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 HEEA078119Controller · malfunctionedAIRCRAFT WILL NOT HOLD ALTITUDE. ALTITUDE CONTROLLER MALFUNCTIONED.SDR AUS20020228Indicator · unserviceable(AUS) AUTOPILOT TURN AND BANK UNIT FAULTY.SDR AUS20020215Selector Switch · mismarked(AUS) AUTOPILOT NAV2 EXTERNAL SWITCH SELECTOR HAD NO MARKINGS.SDR AUS20020213Switch · unserviceable(AUS) AUTO-PILOT CONTROLLER BACK COURSE SWITCH INOPERATIVE.SDR HEEA078024Isolation Mount · failedIN CRUISE FLIGHT, AN AIRFRAME VIBRATION DEVELOPED. MAINTENANCE FOUND THE LATERAL ISOLATION MOUNT FAILED. MAINTENANCE REPLACED THE ISOLATION AMPLIFIER.SDR HEEA078023Isolation Amp · failedIN FLIGHT THE CREW DETECTED A SMOKE ODOR. THE AARS AND NR 2 ELEVATOR SYSTEM WENT OFF LINE. THE CIRCUIT BREAKER FOR THE COPILOT ADI TRIPPED. MAINTENANCE REPLACED THE ISOLATION AMPLIFIER.SDR HEEA078022Amplifier · failedELEVATORS WILL NOT TEST.SDR CA020305002Autopilot Sys · malfunctioned(CAN) ON APPROACH WITH THE AUTOPILOT ENGAGED WHEN AT APPROX. 6300 FT, THE AIRCRAFT PITCHED UP 5-10 DEGREES AND THE AUTO THROTTLES MOVED FORWARD. THE AUTOPILOT WAS DISENGAGFED BY THE COPILOT AND THE AIRCRAFT CONTINUED ITS APPROACH WITH THE AUTOPILOT OFF AND THESDR HEEA077882Amplifier · failedAMPLIFIER KICKS ELEVATORS OFF LINE WHEN ENGAGED.SDR COMA0210005Servo · bindingFLIGHT 5009 PILOT AND COPILOT RUDDER PEDALS BINDING.REPLACED THE RUDDER SERVO.SDR 371PA0003Autopilot SysAutopilot disconnecting without commandsSDR 371PA0002Limit SwitchAuto pilot kicks off line during descent, will not reset.C/A - Cleaned flap limit switch & performed DFCS Bite test. Op's Cks OK. Ref 22-03-11.SDR CA020221006Circuit Board · failed(CAN) "ON FINAL TO TXK A/C WAS ALMOST UNCONTROLLABLE. YAW DAMPER THREW A/C IN A LT BANK & THEN A RT BANK WITH AUTOPILOT OFF. IT SETTLED DOWN ENOUGH TO GET A/C ON GROUND."MAINT SIGN OFF AS FOLLOWS: PERFORMED FCC DIAGNOSTICS T/S IAW CRJ MM. NO DEFECTS NOTED. PSDR SABA020021Warning System · false activationAIRCRAFT 882 ON FLIGHT 5012 CLT TO TLH. AUTOPILOT DISENGAGE LIGHT STARTED BLINKING AND WOULD NOT STOP. AUTOPILOT SYSTEM WAS DEFERRED UNTIL AIRCRAFT RETURNED TO CLT. MAINTENANCE IN CLT PERFORMED A SELF TEST OF THE AUTOPILOT SYSTEM. SYSTEM TESTED NORMAL. NOSDR SWIA200210649Circuit Board · faultyAFTER EXCEEDING 250 KTS IAS, RUDDER FLUTTERED UNTIL AIRCRAFT WAS IN LANDING CONFIGURATION. REMOVED AND REPLACED LEFT (UPPER) LHP-4000 CARD IAW A/C MM 22-12-01. OPS CHECKED GOOD ON GROUND.SDR UPS02537585Control Panel · failedINSPECTION TYPE:N/A ACFT AIR TURNBACK DO TO MULTIPLE FLT DIRECTOR AND AUTOPILOT REPORT- COMPLETE FAILURE OF THE MODE CONTROL PANEL. REPLACED MODE CONTROL PANEL IAW MM 22-1-02.SDR AT0200008Actuator · malfunctionedUNCOMMANDED SMALL RUDDER MOVEMENTS IN CHOPPY AIR. NOSE MADE SMALL YAW CHANGES, ACTED LIKE NO YAW DAMP ON. NO PROBLEM NOTED WHILE IN SMOOTH AIR. NEITHER AUTOPILOT ON. PROBLEM STOPPED WHEN RUDDER HYDRAULIC CONT TURNED OFF. REMOVED AND REPLACED YAW DAMPENER SDR SWIA200210682Module · defectiveNR 2 YAW DAMPER WILL NOT STAY ENGAGED. REPLACED LEFT AND RIGHT LIGHTNING/HIRF MODULES IAW CL600 MM 22-12-03. CAT II P/N ON (LT) 822-0287-401, S/N OFF GR8M (RT), P/N ON 822-0332-401, S/N OFF GXTM.SDR SWIA200210640Damper · malfunctionedNR 2 YAW DAMPER WON'T STAY ENGAGED. REMOVED AND REPLACED NR 2 YAW DAMPER. OPS CHECKS CAT II GOOD IAW 22-22-01.SDR 371PA0001Autopilot Sys · malfunctionedAUTO PILOT EXCEEDING COMMANDED SPEEDS IN VNAV PATH, VNAV SPEED, AND LVL CHG. IT PERFORMS UNCOMMANDED LEVEL OFF AND CLIMBS DURING DESCENT (LVL CHG AND VNAV) AUTO THROTTLES NOT DRIVING CLOSED DURING LVL CHG (THIS IS AN INTERMITTENT PROBLEM).SDR GTIA020010Accelerometer · malfunctionedDTW - WHILE LEVEL AT CRUISE THE 'YAW DAMP OFF' LIGHT ILLUMINATED FOR APPROX 5 MINUTES AND BOTH FMA'S SHOWED VERTICAL SPEED AND NO AUTOLAND (PREV SHOWED ALT HOLD) THIS WAS ON DFGC NR 1, SWITCHED TO DFGC NR 2 AND PROBLEM REMAINED, AFTER SEVERAL MINUTES SWITCHED SDR GTIA020011Control Panel · faultyDTW - FLT 114 - FIVE MINUTES AFTER TAKEOFF ATTEMPTED TO ENGAGE AUTO PILOT NR 2 WOULD NOT ENGAGE. TRIED NR 1 IT WOULD NOT ENGAGE. COMPASSES AND ATTITUDE INDICATOR WERE CLOSELY MATCHED. AFTER SEVERAL ATTEMPTS TO ENGAGE AUTO PILOT NR 1 AND NR 2 AUTO PILOT NR 1SDR AALA20020060Dampener · brokenMIA - FLT 2139 - EN ROUTE MIA-CCS - UNCOMMANDED RUDDER MOVEMENT DURING CLIMB-OUT. ISOLATING A/P SYSTEM DID NOT HELP. NO AIRFRAME VIBRATION NOTICES. RETURNED AND LANDED MIA WITHOUT INCIDENT. REPLACED NR 1 AND NR 2 FLIGHT AUGMENTATION COMPUTERS. DID NOT RESSDR SWIA200210562Damper · failedNR 1 YAW DAMPER WILL NOT STAY ENGAGED. REMOVED AND REPLACED NR 1 YAW DAMPER IAW 22-20-00. OPS CHECK GOOD.SDR SWIA200210535Relay · failedYD 2 WILL NOT ENGAGE. REPLACED 2K2CA RELAY (ARM). OPS CHECK GOOD YAW DAMPER SYSTEM. P/N: MS27400-31X.SDR SWIA200210550Control Panel · faultyF/O'S COMMAND BARS STUCK AT 14 DEGREES AND A/P WILL NOT ENGAGE. DURING FLIGHT, ATTITUDE DISPLAY ON MAP, YELLOW PIT ON BOTH CAPTAIN'S AND FIRST OFFICER'S EADIS. FIRST OFFICERS DELTA SYMBOL DISPLAYED 5 DEGREES HIGHER THAN CAPTAIN'S. CAPTAIN'S DELTA SYMBOL DISSDR SWIA200110501Circuit Board · defectiveYD2 INOP STATUS MSG CYCLED ON & OFF DURING DESCENT. REMOVED AND REPLACED BOTH LHP4001 IAW CRJ MM 22-13-03. OPS CHECKS GOOD.SDR AUS20011463Controller · faulty(AUS) AUTOPILOT CONTROL PROGRAMMER FAULTY.SDR SWIA200110477Damper · failedYAW DAMPER 2 INOP. REMOVE AND REPLACE YAW DAMPER NR 2. OPS CHECK GOOD AT THIS TIME IAW 22-22-01.SDR CA020117014Gyro · failed(CAN) ON DEPARTURE FROM AUA - YYZ, A MODERATELY STEADY LATERAL AIRFRAME OSCILLATION ( AT APPROXIMATE RATE OF TWO PER SECOND) STARTED AT 180 KNOTS / 2100 FT ABOVE SEA LEVEL / FLAPS 4 DEGREES. IT STOPPED ONLY WHEN POWER WAS REDUCED TO 1.4 EPR AT 5100 FT ABOVE SSDR GTIA012085Accelerometer · faultyDFGS DOES NOT WORK EITHER AP 1 OR 2, WILL NOT CAPTURE ALTITUDE, HOLD ALTITUDE IN A TURN THERE IS IMMEDIATE DESCENT, DOES NOT WORK IN PERF ON EITHER SIDE BOTH COMMAND BARS DISAPPEAR FROM VIEW WHEN TO GO BUTTONS ARE PUSHED PRIOR TO TAKEOFF THE IAS MACH BUTTON DOSDR SWIA200110466Autopilot Sys · malfunctionedAIRCRAFT DISPLAYED DUTCH ROLL TENDENCIES AT FL330 AT .77 MACH. OSCILLATED 1-2 DEGREES LEFT AND RIGHT WITH 3-4 SECONDS INTERVALS, SKID INDICATOR MOVED APPROXIMATELY 1/8 LENGTH LEFT AND RIGHT. TROUBLESHOT THE SYSTEM IAW MM 22-22-01 AND 22-22-04. EVERYTHING CHSDR HEEA077580Amplifier · malfunctionedCAUSES ELEVATOR TO TRIP OFF LINE.SDR DHL2001707015Autopilot Sys · malfunctionedWHILE ON FINAL APPROACH COURSE WITH BOTH LOCALIZERS AND GLIDESLOPE INITIALLY CAPTURED ON AUTOPILOT, THE AUTOPILOT WAS NOT CAPABLE OF FLYING THE GLIDESLOPE. AIRCRAFT DOVE FOR THE GROUND. PERFORMED OPERATIONAL CHECK OF AUTOPILOT SYSTEM IAW 727 MM CH 22-00 AND SDR GTIA011191Accelerometer · failedDTW - FLT 678 - AT 33,000 FT, LOST NR 2 DFGC. SWITCHED TO NR 1. OK FOR 10 SECONDS THEN LOST IT. NO FMA'S, NO FD, NO AUTO PILOT, NO AUTO THROTTLE. COMPLIED WITH ORH, NO SUCCESS. EVERYTHING CAME BACK ALL BY ITSELF AT 12,000. CHECKED STP, FOUND MANY ACCELERSDR 2001FA0000623Roll Servo · malfunctionedOPEREATOR ENCOUTERED RESTRICTED ROLL AUTHORITY. PRIMARY AP SERVO WAS FOUND TO BE CAUSING RESTICTED CAPSTAN MOVEMENT. SOUNDS LIKE LOOSE PARTS AR FLOATING AROUND INSIDE SERVO BODYSDR COMA0110159GyroFLIGHT #5049 - AFTER T/O, RED FD FLAP ON PILOTS AND COPILOTS EADI.COULD NOT DUPLICATE. SYSTEM TEST WAS NORMAL. AIRCRAFT RETURNED TO SERVICE.SDR 2001FA0000621Roll Servo · malfunctionedOPERATOR THAT ROLL CONTROL BECAME RESTRICTED AND DIFFICULT DURING FLIGHT. INVESTIGATION REVEALED THAT THE PRIMARY ROLL SERVO WAS FOUND TO BE CAUSING RESTRICTION TO CAPSTAN. THIS SERVO WAS REMOVED AND HAS AUDIBLE SOUND OF OBJECTS FLOATING LOOSE INTERNALLY.SDR SWIA200110405Actuator · faultyAIRCRAFT OSCILLATED ABOUT YAW AXIS INFLIGHT INTERMITTENTLY. AIRCRAFT OSCILLATING INFLIGHT AROUND YAW AXIS. REMOVED AND REPLACED NR 2 YAW DAMPER IAW 22-22-01. OPS CHECK GOOD. P/N: 622-9508-001 S/N OFF: 2761 REPLACED NR 1 YAW DAMPER ACTUATOR IAW 22-22-0SDR R7MR34294Module · failedUNIT INOPERATIVE. AUTOPILOT FAULT SHOWS ON PFD AS VERTICAL LINES IN AMBER COLOR. UNABLE TO PERFORM PREFLIGHT AUTOPILOT CHECK. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (N-101HN)(K)SDR SWIA200110407Actuator · malfunctionedIN CRUISE FLIGHT AND DURING DESCENT INTO RNO RUDDER SYSTEM INDICATED UNCOMMANDED RUDDER MOVEMENT LEFT AND RIGHT. REMOVED AND REPLACED LEFT AND RIGHT YAW DAMPER ACTUATORS AND NR 1 AND NR 2 AHRS COMPUTERS. ALL OPS CHECK GOOD.SDR AALA20012082Damper · defectiveLIM - FLT 918 - EN ROUTE LIM-MIA, DURING CLIMB-OUT DETECTED RUDDER VIBRATION. VIBRATION INCREASED AFTER TURNING OFF AUTOPILOT. RETURNED LIM AND LANDED WITHOUT FURTHER INCIDENT. ACCOMPLISHED RUDDER ATTACHMENT INSPECTION AND VERTICAL STABILIZER ATTACHMENT INSSDR HEEA077403Amplifier · malfunctionedPITCH TRIPS AFTER 30 TO 45 MINUTES OF FLIGHT. RESETS BUT ONLY FOR SHORT PERIOD OF TIME.SDR HEEA077402Amplifier · malfunctionedTRIPS OFF WHEN CONTROL IS MOVED.SDR DL72E011852Coupler · failedAFTER TAKEOFF A/C BEGAN TO FISHTAIL. NO YAW DAMPER FLAGS IN VIEW. NO MOVEMENT OF INDICES ON YD INSTRUMENT. RETURN TO AIRPORT FOR LANDING. FOUND LOWER YAW DAMPER FLAG IN VIEW. WILL NOT RETRACT. REPLD YAW DAMP COUPLER. ALSO FOUND LOWER RUDDER POSITION SENSOR SHOSDR R7MR34282Module · shortedUNIT INOPERATIVE. POPS NUMBER 2 APM CIRCUIT BREAKER. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (102HN) (K)SDR 2001UALA02323Control Panel · failed150NM FROM SFO TO ELEC SMELL AND A LITTLE SMOKE IN THE COCKPIT. MODE CONTROL PNL AND AUTO THROTTLE KICKED OFF AND CB POPPED. SMOKE AND SMELL RAPIDLY DISSIPATED. FLT RETURNED TO SFO. MODE CONTROL PANEL P/N 822-0195-102 REPLACED. PRELIMINARY FINDINGS BY COMSDR DL72L011847Transmitter · failedAFTER T/O RUDDER OSCILLATIONS FOLLOWED POM PROCEDURE. FOUND POSITION TRANSMITTER COIL OPEN REMOVED AND REPLACED POS XMTR PER MM ADJ/TEST OF YAW DAMP CHKS GOOD PER MM.SDR DL72L011845Coupler · intermittentON TAKEOFF SLIGHT RUDDER OSCILLATIONS WITH HIGH WIND. AFTER TAKEOFF EXCESSIVE RUDDER MOVEMENT. FOLLOWED YAW DAMP INOP POM PROC. NO HELP. REMOVED AND REPLACED UPPER AND LOWER YAW DAMP COUPLERS PER M/M. SYSTEM TEST NORMAL.SDR SWIA200110390Autopilot Sys · malfunctionedAUTOPILOT TRIM RED LIGHTS CAME ON DURING TAKE OFF, ABORTED. CYCLED AUTO PILOT CIRCUIT BREAKERS OPS CHECK GOOD.
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