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 ASAA2017020619717Control Panel · faultyALTITUDE WINDOW DISPLAY HAS SEVERAL ANOMALIES. IT APPEARS THE IS A "MINUS" SIGN IN FRONT OF THE ALTITUDE. GROUNDED - YES. CONFIRMED ALTITUDE WINDOW DISPLAY IS DISPLAYING INCORRECT. REPLACED MCP AND RESET 9 C/B'S. OPS TEST NML. REF B737-900 AMM 22-11-34. ALL TESDR DALA2017020801052Autopilot Sys · malfunctionedUNCOMMANDED DESCENT WITH NR 1 AUTOPILOT WHEN SLOWING AIRCRAFT IN VNAV ALT HOLD.SDR ASAA2017020419659Control Panel · failedMCP ALTITUDE SELECTOR READOUT HAS DIGITAL NUMERIC BLEED THROUGH. ACFT GROUNDED. REMOVED AND REPLACED DFCS MODE CONTROL PANEL IAW AMM 22-11-34. ALT DEACT REVERSED. TESTS GOOD. PERFORMED DFCS LRU REPLACEMENT TEST FOR MCP TEST GROUP 32 IAW AMM 22-11-34, LAND VSDR ASAA2017020419658Warning Light · false activationF/O FD AMBER LIGHT ON. ACFT GROUNDED. DFCS BITE HAD NO CHANNEL B. CYCLED PWR ON FCC B COMPUTER, NO HISTORY. ACCOMPLISHED THE FOLLOWING TESTS: BITE 35 IAW AMM 22-11-33/401 FOR DFCS LRU INTERFACE TEST FOR FCC, BITE 49 IAW AMM 22-11-00/201 LAND VERIFY AND HGS SSDR HNAA2017020300036Circuit Card · failedAUTOPILOT DISENGAGE CAUTION LIGHT WILL NOT RESET AFTER DC BUSS FAULT DURING ENGINE START. R & R THE AUTOPILOT DISENGAGE PANEL CIRCUIT CARD ASSEMBLY ON PILOT SIDE. OPS CHECKED GOOD IAW MM 22-10-01 AND WDM 22-10-10.SDR ASAA2017012519546Autoland Sys · malfunctionedAUTOLAND FAILED. TOUCHDOWN WELL LEFT OF CENTERLINE. CALM WINDS: (AUTO SPEED BRAKE ALSO DID NOT DEPLOY) HGS ACCEPTABLE FOR USE. ACFT GROUNDED. IAW FIM TASK 22-11 TASK 825, AUTOLAND BITE GROUP 49 GOOD. NO FAULTS IN FAULT HISTORY A & B. ACCOMPLISHED LAND VERIFSDR ASAA2017012419537Autoland Sys · malfunctionedUNSUCCESSFUL AUTOLAND. ACFT BANKED LEFT LAST 100 FEET TOUCHING DOWN CLOSER TO LEFT EDGE LIGHTS THAN CENTERLINE. ACFT GROUNDED. ACCOMPLISHED DFCS FLT FAULT REVIEW, NO FAULT NOTED FOR PREVIOUS LEG BOTH CHANNELS. ACCOMPLISHED LAND VERIFY TEST 49 IAW AMM 22-00-SDR O2GA2017012785501Actuator · malfunctionedAUTOPILOT MISTRIM (E) ILLUMINATED AT FL310 AFTER START OF DESCENT. MANUAL PITCH TRIM WAS FROZEN. BEGAN WORKING AFTER DESCENDING INTO WARMER ALTITUDE FL120. MAINTENANCE REPLACED THE LEFT AND RIGHT PITCH TRIM ACTUATORS. REMOVED ACTUATORS SENT FOR EVALUATION. ASDR UIEA2017012100095Autopilot Sys · malfunctionedWITH RT AUTOPILOT ON, DESCENDING FROM 360 TO 280 IN VNAV. AUTOPILOT DID NOT WORK PROPERLY AND STOP (1) RATE OF CLIMB (2) CAPTURE ALT OF 280. AUTOPILOT DID FLY THROUGH 280 TO APROX. FL279-2788, BEFORE DISCONNECTION OF AP TO STOP DESCENT AND LEVEL OFF AND RETURNSDR ASAA2017011519360Circuit Breaker · trippedAUTO PILOT B INOPERATIVE, WOULD NOT ENGAGE. CIRCUIT BREAKER P6-2 B4 TRIPPED. ACFT GROUNDED. DIGITAL FLIGHT CONTROL SYSTEM (DFCS) BITE PROCEDURE IAW AMM 22-11-00. NO AUTO PILOT DISCONNECT FAULTS FOUND. DUE TO AFCS SYSTEM B ENGAGE INTERLOCK CIRCUIT BREAKER FOSDR ASAA2017011519359Unknown · malfunctionedV NAV INOP AFTER TAKEOFF. GROUNDED - YES. UNABLE TO DUPLICATE PROBLEM. PERFORMED DFCS OPS TEST PER AMM 22-11-00 AND MCP TEST PER AMM 22-11-34, OPS NORMAL. NO HISTORY LAST 30 DAYS. ALSO INBOUND FLT CREW VERBALIZED THAT VNAV OPERATED NORMALLY. CLEARS MEL 22-15Y.SDR CALA2017011300074Computer · faultyAUTOPILOT DOES NOT KEEP THE SAME ALTITUDE WITH ALT HLD PITCH MODE SET CMD A. ENGAGED ON A AUTOPILOT-AIRCRAFT OSCILLATES - + 50 FEET UP TO 400 FT/MIN WHEN ENGUAGED IT PUSHED. REPLACED FLIGHT CONTROL COMPUTER IAW MM 22-11-33. OPS CHECKED GOOD.SDR ASAA2017010919287Relay · failedAUTOPILOT NR 1 & 2 WOULD NOT ENGAGE. ACFT GROUNDED. PERFORMED DFCS BITE, IAW FIM 22-11 TASK 801, FOUND MAINTENANCE MESSAGE 22-11176. STAB TRIM RELAY ISSUE. REPLACED THE STAB TRIM RELAY R64, IAW FIM 22-13 TASK 818. ALL TESTED GOOD.SDR ASAA2017010819272Computer · malfunctionedFCC-B FAILS BITE TEST NR 31. ACFT GROUNDED. ACCOMPLISHED FCC B LRU INTERFACE TEST IAW AMM 22-11-33/401, AND A DFCS LAND VERIFY TEST IAW AMM 22-11-00/201. BOTH TESTS PASSED. COMPLETED LIBRARY TEST 31 AILERON IA EXTENDED MAINTENANCE IAW BITE GROUP 60 IAW AMM 2SDR FDEA201612304580Module · inoperativeDURING DECENT, AUTOPILOT FAILED TO CAPTURE ALTITUDE (5000'). ALT WARNING WORKED. R&R THE STAB TRIM ASSY MODULE, PASSES MCDP TEST 65 AS WELL AS MCDP GROUND TEST 30 AND AUTOLAND TEST 40. RESET 30 DAY TIMER, OK FOR SERVICE. IAW AMM 27-09-00-2, 22-00-00-2.SDR ASAA2016122919198Control Panel · intermittentF/O'S COURSE SELECTOR INTERMITTENTLY WILL NOT SELECT 163 DEGREES. GROUNDED - YES. CONFIRMED. REMOVED & REPLACED DFCS MODE CONTROL PANEL, REF AMM 22-11-34. OPS NORMAL PER SAME. DFCS LRU INTERFACE TEST BITE NR 32 AND LAND VERIFY NR 49 GOOD, REF AMM 22-11-00. HGSSDR A6WA2016122844702Autopilot Sys · inoperativeAIRCRAFT EXPERIENCED SUBSTANTIAL UNCOMMANDED YAW AT 10,000 FEET IN SMOOTH AIR. AUTOPILOT DID NOT DISENGAGE AFTER 2 EPISODES. C/W QRH, DISCONNECTED AND AUTOPILOT AND YD NO FURTHER UNCOMMANDED YAW.SDR ASAA2016122419135Autoland Sys · malfunctionedON A PRACTICE CAT IIIA AUTOLAND APPROACH, AT APPROX 1,000 AGL, AUTOPILOT A DISENGAGED WITH NO APPARENT CAUSE. ALL PROCEDURES PERFORMED WERE STANDARD IAW A CAT III AUTOLAND APPROACH. ONCE NOTED WE PERFORMED A NORMAL MANUAL AAPROACH AND LANDING. ACFT GROUNDED. SDR ASAA2016122219134Switch · failedAUTOPILOT B WILL NOT ENGAGE. ACFT GROUNDED. FOUND CAPTAIN`S A/P DISCONNECT SWITCH INOPERATIVE. REPLACED CAPTAIN`S A/P DISCONNECT SWITCH. INSTALLATION TEST PASSED FOR BOTH SIDES IAW AMM 22-11-41/401. FCC B REMOVED AND RE-INSTALLED FOR TROUBLESHOOTING, INSTALSDR ASAA2016121919099Control Panel · failedVERTICAL DISPLAY ON MCP LIT SEGMENT IS BAD. GROUNDED - YES. REMOVED AND REPLACED MCP, REF AMM 22-11-34, OPS CHECK NORMAL .ACCOMPLISHED MCP LWMP CHECKS, REF LWMP CHECKLIST AMM 22-00-01, ALL TEST PASSED. A/C REMAINS CAT IIIA AUTOLAND & HGS, VERIFIED STATUS SCREWSDR ASAA2016121919098Autoland Sys · malfunctionedAUTOLAND FAILED: A/C DRIFTED 35 FEET LEFT OF CENTERLINE AND THE LEFT WING ROLLED DOWN 3 DEGREES AT ABOUT 50 FEET. WINDS AT 1500 AGL 190 AT 30 KTS, AIRPORT WINDS 030 AT 3 KTS 200 DEGREE WIND SHIFT IN 1500 FEET BUT WITHIN PUBLISHED WIND LIMITS. GROUNDED - YES. PSDR ASAA2016120818981Autopilot Sys · malfunctionedAUTOPILOT B DISENGAGED AT FL 360 TWO TIMES. AUTOPILOT A, WORKED FINE. ACFT GROUNDED. PERFORMED CURRENT STATUS CHECK, NO FAULTS. PERFORMED LAND VERIFY BITE GROUP 49, ALL TESTS PASSED. ACFT REMAINS CAT IIIA AUTOLAND & HGS.SDR E3MA201612070001Autopilot Sys · bindingAUTOPILOT FAILED PREFLIGHT TEST, AUTOPILOT ME LED. DURING TROUBLESHOOTING OF AUTOPILOT SYSTEM BY MAINTENANCE THE AIRCRAFT EXPERIENCED UNUSUAL VIBRATIONS/OSCILLATIONS IN THE HOVER CHECK. FOUND FAULTY ELECTRO HYDRAULIC ACTUATORSDR ASAA2016113018891Control Panel · failedNR 1 AUTOPILOT DROPPED OFF & REENGAGED IT. ACFT GROUNDED. REMOVED AND REPLACED THE DFCS MODE CONTROL PANEL IAW AMM 22-11-000-801 AND 22-11-34-400-801. MODE CONTROL PANEL INSTALLATION TEST PASSED IAW AMM 22-11-34-740-801.SDR ASAA2016112818873Autoland Sys · malfunctionedAUTOLAND UNSUCCESSFUL. (HGS MONITOR FUNCTIONED PROPERLY. AIRCRAFT LINED UP APPROXIMATELY 20 FT RIGHT OF CENTERLINE, BEGAN CORRECTING ABOUT 100 FT ABOVE FIELD ELEVATION. TOUCHED DOWN AT LEAST 35 FEET LEFT OF CENTERLINE AND REQUIRED PILOT INPUT. ILS CRITICAL ZOSDR ASAA2016112818872Module · failedSTAB OUT OF TRIM LIGHT CAME ON AT FL320. RAN QRC/QRH. AUTOPILOT NOT TRIMMING. ELECTRIC TRIM WORKED NORMALLY. ACFT GROUNDED. VERBAL FROM CREW AUTOPILOT B IN CMD, DFCS FFR SHOWS NO PREVIOUS FLIGHT FAULT FOR CH "A", CH "B" SHOWS MESSAGE 22-11830 FOR PREVIOUS FLIGSDR ASAA2016112418803Control Panel · failedVERTICAL SPEED DISPLAY HAS ILLUMINATION THAT SHOULD NOT BE THERE. ACFT GROUNDED. REMOVED AND REPLACED MODE CONTROL PANEL IAW AMM 22-11-34. INSTALLATION TEST PASSED IAW AMM 22-11-34-740-801. ACCOMPLISHED DFCS MCP LRU INTERFACE TEST GRP BITE 32 AND LAND VERIFY TSDR ASAA2016112018764Control Panel · failedMODE CONTROL PANEL FAILED DFCS TEST 60.62. ACFT GROUNDED. REPLACED DFCS MCP AND TESTED, IAW AMM 22-11-34/401, DFCS BITE GROUP 32 AND LAND VERIFY 49 AND HGS SENSOR TEST FOR FCC/AT, IAW SMM 34-36-00. ALL OPS NORMAL.SDR 2016FA0000569Control Panel · malfunctionedPILOT COULD NOT SELECT AN ALTITUDE ON THE AUTO-PILOT ALTITUDE PRESELECT FUNCTION. THE CONTROLLER KEPT CHANGING ALTITUDES INSTEAD OF THOSE SELECTED. TWO MORE FLIGHT GUIDANCE PANELS FAILED.SDR 2016F00239Autopilot Sys · disconnectedAT CRUISE AUTOPILOT DISCONNECTED AND AIRCRAFT TRIED TO PITCH UP.SDR ASAA2016111218618Warning Flag · activatedDURING PREFLIGHT FO'S FD FLAG APPEARED ON PFD. ACFT GROUNDED. FD FLAG NOT PRESENT, MESSAGE 22-11317, WITH NO OTHER REOCCURRENCE IN ALL OF DFCS FLT HISTORY. ACCOMPLISHED DFCS LRU INTERFACE TEST FOR FCC BG 35, TEST PASSED.SDR ASAA2016111118617Autopilot Sys · malfunctionedDESCENDING THROUGH FL245, AUTOPILOT DISENGAGED. A/C REMAINED LNAV/VNAV PATH AND I WAS ABLE TO RE-ENGAGE SUCCESSFULLY. GROUNDED - YES. BITE CHK DFCS, NO CURRENT FAULTS, OPS NORMAL, IAW FIM 22-11 TSK 801. PERFORMED B737-800 FIM 22-11 TASK 801 CURRENT STATUS TESTSDR FDEA201611113979Control Unit · malfunctionedDURING CLIMBOUT AND TWICE DURING CRUISE, AIRCRAFT YAWED ABRUBTLY AND UNCOMMANDED. ALL FLT CONTROL PARAMETERS CHECKED NORMAL. SET FAULTS FCC NR 1 WITH TRANS FLAG.AND FMC 1 & 2 WITH NCD. R & R NR 1 FAC AS A PRECAUTION IAW MM 22-18-34-04 AND PERFORMED AFS/LSDR ASAA2016110918616Display · defectiveCAPTAIN`S MCP CRS SELECTOR WINDOW HAS DAMAGED SEGMENTS. ACFT GROUNDED. REMOVED & REPLACED THE MODE CONTROL PANEL IAW AMM 22-11-34, INSTALLATION TEST PASSED. ACCOMPLISHED DFCS LRU INTERFACE TEST FOR MCP 32, LAND VERIFY TEST 49 & HGS SENSOR TEST FOR FCC/AT IAWSDR ASAA2016102818500Warning Flag · false activationAMBER FD FLAG DISPLAYED ON FIRST OFFICER'S ATTITUDE INDICATOR. ACFT GROUNDED. CYCLED "B FCC DC" CIRCUIT BREAKER, FCC B RECOVERED. PERFORMED DFCS LRU INTERFACE TEST FOR FCC, LAND VERIFY TEST, AND HGS SENSOR TEST FOR FCC/AT, IAW AMM 22-00-01, LWMP CHECKLIST. ASDR ASAA2016102718499Warning Flag · false activationDURING PRE-FLIGHT "FD" FLAG ON CAPTAIN`S PFD. ACFT GROUNDED. HAD TO CYCLE FCC A DC CIRCUIT BREAKER BEFORE DFCS WILL GO INTO BITE. CURRENT STATUS PASSED. ACCOMPLISHED DFCS LRU INTERFACE TEST ONLY FOR FCC A, TEST PASSED, IAW AMM 22-11-33.SDR ASAA2016102118436Display · malfunctionedFD FLAG ON COPILOT PFD ON PREFLIGHT NOT ABLE TO GET FD WHEN TURNING IT ON. GROUNDED - YES. CYCLED GND POWER TO A/C, FD FLAG NO LONGER SHOWS AND FD TURNS ON NORMALLY REF B737-800 FIM 22-11 TASK 801, DFCS BITE SHOWS NO CURRENT FAULTS.SDR ASAA2016102018435Control Panel · malfunctionedAUTOPILOT LIGHTED DIGITS FOR CRS SPD HDG ALT DO NOT DIM ALL OTHER A/P LIGHTS OPERATE NORMALLY. ACFT GROUNDED. REPLACED DFCS MODE CONTROL PANEL, IAW AMM 22-11-34. INSTALLATION TESTED NORMAL.SDR ASAA2016102018434Warning Flag · false activationCAPTAIN`S FLIGHT DISPLAY FLAG SHOWED AT POWER TRANSFER. ACFT GROUNDED. VERIFIED, DFCS SHOWS CHA UNAVAILABLE, CYCLED FCC DC C/B P18-1 PANEL. FCC A CH RESTORED, F/D FLAG DISAPPEARED. ACCOMPLISHED LRU REPLACEMENT TEST FOR FCC A IAW AMM 22-11-33 TEST PASSED.SDR ASAA2016101918415Control Panel · malfunctionedDURING SHUTDOWN, MCP WENT DARK. ACFT GROUNDED. CYCLED MCP-1AND 2 CIRCUIT BREAKER AND MCP DISPLAY CAME BACK TO LIFE. ACCOMPLISHED MCP REPLACEMENT TEST IAW AMM 22-11-34 AND MCP TEST OPS CHECKED GOOD. DFCS LRU INTERFACE TEST GROUP 32 OPS CK GOOD IAW AMM 22-11SDR ASAA2016101518337Control Panel · failedA AUTOPILOT DISCONNECTED TWICE FL 350 ON ITS OWN. ACFT GROUNDED. REMOVED & REPLACED DFCS MCP IAW AMM 22-11-34, OPS NORMAL. GROUND VERIFICATION SUCCESSFUL.SDR ASAA2016101318336Autoland Sys · malfunctionedUNSUCCESFUL AUTOLAND. JUST PRIOR TO FLARE, RECEIVED A APPROACH WARNING WITH ROLLOUT CAUTION. TOWER CONFIRMED THE APPROACH AREA WAS PROTECTED. ACFT GROUNDED. PERFORMED LANDING DFCS BITE GROUP 20 FAULT REVIEW IAW FIM 22-11 TASK 801, NO FAULTS AND NO CURRENT FASDR ASAA2016101018254Control Panel · failedHEADING SELECT KNOB ON MCP IS BROKEN. ACFT GROUNDED. REPLACED MCP IAW AMM 22-11-34. ACCOMPLISHED LWMP TESTS, DFCS LRU INTERFACE TEST FOR MCP, LAND VERIFY TEST AND HGS SENSOR TEST FOR FCC/AT. ALL TESTED GOOD IAW AMM 22-11-34, AMM 22-11-00, AND SMM 34-36-00.SDR 2016FA0000497Circuit Breaker · trippedAUTOPILOT FAIL BLUE CAS ACCOMPANIED BY PITCH TRIM CIRCUIT BREAKER OPENED. ONE RESET, OPENED AGAIN, RAN QRH FOR AUTOPILOT FAIL BLUE CAS AND ONE A1 CIRCUIT BREAKER RESET ON GROUND OPENED AGAIN.SDR ASAA2016100518221Control Panel · faultedLARGE DOT IN MCP VERTICAL SPEED WINDOW. ACFT GROUNDED. VERIFIED, REMOVED & REPLACED MODE CONTROL PANEL IAW AMM 22-11-34, INSTALLATION TEST PASSED. ACCOMPLISHED DFCS LRU INTERFACE FOR MCP NR 32, LAND VERIFY TEST NR 49, & HGS SENSOR TEST FOR FCC/AT IAW AMM 22-SDR ASAA2016100218185Computer · failedCAPT FD WARNING SYMBOL. FD COMMAND BAR AND LIGHT ON MCP ALSO NOT WORKING. GROUNDED - YES. FCC A WOULD NOT GO INTO BITE. REMOVED AND REPLACED FCC A IAW B737-800 AMM 22-11-33. OPS CHECKED NORMAL. ACCOMPLISHED LRU REPLACEMENT TEST DFCS/FCC/AT, REF B737-800 AMM 22SDR ASAA2016100218184Circuit Breaker · trippedAFCS SYS A WARN LIGHT (BAT) BREAKER POPPED. ACFT GROUNDED. INSPECTED AND RESET C/B AFCS SYS A WARN LT (BAT), IAW AMM 20-60-01. OPS CHECKED AFCS ANNUNCIATOR, IAW AMM 22-11-32. OPS CHECKED NORMAL.SDR MFGA201609280001Unknown · malfunctionedCREW REPORTED THAT WITH THE AUTOPILOT ENGAGED THEY EXPERIENCED AN OUT OF TRIM CONDITION. ATTEMPTS MADE TO TRIM THE ACFT BACK TO NEUTRAL WERE UNSUCCESSFUL. CREW DECLARED AN EMERGENCY AND PERFORMED A FLAPS 10 DEGREE LANDING.SDR MFGA2016F00194Autopilot Sys · out of trimCREW REPORTED THAT WITH THE AUTOPILOT ENGAGED THEY EXPERIENCED AN OUT OF TRIM CONDITION. ATTEMPTS MADE TO TRIM THE ACFT BACK TO NEUTRAL WERE UNSUCCESSFUL. CREW DECLARED AN EMERGENCY AND PERFORMED A FLAPS 10 DEGREE LANDING.SDR ASAA2016092218109Control Panel · malfunctionedMCP MODE SELECTOR SWITCH LIGHTS ILLUMINATION WHEN SELECTED VERY DIM. ACFT GROUNDED. REMOVED & REPLACED MCP PANEL, REF B737-800 AMM 22-11-34. INSTALLATION TEST PASSED. ACCOMPLISHED ADDITIONAL TESTING, DFCS LRU INTERFACE TEST FOR MCP NR 32, 49 LAND VERIFY TEST,
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