRIMARY PITCH TRIM WOULD NOT FUNCTION. PERFORMED HORIZONTAL TRIM SYSTEM FUNCTIONAL TEST AND RAN SDR FDKA200703111Autopilot Sys · malfunctionedFDM 5969 AVL-ATL (0329 PHX LCL). AUTO PILOT AND YAW DAMP FAIL MESSAGES AT POWER UP. CYCLED AIRCRAFT POWER AND FAULT CLEARED.SDR HALA0700085Receiver · malfunctionedETOPS SIGNIFICANT SYSTEM, "NO LAND 3" DISPLAYED ON ASA WITH APP MODE NOT SELECTED AND AUTOPILOT/FD ENGAGED OR NOT ENGAGED (ASA NO LAND 3 DISPLAYED IN CRUISE FL 340 NO RESET), (ON APP AMBER LOC AND G/S FLAG CAPT ADI. REPLACED NR 1 MMR, OPS CK OK PER MM 34-31-0SDR DXTA200701968Motor · inoperativeAIRCRAFT CONTINUOUSLY DUTCH ROLLS, ALL ALTITUDES AND SPEEDS- ONE TO TWO DEGREES LEFT & RIGHT. SWAPPED YAW DAMPERS ON UPPER RUDDER- STILL NO IMPROVEMENT. REMOVED AND REPLACED AILERON SERVO MOTOR IAW CE750 MM CH 22-10-01. GROUND CHECKED GOOD.SDR NWAA070643224Computer · malfunctionedAT CRUISE, FLIGHT LEVEL 340, FAC 1 FAIL LIGHT ECAM MESSAGE ANNUNCIATED. COMPLIED WITH COM PROCEDURE, BURNED INSULATION ODOR NOTED ON FLIGHT DECK, 1ST CLASS. ODOR DISSIPATED WITH FAC TURNED OFF, CIRCUIT BREAKER PULLED. FLIGHT DIVERTED TO MIA. AIRCRAFT LANDESDR DXTA200701963Warning System · malfunctionedAFTER ONE HOUR OF CRUISE FLIGHT THE TRIM CLACKER ACTIVATED AND RAN CONTINUOUSLY (AUTO-PILOT WAS NOT TRIMMING) AT LOWER ALTITUDES AND HIGHER TEMPS THE CLACKER SILENCED AND WORKED NORMALLY. C/W AUTOPILOT GROUND FUNCTIONAL CHECKS. SYSTEM OPS CHECKS GOOD ON GROUNDSDR DXTA200701927Computer · malfunctionedAUTO PILOT PITCHED OVER FROM LEVEL FLIGHT AT FL360 AND MACH .78 OR 260 KTS IND. WE LOST 450 FT UPON THE VIOLENT PITCHING MOMENT AND VERY ABRUPT TAIL FLUTTER. THIS HAPPENED ON THE L-AFCS, FLIGHT DIRECTOR VERY ERRATIC IN ALL MODES AFTER PITCHING MOMENT. REPLASDR DXTA200701907Trim System · stuckAFTER TAKEOFF, COULD NOT ENGAGE AUTOPILOT. MANUAL PITCH TRIM STUCK, COULD NOT MOVE. ELECTRIC TRIM NORMAL. YAW DAMPER OPS NORMAL, PRESSED AUTOPILOT RELEASE BUTTON SEVERAL TIMES IN ORDER TO GET AUTOPILOT TO ENGAGE WITH NO SUCESS . AFTER LANDING , MANUAL SDR FDKA200701030Autopilot Sys · malfunctionedFDM 6137 JFK-ORF (0744 PHX LCL). AUTO PILOT WILL NOT ENGAGE. RESET SYSTEM, OPS CHECK GOOD.SDR DXTA200701874Trim System · failedAUTOPILOT PITCH TRIM FAILED AFTER TAKEOFF WE WERE UNABLE TO CONTROL TRIM W/YOKE THUMB SELECTOR AUTOPILOT WAS FUNCTIONAL AFTER WE TRIMMED AIRCRAFT IN SECONDARY DISCONNECT POSITION TRIM BECAME SEMI FUNCTIONAL UPON ARRIVAL. TROUBLESHOT SYSTEM AND DETERMINED THATSDR UPS07M48877Computer · inoperativeATB - DURING T/O "AP OFF" AND "ATS OFF" AND WILL NOT ENGAGE. DURING CLIMB, CRUISE AND DESCENT ALL ENGINE AND FMS UNAVILABLE. REMOVED AND REPLACED FCC-1 IAW MM 22-01-03-4.SDR DXTA200701842Squat Switch · disconnectedAUTOPILOT WILL NOT FOLLOW HEADING BUG COMMAND. FOUND BOTH SQUAT SWITCHES DISCONNECTED. RECONNECTED BOTH SQUAT SWITCHES IAW MM 32-60. PERFORMED OPERATIONAL CHECK OF AUTOPILOT. OP CHECKS GOOD.SDR FDKA200701003Yaw Damper · disengagedFDM 6189 BDL-JFK (0520 PHX LCL). ABORTED TAKEOFF DUE TO THE YAW DAMPNER SYSTEM DISENGAGING WHEN INITIATING TAKEOFF ROLL. MX TROUBLESHOT AND OPS CHECKED GOOD.SDR QXEA200700009Irs · failedDEN - FLIGHT 4340, RECEIVED A YAW DAMPER INOP STATUS MESSAGE, PITCH FEEL FAULT STATUS MESSAGE, AUTOPILOT FAILURE, AND PFD AND MFD FAILURES (RED X) ON FO SIDE. RETURNED TO THE FIELD AND ACCOMPLISHED A UNEVENTFUL LANDING. MAINTENANCE REPLACED THE NR 2 INERITALSDR MASA200602765Yaw Damper · failedASH 2973 FAT. ABORTED TAKEOFF DUE TO A YD NR 1 FAILED. MX RE-ENGAGED THE YD AND DEPARTED WITHOUT INCIDENT.SDR MASA200602766Computer · malfunctionedASH 2973 PHX. CREW REPORTED A YD NR 1 DISENGAGING. MX REPLACED THE FCC NR 1 CARD.SDR MASA200602752Actuator · malfunctionedASH 7118 IAD. PILOT REPORTED THAT THE NR 2 YAW DAMPER WOULD NOT ENGAGE. MX REMOVED AND REPLACED ACTUATOR NR 2.SDR SWIA200617452Computer · malfunctionedAFTER DISCONNECTING A/P ON APPROACH AT 500 FEET AILERONS FELT FROZEN IN POSITION. REPLACED 1A AND 2A FCC CARDS. OPS CHECK GOOD IAW MM 22-11-00. P/N OFF: 622-9815-704, S/N OFF: SCLW.SDR MASA200602739Computer · malfunctionedASH 2753 PHX. YD1 DISCONNECTED IN FLIGHT. MX RESET FCC, OPS CHECKED GOOD.SDR CA061221004Autopilot Sys · malfunctioned(CAN) DURING AN APPROACH TO RUNWAY 24 RIGHT AT THE MFG PLANT, BOTH AUTO-PILOTS WENT OFF LINE. THE MASTER CAUTION LIGHTS WERE OFF ON THE AUTO-PILOTS. A/C WAS ABLE TO LAND. (TC NR 20061221004)SDR DXTA200601799Warning Light · illuminatedHAD MASTER CAUTION FOLLOWED BY TWO FADEC FAIL MESSAGES DURING TO ROLL ABORTED - LIGHTS WENT OUT "YD LOWER FAIL" CAME ON DURING ABORT AND STAYED ON. PURGED LARGE AMOUNT OF WATER FROM NR 1 PITOT SYSTEM IAW : CE 750 M/M 34-11-01. ACCOMPLISHED PITOR/STATIC SYSTEMSDR DXTA200601786Processor · inoperative(MAU 1 FAILURE), AMBER CAS NO AIR DATA, AHRS; AUTO PILOT' ETC, ON LT SIDE IN FLIGHT. REPLACED NR 1 NIC PROC MODULE IAW MM 34-17-00. OPS OK IAW MM 34-23-10.
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