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 SWIA200412830Computer · malfunctionedINFLIGHT AUTOPILOT WOULD NOT HOLD ALTITUDE EITHER SIDE. REPLACED CAPTAINS AUTOPILOT COMPUTER WITH SERVICEABLE UNIT. OPS CHECK GOOD.SDR BAQA092505Actuator · stickingYAW ACTUATOR STICKING, TAP UNIT IT MOVES. HARDCARD ENCLOSED. REPLACED WITH SERVICABLE UNIT. 02/04/2004SDR SWIA200412838Computer · malfunctionedCAPTAIN SIDE FCP HAS A RED TRIM WARNING ACCOMPANIED WITH COMPUTER FLAG ON ADI. REPLACED LEFT APC65 WITH SERVICEABLE UNIT. ALL FUNCTIONAL CHECKS FOUND GOOD. P/N: 622-8315-402, S/N ON: 2470, S/N OFF: 1641.SDR 371PA0034Computer · malfunctionedAUTOPILOT DRIFTED OFF ALTITUDE IN CRUISE +320 FT, THEN RECAPTURED ASSIGNED ALTITUDE. PLACED AUTOPILOT ALTITUDE HOLD ON MEL 22-1. REPLACED "A" FLIGHT CONTROL COMPUTER PER MM 34-60. PERFORMED FCC TEST AND LAND VERIFY. TEST NORMAL.SDR SWIA200412816Computer · malfunctionedRED FD ON BOTH PRIMARY FLIGHT DIRECTOR'S, FD1 FAIL STATUS MESSAGE AND YD1 INOP STATUS MESSSAGE IN FLIGHT. RETURNED TO SLC. REMOVED AND REPLACED NR 1 FCC 4000 CARD. OPS CHECKS GOOD IAW 22-11-00 AND 22-12-14.SDR BAQA092792Actuator · inoperativeUNIT IS BEING SENT TO AEC FOR WARRANTY REPAIR. REASON FOR REMOVAL, BOTH ROLL ACTUATORS WERE INOPERATIVE. REPLACED WITH SERVICEABLE UNIT FROM ASSET (S/N 634)SDR SWIA200412808Computer · malfunctionedON DESCENT AND DURING APPROACH, THE CONTROL WHEEL WOULD INTERMITTENTLY JERK, BUT THE AUTOPILOT DID NOT DISCONNECT. REMOVED AND REPLACED FCC NR 2 CARD AND ELEVATOR SERVO IAW MM 27-12-14, MM 22-11-24. OPS CHECKS GOOD. SERVO P/N: 622-5027-001, S/N OFF: 2935.SDR SWIA200412795Computer · malfunctionedAUTOPILOT ON CAPT'S SIDE DOES NOT PASS FIRST FLIGHT OF DAY CHECKS. REPLACED NR 1 AUTOPILOT COMPUTER. OPS CHECKED GOOD.SDR 252TR0015Receiver · malfunctionedCHANNEL-A AUTOPILOT WILL NOT CAPTURE VOR-LOC. PLACED A-CHANNEL AUTOPILOT ON MEL 22-1. REPLACED NAV. RECEIVER AND PERFORMED AUTO-PILOT LRU VERIFICATIN BITE TEST PER MM 22-00. AUTO-PILOT CHECKS NORMAL.SDR U30A200400001Computer · faultyPRIOR TO DEPARTURE OF FLT 308 IN BWI (BWI-CUN), THE NR 2 FMGC (FLIGHT MANAGEMENT GUIDANCE COMPUTER) WENT INOP (ECAM MESSAGE AP2 & CAT 3 DUAL INOP). THE NR 2 FMGC WAS DEFERRED PER MEL 22-83-01. THE NR 2 FMGC WAS REPLACED IAW AMM 22-83-34-401 AND OPS CK'D OK 2SDR AUS20040025Autopilot Sys · faulty(AUS) NEITHER AUTOPILOT WOULD TRIM THE AIRCRAFT.SDR SWIA200412805Computer · malfunctionedON TAXI OUT, SELECTED AP TO F/O. RECEIVED AP FAIL LIGHT ON MAP AND ASSOCIATED AP DIS & AP ON FCP. REPLACED F/O'S AP COMPUTER. OP CHECKS GOOD.SDR SWIA200412801Control Panel · malfunctionedAFTER LANDING, AUTOPILOT KEPT RE-ENGAGING ITSELF, WOULD RE-ENGAGE ON BOTH SIDES REPEATEDLY. REPLACED AUTOPILOT CONTROL PANEL. OPS CHECK GOOD ON BOTH SIDE AUTOPILOT.SDR SWIA200412791Computer · malfunctionedON TWO OCCASIONS THE YAW DAMPNER CAPTAIN'S SIDE DISENGAGED, HOWEVER THE AUTO PILOT REMAINS ON EVEN AFTER LANDING THEN TURNING OFF THE AUTO PILOT, YAW DISENGAGED REMAINS ILLUMINATED. REPLACED NR 1 AUTOPILOT COMPUTER. OPS CHECKS GOOD PER MM 22-11-00.SDR 015042Computer · odorR ENVIR OFF LIGHT FAILS TO ILLUMINATE WITH BLEED AIR VALVE IN OFF POSITION, ELECTRICAL ODOR IN MAIN CABIN. SOURSE OF ODOR YAW DAMP COMPUTER, YAW DAMP COMPUTER DEFERRED PER MEL 22-1 CAT C.SDR 016041Computer · malfunctionedRT ENVIR OFF LIGHT FAILS TO ILLUMINATE WITH BLEED AIR VALVE IN OFF POSITION ELECTRICAL ODOR IN MAIN CABIN. SOURSE OF ODOR YAW DAMP COMPUTER. YAW DAMP COMPUTER DEFERRED PER MEL 22-1 CAT C.SDR 015043Computer · malfunctionedRIGHT ENVIR OFF LIGHT FAILS TO ILLUMINATE WITH BLEED AIR VALVE IN OFF POSITION, ELECTRICAL ODOR IN MAIN CABIN. SOURSE OF ODOR YAW DAMP COMPUTER. YAW DAMP COMPUTER DEFERRED PER MEL 22-1 CAT C.SDR SWIA200412772Computer · malfunctionedYAW DAMP NR 2 DISENGAGED ON THE GROUND AT SLC AND WOULD NOT RE-ENGAGE. REMOVED AND REPLACED NR 2 FCC CARD PER CRJ MM 22-12-14. OPS CHECKS GOOD.SDR 2004UALA00026Coupler · malfunctionedYAW DAMPER TRIPPED OFF. *S/D* REPLACED YAW DAMPER COUPLER.SDR SWIA200412763Computer · malfunctionedEN ROUTE TO SLC AUTOPILOT FAILED FOLLOWED BY YD1, FD1, TERRAIN FAIL STATUS MSGS. LEFT SIDE WITNESS LIGHT ON FCP DO NOT ILLUMINATE. REPLACED NR 1 FCC CARD. AUTOPILOT OPS CHECK GOOD IAW 22-10-00.SDR 04005316Servo · faultyDURING OPERATION OF AIRCRAFT CREW REPORTED OSCILLATIONS IN VERTICAL MODE OF FLIGHT DIRECTOR WITH AUTOPILOT DISCONNECTING. THE AUTOPILOT SERVO WAS FOUND FAULTY AND WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTSDR SWIA200412756Control Panel · malfunctionedYAW DAMPER 2 WOULD NOT ENGAGE. REMOVED AND REPLACED YAW DAMPER PANEL. OPS CHECK GOOD AT THIS TIME. P/N OFF: 601R51594-1.SDR AUS20040004Control Panel · failed(AUS) AUTOPILOT MODE CONTROL PANEL FAILED.SDR 249TR0021Battery · failedHEADING, IAS, COURSE BUGS WILL NOT CHANGE. A/P FLIGHT DIRECTOR SYSTEM TEST PERFORMED IAW MM 22-11-01. REPLACED BATTERY IAW MM 24-31-11. TEST OK.SDR 249TR0002AAComputer · malfunctionedHEADING, IAS, COURSE BUGS WILL NOT CHANGE. A/P FLIGHT DIRECTOR SYSTEM TEST PERFORMED PER MM 22-11-01. REPLACED BATTERY PER MM 24-31-11. TEST OK.SDR 219PA0011Coupler · damagedYAW DAMPER LIGHT STAYS OFF WHEN SWITCHED FROM ON TO OFF. REPLACED YAW DAMPER COUPLER, OPS CHECKS NORMAL PER MM 22-12-01.SDR SWIA200412746Computer · malfunctionedCAPTAIN'S AP FAILS IN FLIGHT. REMOVED AND REPLACED AUTOPILOT NR 1 COMPUTER WITH SERVICEABLE UNIT. OPS CHECK GOOD IAW MM 22-10-00.SDR 0401413Servo · faultyDURING OPERATION OF AIRCRAFT CREW REPORTED OSCILLATIONS WITH THE AUTOPILOT ENGAGED. THE AILERON SERVO MOTOR WAS FOUND FAULTY AND WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE.SDR SWIA200312738Computer · malfunctionedA/P DISCONNECTED IN FLIGHT WHEN FLIGHT DIRECTOR FAILED ON F/O'S SIDE. A/P WOULD NOT RE-ENGAGE ON CAPTAIN'S SIDE. AFTER 15 MINUTES F/O'S FLIGHT DIRECTOR CAME BACK AND RE-ENGAGED A/P. REMOVED AND REPLACED FCC NR 2. OPS CHECKS GOOD IAW CRJ MM 22-12-14.SDR SWIA200312754Computer · malfunctionedF/O'S YAW SYSTEM DISENGAGES. REPLACED NR 2 AUTOPILOT COMPUTER IAW MM 22-10-02. OPS CHECK GOOD.SDR SWIA200312737Computer · malfunctionedF/O'S FD FAIL MESSAGE. AP KICKS OFF IN FLIGHT ALONG WITH YD NR 2. AP DOES NOT RE-ENGAGE. REMOVED AND REPLACED THE NR 2 FCC 4000 IAW AMM 22-12-14. OPS CHECKS GOOD.SDR 03360316Computer · faultyDURING AIRCRAFT OPERATION THE CREW REPORTED OSCILLATIONS WITH THE AUTOPILOT SYSTEM ENGAGED. THE AUTOPILOT COMPUTER WAS FOUND TO BE FAULTY AND WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND THE AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE.SDR BAQA091640Control Unit · failedUNIT FAILED OUT OF BOX UPON INSTALLATION REPLACED WITH SERVICABLE ASSET.SDR MASA200300504Computer · inoperativeCREW REPORTED AUTO-PILOT DISCONNECT IN-FLIGHT DUE TO AN IC600 FAULT. MX REPLACED THE IC600 COMPUTER. OP CHECKS GOOD.SDR SWIA200312708Computer · malfunctionedAP PITCH TRIM CAUTION MESSAGE AT 6500 FEET MSL (2300 AGL) ON FINAL. REMOVED AND REPLACED FCC 4000 CARDS 1A & 2A IAW MM 22-12-14. OPS CHECK GOOD. P/N: 622-9815-704, S/N OFF: 854.SDR SWIA200312707Control Panel · malfunctionedWITH AUTOPILOT ENGAGED PASSING 15,000 FT AIRPLANE PITCHED UP UNCOMMANDED. AFTER LEVELING AT 16,000 FT, RECONNECTED A/P. ALTITUDE LIGHT ALT ON FCP (CA AND F/O SIDES) WOULD NOT REMAIN ILLUMINATED. REMOVED AND REPLACED AUTO PILOT CONTROL PANEL IN CENTER CONSOLESDR SWIA200312706Computer · malfunctionedCAPTAINS AUTOPILOT WILL NOT ENGAGE. INSTALLED SERVICEABLE NR 1 AUTOPILOT COMPUTER AS NEEDED. OPS CHECKS GOOD. P/N ON 622-8315-403, S/N OFF 2901.SDR 03349311Computer · malfunctionedDURING DESCENT THE CREW REPORTED THE AIRCRAFT PITCHING UP AND DOWN WHILE ON THE GLIDESLOPE. FLIGHT LANDED UNEVENTFULLY AND PASSENGERS DEPLANED NORMALLY. THE AUTOPILOT COMPUTER WAS FOUND TO BE INOPERATIVE AND WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WASDR 250TR0026Computer · malfunctionedCAPTAIN'S FLIGHT DIRECTOR FLAG IN VIEW. REPLACED NR 1 FLIGHT CONTROL COMPUTER PER MM 22-11-331. OPS CHECKS GOOD.SDR QXEA200301552Dampener · failedAUTO-PILOT DISENGAGED AT CRUISE FLIGHT AS WELL AS THE YAW DAMPER DISCONNECTED. COMPLIED WITH CHECKLIST AND UNABLE TO RESET YAW DAMPER OR AUTOPILOT. REMOVED AND REPLACED YAW DAMPER ACTUATOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.SDR SIMA200334101Control Unit · inoperativeORD - FLT 3967 - DURING CRUISE FLIGHT CREW REPORTED A MAIN AND BACKUP TRIM INOPERATIVE WARNING. MAIN SYSTEM WAS RESTORED BY RESETTING BREAKER. BACKUP TRIM WOULD NOT RESTORE. MAINTENANCE LUBRICATED THE BACKUP TRIM SWITCH AND DRAINED THE NR 1 AND 2 PITOT SYSTSDR SWIA200312652Control Box · malfunctionedCAPTAIN'S AND FIRST OFFICER'S AUTOPILOT INOP. REPLACED AP TRANSFER BOX AS REQUIRED. SYSTEM OPS CHECK GOOD IAW CH 22-10-00 EMB 120 MM.SDR SWIA200312644Computer · malfunctionedCAPTAINS FLIGHT DIRECTOR COMMAND BARS PITCH UP ABRUPTLY IN FLIGHT TO 20 DEGREES AND NOSE UP AND 20 DEGREES LEFT AND RIGHT TURN. INSTALLED SERVICEABLE AUTOPILOT COMPUTER ON CAPTS SIDE. OPS CHECK GOOD.SDR AUS20031246Servo · failed(AUS) AUTOPILOT ROLL SERVO FAULTY.SDR SWIA200312630Control Panel · malfunctionedNEITHER CAPTAIN NOR F/O'S AUTOPILOT WILL CAPTURE AND FOLLOW THE COMMAND BARS, NOR WILL IT CAPTURE AN ALTITUDE. REMOVED AND REPLACED APP-65A AUTOPILOT CONTROL PANEL AND REPLACED ELEVATOR SERVO IAW EMB 120 MM 22-10-04. OPS CHECK GOOD. SERVO P/N: 622-5734-002SDR SWIA200312611Computer · malfunctionedF/O ADI SHOWS COMPUTER FLAG. AUTO PILOT DOES NOT ENGAGE ON F/O SIDE. REPLACED APC-65B. OPS CHECKS GOOD.SDR 03321306Computer · intermittentDURING FLIGHT CREW REPORTED THE AUTOPILOT SYSTEM DISENGAGING EVERY 8 MINUTES. THE FAULT WAS VERIFIED AND THE AUTOPILOT COMPUTER WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE.SDR 249TR0020Coupler · failedYAW DAMPER SWITCH WILL NOT LOCK ON. TRIPS BREAKER. PLACED ON MEL 22-3-1. 11/20/2003: REPLACED YAW DAMPER COUPLER. OPS NORMAL PER MM 22-12-01. CLEARED MEL 22-3-1.SDR SWIA200312602Indicator · malfunctionedCA'S AP DOES NOT HOLD ALTITUDE. REMOVED AND REPLACED NR 1 APC-65B. OPS CHECK GOOD IAW MM 22-11-00. P/N: 622-8317-402, S/N OFF: 4147.SDR SWIA200312592Computer · malfunctionedF/O AUTOPILOT CONTINUES TO MAKE UNCOMMANDED SMALL FORE AND AFT PITCH CHANGES. REMOVED AND REPLACED NR 2 AUTOPILOT COMPUTER WITH A SERVICEABLE COMPUTER. OPS CHECK GOOD IAW 22-10-00.
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