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 DXTA200500672Autopilot Sys · malfunctionedAFTER TAKEOFF FROM KBAZ THE YAW DAMP AND AUTOPILOT FAILED TO ENGAGE. BOTH LEFT & RIGHT AP CHANNELS WERE ATTEMPTED WITH NO RESULTS. FLIGHT DIRECTOR FUNCTIONED NORMALLY. OPS CHECK A/P SYSTEM CHECK IS GOOD, POWER UP A/C FOR SEVERAL HRS CHECKING A/P OPS CHECK GSDR DXTA200500667Autopilot Sys · malfunctionedWHEN AUTOPILOT A-SIDE ENGAGED SYSTEM FLAGGED FAIL CYCLED TO B-SIDE, AND DEFECTED RIGHT RUDDER INPUTS RUDDER INPUTS BECAME INCREASINGLY AGGRESSIVE PIC AND SIC COMMAND BARS SHOWED 2-3 DEGREES TO BANK DISAGREEMENT. RAN AUTOPILOT TEST IAW CE650 MM 22-10-00; NO DESDR AU510001513Trim Switch · faultyNR 2 TRIM SWITCH FAULTY.SDR MASA200500272Module · sticksASH 2858 CLT - HAD AN AUTO PILOT FAIL BECAUSE OF AN AILERON MIS-TRIM. MAINTENANCE REPLACED THE TRIM CONTROL MODULE.SDR PIDA2005002Control Panel · failedFIRST OFFICER'S COURSE SELECTOR WILL NOT TUNE IN COURSE. PLACED ON MEL 22-16-E. 04/03/2005: REPLACED AUTO PILOT MODE CONTROL PANEL AND OPS CHECKED PER MM 22-11-34.SDR RYNA200500010Autopilot Sys · malfunctionedIMMEDIATELY AFTER TAKEOFF FROM TUS, THE AUTOPILOT PORPOISED IN PITCH. THE AIRCRAFT WAS RETURNED TO TUS AND LANDED WITHOUT INCIDENT. AMENDMENT TO BE FILED UPON COMPLETION OF TROUBLESHOOTING AND CORRECTIVE ACTION.SDR UPS05544232Computer · inoperativeEMERGENCY DECLARED. ON CLIMBOUT APPROX 20,000 FT CAPT'S AIRSPEED, ALT & VSI FAILED. CAPT SWITCHED TO ALT AIR DATA SWITCH, ALL CORRECTED AT APPROX 25,000 FT, BEGAN TO RECEIVE OVERSPEED WARNINGS (FAST/SLOW). AT 41,000 AUTOTHROTTLE COULD NOT MAINTAIN PROPER AISDR 252TR0037Coupler · damagedYAW DAMPER IS INOP. PLACED ON MEL 22-3. REPLACED YAW DAMPER COUPLER PER MM 22-11-141. OPS AND BITE CHECK OK.SDR MASA200500200Ahrs · failedASH 2796 CLT - HAD AN AUTO PILOT DISENGAGE DUE TO AN AHRS INOP. MAINTENANCE REPLACED THE AHRS COMPUTER.SDR F3LA200500012Computer · faultyFLIGHT CREW REPORTED ECAM FLIGHT CONTROL ELAC 2 PITCH FAULT (PASSING THROUGH FL180). AIRCRAFT RETURNED TO DEN AND LANDED WITHOUT INCIDENT. REPLACED NR 2 ELAC COMPUTER PER AMM 27-93-PB401; REPLACED THS ACTUATOR POSITION TRANSDUCER PER AMM 27-44-PB401; AND REPSDR A6WA200540091Computer · malfunctionedRUDDER FLUTTER INFLIGHT, ALL CONDITIONS, AUTOPILOT ENGAGES. REMOVED AND REPLACED FCC NR 1 IAW 22-12-14. PERFORMED OPS TEST IAW AMM 22-11-00. OPS CHECK GOOD. AIRCRAFT CERTIFIED FOR RVSM. (M)SDR 237TR0009Indicator · inoperativeNR 1 FLIGHT DIRECTOR INOP. PLACED ON MEL 34-12. 03/14/2005: REPLACED NR 1 ADI AND OPS CHECKED PER MM 22-11-01.SDR MALA050254Computer · malfunctionedAFTER TAKEOFF AUTOTRIM WARNING AND AUTOPILOT DISCONNECT. AUTOTRIM WARNING EXTINGUISHED. CREW NOTED AN UNUSUAL SMELL IN THE FLIGHT DECK. REPORTED, SMELLS LIKE INSULATION. AIR RETURN TO DTW. PERFORMED OP CHECK OF AUTOTRIM SYSTEM. CND PROBLEM. AUTOTRIM OP SDR A6WA200540079Yaw Damper · defectiveON DESCENT THROUGH 9000 FEET, LOUD REPEATED BANGING SOUND FROM AIRCRAFT. COMBINED WITH SHARP REPEATED LEFT YAW MOTIONS. C/W SECU CHECKS, SPOILER AND SPOILERON CHECKS. CHECKED HYD SYSTEM HEAT EXCHANGER. CHECKED RUDDER AND RUDDER TRIM SYSTEM. COMPLIED WITH SDR COMA0560134Servo · malfunctionedFLIGHT 4941 ELEVATOR CONTROL STIFF AUTO PILOT DISCONNECTED. REPLACED THE ELEVATOR SERVO.SDR DXTA200500588Cable · crackedAT FL410 WITH AUTOPILOT ENGAGED, ACFT BEGAN 10 DEG LT & RT ROLL OSCILLATION WITH A 1 SEC TIME AMPLITUDE. OSCILLATIONS CONTINUED 18 MINS. OPS NORMAL WITH AP DISENGAGED. DESCENDED TO FL360. RE-ENGAGED AP & 5 MINS LATER AUTO PILOT ENGAGED, OSCILLATIONS BEGAN SDR 390WL0001Selector · unknownAUTO FLIGHT MODE CONTROL PANEL VERTICAL SPEED SELECTOR INOP. PLACED ON MEL 22-14-(1). NO FAILURES OR IN FLIGHT FAULTS NOTED. PASSED AUTO PILOT TESTS FOR DFCS GROUP 11.56. NO FAULTS EXIST CURRENT OR INFLIGHT. CLEARS MEL 11-14-1.SDR DXTA200500580Autopilot Sys · malfunctionedDURING CRUISE, AUTOPILOT INPUTS FOR AILERON & UPPER RUDDER CONTROL OSCILLATES CONTINUOUSLY. TURBULENCE INCREASES THE INTENSITY & FREQUENCY OF OSCILLATIONS. APPLIED PRESSURE ON FLT CONTROLS (AILERON & RUDDER PRESSURE). ON CONTROL PANEL SYNOPTIC AILERON MOVESSDR QXEA200500140Control Panel · inoperativeSEA - ON FLIGHT NUMBER 2244, IN CRUISE MOST FLIGHT GUIDANCE COMPUTER BUTTONS WERE INOPERATIVE. AUXILARY BUTTONS WORKED. WHEN NAV SEL BUTTON WAS PUSHED IN ENGAGED THE AUTO PILOT. MAINTENANCE REMOVED AND REPLACED FLIGHT GUIDANCE COMPUTER CONTROL PANEL. OPERASDR 234TR0027Computer · malfunctionedNUMBER 2 ADI HAS FLIGHT DIRECTOR FLAG. REPLACED NR 2 FLIGHT CONTROL COMPUTER. OPS CHECKS GOOD PER MM 22-11-01.SDR ASMF200501010Computer · failedCAPTAIN REPORTED DFGC MISC DATA FAIL LEGEND ON BOTH MCDUS SCRATCH PADS, AUTOMATIC PILOT 1 AND 2 WERE UNABLE DURING FIVE MINUTES AFTER TAKEOFF, ATS WAS UNABLE WITH FMAS IN TAKEOFF MODE, CAPTAIN VHF NAV OSCILLATING, CRUISE INDICATOR WITHOUT MOVEMENT IN ND SCREENSDR PIDA06003Force Limiter · malfunctionedA & B AUTO PILOT DISCONNECTS. REPLACED AILERON FORCE LIMITER PER MM 22-11-13. OPS CHECKS GOOD.SDR 249TR0104Circuit Breaker · trippedAUTO PILOT WILL NOT FOLLOW COMMANDED INPUTS FROM PILOT AND FLIGHT DIRECTOR. RESET STABILIZER TRIM CIRCUIT BREAKER. SYSTEM TESTS GOOD PER MM 22-11-01.SDR AWXA200500008Yaw Damper · leakingEN ROUTE FROM EWR TO PHX RECEIVED ECAM MESSAGE FOR GREEN HYD RESERVOIR LOW. DECLARED EMERGENCY & LANDED WITHOUT FURTHER DIFFICULTY. MAINTENANCE TROUBLESHOT & FOUND FLUID LEAKING FROM THE TOP OF NR 1 YAW DAMPER (3CC1), ISOLATED THE NR 1 YAW DAMPER AND ISSUED SDR DLM88041155Annunciator · faultyF/O REPORTS SMOKE COMING FROM AROUND F/O FMA. REPLACED FMA.SDR QXEA200400927Autopilot Sys · malfunctionedCREW FOLLOWED ABNORMAL CHECKLIST AND TURNED OFF AUTOPILOT WHEN THEY RECEIVED A MASTER CAUTION "AUTOPILOT RIGHT TRIM" MESSAGE. MAINTENANCE PERFORMED FUNCTIONAL TEST OF AILERON TRIM SYSTEM. THE FUNCTIONAL AND OPERATIONAL TESTS WERE GOOD. THE OPERATIONAL CHECKSDR 249TR0100Actuator · leakingEVIDENCE OF FLUID LEAK FROM -A- SYSTEM AUTO PILOT ELEVATOR SERVO ACTUATOR. FOUND -B- SYSTEM AUTO PILOT ACTUATOR LEAKING DOWN ONTO -A- SYSTEM ACTUATOR. REPLACED -B- SYSTEM ACTUATOR PER MM 22-11-261.SDR A6WA200440220Control System · bindingFIRST OFFICER REPORTED RT AILERON BINDING ON APPROACH WITH AUTO PILOT SELECTED OFF. INSPECTED AILERON CONTROL SYSTEM IAW SL. FOUND NO EVIDENCE OF MOISTURE OR PULLEY BINDING. NO FAULTS IN MDC. PERFORMED OPS CHECK OF AUTOPILOT, OPS CHECK GOOD IAW 27-11-00.SDR 04343661Computer · inoperativeEVENT SUMMARY STATED PITCH AND ROLL CONTROLS EXTREMELY STIFF ON FINAL. AUTO PILOT WAS DISCONNECTED FLAPS AT 20. REMOVED AND REPLACED NR 2 FCC.SDR 237TR0008Switch · malfunctionedFLIGHT DIRECTOR BAR GOES AWAY WHEN TOGA IS PRESSED. PLACED ON MEL 22-17. 12/08/2004: REPLACED SWITCH IN RIGHT HAND THROTTLE. FLIGHT DIRECTOR OPS CHECKS GOOD PER MM 22-11-01.SDR MASA200400661Ahrs · malfunctionedASH 2665 CLT - AUTO PILOT FAILED IN FLIGHT. MAINTENANCE REPLACED THE NR 2 AHRS.SDR DXTA200400454Autopilot Sys · malfunctionedDURING GO AROUNDS (AFTER A COUPLE APPROACHES) THE AUTO-PILOT DISENGAGED MULTIPLE TIMES AFTER IT WAS RE-ENGAGED IN STABILIZED CLIMB/LEVEL OFF AND IN LEVEL FLIGHT. ON SECOND MISSED APPROACH BOTH FMS UNITS FAILED FOR ABOUT 30 SECONDS ALONG WITH THE AUTO-PILOT DISDR DHL2004801014Transfer Valve · failedRUDDER INDICATOR WAS FULL LEFT. IT TOOK 5 1/2 UNITS TO MAINTAIN STRAIGHT AND LEVEL. WHEN THE RUDDER TRIM WAS MOVED TOWARD ZERO THE AIRCRAFT MADE AN AGGRESSIVE ROLL TO THE LEFT. DID NOT TRY TO FLY AIRCRAFT WITH YAW. REMOVED AND REPLACED ROLL SERVO DRIVE IASDR DXTA200400450Computer · malfunctionedIN FLIGHT AT 17,000 FT AND 320 KTS FELT A SHARP RUDDER KICK WITH THE AUTOPILOT ON, YD FAIL UPPER -B- AMBER CAS MESSAGE ILLUMINATED. REMOVED AND REPLACED -B- YSAC (UPPER) IAW 750 MM 27-24-01. OPS CHECKED GOOD.SDR MALA040729Computer · malfunctionedAFTER TAKEOFF, YAW DAMPER WOULD NOT ENGAGE. NOTED BREAKERS N10 AND N11C/B POPPED, RESET BREAKERS, RECEIVED AUTOPILOT DISCONNECT TONE, ENGAGE YAW DAMPER AND RECEIVED AUTO TRIM MASTER WARNING. PERFORMED QRH MEMORY ITEMS RUDDER KICKED LEFT, DURING YAW DAMPER APSDR DXTA200400447Position Sensor · inoperativeYD FAIL UPPER A CAS MESSAGE DURING CLIMB. DETERMINED UPPER RUDDER POSITION SENSOR -A- WITH FAULT. REPLACED SENSOR -A-, DUE TO CAS MESSAGE DURING CLIMB, WITH FAULT. INSTALLED NEW SENSOR UNIT INTO -A- POSITION. DETERMINED UPPER RUDDER POSITION SENSOR "A" WITSDR ABXA040373Computer · defectiveAUTOPILOT DID AN UNCOMMANDED 3000 FT MIN DESCENT WITH PITCH WHEEL IN ALTITUDE DETENT. FLIGHT 158, STA ALB. COULD NOT DUPLICATE. SUSPECT PITCH COMPUTER INSTALLED FOR TRIM PROBLEM CAUSING DIFFICULTIES WITH ALT HOLD. REMOVED AND REPLACED PITCH AXIS COMPUTER. SDR IXXA0400117OComputer · weakDURING CRUISE FROM RJTY AIRCRAFT YAWS TO THE RIGHT WHEN YAW DAMPER IS TURNED ON. THE AUTOPILOT RUDDER IS OFF SCALE RIGHT INDICE AUTOPILOT RUDDER OFF SCALE RIGHT. MAINTENANCE TROUBLESHOT AUTOPILOT SYSTEM AND FOUND YAW AND ROLL CHANNEL COMPUTERS WEAK. REMOVEDSDR 66269Yaw Damper · malfunctionedYAW DAMPER ENGAGED ON TAKEOFF ROLL, CREW ABORTED TAKEOFF GOT AND YAW DAMPER/RUDDER BOOST FAIL ANNUN WHEN TAXIING. RETURNED TO GATE AND THE SYSTEM WAS DEFERRED WITH NO FURTHER INCIDENT. COULD NOT DUPLICATE ON GROUND YAW DAMPER OPS CK NORMAL.SDR Z1RA097890Autopilot Sys · intermittentNR 2 ROLL CHANNEL ROCKING BACK AND FORTH ON AUTOPILOT SYSTEMSDR CA041022002Control Panel · failed(CAN) AFTER DEPARTURE YVR ENROUTE LAX, CREW NOTICED NUMBEROUS FAILURES IN AUTOFLIGHT MODE CONTROL PANEL.NOT ABLE TO SELECT SPECIFIC HEADING. HEADING INDICATIONS ON CAPT/FO EHSI DIFFERENT. UNABLE TO SELECT ALTITUDE, ALSO AUTOPILOT WOULD NOT CONTROL AIRCRAFT TOSDR 371PA0085Indicator · false indicationYAW DAMPER INDICATOR INDICATES FULL RT. REPLACED YAW DAMPER INDICATOR. SYSTEM OPS CHECKS GOOD IAW MM 22-12-01..SDR QXEA200400713Computer · malfunctionedRDM- AFTER TOUCHDOWN, BOTH MAIN GEAR ON THE GROUND, NOSE IN THE AIR, RT AILERON APPLIED FOR CROSSWINDS, CONTROL COLUMN FROZE IN PLACE AND HAD TO BE OVERPOWERED. BOTH PITCH AND ROLL STUCK IN PLACE. AIRCRAFT ACCOMPLISHED AN UNEVENTFUL TAXI TO THE GATE. FIRST SDR DXTA200400425Controller · malfunctionedWITH AUTOPILOT ENGAGED, IN A LT TURN, LVL FLIGHT MASTER WARNING ILLUMINATED + CAS MESSAGE RETRIM RT WING DOWN WAS DISPLAYED. THIS HAPPENED TWICE, IN EACH CASE THE AUTOPILOT WAS DISENGAGED BY PILOT. WINGS LEVELED AND LIGHTS EXTINGUISHED. COMPLETED INSPECTIOSDR A6WA200440145Computer · malfunctionedON COMMAND OF AUTOPILOT DISENGAGEMENT, PITCH CONTROL DID NOT DISENGAGE FOR APPROX 5-10 SECONDS.SDR DJFA2004022Contact · dirtyCREW REPORTED THAT AFTER NORMAL TAKEOFF, THE YAW DAMPER AND AUTOPILOT FAILED TO ENGAGE ON SEVERAL ATTEMPTS. AIRCRAFT THEN DIVERTED TO DAL. MAINTENANCE CLEANED THE CONTACTS AT THE YAW RATE SENSOR AND APS-65. GROUND CHECK WAS GOOD. AIRCRAFT RETURNED TO SERVISDR SB04135Control Panel · faultyDURING A HEADING CHANGE, THE AUTOPILOT ROLLED THE AIRCRAFT INTO A 40 DEGREE BANK BEFORE THE PILOT COULD DISCONNECT IT. MAINTENANCE REPLACED THE MODE CONTROL PANEL.SDR SB04130Control Panel · faultyDURING CRUISE, EN ROUTE FROM PHL TO DFW, CREW REPORTED THE CHANNEL A AUTOPILOT DROPPED OFF FOLLOWED BY THE AUTOPILOT MODE CONTROL WINDOW DISPLAYING 50,000 FEET. THE LEFT NAV THEN DROPPED OFF LINE. FLIGHT DIVERTED TO PIT AND LANDED WITHOUT FURTHER INCIDENT. SDR IXXA0400107OComputer · failedAFTER TAKEOFF FROM WSAP, YAW DAMPER ENGAGED, RUDDER KICKED TO THE LEFT. DISENGAGED YAW DAMPER. CREW TRIED TO RE-ENGAGE YAW DAMPER AND RUDDER KICKED LEFT AGAIN, TURNED OFF YAW DAMPER. CREW RETURNED AIRCRAFT TO WSAP AND LANDED WITHOUT INCIDENT. AN INVESTIGATSDR IXXA0400106O9Yaw Damper · malfunctionedAFTER TAKEOFF FROM WSAP, YAW DAMPER ENGAGED, RUDDER KICKED TO THE LEFT. DISENGAGED YAW DAMPER. CREW TRIED TO RE-ENGAGE YAW DAMPER AND RUDDER KICKED LEFT AGAIN, TURNED OFF YAW DAMPER. CREW RETURNED AIRCRAFT TO WSAP AND LANDED WITHOUT INCIDENT. AN INVESTIGAT
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