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 ASAA2016091918072Autopilot Sys · malfunctionedBOTH LEFT AND RIGHT AUTOPILOT DISENGAGE SWITCHES WOULD DISENGAGE AUTOPILOT. HOWEVER NEITHER SWITCH WOULD SILENCE HORN. GROUNDED - YES. FOUND C/B AFCS SYS A WARN LIGHT (BAT) OUT. DETERMINED C/B COULD BE RESET IAW AMM 20-60-01. LAND VERIFY PASS GROUP 49, IAW AMMSDR ASAA2016091918071Control Panel · failedF/O'S COURSE INDICATOR NOT ILLUMINATED. GROUNDED - YES. REMOVED AND REPLACED MCP, IAW AMM 22-11-34, OPS CHECK NORMAL. ACCOMPLISHED MCP LWMP CHECKS, REF LWMP CHECKLIST IAW AMM 22-00-01, ALL TESTS PASSED. ACFT REMAINS CATIIIA AUTOLAND & HGS, VERIFIED STATUS SCRESDR ASAA2016091818069Control Panel · failedVERTICAL CONTROL WHEEL, UP/DOWN, DOES NOT CHANGE VERTICAL SPEED AFTER SETTING A HIGHER OR LOWER ALTITUDE IN THE ALTITUDE ALERT WINDOW. LEVEL, CHANGE, MODE OPERATES NORMALLY, BOTH A/B AUTOPILOT OPERATE NORMALLY. ACFT GROUNDED. R & R DFCS MODE CONTROL PANEL, SDR ASAA2016091818073Autothrottle Sys · malfunctionedTESTED AUTOLAND & HGS DONE, WIND WAS 2W 10 KTS ON 16R, APPROACH WAS NORMAL WITH NO FAULTS, HAD A BIT OF AN EXCESSIVE FLARE AND ABOUT 50 FEET LONGER BEFORE TOUCH DOWN THAT WAS UNCOMFORTABLE AND FELT IN DANGER OF TAIL STRIKE, BUT DID NOT. ACFT GROUNDED. ACCOMPLISDR ASAA2016091718068Control Panel · failedF/O SIDE COURSE WINDOW SHOWS INCORRECT NR WHEN TURNING FROM 099 TO 110 & 120-140, IE EXTRA LIGHT APPEAR. ACFT GROUNDED. VERIFIED F/O COURSE WINDOW SHOWS INCORRECT DISPLAY OF NRS. REPLACED MCP PANEL, REF AMM 22-11-34. GROUND VERIFICATION GOOD. ACCOMPLISHEDSDR ASAA2016091518044Unknown · malfunctionedDURING AUTOLAND AND HGS APPROACH TO 16R AIRCRAFT BEGAN TO PITCH DOWN ABRUPTLY RT AT POINT IT SHOULD HAVE INITIATED FLARE. AUTOPILOT WAS DISCONNECTED AND ACFT LANDED MANUALLY. ACFT GROUNDED. ACCOMPLISHED DFCS FFR, GROUP 10 AND GROUP 11, ALL TEST PASSED AND NSDR A6WA201644333Unknown · malfunctionedON CLIMBOUT, EXPERIENCED SEVERAL OCCURRENCES OF UNCOMMANDED YAW. ACFT WOULD YAW TO ALMOST FULL BRICK OF DEFECTION, THEN JOLT BACK TO CENTER, FOLLOWED BY SMALL JOLT LT AND RT WITH INDICATION FCC-AMP-Y, RT: 6547, REPAIR RT: 008000, INTERROGATED FCC AND FOUND SDR ASAA2016091318004Control Panel · malfunctionedRIGHT HALF OF FLIGHT CONTROL PANEL BACKLIGHTING INOPERATIVE. ACFT GROUNDED. VERIFIED THAT RT SIDE OF MCP BACKGROUND LIGHTS ARE INTERMITTENT. REPLACED MCP, OPS NORMAL, REF AMM 22-11-34. ACCOMPLISHED BITE GROUP NR 32 DFCS LRU INTERFACE TEST, MCP AND NR 49 LASDR ASAA2016091017987Computer · malfunctionedAUTOTHROTTLES WILL NOT ENGAGE. ACFT GROUNDED. AUTOTHROTTLE SYS LOGGED MULTIPLE FAULT MESSAGES 22-31412 & 22-31413, ELECTRONIC ENGINE CONTROL DATA INV. REF WDM 73-24-21. NO FAULTS LOGGED IN NR 1 & 2 DEU'S, R & R FCC A IAW AMM 22-11-33, OPS CHECK NORMAL.SDR VNAA2016090900006Unknown · malfunctionedUNCOMMANDED ROLL ON APPROACH. THE CREW CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT AND PERFORMED CHECKS IAW THE AMM. OPS CHECKED GOOD. THE ACFT WAS RELEASED FOR SERVICE.SDR ASAA2016090817972Autoland Sys · malfunctionedUNSATISFACTORY AUTOLAND. ACFT LANDED OUTSIDE PARAMETERS. ACFT LANDED WELL RT OF CENTERLINE. PILOT INTERVENTION REQUIRED. ACFT GROUNDED. ACCOMPLISHED FIM 22-11, TASK 801. NO FAULTS FOUND. ACCOMPLISHED LAND VERIFY TEST 49 AMM 22-11-00/201 & HOUSINGS SYS TSDR ASAA2016090417899Control Panel · faultedAUTOPILOT B DISENGAGED TWICE DURING CRUISE FLIGHT, AT FL 340 FT AND AT 10,000 FT DURING DESCENT. ACFT GROUNDED. PERFORMED DFCS BITE BOTH A & B SHOWED FAULTS IN FLT 1. R & R MCP IAW AMM 22-11-34 ALL TEST PASSED.SDR ASAA2016090217900Light · inoperativeMCP PANEL HAS NO LIGHTS. ACFT GROUNDED. CYCLED POWER TO MCP & ALL LIGHTS RETURNED TO NORMAL. PERFORMED FIM 22-11 TASK 803 ALL TESTS PASSED. PERFORMED DFCS LRU INTERFACE TEST FOR MCP IAW AMM 22-11-34 ALL TESTS PASSED & HGS SYSTEM TEST PASSED IAW AMM 34-36-00.SDR ASAA2016090117898Lamp · inoperativeVNAV BUTTON LIGHT BURNED OUT. ACFT GROUNDED. REMOVED AND REPLACED THE CONTROL PANEL IAW AMM 22-11-34, OPS CHECKED NORMAL.SDR ASAA2016083017863Control Panel · malfunctionedVNAV LIGHT ON FMA SELECT PANEL ON MODE CONTROL PANEL IS BURNED OUT. ACFT GROUNDED. CANNOT DUPLICATE. MCP MODE SLECT LIGHTS OPS NORMAL PER DFCS BITE GROUP 60.50, MCP TESTS.SDR ASAA2016083017862Control Panel · failedAUTOPILOT ENGAGE BUTTON LIGHTS INOPERATIVE. AUTOPILOT FUNCTIONS NORMALLY. ACFT GROUNDED. DUPLICATED DISCREPANCY. REMOVED AND INSTALLED A NEW MCP, IAW AMM 22-11-34. ACCOMPLISHED INSTALL TEST, IAW AMM 22-11-34. ACCOMPLISHED LWMP CHECKLIST DFCS LRU INTERFACESDR A6WA201644278Yaw Damper · defectiveWHILE IN CRUISE, ACFT HAD UNCOMMANDED YAW TO LEFT. YAW DAMPERS REMAINED ENGAGED AT ALL TIMES. UNCOMMANDED YAW WAS INTERMITENT AND RANDOM IN NATURE. REQUEST INSPECTION. REMOVED AND INSTALLED NEW LINER ACUATOR YAW DAMPER IAW 22-22-01. OPS CHECKED GOOD IAW SDR P5CA2016083000248Module · malfunctionedSTABILIZER TRIM UNSCHEDULED STATUS. SRM R & R, TESTED OK IAW AMM 27-41-01, LP691776M8. STABILIZER COMPARTMENT RELATED PARTS INSPECTED NORMAL. FCC L, C, R AND SRM L AND R RERACKED, STABILIZER TRIM GROUND TEST CUTOUT PASSED IAW AMM 22-11-00.SDR AALA20160828002Trim System · faultyUSING AUTOPILOT NR 2 ACCELERATING OUT OF 10K, AIRCRAFT FLEW IN A RIGHT BANK WITH NO RUDDER TRIM. TURNED OFF AUTOPILOT, COULD NOT TRIM THE AIRCRAFT INTO COORDINATED FLIGHT. THE FLIGHT DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. RSDR VNAA2016082700034Yaw Damper · faultyUNCOMMANDED RUDDER INPUT AND YAWING IN FLIGHT, YAW DAMPER 2 KICKED OFF IN FLIGHT. THE CREW CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R YAW DAMPER 2 AND PERFORMED CHECKS IAW THE AMM. THE ACFT WAS RELEASED FOR SERVICE.SDR ASAA2016082517806Knob · inoperativeF/O COURSE SELECTOR KNOB INOPERATIVE. ACFT GROUNDED. COULD NOT DUPLICATE PROBLEM. PERFORMED OPS TEST OF MCP IAW AMM 22-11-34/401 ALL TESTS PASSED. PERFORMED LAND VERIFY TEST IAW AMM 22-11-00/201 & HGS SYSTEM TEST IAW AMM 34-36-00. ALL TESTS PASSED ACFT RSDR ASAA2016082217781Unknown · malfunctionedMCP VERT SPEED SELECTOR WHEEL INOPERATIVE. ACFT GROUNDED. UPON ACFT POWER-UP AT REMOTE LOCATION, VERTICAL SPEED SELECTOR KNOB AND DISPLAY OPS NORMAL. FLIGHT DIRECTORS ON, V/S MODE COMMAND BARS ON, PRIMARY FLIGHT DISPLAYS AND CONTROL COLUMN FOLLOW V/S KNOB. SDR ASAA2016081717738Control Panel · failedA/P A WILL NOT ENGAGE. ACFT GROUNDED. DUPLICATED DISCREPANCY. REF FIM TASK 22-11-00-810-801. DIGITAL FLIGHT CONTROL SYSTEM, DFCS, BITE PROCEDURE FOUND FAULTS 22-11625 AND 22-11626. MCP PANEL FAULTS. ABLE TO DUPLICATE DISCREPANCY. REMOVED AND INSTALLED NSDR ASAA2016081617722Warning Light · false activationAFTER PUSH BACK AND MASTER CAUTION RECALL, MASTER CAUTION AND PLT CONTROL LIGHTS ILLUMINATED AS WELL AS MACH TRIM FAIL. MACH TRIM FAIL LIGHT GOES OUT WHEN MASTER CAUTION IS RESET. FD FLAG ON CAPTAIN`S DISPLAY. ACFT GROUNDED. PERFORMED FCC RESET CYCLED CIRCUSDR A6WA201644231Damper · unknownUNCOMMANDED YAW AT FL210, INITIAL ROLL TO THE RIGHT THEN PULSED BACK AND FORTH GENTLY. RAN IAC AND QRH, PROBLEM DISCONTINUED WHEN YAW DAMPER DISCONNECTEDSDR ASAA2016081317710Autoland Sys · malfunctionedHGS AUTOLAND APPROACH WARNING. ACFT GROUNDED. PERFORMED LAND VERIFY BITE NR 49 WITH NO FAULTS.SDR HNAA2016081500248Controller · inoperativeUPON ROTATION YAW DAMPER AP SELECT AND HSI SELECT ON 801 PANEL BECAME INOPERATIVE. R&R AFCS CONTROLLER AS REQUIRED IAW AMM 22-10-01. OPS AND TEST ON GROUND GOOD. OK FOR SERVICE.SDR ASAA2016080917655Autopilot Sys · disconnectedAT ALTITUDE LEVEL FLIGHT, FL 350, STEADY STATE FLIGHT CONDITIONS, AUTOPILOT A DISCONNECTED FOR NO REASON. ACFT GROUNDED. PERFORMED DFCS BITE CURRENT STATUS AND FLIGHT HISTORY FAULT REVIEW, REF FIM 22-11, TASK 801. NO CURRENT FAULTS FOUND. FOUND AUTOPILOT DSDR ASAA2016080917654Autoland Sys · malfunctionedDURING PRACTICE HYBRID APPROACH, TRACKING & ALIGNMENT WAS GOOD UNTIL APPROXIMATELY 10-15 FEET AGL. AT THAT POINT THE ACFT BEGAN DRIFTING TO THE RIGHT OF CENTERLINE. AT TOUCHED DOWN, THE ACFT WAS WELL RIGHT OF THE RUNWAY CENTERLINE & CONTINUED DRIFTING RIGHT. SDR ASAA2016080717640Warning Light · false activationSPEED TRIM FAIL LIGHT ILLUMINATED ON RECALL. ACFT GROUNDED. ACCOMPLISHED DFCS FLT FAULT REVIEW, IAW FIM 22-11 TASK 801, LEG 1 A SIDE LOGGED 22-11700, LEG 1 B SIDE LOGGED 22-11182. ACCOMPLISHED FIM 22-12 TASK 805, PITCH CWS FORCE TRANSDUCER CAPT, AND FIM 22SDR ASAA2016080717638Control Panel · failedMCP ALTITUDE SELECTORS IS NOT WORKING PROPER AND CHANGING ALTITUDE ON ITS OWN. DIFFICULT OR IMPOSSIBLE TO MAKE SELECTIONS. ACFT GROUNDED. ACCOMPLISHED DFCS BITE TEST, NO FAULTS LOGGED. REMOVED & REPLACED DFCS MCP AS A PRECAUTION, IAW AMM 22-11-34/401. ACCOSDR ASAA2016080617611Unknown · malfunctionedACFT AUTO LANDED APPROXIMATELY 20-25' RT OF CENTERLINE. RUNWAY SYMBOLOGY WAS OFFSET IE: POINTING LEFT. ACFT GROUNDED. ACCOMPLISHED HGS FAULT REVIEW REF SMM 34-36-00. CURRENT NO FAULTS FOUND. ACCOMPLISHED FIM 22-11, TASK 825. FOUND FAULTS 22-11199 MACH TRISDR ASAA2016080317601Unknown · unknownA AUTOPILOT DISENGAGED AT FL360 DURING CRUISE. ACFT GROUNDED. ACCOMPLISHED DFCS BITE FLT FAULT, LAST LEG MSG 22-11607 FAULTED 3 TIMES AT FL360, REF B737-800, FIM 22-11-00. ACCOMPLISHED FIM 22-11-803, MCP TESTS. ALL TESTS PASSED. ACCOMPLISHED FCC A OPS LRUSDR ASAA2016080217595Transmitter · failedWHILE PERFORMING LWMP TRAINING, DFCS LIBRARY TEST NR 31 FAILS FOR CHANNEL B SPOILER POSITION SENSOR 9 AND DFCS SENSOR VALUES SHOWS NO INPUT TO FCC-B FROM SPOILER NR 9 POSITION SENSOR. ACFT GROUNDED. REF WDM 22-11-31-4 AT M930 SPOILER 9 POSITION SENSOR, SWAPPSDR ASAA2016073117565Control Panel · failedMCP AUTOPILOT B ENGAGE SWITCH INTERNAL LIGHT PARTIALLY INOPERATIVE. ACFT GROUNDED. REMOVED AND INSTALLED NEW MCP. PERFORMED MCP OPS TEST, IAW AMM 22-11-34/501. SYSTEM CHECKS NORMAL.SDR ASAA2016073117564Autoland Sys · malfunctionedDURING AUTOLAND AND HGS APPROACH SURVEY AIRCRAFT DRIFTED AND TOUCHED DOWN APPROXIMATELY 40 FEET LEFT OF CENTERLINE. CRITICAL AREA WAS CLEAR AND WINDS WERE REPORTED WITHIN LIMITS AND ND WIND DISPLAY SHOWED WINDS IN LIMIT. TOUCH DOWN OCCURRED SMOOTHLY BUT WAS NOSDR ASAA2016072917552Autothrottle Sys · malfunctionedDURING TAKEOFF ROLL, AUTOTHROTTLE DID NOT SET THE CORRECT N1 PRESCRIBED BY THE FMC. FMC PRESCRIBED N1 OF 94.8%,AUTOTHROTTLE ACTUALLY SET 90%. POWER HAD TO BE MANUALLY INCREASED. ACFT GROUNDED. A/T LOGGED T/O SET LOW MSG 22-31678, 22-21677, 22-31676, AND 2SDR ASAA2016072917551Warning Message · false activationHGS APPROACH WAS SUCCESSFUL. AUTOLAND UNSUCCESSFUL. APPROACH WARNING OCCURRED AT JUST UNDER 100' AGL. AIRCRAFT FLEW APPROACH FINE UNTIL APPROXIMATELY 100 FEET. THE TRIM SEQUENCE APPEARED TO BE NORMAL. ACFT GROUNDED. NO FAULTS LOGGED IN DFCS A & B. HGS LOGSDR A6WA201644157Unknown · malfunctionedINTERMITTENT UNCOMMANDED YAW DURING CRUISE AND DECENT. YD2 DISENGAGED PRIOR TO APPROACH RE-ENGAGED ALTHOUGH YAW MOTION CONTINUED.SDR A6WA2016080144144Autopilot Sys · disconnectedAUTOPILOT INTERMITTENTLY DISCONNECTS AFTER BEING ENGAGED.SDR ASAA2016072117458Unknown · unknownMCP LIGHTS INOPERATIVE. ACFT GROUNDED. RESET CIRCUIT BREAKERS, MCP DC 1 & MCP DC-D CHECKED GOOD. PERFORMED FIM 22-11 TASK 803. ALL CHECKED GOOD.SDR FDEA201607202562Control Panel · odorON FLIGHT CONTROL CHECK. PREMATURE REMOVAL, INSTALLATION OFF MPN: 4059032-901, POS: ON SRL: 94110395, TAG NR: 2676C8 ON MPN: 4059032-901, CPN: 2210019, SRL: 99010475, TAG NR: D61528, REASON CODE: PREMATURE REMOVAL, INSTALLATION OFF MPN: 4059001-908, POS: 1, SSDR ASAA2016071917426Autopilot Sys · malfunctionedIN LNAV/VNAV MODE, AUTOPILOT ENGAGED, FAILED TO CAPTURE WAYPOINT ALTITUDE AND AIRSPEED ON ARRIVAL. ON APPROACH, APPROACH MODE WOULD NOT ARM. AUTOPILOT A USED FOR ALL. ACFT GROUNDED. AFTER ARRIVAL FOUND NR 2 NAV HAD VOR FREQ PREVENTING APPROACH MODE. NO FASDR ASAA2016071817416Control Panel · failedMCP PANEL ALTITUDE SELECTION SCREEN 1ST DIGIT UNREADABLE. ACFT GROUNDED. 10,000 FOOT DIGIT BURNED INTO DISPLAY LOOKS LIKE A FAINT NR 3 ALL THE TIME. REPLACED DFCS MODE CONTROL PANEL. INSTALLATION TEST PASSES, IAW AMM 22-11-34-400-801. ACCOMPLISHED LAND VERIFSDR ASAA2016071017328Autopilot Sys · malfunctionedA REQUESTED AUTOLAND WENT AWRY, CAME IN ON G/S BUT TO RIGHT OF COURSE AT 50 FT. RADAR ALTIMETER RECEIVED AN APPROACH WARNING IN THE HUD. DISCONNECTED A/P AND LANDED MANUALLY. ACFT GROUNDED. NO FAULTS LOGGED IN DFCS A & B LAST 10 LEGS. ACCOMPLISHED LAND VERISDR ASAA2016070817304Control Panel · failedBOTH GREEN LIGHTS IN "HDG SEL" BUTTTON ON AFCS MCP INOP. ALL BUTTON FUNCTIONS ARE NORMAL. ACFT GROUNDED. REMOVED AND REPLACED MODE CONTROL PANEL IAW AMM 22-11-34-740-80, OPS NORMAL IAW AMM 22-11-34-740-801. ACCOMPLISHED DFCS MCP LRU INTERFACE TEST, GROUP BITESDR ASAA2016070717303Autopilot Sys · malfunctionedDURING CRUISE, IN SMOOTH AIR AT FL 340. THE "CMD A" AUTOPILOT DISENGAGED. IT WAS IMMEDIATELY RE-ENGAGED AND WORKED NORMALLY UNTIL IT DISENGAGED AGAIN DESCENDING THROUGH FL 300 AT 280 KTS. IT WAS RE-ENGAGED NORMALLY. WE FLEW THE REMAINDER OF THE FLIGHT ON THSDR ASAA2016070317215Control Panel · failedMODE CONTROL PANEL ALTITUDE SEEMS TO BE STUCK AT 50,000 IN ADDITION THE IAS SPEED NOW DOES NOT CONTROL THE MCP COMMANDED SPEED. ACFT GROUNDED. REMOVED AND REPLACED DFCS MODE CONTROL PANEL, IAW AMM 22-11-34. MODE CONTROL PANEL INSTALLATION TEST GOOD. RE-RACK FSDR ASAA2016070117248Circuit Breaker · openON RECALL SPEED TRIM FAIL AND MACH FAIL LIGHTS ILLUMINATED. ACFT GROUNDED. FOUND CIRCUIT BREAKER SYS A FCC DC 1 ON P18-1 OPEN. RESET PER AMM 20-60-01. PERFORMED MACH TRIM AND SPEED TRIM TEST PER AMM 22-11-00. ALL TESTS PASSED A/C OK FOR SERVICE.SDR ASAA2016063017227Circuit Breaker · openCAPTAIN`S DISPLAY FLAGGED, ACFT GROUNDED. FOUND CIRCUIT BREAKER SYS A FCC DC 1 ON P18-1 OPEN. RESET IAW AMM 20-60-01, ACCOMPLISHED DFCS CURRENT STATUS TEST WITH NO DISCREPANCIES NOTED. FLT FAULT REVIEW SHOWED NO FAULTS. GROUND VERIFICATION SATISFACTORY. IAW
Back to JASC 2210