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.
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 20010125CW007Servo · misinstalledFOUND PITCH SERVO INOPERATIVE DUE TO WATER CONTAMINATION. FOUND SERVO ON TOP OF MOUNTING BRACKETT AND CLUTCH DRIVE ON TOP OF BRACKETT. SERVO AND CLUTCH DRIVE GEARS WERE ONLY SPLINING ABOUT .0156, AFTER SEVERAL TEST, UNIT WOULD FAIL. INSTALLED NEW SERVO AND SDR SWIA972133Autopilot Sys · malfunctionedWHILE ON AUTOPILOT WITH FMS COUPLED DURING DESCENT AIRCRAFT BEGAN AN UNCOMMANDED RIGHT TURN OF 25 DEGREES BANK. DISCONNECTION OF AUTOPILOT RESULTED IN SIGNIFICANT UNCOMMANDED YAW REQUIRING UNUSUAL AMOUNTS OF LEFT RUDDER AND AILERON CONTROL PRESSURES CONDITIONSDR RAAA00B1078Accessory Unit · defectiveLOWER YAW DAMPER INOP. REPLACED AUTO/PILOT ACCESSORY UNIT, OPS CHECK GOOD PER RAA GMM.SDR WRLA200013Autopilot Sys · inoperativeBOTH FCC FAULTED, AUTO PILOT INOP AFTER TAKEOFF. RETURN TO SERVICE ON AP1, AP2, FCC1 AND FCC2. ALL RETURN TO SERVICE TEST PASSED.SDR CA001201002Switch · failed(CAN) AIRCRAFT HAD 2 AIR TURNBACKS DUE TO NR 2 PITCH TRIM LEVER DISENGAGING DURING CLIMB. THE NR 1 PITCH TRIM SYSTEM WAS ON MEL, AT THIS TIME. AFTER THE FIRST TURNBACK, THE NR 2 FLIGHT AUGMENTATION COMPUTER WAS REPLACED. THE NR 2 FAC TESTED SERVICEABLE. NR 1 SDR 20010212SG015Filter · faultyYAW DAMPER COUPLER DISENGAGED DURING CLIMB-OUT. WOULD NOT RE-ENGAGE. ITEM WAS DEFERRED IAW MEL. OPEN DEFERRAL WAS CLEARED BY REPLACING THE YAW DAMPER COUPLER. THE FAILURE WAS CONFIRMED BY REPAIR STATION. FAULTY COMPONENT WAS IDENTIFIED AS CHASIS FILTER. SDR E6RA200022001Filter · shortedYAW DAMPER COUPLER DISENGAGED DURING CLIMB OUT. WOULD NOT RE-ENGAGE. ITEM WAS DEFERRED IN ACCORDANCE WITH MEL. OPEN DEFERRAL WAS CLEARED BY REPLACING THE YAW DAMPER COUPLER.THE FAILURE WAS CONFIRMED BY THE REPAIR STATION. FAULTY COMPONENT WAS IDENTIFIED AS THESDR SIMA2673Warning Light · illuminatedJFK - FLIGHT 5019 - CREW REPORTED AUTO TRIM LIGHT ILLUMINATED AFTER LANDING GEAR RETRACTION. UNABLE TO EXTINGUISH LIGHT FOLLOWING CHECKLIST PROCEDURES. CREW RETURNED TO JFK. MAINTENANCE PERFORMED OPERATIONAL CHECK OF AUTOPILOT AUTO TRIM IAW SAAB MM 22-10-00SDR SWIA971991Afcs · malfunctionedON TAKEOFF ROLL ''''AUTO PILOT FAIL'''' AND TRIM FAIL LIGHTS ILLUMINATED ON MAP. TAKEOFF WAS ABORTED ON THE RUNWAY. INSPECTED WIRING TO AUTO PILOT COMPUTERS, FCP''S, APP-65A AND MAP PANEL. ALSO INSPECTED ALL APPLICABLE CONNECTORS FOR CONDITION AND SECURITY.SDR MASA00115Control Unit · inoperativeFLT 5122 - CMH-MDW - IN FLIGHT, THE CREW RECEIVED A MACH TRIM EICAS MESSAGE. THE AIRCRAFT RETURNED TO THE FIELD WHERE MAINTENANCE REPLACED THE HSTCU AND A TEST FLIGHT WAS PERFORMED. THE TET FLIGHT WAS SATISFACTORY AND THE A/C WAS RETURNED TO SERVICE WITHOUT SDR AU001031Relay · misinstalled(AUS) NAVIGATION RELAY BOX WIRES CR101 AND CR102 (HSI COURSE ERROR TO AUTOPILOT) NOT CONNECTED.SDR MALA000537Afcs · malfunctionedEN ROUTE FROM MEM TO CLT AUTOPILOT CAUSED A/C TO PITCH DOWN. CREW TURNED OFF A/P. SUDDEN PITCH CAUSED F/A TO BE INJURED. MAINTENANCE DEFERRED A/P UNDER THE DIRECTION OF MAINTENANCE CONTROL OVER THE PHONE.SDR C2XA00CL062Switch · looseON APPROACH TO CLE CREW REPORTED RIGHT SIDE OF FIRST OFFICER''S CONTROL WHEEL (YOKE) WAS EMITTING SMOKE. A EMERGENCY WAS DECLARED AND A/C LANDED AND TAXIED TO GATE WITHOUT FURTHER INCIDENT. MX INSPECTED AND REASSEMBLED THE FIRT OFFICER''S FLIGHT DIRECTOR SYNC,SDR C2XA00IA249Afcs · malfunctionedSJT - FLT 2931 - THE CREW REPORTED THAT AT 14,500 FEET, THE AIRCRAFT PITCHED ABRUPTLY UP AND THE AUTO PILOT DISCONNECTED. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT FOR THE PURPOSE OF A FERRY FLIGHT, AND APPROVED THE FERRY FLIGHSDR 2000UALA00466Circuit Breaker · pulledAUTOPILOT WILL NOT HOLD ALTITUDE AND SPEED TRIM FAIL LIGHT ILLUMINATED. *S/D* FOUND STAB TRIM CIRCUIT BREAKER PULLED. RESET STAB TRIM BREAKER AND ACCOMPLISHED DIGITAL FLIGHT CONTROL SYSTEM TESTS, ALL TESTS CHECKED NORMAL.SDR 2000UALA00454Control Panel · failedAUTOPILOT MASTER CONTROL PANEL FAILED. *S/D* REPLACED AUTOPILOT MODE CONTROL PANEL. NO FURTHER FAILURES HAVE BEEN EXPERIENCED.SDR TWAA0011802Computer · malfunctionedTHE LEFT AUTOPILOT SELF-ENGAGED DURING TAKEOFF. ABORTED TAKEOFF AND RETURNED TO THE GATE. THE LEFT AUTOPILOT WAS DEACTIVATED AND DEFERRED PER MEL. CHECK-C 2-20-00 LAX. ---OPEN--- S/D. THE AUTOFLIGHT CONTROL SYSTEM MODE CONTROL PANEL (MCP) WAS REPLACED. TSDR CA000714014Computer · failed(CAN) BOTH DLC AUTO SPOILER FAILED AFTER LANDING WITH SPOILER DEPLOYED. BOTH YAW / SAS FAIL LIGHTS ON AND AUTO PILOT B HANDLE LOCKED OFF.MAINTENANCE RESET THE FLIGHT CONTROL COMPUTER AS PER MM 22-00-01 AND ALL RETURNED TO NORMAL.. FLIGHT CONTROL COMPUTER REPLASDR AALA20001276Autopilot Sys · malfunctionedLHT - FLT 0131 - ON CLIMB-OUT AT APPROXIMATELY FL 220 WITH AUTOPILOT OFF, FLAPS AND SLATS UP, PITCH TRIM 1 AND 2 ON YAW DAMPER 1 AND 2 ON. UNCOMMANDED FLIGHT CONTROL INPUT KICKED AIRPLANE FROM SIDE TO SIDE (SUSPECT RUDDER), DEFINITELY NOT ROLLING MOMENT, ACCOSDR SWIA971830Controller · malfunctionedAIRCRAFT CONDITIONED TO PITCH UP WITH AUTOPILOT OFF PULLED DISCONNECT TO CONTROL AIRCRAFT TROUBLESHOT AUTO PILOT AND TRIM SYSTEM FOUND BAD APP 65A. REMOVED AND REPLACED APP 65, RECONNECTED ELEVATOR DISCONNECT SYSTEM AND PERFORMED OPS CHECKS OF AUTO PILOT AND SDR DL733001134Actuator · failedAT FL 270, BEGINNING DESCENT, EXPERIENCED UNCOMMANDED ABRUPT ROLL APPROX 35-40 DEGREES TO THE LEFT. AUTOPILOT REVERTED TO CWS PITCH AND ROLL. YAW DAMPER IND SHOWED NO ABNORMAL INDICATIONS. NO TURBULENCE IN AREA. A/C IN CLEAN CONFIG. A AUTOPILOT ENGAGED ATSDR DL733001080Sensor · failedB-SYSTEM A/P APPROACHING FL 350, RAPID ROLL LEFT, DISCONNECTED AT FL 350, RE-ENGAGED B A/P, SLOWLY ROLLED RT DISCONNECTED, ENGAGED A A/P. ALSO, UNCOMMANDED SLOW ROLL TO RT, DISCONNECTED, HAD FLEW REST OF FLT. REPLACED AILERON POSITION SENSOR AND MCP PANEL.SDR ASOA00043SCircuit Board · inoperativeFLT 4511 - DURING CRUISE AT FL 260 AN AP PITCH TRIM MESSAGE APPEARED AND WENT OUT BY ITSELF. UPON DESCENT TO FL 240 CREW RECEIVED AN AP PITCH TRIM AND STAB CHANNEL 1 MESSAGE. AFTER FOLLOWING QRH PROCEDURES, THE PROBLEM APPEARED SOLVED. UPON SECOND DESCENT, SDR ASOA00043Warning System · activatedFLT 4511 - DURING CRUISE AT FL 260, AN APU PITCH TRIM MESSAGE APPEARED AND WENT OUT BY ITSELF. UPON DESCENT TO FL 240, CREW RECEIVED AN 'APU PITCH TRIM' AND 'STAB CHANNEL 1' MESSAGE. AFTER FOLLOWING QRH PROCEDURES, THE PROBLEM APPEARED SOLVED. UPON SECOND DSDR 0001459874Check Valve · cloggedEN ROUTE FROM BDL TO DTW, THE AIRCRAFT BEGAN AN UNCOMMANDED GRADUAL BANK. DISCONNECTED AUTOPILOT AND FOLLOWED COM PROCEDURES. REGAINED COMPLETE FREEDOM OF MOVEMENT OF CONTROLS PRIOR TO APPROACH AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND CHECK VALVE FOR SDR MALA000253Connector · looseANYTIME TURBULENCE IS ENCOUNTERED ON CLIMBOUT WE LOSE BOTH FLIGHT DIRECTORS, YAW DAMPENER, FTC, AUTOPILOT, AUTOTHROTTLE, TRP, ALTITUDE READOUT ON MCP. MX COULD NOT DUPLICATE PROBLEM. RERACKEDK NR 1 & NR 2 ADC. RESTATED NR 2 ALTIMETER CANNON PLUG. PERFORMED OSDR MALA000252Control Panel · failedTURBULENCE CAUSES FLIGHT DIRECTOR, YAW DAMPER, FTC, AP,AT, TRP AND ALTITUDE READOUT TO FAIL RESETTING AP MASTER RESTORES ITEMS WITH NO FURTHER PROBLEMS FOR REST OF FLIGHT. MX REPLACED MODE CONTROL PANEL DUE TO MANY MCP FAULTS. FGC SYSTEM OPS CHECK GOOD.SDR MALA000247Control Panel · failedWHEN TURBULENCE ARE ENCOUNTERED WE LOSE BOTH FLIGHT DIRECTOR, YAW DAMPER, FTC, AUTOPILOT, AUTOTHROTTLE, TRP, ALTITUDE READOUT ON MCP. ONCE IN SMOOTH AIR EVERYTHING CAN BE RESET BUT REPEATS AS SOON AS TURBULENCE ARE ENCOUNTERED. MX REMOVED AND REPLACED DISDR 20000413SH062Roll Servo · inoperativeFOUND AUTOPILOT ROLL SERVO IDLER GEAR ATTACH NUT BACKED OFF SCREW AND OUTPUT GEAR BEARINGS DEFECTIVE DURING COMPLIANCE WITH SB KS271C-5 ALERT DATED FEB 1, 2000. SUBMITTER STATED FAILURE COULD CAUSE SERVO TO REMAIN ENGAGED EVEN WHEN AUTOPILOT IS DISENGAGED. SDR USAASB00078Coupler · failedTPA - FLT 8050 - FLIGHT RETURNED TO FIELD AT TPA DUE TO EXCESSIVE RUDDER TRIM TO MAINTAIN WINGS LEVEL. A CORRECTION OF 3 TO 3.5 DEGREES LET, AT 250 KNOTS, AT FL100 WAS REQUIRED. FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCESDR 20000417SH015Servo · failedSECONDARY YAW DAMPER SERVO SN 1053M FAILED TO ENGAGE. THIS SERVO HAS ONLY 79.5 HOURS SINCE LEARJET FACTORY OVERHAUL. THIS SERVO SHOULD GO 3,000 HOURS BETWEEN MANDATORY OVERHAULS. INSTALLED A WARRANTY REPLACEMENT SERVO AND OPS CHECKED GOOD. (X)SDR CA000320010Dampener · leaking(CAN) GREEN HYDRAULIC LOW LEVEL ANNUNCIATOR ON. LEFT YAW DAMP FOUND LEAKING.SDR SWAA000512Yaw Damper · malfunctionedACFT EXPERIENCED A MOMENTARY UNCOMMANDED YAW DURING APPROACH. REMOVED AND REPLACED YAW DAMPER COUPLER, P/N 4036952-906, S/N 94023899, RUDDER PCU, P/N 65-44861-12, S/N 3425AC, AND SOLENOID VALVE, P/N 881600-1001, S/N 16126 PER MM.SDR 20000518SH013Circuit Breaker · failedDURING TROUBLESHOOTING OF KING KAP-140 AUTOPILOT SYSTEM, FOUND AUTOPILOT CIRCUIT BREAKER TO BE THE ''NON-PULLABLE'' TYPE CONTRARY TO THE PILOT OPERATING HANDBOOK EMERGENCY PROCEDURES FOR AUTOPILOT RUNAWAY **TONY, ISAAC PUT ENG IN SYS**TRIM INDICATION. UPON FLSDR DHL2000806001Autopilot · failedAUTOPILOT WILL NOT TRACK, ROLLS 30 DEGREE BANK TURNS. DEFERRED PER MEL 22-1.SDR AU001299Computer · faulty(AUS) AUTOFLIGHT CONTROL SYSTEM (AFCS) COMPUTER FAULTY.SDR HEEA065863Amplifier · malfunctionedROLL CHANNEL WILL NOT ENGAGE.SDR AWXA0000014Transducer · malfunctionedAIR TURNBACK FLIGHT CONTROL FAULTS, REF LP 7584603, NR 2 ELAC PITCH FAULT WHILE CLIMBING THROUGH 18,000 FT. REMOVED AND REPLACED COMMAND AND MONITOR UNIT TRANSDUCERS. ALSO, EXTENSIVELY TROUBLESHOT WIRING PER TECH SUPPORT ALERT. AIRCRAFT HAS REPETITVE ELAC 2SDR CA000209030Damper · leaking(CAN) AFTER REACHING CRUISE ALTITUDE GREEN HYD SYS SLOWLY DECREASED UNTIL ECAM WARNING ILLUMINATED. INVESTIGATION FOUND LEFT YAW DAMPENER ACTUATOR LEAKING. YAW DAMPENER REPLACED.SDR HEEA065584Sensor Dualrate · malfunctionedSCAS YAW KICKS OFF IN TURBULENCE. PART IS BAD FROM STOCK. WAS INSTALLED FOR TROUBLESHOOTING AND CAUSED A DIFFERENT PROBLEM. TIME SINCE REPAIR 0:00.SDR 2000ZZZM88Yaw Damper · malfunctionedYAW DAMPER ENGAGED ON TAKEOFF ROLL. TAKEOFF ABORTED. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE FLIGHT CONTROL PANEL. SYSTEM TESTS SATISFACTORY. (M)SDR HEED065803Amplifier · failedAMPLIFIER TRIPS CIRCUIT BREAKER. REPLACED UNIT.SDR 9905413218Yaw Damper · leakingDURING DESCENT, RECEIVED HYD G RSVR LOW LVL ECAM MESSAGE. FOLLOWED COM PROCEDURES AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED LEAKING YAW DAMPER 3CC1. OPERATIONAL CHECK NORMAL.SDR HEED065778Amplifier · failedAMPLIFIER TRIPS CIRCUIT BROKEN. REPLACED UNIT.SDR AT9900910Pcu · malfunctionedDURING CRUISE, EXPERIENCED RUDDER HARDOVER. AIRPLANE ROLLED LEFT THEN RIGHT APPROX 30 DEGREE BANK WITH AUTOPILOT ON. REMOVED AND REPLACED FLIGHT DATA RECORDER, COCKPIT VOICE RECORDER, YAW DAMPER COUPLER, RUDDER AUXILIARY POWER CONTROL UNIT, RUDDER MAIN POWERSDR USAASB99294Coupler · failedBWI - FLT 2674 - EN ROUTE FROM TPA TO BOS, AT FL230, A/C ENCOUNTERED SOME LIGHT CHOP AND STARTED TO OSCILLATE. YAW DAMPER APPEARED NORMAL WITH NO LIGHT INDICATIONS. AIRCRAFT CONTINUED TO OSCILLATE. CAPT LEVELED FLT AT FL310 AND TURNED YAW DAMPER OFF. NO CHSDR 99UAL900627Afcs · malfunctionedON CLIMBOUT THE AIRCRAFT EXPERIENCED UNCOMMANDED YAW AND THE AUTOPILOT DISCONNECTED. *S/D* PINS 25 AND 26 SHORTED TO PIN 24 IN CONNECTOR 4079J OF THE E1-3 SHELF. REMOVED THE SHORT, OPERATIONS CHECK NORMAL.SDR AWXA9900434Transducer · failedAMBER FLT CONT ELAC 2 PITCH FAULT MSG ON UPPER ECAM. REPLACED TRIMMABLE HORIZONTAL STABILIZER TRANSDUCER, OPS CK GOOD. CURRENT HISTORY: 27 NOV A/C WAS WRITTEN FOR PITCH FAULT WITH NO FAULT FOUND. REPLACED ELAC2, TEST GOOD. RECOMMENDATION: REMAIN OPEN PESDR HEEA065139Amplifier · failedPITCH AND ROLL WILL NOT STAY ENGAGED.SDR HEEA065132Actuator · failedELEVATOR SYSTEM WILL NOT MONITOR TEST.
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