JASC 2210
Service difficulty reports · 4,016
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 ASAA2014030107026Button · malfunctionedLIGHT INOPERATIVE ON VNAV SELECTOR BUTTON ON MCP. ACFT GROUNDED. PERFORMED DFGS LRU TEST FOR MCP IAW MM 22-11-33/401 & THE HYD OFF PORTION OF THE LAND VERIFY IAW MM 22-11-00 / 201. BOTH PASSED. NO DEFECT NOTED.SDR ASAA2014022807027Autoland Sys · malfunctionedAUTOLAND TOUCHED DOWN BEYOND LATERAL LIMITS TO THE LT OF CENTERLINE. NO OBSERVED TRAFFIC IN ILS CRITICAL AREA. DID NOTICE LOC WAVERING BACK AND FORTH AT APPROXIMATELY 500-600' WHICH MAY HAVE BEEN ATTRIBUTED TO DEPARTING ACFT BUT LOC SEEMED TO TRACK NORMALLY ASDR USAA2014022700004Autopilot Sys · malfunctionedAT CRUISE AILERON FIRST OFFICER PFD INDICATION 40 LT OFF COURSE, LATER CHANGING TO 9R OFF COURSE. WHILE CAPT PFD SHOWED ON COURSE, FIRST OFFICER FLIGHT DIRECTOR COMMANDING A RT TURN CHANGING TO A LT TURN WITH AUTO PILOT 1 ENGAGED. CROSS CHECKED WITH A VOR SHSDR ASAA2014022406978Autoland Sys · malfunctionedUNSUCCESSFUL AUTOLAND-TOUCHED DOWN BEYOND LATERAL LIMITS TO THE LT OF CENTERLINE. ACFT GROUNDED. RESET SYS, RAN LAND VERIFY TEST, COMPUTER FAULT HISTORY. NO RELATED FAULTS, REF AMM 22-11-00, OPS CHECK GOOD.SDR IPXA2014022682044Computer · faultedLEVEL ONE SINGLE LAND WARNING RECEIVED AT CRUISE AND APPROACH, LEVEL 2 FCC1A DATA FAULT WARNING RECEIVED WITH LEVEL 1 SELECT YAW LOWER B OFF AND SELECT LSAS LIB OFF WARNINGS. CHECKLIST PROCEDURES FOLLOWED. CHECK CURRENT FAULT, FOUND FCC 1 DATA FAIL RECYCLESDR USAA2014022400025Unknown · malfunctionedCREW ADVISED BELOW 10,000 FEET, THEY RECEIVED AN ELAC 1 & 2 ECAM WITH AUTOPILOT NR 1 ON. AUTOPILOT DISCONNECTED COMPLIED WITH ECAM & STANDARD OPERATIONS. RESET ELAC NR 2 & IT OPERATED NORMALLY WITH AUTOPILOT NR 1 ENGAGED. CREW DECLARED AN EMERGENCY & LANDED SDR FDEA201402210391Computer · malfunctionedDURING GO AROUND FROM RUNWAY 8L, AFTER FLAG ELECTED TO 28, ACFT ACCELERATED TO APPROX 230 WHILE ON AUTO FLIGHT. FCP HAS BEEN SET TO 4000 FEET & ACFT FAILED TO LEVEL OFF AT ALTITUDE. FIRST OFFICER AS PF DISCONNECTED AUTO PILOT & ATTEMPTED TO RETURN ACFT TO SDR SIMA20140220001Autopilot Sys · malfunctionedWHEN ON THE APPROACH THE AP DID A HARD RT TURN & THEN A HARD LT TURN. FLIGHT CREW PLACARDED IAW MEL 22-01.SDR CALA2014022190413Yaw Damper · malfunctionedYAW DAMPER 1 INOPERATIVE AUTO FLT. CYCLED BREAKERS B 3 & 4, RESET FAC1. PERFORMED AFS TEST IAW MM22-96-00, CHECKED GOOD.SDR ASAA2014021806895Sensor · faultedDURING PREFLIGHT "SPEED TRIM FAIL" ILLUMINATED. ACFT GROUNDED. DFCS BITE SELF TEST SHOWS FCC-B SELF TEST FAIL. FAULT 22-11338, 22-11126 ELEVATOR POS SEN-2 FAULTS. VERIFIED FAULT. REPLACED ELEVATOR POSITION SENSOR IAW MM 22-11-30. OPS NORMAL. ACCOMPLISHESDR SWIA201436390Autopilot Sys · malfunctionedUNCOMMANDED TURN BY AUTOPILOT WITHOUT INPUT. FLT 5332 TROUBLE SHOT AUTOPILOT SYS, NO SIGNIFICANT MDC FAULTS FOUND. SERVO SPIN TEST GOOD, RAN THE NAV TESTER & HEADING WORKS FINE WHEN ENGAGED. COULD NOT DUPLICATE, AUTOPILOT OPERATIONS CHECKED GOOD IAW AMM.SDR CA140218002Servo · faulted(CAN) THE RT SIDE ELECTRIC TRIM DID NOT RESPOND WHEN NOSE DOWN TRIM WAS SELECTED ON CLIMBOUT. ACFT RETURNED TO MAINTENANCE BASE & LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AFFECTED SYS IN DETAIL AND FOUND THE ELEVATOR TRIM SERVO PN: 622-5734-002 TO BSDR SIMA20140211008Control Cable · brokenAILERON AUTOPILOT CABLE HAS BROKEN STRANDS AT THE SERVO MOTOR DRUM. R & R AILERON AUTOPILOT CABLE IAW AMM 27-11-00. REFER TO NON-ROUTINE E367248 FOR OPERATIONS CHECK OF AILERON SERVO.SDR YENA20140207024Fms · failedAIR RETURN, GROSS NAV ERROR DURING TAKE OFF, NO ECAM. TROUBLESHOT NR 1 FMGC, UNABLE TO DUMP DATA FROM KPBI TO KBOS, EVEN WHEN SWITCHING DATABASES. ATTEMPTED SEVERAL RESETS OF FMGC NR 1 AND NR 2, UNSUCCESSFUL. RELOADED FMS NR 1 WITH CURRENT DATA IAW 22-70-00SDR A6WA201441114Actuator · faultyDURING CLIMB ACFT YAWED UNCOMMANDED. COMPLIED WITH QRH, DISCONNECTED YAW DAMPERS & YAWING PERSISTED. FD NR 2 WAS ENGAGED. ACFT RETURNED TO PHL, EMERGENCY DECLARED. LANDED AT 46,900 LBS, NORMAL LANDING. IAW WO 212612 WC 5 FOR TROUBLESHOOTING & WORK PERFORMSDR 9JLA201402123197Circuit Card · defectiveTHE CREW REPORTED THAT ON 2014/01/26 THAT THE YAW DAMPENER DISENGAGED DURING FLIGHT WHILE IN TURBULENCE, THE NR 1 FCC CARD WAS REPLACED WITH A TESTED UNIT PN 822-1019-313 & SN 1C68V. FUNCTIONAL CHECKS WERE SATISFACTORY & THE ACFT WAS RETURNED TO SERVICE. THESDR ASAA2014020206756Computer · failedSTABILIZER OUT OF TRIM LIGHT AT FL 385, 12 KTS FASTER THAN COMMAND SPEED. OUT OF TRIM WHEN AUTOPILOT A ENGAGED, WAS NOT TRIMMING. ACFT GROUNDED. HARD FAILURE DURING SPEED-STAB BITE LIBRARY TEST 60.32, REPLACED FCC "A" IAW AMM 22-11-33, OPS CHECK GOOD. BITSDR ASAA2014012712501Autopilot Sys · malfunctionedWHILE PERFORMING AN AUTOLAND, BOTH AUTOPILOTS DISCONNECTED AT 1000 FEET. ACFT GROUNDED. FOUND DFCS A FAULT 22-11189 AILERON SYNC INVALID LAST LEG. ACCOMPLISHED FIM 22-12 TASK 813. AILERON SENSOR RIGGING WITHIN TOLERANCE, REPAIR CONFIRMATION, OPS NORMAL. ASDR CALA2014012290212Autoland Sys · malfunctionedAUTO LAND UNSATISFACTORY EXCESSIVE WING ROCKING ON SHORT FINAL. WINDS GUSTING TO 20 KTS MINIMAL CROSS WIND. UNSUCCESSFUL AUTO LAND REPORTED, PERFORMED TEST 30 IAW MM 22-00-00. ALL TESTED GOOD AT THIS TIME, OK TO CONTINUE.SDR CALA2014012190205Warning System · activatedAUTO FLT YAW DAMPER 2 DISPLAYED ON UPPER ECAM SCREEN.SDR FDEA201401150102Autoland Sys · malfunctionedAFTER BLOCK OUT, ACFT WENT TO SINGLE LAND 1, NO AUTO LAND. RELEASED FOR SERVICE IAW MEL 22-10-03 CATEGORY C. AUTO LAND SYS INOPERATIVE.SDR SIMA20140112001Unknown · malfunctionedDURING APPROACH ON FLIGHT 3145 CREW REPORTED BELOW 2500 RADIO ALTITUDE CAPTAIN DISCONNECTED THE AUTO PILOT USING THE QUICK DISCONNECT BUTTON. THERE WAS NO AUTOPILOT, AUTOPILOT AURAL WARNING. THE ACFT WAS REMOVED FROM SERVICE. ACCOMPLISHED AUTOPILOT FUNCTIONSDR SWAA2014011524121Unknown · failedPOWERED UP USING EXTERNAL POWER A STRONG ELECTRICAL SMOKE SMELL OCCURRED. R & R IFSAU IAW AMM.SDR USAA2014010600032Autoland Sys · malfunctionedAUTO LAND FAILURE BELOW 100' RA. CAPTAIN DISCONNECTED AUTOPILOT & LANDED VISUALLY. ACCOMPLISHED A321 TSM 22-00-00-810-801A, NO FAULTS. ACCOMPLISHED RA 1 & 2 RAMP TEST IAW A321 AMM 34-42-00-730-002A & RA 1 & 2 BITE IAW 34-42-00-740-002A, NO FAULTS FOUND. ACSDR ENHA20140103Autopilot Sys · malfunctionedAFTER REACHING A CRUISE ALTITUDE OF 4000 ON AN IFR FLT THE AUTOPILOT BEGAN TO MALFUNCTION. THE PILOT OBSERVED THE COMMAND BARS ON THE FLIGHT DIRECTOR GOING OUT OF VIEW & ALTITUDE STARTING TO GRADUALLY DESCEND. AT THIS POINT THE PILOT ATTEMPTED TO CORRECT THESDR ASAA2014010112294Transmitter · faultedTWICE ON ILS, LOC AND G/S CAPTURED, ACFT NOSED OR PITCHED DOWN EXCESSIVELY. VISUAL CHECK END OF RUNWAY G/S TRANSMITTER WAS NOT BLOCKED, AUTOPILOT. ACFT GROUNDED. C REW VERBAL INFO -A/P DID NOT DISCONNECT ON EITHER TIME. CREW DISCONNECTED A/P. NO FLT FAULTSDR ASAA2014010112293Computer · malfunctionedCRUISING AT F370, AUTOPILOT A, DISCONNECTED IN SMOOTH AIR. CONNECTED OK. FINISHED THE FLIGHT USING AUTOPILOT B. NO PROBLEMS NOTED. ACFT GROUNDED.SDR ASAA2013122912262Autopilot Sys · malfunctionedAUTOPILOT A DISENGAGED TWICE WHILE IN CRUISE FL 360 & MMO 0.79. ACFT GROUNDED. CHECKED FAULT REVIEW, 2 OCCURRENCES OF A/P DISCONNECT AT FL 360, BOTH FAULT MCP MX MSG 22-11607. ACCOMPLISHED FIM TASK 22-817 MODE CONTROL PANEL TESTS. ALL TESTS PASS.SDR ASAA2013122412229Autoland Sys · malfunctionedON A CAT III AUTOLAND, AFTER NORMAL LANDING, AUTOTHROTTLES MOVED THRUST LEVERS FORWARD. ACFT GROUNDED. UNABLE TO DUPLICATE DEFECT. DFCS GROUP NR 20, FAULT REVIEW AND A/T FAULT HISTORY SHOWED NO FAULTS. PERFORMED AUTOTHROTTLE SYS OPS TEST IAW MM 22-31-00-710SDR ASAA2013122212214Computer · no testLAND VERIFY TEST FAILED 60.35 FCC-A ELEV POS SEN-1 MESSAGE 22-11125. ACFT GROUNDED.SDR SWIA201335666Mcu · failedAIRPLANE PITCHES CONTINUALLY IN A WAVE LIKE PATTERN WITH AUTO PILOT ON. ELEVATOR TRIM IS IN CONSTANT MOTION UP & DOWN A FEW TENTHS OF A DEGREE IN BOTH DIRECTIONS. FLT 4611 REPLACED MOTOR CONTROL UNIT & ELEVATOR SERVO IAW AMM. PASSED IN FLIGHT FUNCTIONAL CHESDR FDEA201312143000Autopilot Sys · malfunctionedNR 1 AUTOPILOT ALTITUDE WANDERS FROM SELECTED ALTITUDE TO UP TO 800 FEET LOW. NR 1 AUTOPILOT DISENGAGED TWICE IN FLIGHT. ACFT TRIMMED NORMALLY. PERFORMED SUCCESSFUL AFS TESTS BOTH FCCS IAW MM 22-00-00-5 AND FOLLOWING RVSM FLOW CHART IAW AMM 34-10-00-2. PSDR CALA2013121693712Control Panel · faultySPEED SELECT ON MODE CONTROL PANEL STUCK AT 160 KNOTS. REPLACED AFCS MODE CONTROL PANEL, CHECKED NORMAL.SDR DALA13070130189Computer · failedAFTER APPROXIMATELY 4 HRS OF FLIGHT, WITH ACFT LEVEL AT 370, SMELLED ELECTRICAL ODOR. SHORTLY AFTER, NOTED NO LAND 3 ON AUTO LAND STATUS, ODOR DECREASED CONTINUOSLY TO ZERO BY END OF FLIGHT. PERFORMED TROUBLESHOOTING IAW FIM 22-02, FAULT TREE 808 , PERFORMEDSDR CALA2013120393419Fcu · stuckALT SELECTOR STUCK IN HUNDREDS POSITION. REPLACED FCU IAW AMM & ACCOMPLISHED CATIII TEST IAW 22-97-00, BOTH TESTED OKAY.SDR DXTA2013120205587Autopilot Sys · malfunctionedAT FL380 AUTO PILOT KICKED OFF SEVERAL TIMES THEN FAILED. HAND FLYING THE AILERONS WERE STICKING. FLYING AT FL280 AFTER APPROXIMATELY 1 HOUR THE AILERONS STOPPED STICKING & THE AUTOPILOT RESET. APPLIED POWER TO THE AIRCRAFT & PERFORMED FREEDOM OF MOVEMENT CHSDR HALA2013112800173Autoland Sys · malfunctionedNO LAND 3, NO AUTOLAND ANNUNCIATED ON AUTOLAND STATUS PANEL. MCDP BITE, LAST FLIGHT FAULT SHOWS "RA-C" CODE 130861. TROUBLESHOT IAW FIM 22-02-00, FIG 112 TO BLOCK 22. BITE TEST OF CENTER R/A "PASS" PERFORMED MCAP TEST 40 IAW AMM 22-00-02, TEST PASS.SDR ASAA2013112796551Autoland Sys · malfunctionedAUTOLAND NOT SUCCESSFUL. LANDED 16R WITH ILS CRITICAL AREA CLEAR. AIRCRAFT DRIFTED RT OF CENTERLINE DURING THE FLARE. AIRCRAFT TOUCHED DOWN AT APPROXIMATELY THE 1200 POINT AND APPROXIMATELY 50 RT OF CENTERLINE. WIND WAS CALM. ACFT GROUNDED. NO FAULTS LOGGESDR SWIA201335424Actuator · faultyMINOR BUT ABRUPT YAW TO THE RT & SLIP SKID INDICATING EXCESS RT RUDDER. TRIMMED LT RUDDER & A FEW MINUTES LATER NOSE YAWED LT REQUIRED RT RUDDER TRIM TO CENTER SLIP SKID. FLT 6393 REPLACED NR 2 YAW DAMPENER ACTUATOR. PN ON OFF DL2233M1-1 SN OF 1344 SN OFFSDR A6WA201312024043Autopilot Sys · malfunctioned3925DLY NON COMMANDED YAW MOTION TO THE RT AT FL290 SAT 46C ON FLIGHT DIRECTOR NR 2 FOR APPROXIMATELY 2 SECONDS. YAW DAMPER REMAINED ENGAGED, NO FURTHER OCCURRENCES. INTEGRATED FCC & REPORTS CUT R OCCURRENCE, IAW FIM 22-22, ACTION REQUIRED IS NONE. PERFORMEDSDR SWIA201335413Yaw Damper · failedYD NR 2 KICKS OFF & THERE IS A NOTICEABLE KICK IN THE RT RUDDER. IF RUDDER TRIM MOVES ABOUT A HALF BAR DEFLECTION TO THE LEFT THEN YD 2 DISENGAGES. FLT#4764 REPLACED NR 2 YAW DAMPER IAW AMM. PN DL2233M1-1 SN 3507 SN OFF 3169 PN S24665-134.SDR ASAA2013112596531Control Panel · failedWHILE PERFORMING LAND VERIFY TEST, A AUTOPILOT WOULD NOT ENGAGE WITH FAULT 22-11251. FOUND AN AUTOPILOT ENG INTERLOCK CIRCUIT BREAKER TRIPPED AND WOULD NOT RESET. ACFT GROUNDED. REPLACED MODE CONTROL PANEL, IAW MM 22-11-34, CHECKED GOOD. LLRU REPLACEMENT TSDR ASAA2013112396502Selector · malfunctionedON MCP CAPTAIN`S COURSE SELECTOR IS FROZEN ON 347. RESET IT AGAIN DURING DESCENT AND IT WORKED OK. ACFT GROUNDED. PERFORMED FIM TASK 22-11-803 MODE CONTROL PANEL TEST, ALL TEST PASSED. CPT COURSE WINDOW OPERATES NORMALLY. OK FOR CONTINUED SERVICE.SDR ASAA2013112296499Relay · unknownDURING CLIMB, PASSING LOW 20,000 F/O ATTEMPTED TO ENGAGE AUTOPILOT B, WOULD NOT ENGAGE. TRIED AUTOPILOT A, CWSA, CWSB, BOTH MASTERS - NO COMBINATION WOULD WORK. NO WARNING, CAUTIONS OR HORNS RECEIVED. ALL CBS CHECK GOOD. ACFT GROUNDED. DIVERSION TIME - 46 SDR ASAA2013112196485Autopilot Sys · malfunctionedWITH AUTOPILOT B ENGAGED AT FL 360 IN LNAV & VNAV F/O MAP DISPLAYED AMBER VTK FLAG. PFD SHOWED AMBER LANDING ALT. AUTOPILOT B COMMAND CHANGED. LNAV DISENGAGED. FOLLOWED QRH ITEMS. VTK & LDG ALT AMBER FLAGS WENT AWAY. ACFT GROUNDED. ACCOMPLISHED DFCS BITSDR ASAA2013112096474Computer · failedAT CRUISE, AUTOPILOT A DISENGAGED, CAPTS SPEED & ALTITUDE TAPES DISAPPEARED, SPD & ALT CAUTION LIGHTS APPEARED ON PFD, MACH TRIM FAIL ILLUMINATED ON RECALL AND CAPTAINS PITCH STEERING BAR DISAPPEARED. CONDITION LASTED 15 SECONDS. THIS ANOMOLY OCCURED 5 MORE TSDR ASAA2013111896461Control Panel · lockedDURING TAXI OUT, MCP ALITTUDES LOCKED UP AND NO CHANGES COULD BE MADE. BOTH FDS WERE INOPERATIVE, AND SPEED WINDOW COULD NOT BE CHANGED. A/TS WOULD NOT ARM EITHER. ACFT GROUNDED. RESET POWER TO MCP. PERFOMED MCP TEST IAW FIM 22-11-00-810-803. TEST PASSED.SDR ASAA2013111896454Control Panel · faultedAFTER SELECTING APU ON BUSSES, MCP ALTITUDE AND FD LOCKED UP. ACFT GROUNDED. DEU 1 AND 2 BITE SHOWS CURRENT STATUS FAULTS ON A/T, FCC A AND FCC B. CYCLED POWER TO MCP, FCC A AND FCC B COMPUTERS. OPS RESTORED TO MCP. OPS CHECKED NORMAL 22-11, TASK 803. HGSDR ASAA2013111796447Computer · disconnectedAUTOPILOT A DISCONNECTED DURING CLIMB FOR NO APPARENT REASON. AUTOPILOT A WAS REENGAGED AND OPERATED FINE FOR ABOUT AN HOUR. THEN WHILE AT CRUISE, AUTOPILOT A DISCONNECTED AGAIN, AND AGAIN FOR NO OBVIOUS REASON. AUTOPILOT A WAS REENGAGED AND OPERATED FINE. SDR CA131115004Control Panel · failed(CAN) UNCOMMANDED ACCELERATION ON DEPARTURE. AFTER MANUALLY FLYING FROM THE DEPARTURE UNTIL PASSING 6000FT CLIMBING TO FL 340, STABILIZED ON LOMVI TRACK WITH FMC/FCP IN FMS1/CLB MODE AND SPEED BUG AT 200KTS, WE EXPERIENCED AN UNCOMMANDED ACCELERATION WHEN ENGA
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