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 ASAA2018073125587Circuit Breaker · trippedON MASTER CAUTION RECALL GOT MACH TRIM FAIL LT. GROUNDED - YES. RESET FCC A C/B. ACCOMPLISHED MACH TRIM ACT TEST REF AMM 22-11-24-740/801, PASSED.SDR ASAA2018080125573Unknown · malfunctionedAUTOLAND UNSATISFACTORY. AT APPROX 70 FEET AGL, AUTOPILOT COMMENCED A LEFT BANK, FOLLOWED QUICKLY BY AN APPCH WARNING. GROUNDED - YES. ACCOMPLISHED LLM MAINTENANCE PRACTICES FOR LLM SPECIAL CONDITION. INBOUND CONDITION RELATED TO AUTOLAND PER AMM 22-00-01-730-SDR ASAA2018073125586Sensor · out of adjustSTAB TRIM MOTOR FAILED TEST PER AMM 22-11-81-710-801, AMM 27-41-00-700-801, ACCOMPLISHED STAB ELEC TRIM SYSTEM TEST REF AMM 27-41-00-700-803, TEST NORMAL, COULD NOT DUPLICATE FAILED TEST. UNABLE TO PERFORM LAND VERIFY DUE TO FCC-A FAILURE. SUSPECT STAB POS SENSDR ASAA2018073025574Unknown · malfunctionedPER RELEASE, AUTOLAND REQUESTED. AUTOLAND CONSIDERED UNSUCCESSFUL DUE TO LANDING 50 FEET RIGHT OF CENTERLINE. GROUNDED - YES. PERFORMED AMM 22-00-01-730-807, FFR SHOWED NO FAULTS LAST FLIGHT ON A OR B, LAND VERIFY TEST NML, REF AMM 22-11-00/201.SDR SWAA2018072623839Computer · failedDIVERSION, YAW DAMPER FAILED AT 5000 FEET ON CLIMB OUT COMPLIED WITH QRH, LIGHT REMAINED ILLUMINATED THROUGHOUT FLIGHT. R&R STALL MANAGEMENT YAW DAMPENER COMPUTER PER AMM.SDR ASAA2018072425523Control Panel · defectiveF/O'S MCP COURSE WINDOW 100'S AND 1'S DIGIT INOP (VERY DIFFICULT TO READ AS THEY STICK). GROUNDED - YES. REMOVED & REPLACED MCP REF AMM 22-11-34-400-801. ACCOMPLISHED MCP INSTALLATION TEST REF AMM 22-11-34-740-801. OPS CK GOOD. ACCOMPLISHED DFCS LRU REPLACEMENSDR HNAA2018072600171Unknown · malfunctionedON CLIMBOUT, A/P FAILED ALONG WITH NR 1 AHRS. PERFORMED AMM TASK 22-11-00-700-803-A. OPS CHECK OF AUTOPILOT AND AHRS SYSTEMS SEVERAL TIMES WITH NO DEFECTS NOTED. OK FOR SERVICE AT THIS TIME.SDR ASAA2018071925470Control Panel · malfunctionedMODE CONTROL PANEL (MCP) APPEARS TO BE DE-POWERED (ALL WINDOWS DARK). GROUNDED - YES. POWERED DOWN A/C PER AMM 20-60-99. REGAINED LIGHTS TO MCP. ACCOMPLISHED MCP TEST REF AMM 22-11-34. ALL OPS CK'D NORMAL.SDR RU3A20180714030Autopilot Sys · malfunctionedPILOT SIDE AUTOPILOT UNCOMMANDED CLIMB ON TWO OCCASIONS. COMPLETED AUTOPILOT SYSTEM FUNCTIONAL TEST AND LEAK TEST WITH NO FAULTS FOUND.SDR DALA2018071604502Rod End · corrodedCORROSION ON TRAILING EDGE ROD END OF YAW DAMPER. REMOVED, REPLACED AND FUNCTIONAL CHECK.SDR ASAA2018071625396Unknown · malfunctionedAUTOLAND UNSUCCESSFUL, PLANE SLOWED 5 KNOTS TO REF AND SEEMED NOT TO TRIM AT APPROXIMATELY 75 FEET. GROUNDED - YES. PERFORMED FIM 22-11 TASK 801. NO FAULTS LOGGED EITHER DFCS LAST FLIGHT. PERFORMED LAND VERIFY BITE 49 -GOOD. NO HISTORY LAST 90 DAYS PLUS.SDR ASAA2018071625373Not Reported · malfunctionedAUTOLAND NOT SUCCESSFUL, SEA RUNWAY 34L, AIRCRAFT CENTERLINE 40' LEFT OF RUNWAY CENTERLINE TOUCHDOWN. GROUNDED - YES. ON DEFERRAL.SDR ASAA2018070425283Unknown · malfunctionedHGS AIII AND AUTOLAND FAILED. ON LOC CAP, BOTH AUTOPILOTS DISCONNECTED. MOMENTARY FMC DISAGREE ON FO'S SIDE ILLUMINATED. MOMENTARY RA FAIL FLAG AT 5000' / FO'S FD DROPPED OFF. IN THE FLARE USING HGS ONLY, THE FLIGHT PATH CUE DISAPPEARED. GROUNDED - YES. RESET SDR ASAA2018070225274Unknown · malfunctionedAP A DISCONNECTED TWICE IN CRUISE. ALSO CAPT PITCH BAR WAS OUT OF VIEW WITH AP A IN USE. GROUNDED - YES. FAULT FLIGHT REVIEW SHOWED LEG 11 WITH 13 FAULTS RELATING TO NR 1 SMYD. NR 1 SMYD SHOWED FAULT MESSAGE 22-21001 LEGS 11, 33 & 40 ON THE GROUND AND INTERMITSDR ASAA2018070225240Warning System · false activation"FLT CONT" MASTER CAUTION LIGHT ILLUMINATED JUST AFTER ROTATION ON TAKEOFF FOR APPROXIMATELY 2 SECONDS & THEN WENT OUT. NO SECONDARY OR ABNORMAL INDICATIONS OBSERVED. GROUNDED - YES. CURRENT STATUS BITE OF DFCS SHOWS NO CURRENT FAULTS. LAST LEG FAULT SHOWS CHASDR ASAA2018063025282Control Panel · defectiveMCP ALT SELECTOR BLEMISH IN MIDDLE OF DISPLAY-DISPLAY STILL READABLE. GROUNDED - YES. REMOVED & REPLACED MCP REF AMM 22-11-34. ACCOMPLISHED MCP INSTALLATION TEST REF AMM 22-11-34-740-801, LRU REPLACEMENT (GP 32) TEST (MCP) REF AMM 22-11-34/501, DFCS LAND VERIFSDR HALA2018062800202Cdu · faultyATB, RETURNED TO HNL DUE TO AUTO FLT FCU FAULT. REPLACED NR 3 MCDU.SDR HALA2018062700312Cdu · malfunctionedATB - ETOPS SIGNIFICANT SYSTEM. AUTO FLT FCU FAULT INOP SYS PART FCU. REMOVED AND REPLACED MCDU NR 3 PER AMM 22-82-12. OPERATIONAL CHECK OK. AIRCRAFT TO REMAIN IN LAND "3" STATUS. UNIT, DISPLAY.SDR ASAA2018062725216Control Panel · defectiveVERTICAL SPEED WINDOW HAS SPOTS SHOWING. GROUNDED - YES. CONFIRMED FAULT, MCP SPD LCD WINDOW HAS NUMEROUS BLACK SPOTS. REMOVED & REPLACED MCP REF AMM 22-11-34. ACCOMPLISHED DFCS MCP TEST REF AMM 22-11-34-740-801, LRU REPLACEMENT TEST (GP 32) REF AMM 22-11-34/5SDR ASAA2018062625217Control Panel · faultyFO'S COURSE DISPLAY WINDOW ON MCP IS BLANK. GROUNDED - YES. REPLACED DFCS MODE CONTROL PANEL REF AMM 22-11-34-400-801, OPS NORMAL REF MM 22-11-34-740-810. ACCOMPLISHED DFCS MCP LRU REPLACEMENT TEST, OPS NORMAL REF MM 22-11-34/501. ACCOMPLISHED LAND VERIFY TESTSDR ASAA2018062625210Control Panel · failedAFTER TAKEOFF THE ALTITUDE WINDOW CHANGED OFF THE PRESELECTED ALTITUDE. WHEN TRYING TO CHANGE THE ALTITUDE BACK THE SELECTOR KNOB WOULD NOT WORK. A SLIGHT PUSH/PULL OF THE KNOB AND WE COULD CHANGE THE ALTITUDE AGAIN. ADDITIONALLY THE BARO BUG ALTITUDE ON DID NSDR ASAA2018062525198Unknown · malfunctionedVNAV DISCONNECT DURING ARRIVAL- COULD NOT RE-ENGAGE. GROUNDED - YES. PERFORMED FIM 22-11 TASK 801, BITE PROC. WITH LAND VERIFY, INTERACTIVE & SURFACE TEST PASSED. CHECKED GOOD. OPS NORMAL.SDR 7SJA201808150001Autopilot Sys · malfunctionedAFTER TAKEOFF, DURING CLIMB OUT, CREW ENGAGED THE AUTOPILOT AND EXPERIENCED AN UNCOMMAND AUTOPILOT PITCH AND YAW. DISCONNECTED THE AUTOPILOT AND RETURNED TO DEPARTURE.SDR COEA2018062101909Unknown · malfunctionedFLIGHT 7779/ENROUTE YKM-GEG DISCREPANCY: ON CLIMB OUT, THE ELEVATOR TRIM AND FLAP INDICATOR TAB WERE ROCKING BACK AND FORTH. FLAPS WERE MOVING UP AND DOWN UNCOMMANDED. AIRCRAFT LANDING WITHOUT FURTHER INCIDENT IN GEG. NO EMERGENCY DECLARED. MAINTENANCE INSPECTSDR ASAA2018062195141Autopilot Sys · malfunctionedAUTOPILOT A DISCONNECTED DURING CRUISE, WITH ALL OTHER INDICATIONS NORMAL. AUTOPILOT A WAS ENGAGED BUT DISCONNECTED EARLY DURING DESCENT, AUTOPILOT B USED FOR REMAINDER OF FLIGHT. ACFT GROUNDED. FLIGHT FAULT REVIEW LOGGED MCP DATA INV, MESSAGE 22-11607, ASDR ASAA2018061985112Switch · inoperativeN1 PUSHBUTTON SWITCH ON THE MODE CONTROL PANEL WAS INOPERATIVE. ACFT GROUNDED. REMOVED, REPLACED AND TESTED DFCS MODE CONTROL PANEL IAW AMM 22-11-34. MCP INSTALLATION TEST PASSED. PERFORMED LRU REPLACEMENT TEST FOR MCP IAW AMM 22-11-34/501 AND LAND VERIFY SDR ASAA2018061865071Autoland Sys · malfunctionedAUTOLAND, AUTOPILOT STEERED LEFT THEN RIGHT IN FLARE. LEFT MAIN WHEEL TOUCHED DOWN ON CENTERLINE. ACFT GROUNDED. ACCOMPLISHED LAND VERIFICATION TESTS IAW AMM 22-11-00-700-801, AND ALL LLM TESTS LISTED IN AMM 22-00-01-730-803. ALL TESTS PASSED. NO HISTORY LASDR ASAA2018060924991Control Panel · malfunctionedMCP IAS/MACH KNOB WILL NOT CHANGE AIRSPEED NUMBER. IT IS FROZEN. GROUNDED - YES. RESET MCP C/B'S REF AMM 22-11-34, IAS WINDOW OPERATED NORMALLY & THEN FAILED AGAIN AFTER MCP TEST. REMOVED & REPLACED MODE CONTROL PANEL PER AMM 22-11-34, INSTALL TEST PASSED. RESDR SIMA20180608003Controller · unknownFLIGHT GUIDANCE CONTROLLER WAS UNRESPONSIVE IN FLIGHT. PERFROMED A FUNCTIONAL TEST OF AUTOPILOT IAW AMM 22-11-00. FNT PASSED NO FAULT FOUND.SDR ASAA2018060864960Control Panel · malfunctionedIAS, MACH SPEED SELECTOR WAS FROZEN WITH SPEED AT 157. ACFT GROUNDED. PERFORMED FIM 22-32, TASK 803, DFCS BITE SHOWS FAULT 22-4003. PERFORMED MCP PANEL TEST IAW FIM 22-11, TASK 803 ALL TESTS PASSED. BUT IAS/MACH KNOB STILL INOPERATIVE. REMOVED AND REPLACSDR ASAA2018060224890Warning Message · unknownCAT II APPROACH AUTOLAND FAILED. AT 20-30 FEET APPROACH WARNING ANNUNCIATED, ON SPEED 138 KIAS ON GLIDESLOPE AND LOC, FLAPS 40 DEG VFR CONDITION. GROUNDED - YES. ACCOMPLISHED FLT FAULT REVIEW, GRP BITE 10, NO FAULTS REF B737-800 FIM 22-11 TASK 801. ACCOMPLISHESDR ASAA2018060044889Control Panel · failedAUTOPILOT A WILL NOT ENGAGE. ACFT GROUNDED. FAULT REVIEW MESSAGES 22-11625, 22-11626, 22-11254, 22-11259. DFCS BITE GRP 70 MCP TESTS FAIL. REPLACED THE MCP IAW AMM 22-11-34, INSTALLATION TEST PASSED. BITE GRP 70 ALSO PASSED. ADDITIONAL LLM TESTS BITE GRP 32SDR SIMA20180601001Proximity Sensor · failedAFCS FAULT MULTIPLE ERRONEOUS MSGS ON SHORT FINAL, EMERGENCY DECLARED. REMOVED AND REPLACED THE NR 1 PSEM ON MAU 1 IAW AMM 32-61-01, LOADED SOFTWARE IAW AMM 45-45-00. OPS CHECKED GOOD IAW AMM 22-11-00.SDR ASAA2018060124864Control Panel · intermittentALTITUDE SELECTOR, ON THE MODE CONTROL PANEL WAS INTERMITTENT. CAN NOT ALWAYS SELECT THE ASSIGNED ALTITUDE. ACFT GROUNDED. REPLACED DFCS MODE CONTROL PANEL, OPS CHECKED GOOD IAW MM 22-11-34, ACCOMPLISHED LLM MAINT TEST FOR MODE CCONTROL PANEL AND ALL TESTSDR RJEF20180529001Fcu · malfunctionedDURING CLIMB, THE AIRCRAFT HAD A FAILURE OF THE KNOB SELECTORS SPEED AND HEADING OF THE FCU, LATER, THE AIRCRAFT DIVERTED, AFTER AN UNEVENTFUL LANDING THE PILOT REPORTED THE FCU SPEED AND HEADING KNOBS BECAME INOPERATIVE WITH NO ECAM MESSAGE OR ANY APPARENT SDR ASAA2018052624815Control Panel · lockedMODE CONTROL PANEL ALTITUDE WINDOW IS LOCKED UP. ALL OTHER WINDOWS OPERATE NORMALLY. GROUNDED - YES. SUSPECT MCP LOCKED IN MAINT BITE. POWERED A/C DOWN. POWERED A/C UP. OPS CHECK DFCS MCP GOOD. REF AMM 22-11034. NO HISTORY 60 DAYS.SDR ASAA201805224726Autopilot Sys · malfunctionedWHILE ON THE GROUND, VNAV DISSENGAGES AFTER 15 SECONDS, LNAV DISENGAGES A FEW SECONDS AFTER. ACFT GROUNDED. VERIFIED DISCREPANCY, PERFORMED DFCS BITE IAW AMM 22-11-00. PERFORMED DFCS LRU REPLACEMENT TEST IAW FIM 22-11, TASK 802. ALL TESTS PASSED. SYS RETURSDR ASAA2018051824695Autoland Sys · malfunctionedON SHORT FINAL, AUTOLAND APPROACH, ACFT DEVIATED LEFT OF CENTERLINE AND APPROACH WARNING INDICATION DISPLAYED. CRITICAL AREA WAS PROTECTED DUE TO WEATHER. XTM RATE EXCEED DISPLAYED IN RECORDED FAULTS AFTER LANDING. ACFT GROUNDED. BITE CHECKED IAW FIM 22-SDR HALA208051700236Autopilot Sys · malfunctionedAT 2800 FT , JUST AFTER GLIDESLOPE CAPTURE FOR ILS WITH CTR AUTOPILOT ENGAGED, AUTOPILOT ABRUPTLY PITCHED DOWN TOWARD F/D, COMMAND INDICATING 8 DEG. NOSE DOWN. AUTOPILOT NAV DISCONNECTED MANUALLY TO MAINTAIN AIRCRAFT CONTROL. GLIDESLOPE INDICATION SHOWED ON GLSDR ASAA2018051524642Sensor · out of adjustDURING CRUISE AT FL 320, -A- AUTOPILOT DISCONNECTED TWICE. -B- AUTOPILOT WORKED PERFECTLY. ACFT GROUNDED. PERFORMED A STAB POSITION SENSOR ADJUSTMENT & TEST IAW AMM 22-11-31-820-801. FOUND STAB -A- AND -B- SENSORS ON OPPOSITE ENDS ON THE LIMITS.6 ADJUSTEDSDR ASAA2018051324619Warning System · false activationCA FLT DIR FLAG CAME ON, 10 MIN PRIOR TO DEPARTURE. GROUNDED - YES. CYCLED A/C POWER REF AMM 22-60-99 CAP T/O RETURN TO NORMAL ACCOMPLISHED DFGS F/D TEST NORMAL REF AMM 22-11-00 A/C OK OPS CHECK NORMAL.SDR IXXA20180421018Autopilot Sys · malfunctionedAT FL 370, CRUISE FLIGHT AUTOPILOT EICAS OFF. RE-ENGAGED THE AUTOPILOT EICAS OFF AGAIN. TRIED LEFT AND RIGHT AUTOPILOT, AUTOPILOT OFF QUICKER. CENTER ON AGAIN STAYED ON UNTIL DESCENT, H/S USED AUTOPILOT OFF, DESCENT TO FL 280, NON RVSM HAND ROLL DIFFICUSDR ASAA2018041624258Computer · malfunctionedSPEED TRIM FAILED AND MACH TRIM FAILED, COMES ON WITH M/C RECALL AND RESET. ACFT GROUNDED. FOUND FCC-A FAULTED DURING POWER TRANSFER. CYCLED POWER TO FCC-A & PERFORMED DFCS BITE CHECK, CURRENT STATUS & FLT DIRECTOR TEST GROUP 12 IAW FIM 22-11 TASK 801. PESDR AALA201804205001Dfgs · malfunctionedDURING HEAVY CROSS WINDS, USING THE NR 2 AUTOPILOT, TWO MISSED APPROACHES WERE MADE. DIVERTED AND LANDING WAS UNEVENTFULLY WITH NR 1 AUTOPILOT. PERFORMED A FLIGHT FAULT REVIEW, FIRST APPROACH, AUTOPILOT CAPTURED LOC 2 GLIDESLOOP THEN WENT TO VERT SPEED. SDR ASAA2018041424241Autopilot Sys · malfunctioned2.5 HOURS INTO FLT, AUTOPILOT A DISENGAGED. REENGAGED AND WORKED FINE. ACFT GROUNDED. PERFORMED LIBRARY TEST 49 LAND VERIFY AND LIBRARY TEST 32 MCP IAW AMM 22-11-00, SYSTEM MCP CHECKED GOOD, NO DEFECTS NOTED, NO HISTORY LAST 60 DAYS.SDR 2018F00152Control Panel · failedAFTER TAKEOFF, MCP WAS NOT WORKING PROPERLY, BUTTONS FROZE. REPLACED THE MCP.SDR ASAA2018040124105Light · inoperativeTHE LIGHT ON THE VNAV BUTTON AND THE A/T ARM LIGHT ON THE MCP WERE INOPERATIVE. ACFT GROUNDED. REMOVED AND REPLACED DFCS MODE CONTROL PANEL IAW AMM 22-11-34. MCP INSTALLATION TESTED GOOD IAW AMM 22-11-34. LRU REPLACEMENT TESTED FOR MCP, BITE TEST GROUP 32, TSDR HALA2018032700124Warning Message · false activationAUTO FLT FCU FAULT. PERFORMED AN AFS SYS TEST IAW AMM 22-96-00. MESSAGE CLEARED. TESTED OK. OK FOR SERVICE.SDR 2018FA0000113Autopilot Sys · malfunctionedAIRCRAFT EXPERIENCED A FAILURE OF THE PITCH TRIM ACTUATION IN FLIGHT AFTER THE AUTOPILOT AUTO TRIMMED THE PITCH TO A FULL NOSE DOWN POSITION.SDR DALA2018032001807Autopilot Sys · trippedALL THREE AUTOPILOTS TRIPPED OFF DURING APPROACH. COMPLETED MCDP TEST 30, AND TEST 40 ,AUTO LAND IAW FIM 22-00-03, NO FAULTS NOTED.
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