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 N6WA2013080402Autopilot Sys · malfunctionedUNABLE TO CONTROL ALTITUDE WITH AUTOPILOT ENGAGED (RETURN FROM FLIGHT, FUEL REQUIREMENT FOR A/P INOPERATIVE.SDR ASAA2013080395729Control Panel · failedTHE MODE CONTROL PANEL AUTO PILOT CMD FOR AN AUTO PILOT SWITCH LIGHT ARE INOP. ACFT GROUNDED. REPLACED DFCS MCP IAW AMM REF 22-11-34-000-801/22-11-34-400-801. OPS CKS GOOD IAW AMM REF TASK 22-11-34-740-801. PERFORMED ADDITIONAL MINIMUM TESTS TO MAINTAIN ACSDR REXA2013080301551Computer · malfunctionedDURING CLIMB THRU 16000 FT, ACFT JERKED ABRUPTLY LATERALLY DISPLACING ABOUT 10-20 DEGREES. ISSUE CONTINUED TO GET MORE VIOLENT AND VERY ABRUPT. DISCONNECTED THE YAW DAMPER AND ASSUMED MANUAL CONTROL. RUDDER TRIM SEEMED TO INITALLY WORK NORMAL BUT AS THE PROSDR YYFA20130820001Autopilot Sys · malfunctionedAUTOPILOT NR 1 WILL NOT ENGAGE. HAS ROLL MOVEMENT. AUTOPILOT NR 2 ENGAGES FOR A SHORT PERIOD OF TIME BUT ALSO HAS ROLL MOVEMENT BEFORE DISCONNECTING.SDR SWIA201334128Yaw Damper · failedUNCOMMANDED NOSE RT YAW DURING CRUISE, YAW DAMPER CAUTION MESSAGE ALONG WITH THE UNCOMMANDED YAW DAMPER DISCONNECT. FLT#4598 REPLACED NR 2 YAW DAMPER & BOTH FCC`S COMPUTERS. PASSED FUNCTIONAL FLIGHT.SDR ASAA2013072695685Display · malfunctionedDURING CLIMBOUT, LOST ALL VNAV ABILITY AND INFORMATION FROM 8000 TO TOP OF CLIMB. AT LEVEL OFF, TOC, MCDUS IN IN LEGS PAGES FLASHED AND VNAV RETURNED AND FUNCTIONED PROPERLY FOR REMAINDER OF FLIGHT. ACFT GROUNDED. PERFORMED DFCS BITE CHECK AND MOD CONTROL PSDR ASAA2013071795630Unknown · unknownAUTOLAND TOUCHDOWN, RT OF CTR-LINE. ACFT GROUNDED. FFR SHOWS ONE FAULT - LEG FIVE FOR LOC NOT TUNED. CURRENT STATUS TEST PASS, NO FAULTS. ACCOMPLISHED LAND VERIFY TEST, BITE GRP. NR 49, TEST PASS. GROUND VERIFICATION SATISFACTORY.SDR REXA2013071401358Autopilot Sys · malfunctionedAUTOPILOT LEFT AND RIGHT ROLL CONTROL WEAK. AUTOPILOT TRIM ROLL CAUTION.SDR ASAA2013071395584Warning Light · no testCAPTAIN`S AUTO FLIGHT ANNUNCIATOR ALL LIGHTS OUT. FAILS TO TEST. ACFT GROUNDED. ACCOMPLISHED AUTO FLIGHT ANNUNCIATOR TEST AND GVI REF AMM 22-11-32-710-801. OPS CHECKED GOOD. NO DEFECTS NOTED.SDR CA130711009Motor · failed(CAN) THE ELEVATOR SERVO MOTOR WAS RECEIVED IN REPAIRED CONDITION AND INSTALLED, AFTER 3.2 HRS THE CREW WAS CARRYING OUT THE PREFLIGHT FLIGHT CONTROL CHECK AND A LOUD GRINDING NOISE WAS COMING FROM THE AFT PART OF THE ACFT. MAINTENANCE REMOVED THE SERVO MOTORSDR SWIA201333958Yaw Damper · failedYAW DAMP 1 KICKED OFF 3 TIMES IN THE LAST 5 MINUTES OF FLIGHT & AIRCRAFT YAWED LEFT SIGNIFICANTLY. FLT#5182 REPLACED NR 1 YAW DAMPER LINEAR ACTUATOR. PN ON 622-9968-001, SN ON 3467, SN OFF 4212.SDR ASAA2013070695486Autopilot Sys · malfunctionedAFTER LEVEL IN CRUSE FL370 FOR APPROX 15 MINUTES WITH A AUTOPILOT ENGAGED, AUTOPILOT DISENGAGED. AFTER ENGAGING "A" AUTOPILOT IT SEEMED TO WORK. ACFT GROUNDED. BOTH AUTOPILOTS OPERATE NORMALLY, NO HISTORY 30 DAYS.SDR ASMF201308005Autopilot Sys · unknownDURING CRUISE, BOTH AUTOPILOTS WERE OUT OF SERVICE. AIRCRAFT RETURNED. MX PERSONNEL PERFORMED DISENGAGE BAR RESET TEST AND AUTOPILOT SYSTEM CMD A AND B CHECK IAW AMM 22-11-00, TESTED CORRECT.SDR ASAA2013062995354Autopilot Sys · malfunctionedA/P ENGAGED IN COMMAND B LEVEL FLIGHT FL330 DISENGAGED WITHOUT ANY REASON IN SMOOTH AIR, ACFT WAS TRIMMED. ENGAGED COMMAND A AND CONTINUED WITHOUT FURTHER PROBLEMS. ENGAGED COMMAND B ON DESCENT, WORKED NORMALLY. ACFT GROUNDED. PERFORMED FIM TASK 22-11-00-8SDR SWIA201333808Unknown · malfunctionedTHE RUDDER BEGAN KICKING TO THE RT & LT. YAW DAMPER NR 2 TRIPPED OFF. COULD FEEL THE RUDDER BUMPING IN THE PEDALS. FLT#4622 REPLACED BOTH FCC CARDS & NR 2 YAW DAMPER LINEAR ACTUATOR IAW AMM. PN: 622-9815-904 SN: GXDP SN OFF: 2412, PN: 622-9815-904 SN: 1BVCFSDR ASAA2013062395264Unknown · unknown300 AGL, ACFT DRIFTED TO LT EDGE OF RUNWAY. DID NOT CORRECT. CRITICAL AREA WAS CLEAR. ACFT GROUNDED. CAPTAIN MANUALLY DISCONNECTED AUTOPILOT. DID NOT SPECIFY HOW FAR ACFT DRIFTED. NO HISTORY 30 DAYS. PERFORMED FAULT REVIEW, NO FAULTS. PERFORMED LAND VESDR ASAA2013062295241Flight Dir · malfunctionedON TAXI OUT, LEFT NAV WOULD NOT ARM. ACFT GROUNDED. ACCOMPLISHED FLT FAULT REVIEW, GRP BITE 10, NO FAULTS LOGGED. ACCOMPLISHED FLT DIRECTOR TEST, GRP BITE 12, ALL TEST PASSED. ACCOMPLISHED LAND VERIFY TEST, GRP BITE 49, ALL TEST PASSED REF MM 22-00-01. ACFSDR ASAA2013062095240Control Panel · inoperativeAUTOPILOT COMMAND B BUTTON WILL NOT ILLUMINATE AUTOPILOT FUNCTIONS NORMALLY. ACFT GROUNDED. REPLACED MASTER CONTROL PANEL IAW AMM TASK 22-11-34-400-801/22-11-34-000-801. PERFORMED MASTER CONTROL PANEL INSTALLATION TEST IAW AMM TASK 22-11-34-74-801.SDR M3XA201306260136Module · unknownDEPARTED ERLANGER IFR ON A SPECIAL USE DEPARTURE PROCEDURE. ABOUT 15 MINUTES INTO THE FLIGHT LEVEL 6000’ IFR IN IMC CONDITIONS THE AUTO PILOT FAILED. CONTINUED FLIGHT HAND FLYING THE ACFT AND BROKE OUT INTO VFR CONDITIONS APPROX 5 MINUTES LATER AND REMAINED SDR 3BOR2013061800001Control Cable · damagedDURING TAKEOFF ROLL, FLIGHT CREW NOTICED ANOMALIES WITH THE PITCH CONTROL. TAKEOFF WAS SAFELY ABORTED. INSPECTED AND TROUBLESHOT PITCH SYSTEM. FOUND PITCH CONTROL SERVO CABLE RETAINING BALL DISLODGED FROM THE BALL INSERT ON THE PITCH CONTROL SERVO CABLE BARRESDR ASAA2013061795154Unknown · unknownAUTOPILOT B, INOPERATIVE. ACFT GROUNDED. PERFORMED DFCS BITE IAW FIM 22-11, TASK 801, CURRENT STATUS TEST PASSED, NO FAULTS NOTED. PERFORMED DFCS LAND VERIFY TEST IAW MM 22-11-00-700-801, GROUP 49.00 LAND VERIFY TEST PASSED. COULD NOT DUPLICATE MALFUNCTIONSDR QXEA2013061701091Capstan · malfunctionedON LANDING FLARE THE F/O HAD TO USE EXCESSIVE BACK PRESSURE IN THE FLARE. NO CAUTION LIGHTS AND ALL QUANTITIES AND PRESSURES WERE NORMAL. ON TAXI IN WE PULLED BACK ON THE YOKE NUMEROUS TIMES WITH ALL THE SAME (EXCESSIVE FORCE) NEEDED. R & R PITCH SERVO IAW SDR FDEA201306151305Autopilot Sys · malfunctionedACFT WENT INTO AN UNCOMMANDED RIGHT TURN. NOTICED IT HAD GONE INTO HDG MODE AND THE HDG WAS APPROX 112 DEGREES (VS. 030) F/O DISCONNECTED AUTOPILOT AND BANKS 30 LEFT TO REJOIN COURSE. INTERROGATED MAT AND FOUND MAINT MESSAGE 22-11635 NOT ACTIVE. FIM 34-3SDR ASAA2013061495096Autoland Sys · no testPRACTICE AUTOLAND FAIL. CONDITIONS SEA 16L PROTECTED AREA CLEAR INSIDE 8 MILES. COURSE AND GLIDEPATH WERE ERRATIC ALL THE WAY DOWN FINAL. SPEED CONTROL ALSO ERRATIC VARIABLE BETWEEN REF AND REF 15, WINDS WERE 5KTS ON FINAL OR CALM, CALLING 220 AT 8 ON THE GROSDR UALA2013061304073Computer · failedRT FCC FAILURE, FLT DIVERTED. WHILE AT FL380, RECEIVED A NO LAND 3 INDICATION AND THE F/O LOST HIS FLIGHT DIRECTOR BARS. SHORTLY THEREAFTER STARTED TO RECEIVE AN UNUSUAL ODOR CROSS BETWEEN ELECTRICAL AND ODOR OF SHOE POLISH. CREW STARTED TO RUN CHECK LIST ANSDR SAJF2013061702020Control Panel · failed(B-18617) FLIGHT CREW INFORMED BOTH AUTOPILOT TRIPPED OFF IN FLIGHT AT FL260. DURING GROUND OPS CHECK, CONFIRMED THE STABILIZER ELECTRICAL TRIM FUNCTION OUT OF ORDER ALSO. PERFORMED DFCS BITE TEST AND STABILIZER ELECTRICAL TRIM OPS TEST, BOTH RESULTS FAILED.SDR ASAA2013061295086Computer · failedREF T/C 78222000 STEP 2.D.(5) FAILS. WHEN ATTEMPTING TO SELECT V/S MODE ON MCP, MINIMUM SPEED REVERSION ACTIVATES AND V/S REVERTS TO LEVEL CHANGE, WITH UNDERSPEED LIMITING CHARACTER FLASHING IN IAS/MACH DISPLAY. ACFT GROUNDED. SWAPPED FCC A & B, VERIFIED PROSDR ASAA2013060895035Autoland Sys · no testPRACTICE AUTOLAND FAIL. NO WIND, STABLE APPROACH, APPROACH WARN APPEARED MOMENTARILY, FOLLOWED BY A BRIEF PITCH DOWN, THEN STABLE. SIGNAL AND PRESENTION APPEARED STABLE THROUGHOUT APPROACH UNTIL THE WARNING. ACFT GROUNDED. ACCOMPLISHED DFCS FLIGHT FAULT RESDR ASAA2013060695033Light · inoperativeA/P ENGAGE LIGHT IN CMD B-BUTTON INOPERATIVE. ACFT GROUNDED. REVIEW DFCS FFR, NO RELATED FAULTS NOTED. PERFORMED MCP INTERFACE TEST NR 32, REF MM 22-00-01-730-801, TEST PASSED.SDR ASAA2013053194953Autoland Sys · no testEVALUATION AUTOLAND UNSUCCESSFUL, ACFT LINE UP WELL LEFT OF CENTERLINE, FLARED HIGHER THAN NORMAL AND ATTEMPTED TO LAND BEYOND TOUCHDOWN ZONE. PILOT TOOK OVER MANUALLY AND LANDED. ACFT GROUNDED. ACCOMPLISHED FIM 22-11, TASK 825. NO FAULTS ON LAND VERIFY. NSDR ERHA20130604001Yaw Damper · activatedAUTOPILOT WAS RECENTLY INSTALLED THAT HAD A YAW DAMPENER AS AN OPTION. UPON THE TAKEOFF ROLL, THE PILOT CLAIMS THAT THE YAW DAMPENER CAME ONLINE, UNCOMMANDED, CAUSING A LOSS OF DIRECTIONAL CONTROL.SDR ASAA2013052294873Switch · inoperativeAUTOPILOT B WILL NOT ENGAGE IN CMD OR CWS. ACFT GROUNDED. REF WDM 22-11-12 FOUND F/OS S232 A/P DISC SWITCH INOP. REPLACED S232 SWITCH REF MM 22-11-41, OPS CHECK NORMAL.SDR ASAA2013052194866Control Panel · failedAUTOPILOT B WILL NOT ENGAGE. ACFT GROUNDED. REMOVED MODE CONTROL PANEL IAW AMM 22-11-34-000-801. INSTALLED MODE CONTROL PANEL IAW B737-800 AMM 22-11-34-400-801. ACCOMPLISHED OPS CHECK IAW AMM 22-11-34-740-801. OPS CHECK GOOD.SDR ASAA2013051994860Control Panel · failedMCP CMD-B LIGHT OUT. ACFT GROUNDED. R & R DFCS MODE CONTROL PANEL REF MM 22-11-34-400-801. OPS CK NORMAL. PERFORMED ADDITIONAL LWMP TESTS, DFCS LRU INTERFACE TEST FOR MCP GROUP NR 32 REF MM 22-11-34/501. LAND VERIFY TEST GROUP NR 49 IAW MM 22-11-00/201, HSDR ASAA2013051394797Autopilot Sys · malfunctionedAUTOPILOT A DISCONNECTED TWICE IN CRUISE NO OBVIOUS REASON. ACFT GROUNDED. MCP DATA INVALID MSG 22-11607- REF FIM TASK 22-11, TASK 817 & 803 MCP, OPS TEST OK. FULL MCP OVERNIGHT TEST PASSED. NO FAULTS NOTED- CURRENT STATUS OK. GROUND VERIFICATION OF MCP ACCOSDR ASAA2013051094768Control Panel · inoperativeCAPTAINS MCP COURSE SELECTOR NOT FUNCTIONING PROPERLY. ACFT GROUNDED. R & R DFCS MODE CONT PANEL IAW 22-11-34. SYS OPS CKS NORMAL IAW SAME, DFCS BITE GRP NR 35 & 49 GO HGS SENSOR TEST IAW 34-36-00 PASS.SDR ASAA2013051094767Computer · failedAUTOPILOT WILL NOT ENGAGE. ACFT GROUNDED. CONFIRMED FAILURE. REPLACED FCC IAW AMM REF 22-11-33-000-801/22-11-33-400-801 FCC A. OPS CHECKED GOOD.SDR ASAA2013050894743Control Panel · stuckALTITUDE SELECT WINDOW ON THE MCP IS STUCK ON 9000FT. ACFT GROUNDED. ALTITUDE WINDOW ON MCP INTERMITTENTLY GOES TO 50,000 AND 8,100FT ON ITS OWN. ALTITUDE ON BOTH PFDS FOLLOW MCP. REPLACED MCP REF AMM 22-11-34. OPS CHECK NORMAL. LAND VERIFY TEST PASSED RSDR ASAA2013042694619Autoland Sys · malfunctionedAUTOLAND UNSUCCESSFUL. ACFT DOVE FOR RUNWAY DURING LAST 10 FEET CAUSING BOUNCING OF ACFT 3 FEET INTO THE AIR. ACFT GROUNDED. PERFORMED DFCS FAULT REVIEW (BITE GRP 20) IAW FIM 22-11, TASK 801, NO FAULTS. PERFORMED RECORDED FAULT REVIEW OF HGS IAW SMM REF 34SDR RAIA201304180001Autopilot Sys · failedDURING CRUISE FLIGHT THE AUTOPILOT FAILED. THE ELEVATOR JAMMED AND FLIGHT CREW PULLED THE ELEVATOR DISCONNECT. AIRCRAFT MADE AN EMERGENCY LANDING IN CLE. MAINTENANCE RECONNECTED THE ELEVATOR DISCONNECT. REMOVED AND REPLACED THE CVR AND FDR FOR INVESTIGATIOSDR ASAA2013041894547Autopilot Sys · malfunctionedON CLIMBOUT, AUTOPILOT NR 1 CMDA DISENGAGED. RECONNECTED AND IT WORKED NORMALLY FOR THE REST OF FLIGHT. THREE INFLIGHT FAULTS FOR VNAV/LNAV INCORRECT DATA. PERFORMED LWMP TESTS REF FIM 22-11/801 BITE GRP NR 20 AMM 22-11-00/201 BITE GRPNR 49 LAND VERIFY ANDSDR ASAA2013041794525Selector Panel · malfunctionedLEFT MOST DIGIT ON MCP HEADING SELECT DISPLAY IS ALMOST INVISIBLE FROM F/O SEAT. REPLACED MCP REF MM 22-11-34. OPS CHECK NORMAL. ACCOMPLISHED MCP LWMP CHECKS REF CHECKLIST MM 22-00-01, ALL TEST PASSED. ACFT REMAINS CAT III A AUTOLAND & HGS. VERIFIED STATUSSDR ASAA2013041794522Flight Dir · inoperativeCAPTAIN`S FLIGHT DIRECTOR DISAPPEARED AT GLIDE SLOPE INTERCEPT. TRIED TO RESTORE, MOMENTARILY CAME BACK AND THEN DISAPPEARED AGAIN. DFCS FFR LOGGED MMR/ILS RECEIVER-1 & RADIO ALT 1 FOR PREVIOUS FLT WITH NO OTHER OCCURRENCE IN FFR. NO HISTORY IN TRAX PAST 30 SDR PNSA2013041701Control Panel · faultyPILOT SQUAWKED "PITCH KNOB AUTO PILOT PANEL WORKS IN REVERSE" ON FLIGHT LOG PAGE. A PITCH UP COMMAND RESULTED IN A PITCH DOWN CONDITION AND A PITCH DOWN COMMAND RESULTED IN A PITCH UP CONDITION. MAINTENANCE CONFIRMED DEFECT ON GROUND. PANEL WAS CORRECTLY ORSDR ASAA2013041694503Control Panel · inoperativeHEADING SELECT KNOB WILL NOT CHANGE HEADING. REPLACED DFCS MODE CONTROL PANEL AND TESTS NORMAL IAW MM 22-11-34. BITE TEST GROUP NR 32 PASS. DFCS LRU INTERFACE TEST PASS IAW MM 22-11-34. DFCS LAND VERIFIY TESTS NORMAL IAW MM 22-00-00. HGS SENSOR TEST FOR FSDR SWIA201333244Unknown · malfunctionedESTABLISHED ON FINAL, FULLY CONFIGURED AT THE FINAL APPROACH FIX, THE FLIGHT DIRECTOR SWITCHED OVER TO B/C MODE & PITCH MODE. THE AIRCRAFT TURNED 15° TO THE RIGHT. PILOT DISCONNECTED THE AUTO PILOT AND FLEW THE REST OF THE APPROACH. (FLT 4474) PERFORMED FSDR ASAA2013041394454Warning Light · false activationWHILE ACCOMPLISHING LAND VERIFY TEST FCC B FAILED SPEED/ STAB TEST, MSG 22-00026 S154 ELV POS TRIED TEST SEVERAL TIMES. COULD NOT DUPLICATE. PERFORMED FIM22-12/812, FOUND FAULT NOT ACTIVE. ACCOMPLISHED DFCS FLT FAULT REVIEW, CURRENT STATUS NR 10 CK, EXTENDEDSDR ASAA2013041094445Display · malfunctionedVNAV WOULD NOT ENGAGE AFTER TAKEOFF. FUEL AND ETA INFO DISAPPEARED IN FMC UNTIL LEVEL OFF. VNAV WORKED NORMALLY AFTER LEVEL OFF WHEN FUEL AND ETA INFO REAPPEARED IN FMC. IAW AMM 22-00-01, C/W BITE TEST GROUP NR 35 (DFCS LRU INTERFACE TEST FOR FCC) & NR 49 (SDR YENA20130407069I/O Module · failedFLT 978 FLL-BOS, AIR RETURN TO FLL DUE TO AUTO PILOT, AUTO THROTTLE FAILED IN FLIGHT. AUTO THROTTLE AURAL WARNING ON CONTINUOUSLY. TROUBLESHOOTING PER FAULT CODE 22110029PB1 FIM 22-11-00-810-82M. REMOVED AND REPLACED AIOPB1 IN MAU 1 MOD 9/10. GROUND OPS CHSDR ASAA2013040694403Control Panel · inoperativeMCP VERTICAL SPEED MODE INOPERATIVE. R & R MODE CONTROL PANEL IAW AMM 22-11-34-000-801 AND 22-11-34-400-81. OPS CHECK GOOD IAW MODE CONTROL PANEL INSTALLATION TEST - AMM 22-11-34-740-80.
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