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 ASAA1150614Autoland Sys · malfunctionedUNSAT AUTOLAND. AIRCRAFT LANDED 20 FEET TO THE RIGHT OF RUNWAY CENTER LINE 16R. FFR SHOWS NO PROBLEMS LAST LEG. ACCOMPLISHED DFCS LAND VERIFY AND HGS SYSTEM TEST REF MM 34 36 00. OPS NORMAL.SDR UALA2011110105916Indicator · faultyINST-PANEL (STATE LOCATION) LGT EXTIN. CREW COMMENTS: CAPTS AUTOLND STATUS IND INTEGRAL LTNG 90 PERCENT INOP DOWN TO ONE BULB. NEED MORE TIME TO TROUBLESHOOT. -INF- :NEED AUTOLAND STATUS IND PCN (481-9058). -INF- :IND PCN 481-9058 HAVE BEEN PUT IN LOB. SDR SWIA201128305Actuator · failedYAW DAMPER 2 STATUS MESSAGE AFTER UNCOMMANDED RUDDER INPUT. (FLT 4455) REPLACED NR 2 YAW DAMP LINEAR ACTUATOR. P/N: 622-9968-001 S/N OFF: 2215.SDR ASAA11510564Autoland Sys · malfunctionedAUTOLAND / HGS APPROACH AIRCRAFT WAS OFFSET TO THE LEFT OF CENTERLINE ABOUT 1/4 THE WIDTH OF THE RUNWAY. CONDITIONS WERE CAT 1 THEREFORE AUTOLAND WAS ABORTED. ACCOMPLISHED FIM 22 11 00 TASK 825 AND AMM 22 11 00 DFCS GP 49 LAND VERIFY TESTS OPS CHECK NORMAL. SDR ASAA11510551Unknown · malfunctionedWITH AUTO PILOT "B" ENGAGED AIRPLANE ROLLED 1/4 DEGREE LEFT TO RIGHT (INDICATED ON THE AILERON TRIM INDICATOR ON YOKE) FLIGHT ATTENDANTS NOTICED IT MID CABIN. NO ISSUES WITH AUTO PILOT "A" ENGAGED. COULD NOT DUP. DFCS FAULT REVIEW NR 20 LOG NO FAULTS LAST LSDR MASA2011102063882Unknown · malfunctionedCOMMAND BARS DISAPPEAR W/TOGA ON. PERFORMED FUNCTION CHECK OF GO-AROUND MODE WITH NO DISCREPANCIES NOTED.SDR ASAA11510495Circuit Breaker · trippedATTEMPTED AUTOLAND/HGS FAIL. 16L CRIT AREA CLEAR WIND CALM APP WARN IN HGS IN FLARE. TROUBLESHOT SYSTEM AND FOUND CIRCUIT BREAKER SYSTEM A FCC DC TO BE TRIPPED. RESET CIRCUIT BREAKER. OPS CHECK GOOD IAW ASA B737 NG FIM 34 36 00 810 807.SDR UALA2011101105524Control Panel · faultyON TRIPLE AUTOPILOT APPROACH, AT COMPLETION OF AUTOLAND TEST, AIRSPEED BUG WENT UP OVER 200. REPLACED MCP FOR CF377. ACCOMPLISHED CAT III CHECK.SDR ASAA11510494Unknown · malfunctionedON ILS 7L. CHANNEL A SINGLE CHANNEL APPROACH. AUTOPILOT HAD A CONTINUOUS + 1 DEG PORPOISE IN PITCH. FROM 1600 FT TO 800 FT. I DISCONTINUED AUTOPILOT. TOWER SAID THEY HAD NO COMPLAINTS FROM OTHER AIRCRAFT. PERFORMED DFCS CURRENT STATUS QUICK TEST GRP 10 PER SDR ASAA11510493Unknown · malfunctionedAUTOLAND UNSUCCESSFUL LANDED TOO FAR LEFT OF CENTERLINE, ALSO AIRCRAFT PITCHED OVER IN LAST 50 FEET EXCESSIVELY. BUT DID MANAGE TO CORRECT. WINDS WERE CALM CRITICAL AREA CLEAR. UNABLE TO CONFIRM FAULT. 2 FAULTS RECORDED ON DATE OF DISCREPANCY ONE ADIRU FAULSDR AALA20111006LGW01Control Panel · failedMXP - CREW REPORTED ON TAKEOFF ROLL, FIRST OFFICER OBSERVED LOSS OF BOTH FLIGHT DIRECTORS. AFTER TAKEOFF COMMAND AIRSPEED BUGS ALSO NOTED MISSING FROM BOTH SIDES. AUTOPILOT MODE CONTROL PANEL LOCKED UP. NO WARNING INDICATIONS OR EICAS MESSAGES. EMERGENCY DSDR UALA2011100605420Control Panel · failedALTITUDE WON'T GO BELOW 80,000 FT. REPLACED MODE CONTROL PANEL PER MM, OPS NORMAL.SDR UALA2011100505406Control Panel · malfunctionedMODE CONTROL PANEL, HEADING WINDOW DISPLAYS IS BLANK, DOES NOT RESPOND TO HEADING (SEL, HOLD). HEADING STICKS. REPLACED MAIN CONTROL PANEL PER MM. HEADING WINDOW DISPLAY OPS CHECKED NORMAL.SDR UALA2011100505405Control Panel · malfunctionedHEADING SELECT BUTTON ON MAIN CONTROL PANEL INTERMITTENT. REPLACED AFCS MODE CONTROL PANEL PER MM. AIRCRAFT RETURNED TO CAT III STATUS PER MM.SDR C41R201110030104Annunciator · burned outDURING PRE-INSPECTION RUN-UP, TECH FOUND "FD" LIGHT INOP ON AUTOPILOT ANNUNCIATOR. UNIT REMOVED FOR REPAIR.SDR AALA20110930DFW07Circuit Breaker · defectiveDFW - CREW REPORTED CIRCUIT BREAKER 17 POPPED CAUSING AUTOPILOT AND AUTO-THROTTLES TO DISCONNECT. YAW DAMP OFF LIGHT AND MACH TRIM INOPERATIVE LIGHT ILLUMINATED. EMERGENCY DECLARED FLIGHT LANDED DFW WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACEDSDR CA110930008Autopilot Sys · failed(CAN) FLIGHT CREW REPORTED AN AUTO-PILOT FAILURE ON DESCENT. AFTER ATTEMPTING TO RECYCLE THE AP THE FLIGHT EXPERIENCED SOME PITCH OSCILLATION WHICH NECESSITATED TURNING OFF THE AP. IAW SNL-22-0009 INTERIM SOLUTION COMPLETED FIM TASK 22-11-00-810-91T-A AND 22SDR 2011FA0000638Autopilot Sys · malfunctionedAUTOPILOT. COUPLED APPROACHES RESULT ERRATIC ROLL HUNTING AND/OR OVERCORRECTION AND PITCH UNSTABILITY.SDR A9JA3547520110929Interface Unit · defectiveAIRCRAFT IDENTIFIED ABOVE WAS UPGRADED TO AN ASPEN EFD 1000C PRO PFD SYSTEM WITH AN EA 100 AUTOPILOT INTERFACE ON 4/1/2011. ITEMS REMOVED WAS KCS 55A & KI 256 FLIGHT DIRECTOR. THE AIRCRAFT WILL NOT HOLD A STABILIZED APPROACH COUPLED TO THE KFC 200 AUTOPILOT.SDR REXA201100628Autopilot Sys · malfunctionedAUTOPILOT PITCH TRIM CAUTION IN FLIGHT QRH COMPLETE. OPS CHECK AFTER RESET OPS CHECKED GOOD IAW AMM 27-41-15, OPS CHECK GOOD. A/C OK FOR SERVICE.SDR SIMA201126904Warning System · false activationON FLIGHT 4357 THE CREW REPORTED THAT ON THE TAKEOFF ROLL THE CREW STARTED STEERING WITH THE RUDDER PEDALS IT FELT HARD IN STEERING RECEIVED GOT A "YAW DAMP FAIL" MESSAGE ON EICAS. THE CREW ABORTED THE TAKEOFF AND RETURNED TO GATE. THE AIRCRAFT WAS REMOVED SDR REXA201100593Yaw Damper · faultyYAW DAMPNER MOVES RUDDER IN FLIGHT. REMOVED AND REPLACED NR 1 YD ACTUATOR IAW CRJ AMM 22-22-01, OP CHECK GOOD OK FOR SERVICE. REPEAT FROM 9/19/11.SDR REXA201100569Yaw Damper · faultyCREW REPORTED YAW DAMPER WAS KICKING THE RUDDER THE ENTIRE FLIGHT. CREW DID NOT DECLARE EMERGENCY.SDR REXA201100608Actuator · malfunctionedUNCOMMANDED RUDDER INPUTS, SOME OF THEM ABRUPT, DURING CLIMB, CRUISE AND DESCENT AND WITH THE AUTOPILOT ON OR OFF. RUDDER INPUTS REFLECTED ON TURN COORDINATOR AT VARIOUS SPEEDS. REMOVED AND REPLACED YAW DAMPER NR 2 LINEAR ACTUATOR IAW AMM 22-22-01. OPS CHECSDR ASAA11510388Unknown · malfunctionedON DESCENT W/ AUTOPILOT B ENGAGED STAB OUT OF TRIM CAUTION LIGHT ILLUMINATED. IAW QRH DISENGAGED AUTOPILOT STAB DEFINITLEY OUT OF TRIM. RETRIMMED STAB AND RE ENGAGED AUTOPILOT B. NO FURTHER PROBLEMS FOR REMAINDER OF DESCENT. FAULT HISTORY HAS FCC FAULTS FOSDR REXA201100568Yaw Damper · faultyCREW REPORTED AIRCRAFT HAD UNCOMMENTED RUDDER MOVEMENT IN FLIGHT WITH AUTOPILOT ENGAGED AND DISENGAGED. REPORT THE AIRCRAFT WAS KICKING RIGHT. REMOVED AND REPLACED YAW DAMPNER ACTUATOR IAW AMM 22-22-01.SDR ASAA11510364Circuit Breaker · trippedSYS B MACH TRIM CB POPPED ON PREFLIGHT. INSPECTED AREA BEHIND P6 2 PANEL. NO DEFECTS NOTED. INSPECTED AFCS SYS B MACH TRIM DC C/B. NO DEFECTS NOTED. RESET AFCS SYS B TRIM DC C/B AMM 20 60 01. OPS CHECK GOOD REF AMM 22 11 24 740 801.SDR 2011FA0000630Autopilot Sys · failedAUTOPILOT FAILED TO DISENGAGE ON COUPLED APPROACH.SDR UALA2011090204741Control Panel · faultyGLASS PARTIALLY DISTORTED IN MCP ALTITUDE WINDOW FROM CAPS SIDE. ALT WINDOW OKAY FROM F/O'S SIDE. REPLACED MCP PER MM, OP TESTS NORMAL.SDR ASAA11510332Unknown · malfunctionedFD FLAG ON CAPT PRIMARY ATTITUDE GYRO. RECYCLED ACFT POWER ACCOMPLISHED FIM TASK 22 11 00 810 801. DFCS BITE (FD BITE) PASSED NORMAL.SDR UALA2011082404535Control Panel · faultyLOST AUTOPILOT, FLIGHT DIVERTED. MCDP LAST FLT FAULTS SHOWED, 'AP DISC SAM L-FCC L''AP DISC SAM L -FCC C' ' AP DISC SAM R- FCC C' AP DISC SAM R- FCC R'. ALSO HAD FAULT BALL IN SAM ON LT AND RT SAM MODULE. REPLACED RT SAM. REF ITEM 6882003 FOR LT SAM AND MCPSDR AALA20110822DFW02Computer · malfunctionedDFW - CREW REPORTED NAVIGATION SYSTEM ISSUES DURING CLIMBOUT. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. REPLACED NUMBERS ONE AND TWO DIGITAL FLIGHT GUIDANCE COMPUTERS AND NUMBERS ONE AND TWO INERTIAL REFERENCE UNIT COMPUTERS. SYSTEM GRSDR ASAA11510259Autopilot Sys · malfunctionedAUTOLAND NOT SUCCESSFUL. AIRCRAFT LANDED WAY LEFT OF CENTER LINE. PERFORMED "LAND VERIFY" TEST PER AMM 22 11 00 700 801. ALL TESTS PASSED.SDR UALA2011080804159Control Panel · faultyIN FLIGHT IT WAS DIFFICULT TO GET IAS-MACH ON MCP TO CHANGE BETWEEN MACH AND AIRSPEED. COMPLIED WITH MEL. REPLACED THE AFCS MODE CONTROL PANEL PER MM, OPS CHECKED OKAY.SDR UALA2011080804163Actuator · leakingWITH PACKS ON, BURNING OIL SMELL IN CABIN. PER TAXI CREW, SMELL IS PRESENT WITH APU SUPPLYING AIR. OPENED APU COMPT DOORS AND FOUND A LARGE VOLUME OF HYDRAULIC FLUID IN THE APU INTAKE DUCT. FOUND EVIDENCE OF HYD FLUID LEAK INTO LOWER RUDDER COMPT APPEARS TOSDR SWAA115759Panel · faultyDECLARED EMERGENCY - AT ROTATION, SERIES OF FAILURES, AUDIO FOR AUTO PILOT, A/P LIGHTS, YAW DAMPER ILLUMINATED, MACH TRIM FAIL, AND SMOKE REPORTED BY FLIGHT ATTENDANTS. REMOVED AND REPLACED FSAU, FCC'B, LRRA-1, AND MCP IAW MM.SDR ANCF2011052900082Warning Light · illuminatedREJECTED TAKEOFF, DURING TAKEOFF ECAM MESSAGE, THIS MESSAGE (THRUST MESSAGE) APPEARS ON THE ECAM AP REJECTED WAS BELOW 100 KNOTS, MESSAGE "ENGINE THRUST NO SET". IAW AMM TASK 22-96-00-710-001 THE OPS TEST AUTOPILOT SYS WAS PERFORMED, TEST SATISFACTORY. (PFSDR A6WA201140614Warning Message · illuminatedFLIAPS DEGRAGED, WHITE STATUS MESSAGE APPEARED. C/W FIM FAULT RESET PROCEDURE MESSAGE CLEARED.SDR ASAA11510144Unknown · malfunctionedAUTOPILOT "B" CMD BUTTON. THE GREEN LIGHT THAT NORMALLY STAYS ILLUMINATED WHEN THE CMD BUTTON IS SELECTED IS NOW FLASHING. THE AUTOPILOT IS WORKING NORMALLY. ACCOMPLISHED DFCS LAND VERIFY TEST PER AMM PT II 22 11 00/201. ALL TESTS PASSED. VERIFIED "B" CMDSDR 2011FA0000467Servo Drive · stickingDURING LEVEL FLIGHT AT 17,500 FT, WITH THE AUTOPILOT ENGAGED THE ACFT STARTED AN UNCOMMANDED RT BANK TURN WHICH CONTINUED UNTIL THE PILOT OVERRODE THE AUTOPILOT BY FORCE. THE AUTOPILOT DISCONNECT HAD LIMITED EFFECT AND THE ACFT CONTINUED TO REQUIRE LT AILERON SDR UALA2011071503606Computer · faultyWITH CENTER AP ENGAGED RIGHT FCC ONLY PROVIDES VERTICAL GUIDANCE CMND BAR NO LATERAL GUIDANCE. REPLACED RIGHT FCC COMPUTER TESTED OKAY.SDR UALA2011071303522Module · faultyAILERON LOCKOUT EICAS, RTFL. REPLACED R FCC PER MM. PERFORMED SATISFACTORY CAT III CHECK PER MM22-10-00. REPLACED RT STAB TRIM AILERON LOCK MODULE. SYSTEM CHECKS OK AT THIS TIME. MESSAGE CLEARED. ACFT RETURNED TO CAT III SERVICE.SDR MASA2011071303212Computer · malfunctionedUNCOMMANDED SPD BUG CHANGE WITH AUTO PILOT ON CLIMB. PLACED ON MEL. RERACKED FCC 1 AND 2SDR UALA2011071103439B-Nut · looseHYD LEAK ON RT SIDE OFF FUSELAGE JUST AFT OF RT ELEVATOR. SECURED 'B' NUT CONNECTION ON THE LEFT YAW DAMPER SERVO. ACCMP'D HYD SYSTEM GENERAL EXTERNAL LEAK CHECK IAW MM, ALL CHECKS GOOD.SDR AALA20110712TUL01Module · faultyMIA - INFLIGHT STI-JFK. CREW REPORTED AILERON AND AUTO-PILOT FAULTS. EMERGENCY DECLARED FLIGHT DIVERTED MIA LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED STABILIZER TRIM/ELEVATOR ASYMMETRY MODULE. SYSTEM GROUND CHECK NORMAL OPERATION.SDR ASAA11510018Unknown · malfunctionedCAPT "FD" FLAG DISPLAYED. CYCLED AC & DC POWER. CAPT'S "FD" FLAG CLEARED ACCOMPLISHED DFCS BITE AUTOTEST. SYS TEST PASSED. REF AMM TASK 22 11 00 810 801.SDR ASAA1159985Unknown · malfunctionedAUTOLAND TOUCHED DOWN APPX IN LINE WITH LEFT HASH MARK OF RUNWAY WHILE CORRECTING TO THE RIGHT. PERF'D DFCS CURRENT STATUS TEST REF AMM 22 11 00 NO FAULTS BUT FLIGHT FAULT REVIEW REVEALED BOTH A/P'S WITH "VOR/LOC BEAM ANOMALY DETECTED" DURING APPCH/FLARE. ACSDR SWIA201126642Trim Switch · defectivePITCH TRIM RUNAWAY ON LANDING. (FLT 5341) REPLACED BOTH PITCH TRIM SWITCHES, BOTH AUTOPILOT COMPUTERS AND ELEVATOR SERVO.SDR CHQA201100247Yaw Damper · malfunctionedCREW REPORTED DURING CLIMB RECEIVED A RUDDER 1 AND 2 INOPERATIVE MESSAGE, FOLLOWED BY A YAW DAMPER AND AUTOPILOT FAIL MESSAGE ON THE EICAS. RETURNED TO KRDU AND LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED SUCCESSFUL OPERATIONAL CHECKS OF THE RUDDER SYSTEMSDR UALA2011062103048Control Panel · faultyIAS - MACH WON'T CHANGE FROM MACH TO IAS. REPLACED MODE CONTROL PANEL. AIRCRAFT IS CAT 1 ONLY. NEEDS CATII- III CHECK REFERENCE CF ITEM 201.
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