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 ASAA2021083035832Knob · inoperativeMCP ALTITUDE SELECTOR KNOB INOP. GROUNDED - YES. REMOVED AND REPLACED DFCS MODE CONTROL PANEL REF MM 22-11-34/401 OPS CHECK GOOD REF B737-800 MM 22-11-34-740-801. LLM LAND VERIFY COMPLETED REF MM 22-11-00/201. LLM TESTS PASS SEAMC WILL NOTIFIED.SDR ASAA2021082735809Module · faultedAUTOPILOT DISCONNECT WAILER NOISE DOES NOT COME ON WHEN AUTOPILOT IS DISCONNECTED. GROUNDED - YES. PERFORMED B737-800 FIM 22-12 TASK 817 AFTER RESET OF ALERT WARNING MODULE CB SYS OPS CHECK SATISFACTORY SEAMC FELIX NOTIFIED.SDR ASAA2021082735808Control Panel · stuckNOT ABLE TO SET MCP ALTITUDE. ( TRIED A REET BUT STILL NOT WORKING) STUCK AT 37900FT. GROUNDED - YES. PERFORMED A/C POWER DOWN FOR TROUBLESHOOTING REF B737-800 MM 0-60-99. MCP ATTITUDE WAS ABLE TO RESET, AND NO LONGER STUCK @ 37900 FT. PERFORMED DFCS BITE REF SDR ASAA2021082235768Autopilot Sys · disconnectedDURING CRUISE AT FL350. AUTOPILOT B DISENGAGED FOR NO APPARENT REASON. CONDITIONS=SMOOTH WIND 292/16 SAT =42. GROUNDED - YES. REL PER MEL 22-1F B SYSTEM AUTOPILOT INOP. MEL 22-99B CAT 111 AUTOLAND N/A SEAMC NOTIFIED DARREN. DFCS BITE CK SHOWS 22-11607 MCP DATSDR ASAA2021082035754Control Panel · faultedMCP HEADING SELECT WINDOW DIGITS UNREADABLE. GROUNDED - YES. CONFIRMED FAULT, MCP HDG SELECT LCD WINDOW UNREADABLE. REMOVED & REPLACED DFCS MCP REF B737-800 AMM 22-11-34. PERFORMED ALTERNATE DEACTIVATION PROCEDURE REF ASA MAINTENANCE PROGRAM CHAPTER 5, SECTIONSDR ASAA2021081935770Actuator · disengagedAUTOPILOT A DISENGAGED IMMEDIATELY AFTER SELECTION 4 TIMES DURING FLIGHT, AUTOPILOT B OPERATION WAS NORMAL. GROUNDED - YES. (RESOLVED ON W/O: 1882673 TASKCARD: N/R-00001 ) REMOVED AND REPLACED AILERON ACTUATOR FOR CHANNEL "A" AUTOPILOT IAW B737-900 AMM 22-11-2SDR CALA2021081801364Warning Message · intermittentAUTOPILOT A WILL NOT ENGAGE AUTOPILOT B ENGAGES BUT KICKS OFF AF TER STICKERS APPLIED NO GROUND TIME. DEFER REVIEWED FAULT HISTORY AND FOUND "AIL PRESS SW-1" FAULT, PERFORM ED LRU REPLACEMENT TEST "ROLL SENS" TEST, TEST PASSED. REF. FIM TASK 22-13 TASK 804. INSDR ASAA2021081535716Autopilot Sys · faultedWITH AUTOPILOT "B" ENGAGED, DESCENDING VIA THE ANJLL4 ARRIVAL IN "VNAV PATH" ON THE FMA, THE AIRPLANE SPED UP AND FLEW BELOW THE 12000' RETRICTION 3.8 NM BEFORE CIRCUS INTERSECTION. AS IT DID SO, THE AUTOPILOT REVERTED TO CWS. WE IMMEDIATELY STOPPED THE DESCENSDR ENHA202108150071Circuit Breaker · trippedAFTER TAKEOFF, AT APPROXIMATELY 200FT, THE G600 AUTOPILOT ENVELOPE STALL PROTECTION (ESP) SYSTEM ENGAGED AND NOSED THE AIRCRAFT INTO A DESCENT. THE PILOT PUSHED THE AUTOPILOT DISCONNECT SWITCH WHICH BRIEFLY DISCONNECTED THE AUTOPILOT SYSTEM. THE PILOT REPORTEDSDR ASAA2021080335613Autopilot Sys · faultedAUTO PILOT "A" WILL NOT STAY ENGAGED. GROUNDED - YES. ACCOMPLISHED DFCS BITE PROCEDURE REF B737-900 FIM 22-11 TASK 801 FOR CHANNEL A. BITE TESTS PASSED. NO ACTIVE FAULTS IN CURRENT STATUS CHECK. THE 2 FAULTS THAT WERE STORED IN HISTORY ALL PASSED LRU TESTS RELSDR ASAA2021080235607Autoland Sys · malfunctionedAUTOLAND UNSUCCESSFUL. HGS OK. PRIOR TO AND DURING FLARE AIRCRAFT DRIFTED LEFT OF COURSE SIGNIFICANTLY AND AUTOPILOT HAD TO BE DISCONNECTED PRIOR TO TOUCHDOWN. ILS CRITICAL AREA WAS CLEAR. GROUNDED - YES. ACCOMPLISHED DFCS BITE PER B737-800 FIM 22-11 TASK 801 SDR ASAA2021072835553Autoland Sys · faultedUNSUCCESSFUL AUTOLAND. RUNWAY 34L IN SEA. WIND 220/6. FLARE CUE INITIALLY APPEARED THEN DISAPPEARED W/ APPROACH WARNING. AT APPROX 30 FT. CENTERLINE ALIGNMENT WAS GOOD. GROUNDED - YES. ACCOMPLISHED LAND VERIFY TESTS PER B737-900 AMM 22-11-00/201. AND LL LIBRARSDR J7SA2021072800289Autopilot Sys · faultedDIVERTED DUE TO AP FAIL, GSD 2 FAIL, AMS CONTROL FAULT, HSDB FAULT, SWPS ICE SPEED, HSDB FAULT, AND YD FAIL DURING CRUISE AT FL450. CREW LOST ALL TEMPERATURE INDICATIONS (SAT, TAT, OAT), LFT, AND ICING PROTECTION. EMERGENCY DECENT, RAN QRH CHECKLISTS, AND LANDSDR ASAA2021072135465Control Panel · lockedREPEAT WRITE UP. ON DESCENT INTO KSAN, MODE CONTROL PANEL LOCKED UP. STARTED QRH. USE CAPTAINS EMERGENCY AUTH TO DISCONTINUE QRH BELOW 10000 FEET. WEATHER AT DEST, KSAN VFR. CONTROL PANEL INDICATED 50,000 FEET SOME OF WINDOW. COURSE, IAS/ MACH, HEADING WORKED.SDR ASAA2021072035460Control Panel · inoperativeON DESCENT CLEARANCE FROM 270 TO 13000 WHEN WE DIALED 13000 IN THE ALTITUDE WINDOW IT SHOWED 50000 AND WOULD NOT CHANGE UNTIL WE DESELECTED A/P AND CYCLED F/G'S ON AND OFF. GROUNDED - YES. TASK CARD COMPLIED WITH REMOVED AND REPLACED DFCS MODE CONTROL PANEL PESDR ASAA2021071635418Control Panel · inoperativeMCP VERTICAL SPEED WINDOW PIXELS INOP. GROUNDED - YES. REMOVED FLT CREW PLACARD AND VERIFIED DEFECT. REPLACED DFCS CONTROL PANEL REF B737-900 AMM 22-11-34-401. 9 C/B PULLED+ COLLARED AND RESET REF AMM. OPS TEST PASS. VERTICAL SPEED WINDOW RESTORED. THIS TASK CSDR ASAA2021071035337Control Panel · faultedSHORTLY AFTER T/O LOUD CLICKING SOUND COMING FROM MCP PANEL. RAPID CLICKING LASTED APPROX 2MIN. AUTO PILOT B & AUTO THROTTLE ON. ALL OTHER INDICATIONS NORMAL. TURNED OFF AUTO B & AUTO THROTTLE, LATER CLICKING RETURNED BUT MUCH SLOWER, LASTED COUPLE MINUTES. THSDR ASAA2021070235207Control Panel · faultedAUTOPILOT A DISCONNECTED TWO TIME, 30 MINUTES APART. SMOOTH AIR, IN TRIM, RE-ENGAGED OK. SWITCHED TO AUTOPILOT B FOR REMAINDER OF TRIP WITH NO ISSUES. GROUNDED - YES. OPENED & TAGGED 9 C/B, REMOVED & REPLACED MCP, REMOVED TAGS & RESET 9 C/B, PERFORMED LRU REPLSDR CALA2021062800973Actuator · inoperativeA AUTOPILOT INOP...WOULD NOT ENGAGE. B AUTOPILOT INOP AS WELL. B WOULD ENGAGE THEN DISCONNECT ACCOMPLISHED CHECKS OF AUTOPILOT B,PASSES LAND VERIFY MCP TEST 6 HE A AILERON ACTUATOR IS BAD, FAILS AILERON BITE CHK FOR HYDRAUL ICS INPUT. 0.30 TO 60.35 , AUTOPILOSDR ASAA2021062735191Control Unit · faultedCLIMBING THRU FL 300. AUTOPILOT DISENGAGED AND UNABLE TO RE-ENGAGE. AUTOPILOT B ENGAGED OK. LATER IN FLIGHT WAS ABLE TO RE-ENGAGE AUTOPILOT A. GROUNDED - YES. REPLACED THE DFCS MCP PER B737-800 AMM 22-11-34/401. OP CHECKS REQUIRED. OPS CHECK OF MODE CONT PNL GSDR ASAA2021062535180Autopilot Sys · disconnectedAPPROX 45 MINUTES INTO FLIGHT FL370 IN CRUISE, SMOOTH AIR AUTOPILOT A DISCONNECTED AUTOPILOT B ENGAGED NO PROBLEM. AFTER 5 MINUTES RE ENGAGED AUTOPILOT A FOR REMAINDER OF FLIGHT WITH NO FURTHER PROBLEMS. GROUNDED - YES. ACCOMPLISHED REQUIRED TESTS B737-800 AMMSDR ASAA2021062335160Computer · faultedON APPROACH FO'S FLIGHT DIRECTOR DISAPPEARED AND THE AUTOPILOT DISENGAGED AT VOR/LOC CAPTURE WITH APP ARMED. CYCLED FDS BUT UNABLE TO REESTABLISH FO'S FD. GROUNDED - YES. ACCOMPLISHED DFCS LAND VERIFY TEST REF B737-800 AMM 22-11-00, HGS SYSTEM TEST REF HGS 400SDR ASAA2021062335158Autopilot Sys · faultedBOTH A/P'S WOULD NOT ENGAGE. GROUNDED - YES. DIVERSION TIME 27 MINUTES - ADVISED FLIGHT CREW STAB TRIM SWITCH IN CUT-OFF POSITION. ACCOMPLISHED REQUIRED TESTS REF B737-800 AMM 22-11-00 OPS CHECK GOOD CAT IIIA AUTOLAND & HGS QUALIFIED.SDR ASAA2021062035159Sensor · faultedUNABLE TO COMPLETE TC 782223000 FLIGHT MANAGEMENT SYSTEM AND NAVIGATION FUNCTION CHECK, DUE TO FAILURE OF DFCS BITE LIBRARY NUMBER 60.31 AUTO PILOT B AILERON SENSOR 2 FAULT MSG 22-11146 (J18-K13) AND (J1B-H13) AND MSG 22-11340 R AILERON SENSOR EXC INV. GROUNDSDR ASAA2021061935143Control Panel · no testON DESCENT VERTICAL SPEED WAS NOT SELECTABLE WOULD DEFAULT TO CURRENT DESCENT RATE AND WAS NOT CONTROLLABLE. GROUNDED - YES. MCP FAILED V/S LIBRARY TEST. REMOVED AND REPLACED MCP REF B737-800 AMM 22-11-34. OPS CHECK GOOD.SDR ASAA2021061935118Knob · intermittentF/O DCP ALTIMETER ADJUSTMENT KNOB INTERMITTENTLY ADJUST MORE THAN COMMANDED. GROUNDED - YES. PERFORMED DCP ALTIMETER ADJUSTMENT KNOB TEST PER B737-800 AMM 22-11-34. COULD NOT DUPLICATE FAULT. OPS CHECK OK.SDR DALA2021061503256Yaw Damper · faultedSHIP 3276 AUTO FLIGHT YAW DAMPER SYSTEM FAULT. CORRECTIVE ACTION: RESET YAW DAMPER THRU FAC'S NO FAULT AT THIS TIME NO 60 DAY HISTORY PER A320 AMM 22-91 A/C OK FOR SVC. (7827042)SDR AALA202106079006Control Unit · defectiveAIRCRAFT WAS GROUNDED: ON APPROACH INTO ORD THE FLIGHT CREW REPORTED A LOSS OF AIRSPEED INDICATION DUE TO THE SPEED BUG INTERMITTENTLY FROZEN ON FLIGHT CONTROL UNIT. UNABLE TO CONTROL WITH AUTOTHRUST ENGAGED. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED SSDR AALA202106029014Autopilot Sys · malfunctionedAIRCRAFT WAS NOT GROUNDED: AT FLIGHT LEVEL 390 WITH FLIGHT LEVEL 210 SET IN ALTITUDE WINDOW, MANAGED DESCENT SELECTED. AIRCRAFT INITIATED CLIMB. VERTICAL SPEED SELECTED TO REGAIN DESCENT. AIRCRAFT REACHED FL 394 . NO OTHER ISSUES IN DESCENT. MAINTENANCE ACCOMPSDR SWAA2021060178405Computer · inoperativeDURING INITIAL CLIMB OUT; ELECTRIC TRIM BECAME INOP; BOTH SIDES. MANUAL TRIM NORMAL. ; / REMOVED AND REPLACED FCC B AND STAB TRIM RELAY; AMM 22-11-33 AND SWPM 20-81.SDR ASAA2021052234866Autoland Sys · malfunctionedCAT 3 AUTOLAND/HGS 16R WIND 230/6. AIRCRAFT FLARED @ APPROZ 30' BUT DIDNT SETTLE TO RWY. A/C REMAINED AT 20-30'. CLICKED OFF A/P AND LANDED MANUALLY. GROUNDED - YES. UNABLE TO DUPLICATE DEFECT OR PREVIOUS FINDINGS. DFCS FAULT REVIEW SHOWED NO RELEVANT FAULTS. SDR SIMA20210522003Autothrottle Sys · failedABORTED TAKEOFF 90KTS- ON TAKE OFF ROLL WITH AUTO THROTTLE ENGAGED AND THRUST ALREADY SET GOT AT FAIL AND AT FAULT REJECTED T/O PRIOR TO 80 KTS BUT A/C DID GET TO 90KTS BEFORE DECELLERATING ACFT RTG AND SWAP.-C/A-PERFOMED AUTO THROTTLE FUNCTION TEST IAW AMM TASDR ASAA2021051834856Autoland Sys · malfunctionedHGS/ AUTOLAND UNSUCCESSFUL AUTOLAND DID NOT FLARE PROPERLY. FINISHED MANUALLY. GROUNDED - YES. DFCS HAVE NO FAULTS LOGGED FOR LAST FLIGHT LEG. ACCOMPLISHED LAND VERIFY TEST PER B737-800 AMM TASK 22-00-01-730-807, AUTOLAND SYS GND CHECKED SATISFACTORY. ACCOMPLISDR ASAA2021051734844Computer · failedON CLM FO SIDE FD FLAG ILLUMINATED, ON RECALL - MACH TRIM FAIL & SPEED TRIM FAIL ILLUMINATE. GROUNDED - YES. CONFIRMED FCC B FAILED - UNABLE TO ACCESS BITE. R&RD SAME PER B737-900 AMM 22-11-33. ACCOMP LRU REPLACEMENT TEST AND SOFTWARE P/N VERIFICATION, BOTH CKSDR ASAA2021051534843Position Sensor · failedAUTOPILOT A WILL NOT REMAIN ENGAGED. GROUNDED - YES. REMOVED AND REPLACED AILERON POSITION SENSOR IAW B737-900 AMM 22-11-29-000-801 AND AMM 22-11-29-400-801 AND ADJUSTED IAW AMM 22-11-29-820-800, OPS CHECK GOOD. THE LMM TESTS AND LLM STATUS OF AIRCRAFT AND THESDR ASAA2021051434810Actuator · out of rigINFO ONLY AUTOLAND NOT SUCCESSFUL. GROUNDED - YES. ACCOMP LAND VERIFY TEST REF B737-800 AMM 22-11-00/201. TEST FAILED FOR AIL POS SEN-2 AND AIL POS SEN-1. REMOVED AND REPLACED AIL POS SEN REF AMM 22-11-29-400-801. NO HELP. REPLACED THE AILERON POSITION SENSOR SDR FDEA202105141220Control Panel · failedON CLIMB OUT THE MCP ALT WINDOW FROZE AT 5000. TRIED SPINNING THE KNOB PUSHING THE KNOB WITH NO RESULT. DISCONNECTED THE A/P MANUALLY FLEW THE AIRPLANE TO FL230. SHORTLY AFTER LEVEL OFF THE ALT WINDOW BEGAN WORKING. THIS ALT WINDOW SITUATION IS A SAFESDR ASAA2021051334814Autoland Sys · faultedAUTOLAND WITH HGS MONITOR- UNSUCCESSFUL, ACFT EXCEEDED 35 FEET LEFT OF RUNWAY BEFORE TOUCHING DOWN AROUND 35 FEET LEFT OF RUNWAY, NO APPROACH WARN LIGHT ILLUMINATED. GROUNDED - YES. PERFORMED LAND VERIFY TEST REF B737-900 AMM 22-11-00-700-801. VERIFIED REPAIR SDR ASAA2021051234801Autoland Sys · faultedAUTOLAND UNSUCCESSFUL, APPROACH WARN ON FLARE FOR NO APPARENT REASON, ALL WITHIN PARAMETER. GROUNDED - YES. ACCOMPLISHED B737-800 FIM 34-36 TASK 807. NO EXISTING FAULT, LEG 1 HAS FAULT MSG VERTICAL GUIDANCE COMP, NO CAT AIII, PERFORMED HGS-4000 SYSTEM TEST & 7SDR ASAA2021050234715Warning Message · false activationWHEN POWER APPLIED TO ACFT, A MODE CONTROL PANEL LOCKED UP INDICATION DISPLAYED. GROUNDED - YES. PERFORMED MODE CONTROL PANEL TEST IAW FIM 22-11 TASK 803 MCP AUTOTEST PASS, ALL INTERACTIVE TESTS PASSED . NO FURTHER DEFECTS NOTED.SDR ASAA2021042734685Control Panel · malfunctionedDFCS MODE CONTROL PANEL COURSE AND HEADING WINDOWS DON'T DIM OR BRIGHTEN WHEN ADJUSTED. GROUNDED - YES. REPLACED DFCS MODE CONTROL PANEL ALL INSTALLATION TESTS PASS REF B737-800 AMM 22-11-34-400-801. GROUND VERIFICATION SUCCESSFUL.SDR ASAA2021042134630Actuator · faultyAUTOPILOT A IS INOP TRIED TO ENGAGE SEVERAL TIMES AND IT KICKS OFF. GROUNDED - YES. REMOVED AND REPLACED AUTOPILOT AILERON ACTUATOR A PER B737-900 AMM 22-11-25-000-801 / AMM 22-11-25-400-801. ACCOMPLISHED AUTOPILOT AILERON ACTUATOR ADJUSTMENT PER AMM 22-11-25SDR ASAA2021042134628Actuator · faultedDURING ELEV FEEL COMP TEST - FAILED ELEV DUAL AUTHORITY TEST 51.27 - B CHANNEL OUT OF LIMITS. GROUNDED - YES. DID TEST OF "B" ELEV A/P ACT REF B737-800 AMM 22-11-26-820-801. A AND B WITHIN LIMITS AT 2.01. THEN RAN DUAL AUTHORITY TEST REF AMM 22-11-00-820-816 -SDR ASAA2021042034627Autoland Sys · malfunctionedAUTOLAND NOT SUCCESSFUL AIRCRAFT DID NOT FLARE. REQUIRED CORRECTIVE ACTION. GROUNDED - YES. UPON BITE DFCS SHOWS NO ACTIVE FAULTS WITH NO HISTORY. HGS BITE REF SMM 34-36-00 NO ACTIVE FAULTS AND SHOWS FAULTS "ROLLOUT GUIDANCE AND ILS ANOMALY" IN HISTORY WITH ONSDR ASAA2021042034624Indicator · inoperativeN1 LIGHT ON MCP DOES NOT ILLUMINATE WHEN TESTED. GROUNDED - YES. REMOVED AND REPLACED DFCS MODE CONTROL PANEL IAW B737-800 AMM 22-11-34-000-801 AND AMM 22-11-34-400-801, MODE CONTROL PANEL INSTALLATION TEST PASSES IAW AMM 22-11-34-740-801. LLM MAINTENANCE TESTSDR 2021F00048Transmitter · damagedDURING TAXIING THE STABILIZER TRIM WITHOUT MOVEMENT. AIRCRAFT RETURNED TO PLATFORM DUE TO TAXYING THE HORIZONTAL STABILIZER TRIM WITHOUT MOVEMENT. MAINTENANCE PERSONNEL PERFORMED REVISION, DETECTING BITE TO PSEU IAW FIM 22-11 TASK 801 PROCEDURE, SHOWING FAILSDR DALA2021041902285Computer · malfunctionedSHIP 184 -ATB - UNABLE TO ENGAGE ANY AUTOPILOT AFTER TAKEOFF. CORRECTIVE ACTION: TROUBLESHOT PER FIM. REPLACED CENTER FLIGHT CONTROL COMPUTER (FCC) AND THE TOTAL AIR TEMP (TAT) PROBE. AFDS TESTS PASSED.SDR 2021FA0000192Servo · failedGARMIN GSA28 PITCH TRIM SERVO FAILED AFTER APPROXIMATELY ELEVEN MONTHS / 45 HOURS IN SERVICE. FLIGHT INSTRUMENTATION DISPLAYED “AFCS PREFLIGHT TEST FAILED” AND “SERVO HARDWARE FAULT” MESSAGES AND THE AUTOPILOT BECAME INOPERATIVE. THE SERVO DISPLAYED A “RED” STSDR ASAA2021041534593Computer · intermittentA/P "A" WOULD NOT STAY ENGAGED. GROUNDED - YES. TASK CARD COMPLIED WITH PERFORMED DFCS BITE TEST REF B737-900 FIM 22-11 TASK 801. FOUND NO FAULT MESSAGES AT THIS TIME. PERFORMED DFCS BITE TEST QUICK TEST (GROUP 10) AND AUTO PILOT (GROUP 11). ALL SYSTEM TEST PASDR ASAA2021041434582Selector Knob · out of toleranceHEADING SELECT KNOB AND HEADING BUG ARE INTERMITTENTLY OUT OF SYNC WHEN ATTEMPTING TO SELECT A HEADING. GROUNDED - YES. VERIFIED SELECTED HDG WILL INTERMITTENTLY PAUSE & THEN JUMP A COUPLE DEGREES AS HDG IS ADJUSTED. SAME RESPONSE WITH EITHER FCC A OR B AS MAS
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