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 QXEA200800179Servo · jammedPDX - FLIGHT 2193 (OTH-PDX) ON APPROACH WITH THE AUTOPILOT ON, EXPERIENCED A UNCOMMANDED ROLL TO THE LEFT. AUTOPILOT WAS TURNED OFF AND THE WHEEL APPEARED TO BE JAMMED (NO MOVEMENT POSSIBLE). CONTROL THEN BECAME UN-JAMMED AND OPERATED NORMALLY AFTER A FEW SESDR DXTA200802811Pcb · inoperativeINTERCEPTED ILS LOCALIZER WITH AUTOPILOT ENGAGED ABOUT 3 MILES BEFORE GLIDESLOPE INTERCEPT AUTOPILOT ABRUPTLY PITCHED DOWN 4 TO 5 DEGREES THEN UP A FEW DEGREES WITH A SMALL AMOUNT OF BANK. REPLACED 2B10C CARD AND CHECKED IAW A/C SYS MANUAL, COMPLETED IAW MM 22SDR TRAX200800152Autopilot Sys · malfunctionedSTAB TRIM / MACH TRIM / AP ND CAUT MSG ON ARRIVAL INTO COLUMBIA. EMERGENCY DECLARED & EMERGENCY EQUIPMENT ON STANDBY AS A PRECAUTION. AUTOPILOT SYSTEM.SDR UALA2008111300446Accessory Unit · malfunctionedLANDED UNDER AMBER ALERT DUE TO A TRIM PROBLEM. EXTENSIVE TROUBLESHOOTING PERFORMED. FOUND FAULTY AUTOPILOT ACCESSORY UNIT. REPLACED THE AUTOPILOT ACCESSORY UNIT.SDR USAA920080187Computer · odorFLT NR 1650, COCKPIT GLARESHIELD LIGHTING PANEL HAD AND ODOR OF ELECTRICAL HEAT AFTER ADJUSTING RHEOSTATS AREA FOR GLARESHIELD LIGHTING AND PULLED CB Z234 AND Y2345. FLIGHT LANDED WITHOUT INCIDENT AND NO EMERGENCY WAS DECLARED. CLT MAINTENANCE REMOVED AND RSDR 2008FA0000157Yaw Damper · faultyTHIS PART FAILED TO OPERATE DURING FIRST FLIGHT AFTER INSTALLATION AT CRUISE.SDR 2008FA0000101Yaw Damper · faultyTHIS PART FAILED TO OPERATE DURING FIRST FLIGHT, AFTER INSTALLATION, AT CRUISE.SDR DXTA200802746Servo · malfunctionedAUTO PILOT DISCONNECTS IN FLIGHT BY ITSELF. REMOVED AND REPLACED AILERON SERVO IAW MM 22-10-00. C/W AUTOPILOT SERVO DRIVE ADJUSTMENT AND TEST IAW MM 22-10-02. OPS CHECK GOOD.SDR 2008UALA0051Unknown · unknownNO LAND 3 DEGRADATION IN AUTOLAND SYSTEM PRIOR TO APPROACH (BEFORE LAND 3 AUTOLAND STATUS ANNUNCIATION).SDR ASAA0852453Autoland Sys · malfunctionedDURING AUTO LAND EVALUATION THE RIGHT MAIN LANDING GEAR TOUCHED DOWN TO THE LEFT OF THE RUNWAY CENTERLINE. EVALUATION UNSATISFACTORY. PERFORMED FIM 22 11 TASK 825. NO FAULTS LOGGED ON EITHER FCC. PERFORMED LAND VERIFY TEST PER FIM 22 11 00 TASKS 700 801 WISDR DXTA200802741Actuator · inoperativeAPPROX 5 TO 10 MINS AFTER T/O, CYAN FGC A FAIL LIGHT ILLUMINATED. REMOVED AND REPLACED BOTH NR 1 & 2 LINEAR ACTUATOR. WITH REPAIRED UNITS FROM HONEYWELL RS LV22992K PER MM CHAP 27-24-00. GROUND OP'S CHECKED GOOD
SDR HNAA0800003Panel · failedCAPTAINS 802 PANEL IS INOP AND SIMUTANEOULSY SMELLED A STRONG ELECTRONIC SMELL. REPLACED CAPTAINS 802 PANEL, OPERATIONAL CHECK GOOD.SDR UIEA200800005Selector Panel · failedA/P F/D SYSTEM "A" ROLL DC CIRCUIT BREAKER POPPED, PREVIOUSLY DETECTED ELECTRICAL ODOR MOMENTARILY.SDR QXEA200702032Trim System · malfunctionedPDX - FLIGHT 2188 - RECEIVED A MISTRIM NOSE UP AND TRIM NOSE DOWN MESSAGE WHEN LEVELING OFF FROM CLIMB AND DESCENT. RAN CHECKLIST AND DE SELECTED AUTOPILOT. TRIM FORCE WAS OPPOSITE OF MESSAGE, AND MESSAGE WENT AWAY. MAINTENANCE PLACED THE SYSTEM ON MEL 22-1SDR DXTA200702712Computer · inoperativeRUDDER BOOST FAIL LIGHT CAME ON AND YAW DAMPNER/AUTOPLOT KICKED OFF AT F230 LEVEL FLIGHT AT THE SAME TIME. REPLACED #1 FGC-4007 WITH OVH. UNIT IAW ROCKEWELL COLLINS MANUAL 523-0225807-0411A REV 9 OCT. 2005. GROUND OPS CHECK GOOD.SDR HEER118499Transducer · malfunctionedCOLLECTIVE LINK CAUTION ON PFD WITH COLLECTIVE DOWN AND LOCKED WITH ENGINES AT FLY. REPLACED TRANSDUCER.SDR DXTA200702682Controller · inoperativeAUTOPILOT INOP AMBER TURN KNOB INDICATION ON PFD'S. TURN KNOB WAS IN THE CENTER POSITION. POSITION. REMOVED AUTOPILOT CONTROLLER & INSTALLED SERVICEABLE AUTOPILOT CONTROLLER REMOVED FROM A/C 560XL-5176 N876QS FOR CONTINUED SERVICE ON 560-5264 N664QS AUTO PILOSDR DXTA200702672Actuator · inoperativeDURING T/O ROLL PRIOR TO 80KTS WE HAD THE FOLLOWING: RED NO T/O MESSAGE. Y/D NOT CENTERED. FGC FAIL. REMOVED AND REPLACED YD LINEAR ACTUATORS. PERFORMED OPERATIONAL CHECK SATISFACTORY. WORK DONE IAW 750 MM CHAP 27-24-00.SDR SWIA200718941Computer · malfunctionedFLT 6389 - RECEIVED STAB TRIM RUNAWAY AURAL WARNING IN FLIGHT. REPLACED NR 2 FCC UNIT, OPS CHECKS GOOD ON AUTO PILOT AND TRIM FUNCTIONS, IAW 22-10-00.
SDR ASAA0752351Knob · looseSELECTOR KNOB ON ALTITUDE SELECT MCP IS LOOSE. TIGHTENED LOOSE KNOB.SDR 2007UALA04797Autopilot Sys · malfunctionedRTFL DUE TO INABILITY TO ENGAGE AP1 & AP2, CURRENT WEATHER & TURBULENCE IN THE AREA. FOUND FAULTY AUTOPILOT FLIGHT CONTROL PANEL. REPLACED AUTOPILOT FLIGHT CONTROL PANEL.SDR 2009FA0000077Autopilot Sys · failedAUTOPILOT WILL NOT INITIATE, UNABLE TO ENGAGE SYS.SDR AMTA200700590Module · unserviceableRT YAW DAMPER EICAS MSG DISPLAYED. REMOVED AND REPLAYED YDM IAW MM CTL: 22-21-04, OPS CHECK GD. (K)SDR CA071119001Control Module · inoperative(CAN) (ALT) LAMP DID NOT ILLUMINATE ON MODE CONTROL. ALTITUDE CAPTURE WAS NORMAL WITH ALT CAPTIONS (ON) AS DISPLAYED ON BOTH EADI SCREENS. (TC NR20071119001)SDR CA071106012Circuit Breaker · failed(CAN) ENROUTE AT FL300, THE CREW EXPERIENCED AN AUTO PILOT DISENGAGEMENT AS WELL AS THE LOSS OF THE FOLLOWING, YAW DAMPER, MACH TRIM, CAPTS. PITOT STATIC, NR 1 ENG ANTI ICE, RADAR ALTIMETER, NO 2 EGT AND SEVERAL OTHERS. THE CREW ATTEMPTED A RESET OF THE NR 1SDR ASAA0752188Switch · faultyTHE "A" AUTO PILOT WILL NOT ENGAGE. FFR SHOWS CHANNEL AAP DISCONNECT SWITCH INPUT INVALID. REPLACED S231 SWITCH IAW 22-11-41.SDR NOCA16207Computer · intermittentFOUND LEFT A/P ENGAGES INTERMITTENTLY REPLACED LEFT AFCS PER MM 22-11-01.SDR QXEA200701624Unknown · unknownSEA FLIGHT NR 2367: Y/D DISENGAGED IN CLIMB WITH FLASHING MESSAGES ON PFD'S. A/P WAS NOT ENGAGED AT THE TIME. CLEARED MESSAGES PER E/A CHECKLIST. ENGAGED A/P, Y/D WORK NORMAL. MAINTENANCE CLEANED SCREEN ON IOP BOX AND RE-RACKED NR 1 FGM. C/W CAT 3 CHECK IASDR ASAA0752147Control Panel · unknownALTITUDE SELECTOR FROZEN ON MCP PANEL (STUCK AT 50,000). CYCLED MODE CNTL PANEL POWER. DISPLAY CONTROL RETURNED. MCP CHECKS OK.SDR DXTA200702554Control Servo · inoperative(B) HYDRAULIC VOLUME LOW AND ILLUMINATED IN FLIGHT. REMOVED AND REPLACED THE ELEVATOR SERVO. OPS CHECKS GOOD IAW MM 22-10-01.SDR SIMA200729907Dampener · malfunctionedSUBTLE YET NOTICEABLE UNCOMMENTED RIGHT YAW DURING FLIGHT WITH AUTO PILOT ON. AILERONS TRIED TO CORRECT. NO ENGINE TROUBLE. FELT AS THOUGH RUDDER WAS BEING PRESSED. FLT CONTROL SYNOPTIC PAGE REVEALED NOTHING ABNORMAL. CAUTION DISAPPEARED WHEN AUTO PILOT WSDR SIMA200729704Module · malfunctionedYAW DAMPER AND AUTOPILOT WILL NOT ENGAGE. DISCONNECT AURAL ALERT KEEPS COMING ON. GA MODE COMES ON UNCOMMANDED. REMOVED AND REPLACED YAW TRIM MODULE OPERATIONAL CHECK OF THE AUTOPILOT SYSTEM OK AT THIS TIME IAW SAAB AMM 22-10-00. NO DEFECTS NOTED. AIRCRAFSDR ANCF200700025Control Panel · malfunctionedA/T FAILED TO ENGAGE WHEN EPR MODE SELECTED ON T/O THE EPR SW DID NOT ENGAGE. THE T/O WAS DISCONNECTED, IAW MCC THE PROCEDURE FOR T/O WILL PERFORM MANUALLY A SECOND ATTEMPT WAS MADE AND THE TIME TO ENGAGE THE AUTOPILOT INFLIGHT DID NOT ENGAGE L,C OR R. IAWSDR SIMA200729705Yaw Damper · malfunctionedITEM-1 SUBTLE YET NOTICEABLE UNCOMMANDED RIGHT YAW DURING FLIGHT W/AUTO PILOT ON. AILERONS TRIED TO CORRECT. NO ENGINE TROUBLE. FELT AS THOUGH RUDDER WAS BEING PRESSED. FLT CONTROL SYNOPTIC PAGE REVEALED NOTHING ABNORMAL. CAUTION DISAPPEARED WHEN AUTO PILSDR DXTA200702543Computer · faultedON FINAL APPROACH, FGC B FAIL CASS MESSAGE APPEARED AND SYSTEM SWITCHED TO FGC A. CHECKED SYSTEM IN PROPER OPERATION -COULD NOT DUPLICATE- REPOSITIONED NR 1&2 IC-800'S- OPS CHECKED GOOD IAW 750 M/M CH 34-25-01.SDR UPS07150912Control Unit · inoperativeAT FL 390 LOST BOTH AUTOPILOTS, BOTH FLIGHT DIRECTORS AND MODE CONTROL PANEL - A/C WAS DOWN TO BASIC INSTRUMENTS. REMOVED AND REPLACED FCU PER MM 22-15-12-04. OPS CHECK GOOD.SDR 2007UALA04130Sensor · out of adjustIN CLIMBING FLT ACFT PITCHES DOWN AGGRESSIVELY WHEN A OR B A-P SELECTED IN ANY MODE, CLIMB, CRUISE. FOUND ELEVATOR NEUTRAL SHIFT SENSOR MIS-ADJUSTED. ADJUSTED NEUTRAL SHIFT SENSOR. ACCOMPLISHED DFCS BITE. NO FAULTS FOUND. ACFT OK FOR CAT III.SDR WGEA200700012Cable · out of rigON T/O ROLL, APR ARMED, THE A/P INOP AND YAW DAMPER FAIL CAS CAME ON. ABORTED TAKEOFF. CREW PERFORMED PROCEDURES IN QRH AND A/P TEST, ALL APPEARED NORMAL. SECOND T/O SAME. CHECKED CABLE TENSIONS ON YAW, PITCH AND ROLL SERVO'S. FOUND ROLL SERVO TO BE OUT OF SDR DL76L071288Module · faultedDIV DUE AUTOPILOTS WILL NOT ENGAGE-RUDDER RATIO AND AILERON LOCKOUT EICAS MSGS AND LIGHTS ILLUMINATED ON OVERHEAD PNL. MSG CAME ON A 250 KTS GOT STAB TRIM LIGHT FOR 5 SEC MSG DID NOT GO AWAY WHEN WE SLOWED DOWN OR RECONFIGURED /C. FOUND BOTH SAMS FAULTED RESSDR DXTA200702512Actuator · inoperativeTHE LOWER YAW DAMPER FAILED, A CAS MSG AT 60 KTS. REMOVED, REPLACED AND OPS CHECK GOOD OF LOWER YAW DAMP ACTUATOR "A" DUE TO INTERMITTENT FAILURE IAW 750 MM 27-24-00.SDR HALA0700386Autopilot Sys · malfunctionedETOPS SIGNIFICANT SYSTEM, A/P FAILED TO MAINTAIN G.S. PROPERLY AT 1000' ABOVE A/P FLEW AIRCRAFT 1/2 LOW DOT ON GLIDESLOPE. PERFORMED TEST OF BOTH MMR PER FIM 34-31-00 FIG 103. NO DISCREPANCIES. MCDP TEST 1-40-ALL PASSED. NO FLIGHT FAULTS. A/C REMAINS LANDSDR FDKA200708426Manifold · malfunctionedFDM 6157 MCO (1208 PHX LCL) - UNCOMMANDED YAW ON T/O ROLL. PULLED TO THE LEFT. MX REMOVED AND REPLACED NOSE STEERING MANIFOLD.SDR SWIA200718625Computer · malfunctionedUNCOMMANDED RUDDER MOVEMENT IN CLIMBOUT WITH AUTO PILOT ON, FLIGHT NR 5838. REPLACED FCC NR 2 IAW 22-12-14. OPS CK GOOD.SDR DXTA200702411Computer · malfunctionedUPPER RUDDER B IN CRUISE AT FL240 WENT LT 4 TIMES IN 5 MIN CAUSING AIRCRAFT TO YAW WITH A HARD BUMP. REMOVED AND REPLACED YSAC-B COMPUTER WITH UNIT INSPECTED BY HONEYWELL. OPERATIONAL AND RIG CHECK NORMAL. WORK IAW CESSNA 750 MM CHAPT 27-24-01SDR DXTA200702410Computer · malfunctionedAP TRIM FAIL ILLUMINATED WITH (E) DISPLAYED ON PFD. OCCURRED IN CLIMB THROUGH FL400. REPLACED LEFT AND RIGHT FCC-4002 FLIGHT CTRL COMPUTERS I/A/W F2000 MM 34-003. PERFORMED A/P FUNCTIONAL TEST W/ NO DISCREPANCIES NOTED, I/A/W F2000 MM 22-100.SDR 2007UALA03203Actuator · leakingLOST GREEN HYD RESERVOIR FLUID. *S/D* LEAKING YAW DAMPER ACTUATOR. REPLACED YAW DAMP ACT, SERVICED GREEN SYS HYDRO - NO REPEATS SINCE ORIGINAL.SDR DXTA200702382Unknown · unknownWHILE CLIMBING THROUGH FL350 LT AFCS FAILED. COULD NOT ENGAGE R AFCS OR YAW DAMPER. COULD NOT SELECT BETWEEN L & R AFCS. NO A/P OR YAW DAMPER OPERATION. REMOVED AND REPLACED WITH INSPECTED UNITS, BOTH NR 1&2 FLIGHT GUIDANCE COMPUTERS. OPS CHECK OF SYSTEM SHSDR DXTA200702365Motor · failedWITH AUTOPILOT ENGAGED, TRIM CLACKER AUDIBLE MORE THAN NORMAL. AFTER DISENGAGING AUTOPILOT, WE DISCOVERED NEITHER YOKE PRIMARY TRIM SWITCH HAD ANY AUTHORITY, NO CAS MESSAGE. WE ENGAGED SECONDARY TRIM SYSTEM AND MADE A PRECAUTIONARY LANDING WITHOUT INCIDENT.SDR SWIA200718541Button · stickingAIRCRAFT PITCHED RAPIDLY 7-9 DEGREES NOSE UP. THE AIRCRAFT RESPONDED TO CORRECTIVE ACTION FROM FLIGHT CONTROL PANEL. FIRST OFFICER FD BUTTON STICKS. REPLACED FDP IAW AMM 22-11-07. OPS CHECKED GOOD, PN: 822-0044-001, SN OFF: 1GL1L.SDR 07FDEA02562Autopilot Sys · unknownCLOSE R AP 1 AND 2 DO NOT ENGAGE. MTP FAULT REVIEW FOUND FCC 1/ FCC 2/FCU/TORQUE LIMIT RESET A/P 1 AND 2 BOTH FCC AND FCU. PERFORMED AFS/LAND ENGAGE TEST AS PER AMM 22-10-00-5 BOTH A/P CAN BE ENGAGED. A/C RETURNED TO SERVICE. MTP FAULT REVIEW FOUND FCC1/FC
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