JASC 2210
Service difficulty reports · 4,017
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 ASAA2012100893081Computer · failedDURING S/W UPDATE OF FCC B REF T/CSB737-22A1224-NG-1-1. FCC B FAILED. REPLACED FCC B REF MM22-11-33, ETOPS GROUND VERIFICATON, OPS CK NORMAL, S/W CK OK. ACCOMP DFCS LAND VERIFIY NR 49, LRU FCC NR 35 TEST, & HGS SENSOR FCC/AT TEST. ALL TEST NML REF MM22-11-00SDR ASAA2012100293007Warning Message · false activationDISPLAY SOURCE ANNUNCIATOR ON BOTH VDI. RAN CK LIST. NO SECONDARY INDICATIONS NOTED. CAPTAIN'S FLT DIRECTOR DISAPPEARED, APPROX 1500 AGL ON APPROACH. DOWN POWERED AND REAPPLIED POWER TO ACFT. ALL SYSTEMS OPERATE NORMALLY NOW. NO REOCCURRENCE. ACCOMPLISHSDR UALA2012092905500Panel · looseRIGHT SIDE OF FCU LOOSE. SECURED RIGHT SIDE OF FCU PANEL.SDR SWIA201231781Actuator · failedAIRCRAFT YAWED UNCOMMANDED DURING DESCENT. (FLT 6274) REPLACED NR 1 YAW DAMPER LINEAR ACTUATOR IAW AMM. P/N OFF: 622-9962-001 S/N OFF: 3662.SDR UALA2012091305182Control Panel · faultyMODE CONTROL PANEL LANE STATUS MESSAGE DISPLAYED. REPLACED MODE CONTROL PANEL.SDR ASAA2012090692837Control Panel · weakMAIN CONTROL PANEL SPEED WINDOW EXTREMELY DIM. ALL OTHER MCP LIGHTS ARE NORMAL. DID GET IT TO GO BRIGHTER BY TAPPING ON LIGHT PANEL HOWEVER IT DID GO DIM AGAIN. SPEED BUG AND ALL SYSTEMS WORK NORMALLY. ACFT GROUNDED. R & R MODE CONTROL PANEL REF MM 22-11-34SDR ASAA2012090592836Autopilot Sys · malfunctionedAUTOPILOT WOULD NOT ENGAGE. REMOVED RT ADIRU IAW 34-21-01-000-807 AND REMOVED FCC IAW 22-11-33-00-801 FOR T/S IAW FIM TASK 22-11-00-810-807. PERFORMED CONTINUITY CHECK BETWEEN PINS C10 AND C11 OF D3693B AND B1 AND B2 OF D45257P NO FAULTS NOTED. PERFORMED COSDR ASAA2012092992966Control Panel · failedON CLIMBOUT HEADING SELECTOR & BUG INTERMITTENTLY FROZE (BUG DISPLAY ON PFD/ND WOULD NOT MOVE) DURING CRUISE HDG WINDOW WOULD INTERMITTENTLY MOVE ON ITS ON - WITHOUT PILOT INPUT (BUG DISPLAY ON PFD/ND WOULD FOLLOW HEADING WINDOW DISPLAY. ACFT GROUNDED. R & RSDR ASAA2012091592884Warning Light · false activationAUTOLAND APPROACH WARNING IN FLARE & LINED UP 20 TO THE RT OF CENTERLINE. HEADINGS FFR SHOWED RADAR ALTIMETER INVALID FOR LAST FLT, DFCS RECORDED NO FAULT. PERFORMED LAND VERIFY AND HGS SYS TEST REF MM 22-00-01-730-801 ALL TEST PASSED.SDR USAA2012083000004Autopilot Sys · malfunctionedPHL FLT 9010 EN ROUTE ZRH TO PHL. STEADY RYTHMIC YAWING MOTION. NOTICEABLE THRU OUT AIRCRAFT. LASTED APPROX 45 MINUTES. CEASED WHEN TURNED OFF CENTER TANK FUEL PUMPS. ACCOMPLISHED RECOMMENDED TROUBLESHOOTING TASKS; CHECKED ALL FLIGHT CONTROL MODULES FOR SDR CA120828007Circuit Card · failed(CAN) AIRCRAFT WAS OSCILLATING WHILE THE AUTOPILOT WAS ENGAGED AT APPROXIMATELY 10000 FT, AUTOPILOT WAS DISENGAGED, THE OSCILLATING WENT AWAY FLT RETURNED. THE ACFT CONDUCTED AN OVERWEIGHT LANDING. PILOT TALKED WITH MTCE AFTER THE LANDING. CAPTAIN WILL FILSDR UALA2012082904863Autopilot Sys · inoperativeLEFT AUTOPILOT WILL NOT ENGAGE. COMPLETED REMOVAL OF LEFT CLCP FROM MM AND INSTALLED SERVICEABLE UNIT PER MM. OPS CHECKED NORMAL.SDR UALA2012082304733Module · inoperativeLEFT YAW DAMPER INOPERATIVE. REPLACED CSEU PWR SUPPLY MODULE M536 DUE TO "NO 26 VAC" FAULT ON YAW DAMP MODULE-L. YAW DAMP, RUDDER RATIO, POWER SUPPLY AND MCDP CURRENT FAULTS TEST 30 ALL PASS.SDR USAA2012081300022Yaw Damper · faultyDURING TAKEOFF ROLL IN PHX THE AIRCRAFT HAD A FAST BUT MOMENTARY UNCOMMANDED RUDDER MOVEMENT AT APPROXIMATELY 115 KTS. THE FIRST OFFICER WAS FLYING AND HE THOUGHT IT WAS A NOSE RIGHT MOVEMENT. PER LOG PAGE 4854424, REMOVED AND REPLACED LEFT YAW DAMPER. OPS SDR HNAA2012080600896Yaw Damper · failedBOTH YAW DAMPENERS FAILED. YAW DAMPENERS BOTH CHANNELS DE-ACTIVATED IAW APENDIX 1/22-4-1.SDR USAA2012081000010Servo · malfunctionedRUDDER RANDOMLY AND BRIEFLY KICKS RIGHT YAWING THE AIRCRAFT NOTICEABLY. REMOVED AND REPLACED YAW DAMPER ACTUATOR SERVO NR 1. PERFORMED SATISFACTORY CAT 3 AUTOLAND TEST IAW AMM 27-97-00-710-001.SDR ASAA2012082592773Circuit Breaker · trippedFLIGHT DECK PREFLY AFCS INTERLINK 2 CIRCUIT BREAKER DISCOVERED TRIPPED (P6-2). ACFT GROUNDED. RESET CIRCUIT BREAKER IAW MM 20-60-01. INSPECTED WIRING BEHIND P6-2 PANEL, WIRES SHOW NO DAMAGE. PERFORMED INITIAL EVALUATION IAW FIM 22-13-00, TASK 822. NO CURRESDR ASAA2012081992749Autoland Sys · malfunctionedPERFORMED AUTOLAND. AUTOLAND UNSATISFACTORY AUTOPILOT FLARED LATE AND AGGRESSIVE BUT NOT ENOUGH. TOUCHDOWN WAS VERY FIRM AND APPROX 15 FT LEFT OF CENTERLINE. ACCOMPLISHED FLIGHT FAULT REVIEW FOR BOTH FCC A & B. NO FAULTS NOTED. ACCOMPLISHED FIM TASK 22-1SDR ASAA2012081192688Control Panel · inoperativeAUTOPILOT LIGHT WILL NOT ILLUMINATE. ACFT GROUNDED. R & R DFCS MODE CONTROL PANEL IAW AMM 22-11-34, OPS CHECK GOOD IAW AMM 22-11-34-740-801, LRU INTERFACE TEST AND 22-11-00 LAND VERIFY TEST, ACFT IS AUTOLAND AND HGS CAT III QUALIFIED.SDR CA120801003Cable · failed(CAN) DURING CRUISE THE PILOTS SELECTED THE AUTOPILOT ON. THE PLANE WOULD NOT HOLD THE HEADING SELECTED. MAINTENANCE CARRIED OUT AN INSPECTION ON THE AUTOPILOT SYS SUSPECTING THE ROLL SERVO TO BE BURNED OUT. THEY FOUND THE CABLE TO THE SERVO TO BE SNAPPED. SDR 2012FA0000516Control Cable · frayedDURING COMPLIANCE OF SB 7001A11-22-003 (AUTOPILOT SYSTEM CHECK), FOUND RT ELEVATOR LOWER A/P TRIM CABLE FRAYED AT THE UPPER BELLCRANK. SENT CABLE TO TECH REP FOR EVALUATION.SDR CLCA20120727001Button · out of positionDURING DEPARTURE, (VCP) CAPTAINS A/P DISCONNECT BUTTON CAME OUT OF ITS SOCKET, AND CAUSE ELECTRIC SHORT. RETURNED TO VCP. TROUBLESHOOT SYSTEM AND FOUND WIRE LOOSE AT CAPTAINS AP DISCONNECT SWITCH. SECURED WIRE AT CAPTAINS SWITCH CONNECTOR IAW MD-11 AMM 20-3SDR IPXA2M74593Computer · inoperativeCOULD NOT ENGAGE AP1, COULD NOT SWITCH TO NAV 1, CHECKED AND FOUND FCC 1 FAULT, R & R FCC1 THEN CHECKED NO CURRENT FAULT BUT WHILE PERFORM FCC1 CAT3B TEST FOUND PROBABLE CAUSE EL L/O VALVE-LIB SO R & R LIB ELEV ACTUATOR, REMOVED PN 205300-5005, SN AT408.SDR UALA2012072404023Computer · malfunctionedON TAKEOFF, EICAS AUTO PILOT MESSAGE AND LOST BOTH FLT DIRECTOR, AUTOTHROTTLE TRIPPED OFF. RECOVERED AUTOTHROTTLE AND ABLE TO OPERATE CTR AUTOPILOT. BOTH FLT DIRECTOR STILL INOPERATIVE. REPLACED LEFT FCC COMPUTER.SDR UALA2012072404020Computer · inoperativeCAPTAIN'S FLIGHT DIRECTOR INOPERATIVE. REPLACED LT FCC PER AMM.SDR UALA2012071803879Actuator · faultedAUTO FLT 'YAW DAMPER 1' DISPLAYED ON UPPER ECAM SCREEN. NR 1 YAW DAMPER INOPERATIVE. REPLACED ACTUATOR.SDR ASAA2012072192566Computer · malfunctionedFOUND FLAG CAPT. ACFT GROUNDED. PERFORMED FIM TASK 22-11-00-810-801. FOUND FCC NR 1 UNABLE TO TEST FAIL. RESET NR 1 FCC TESTS GOOD. NO FURTHER DEFECTS NOTED.SDR ASAA2012071492533Display · intermittentMCP IAS/MACH WINDOW DISPLAY VERY DIM EVEN WITH MAIN PANEL BRIGHTNESS ALL THE WAY UP. ACFT GROUNDED. COULD NOT DUPLICATE. SHOOK DOWN MODE CONTROL PANEL, MCP IAS/MACH WINDOW DISPLAY CHECKED NORMAL.SDR QXEA2012061700474Warning Light · false activationAP/YD DISENGAGED DURING CLIMB. AP/YD FAIL MESSAGE DISPLAYED ON BOTH PFD'S. COMPLIED WITH EMERGENCY ABNORMAL CHECKLIST. ALSO ON DESCENT "YD NOT CENTERED" MESSAGE DISPLAYED ON BOTH PFD'S. INTERROGATED CDS FCS PAGE NO ASSOCIATED FAULTS FOUND RESET CIRCUIT BREAKSDR CWQR20120613041Bracket · crackedDURING SCHEDULED MX, FOUND RUDDER/ELEVATOR AUTO-PILOT SERVO CABLE BRACKET CRACKED FROM 1 END TO PASS THE FIRST ATTACH FASTENER.SDR ASAA12511656Autopilot Sys · malfunctionedON APPROCH, ILS 29 AUTOPILOT INITIALLY CAPTURED LOCALIZER WITH BOTH CHANNELS ENGAGED, APPOX 5 SECONDS LATER AUTOPILOT DISENGAGED RE-ENGAGED AND SAME THING HAPPENED. PERFORMED LIBRARY GROUP 49 LAND, VERIFIED SYS, OP CHECKED GOOD.SDR ASAA12511660Warning Message · illuminatedON CAT III AUTOLAND, RECEIVED "APPROACH WARNING" AT 30' ABOVE GROUND AS ACFT DRIFTED RT OF CENTERLINE. PERFORMED FIM 22-11, TASK 801 FAULT REVIEW NO FAULTS AND LAND VERIFY BITE GP NR 49 ALL TESTS PASSED. REF MM 22-00-01. OPS NORMAL.SDR CA120604004Control Unit · failed(CAN) THE NR 2 ENGINE AUTO-FEATHERED WHEN POWER WAS APPLIED FOR TAKEOFF. INVESTIGATION REVEALED THAT THE NR 1 TORQUE SENSOR CONDITIONING UNIT WAS LATCHED IN TEST MODE. THE NR 1 TSCU WAS REPLACED AND GROUND RUNS CARRIED OUT. THE ACFT WAS RETURNED TO SERVICE.SDR ASAA12511621Control Panel · no testNR 3 PACK (A/P A/T FMC) ANNUNCIATOR DOES NOT TEST IN THE NR 1 POSITION. ACFT GROUNDED. R & R CAPT'S AUTOFLIGHT STATUS ANNUNCIATOR PANEL REF MM 22-11-32-400-801.SDR ASAA12511612Unknown · unknownAUTOPILOT ENGAGE, B LIGHT DOES NOT ILLUMINATE. ACFT GROUNDED. ACCOMPLISHED DFCS LRU INTERFACE FOR MCP CHAN B AND VERIFIED CMD B ENGAGE LIGHT ILLUMINATES WHEN PUSHED REF MM 22-11-34. OPS NORMAL.SDR GN0A05282012Control Panel · contaminatedFLIGHT 15976 (MER) TO (GCN): WHILE CLIMBING THROUGH 11,000FT THE AUTO-PILOT ENGAGED WITHOUT THE CREW SELECTING THE SYSTEM ON. NEITHER CONTROL WHEEL A/P DISCONNECT SWITCH WOULD DISENGAGE THE AUTO-PILOT. THE FIRST OFFICER HAD TO HOLD DOWN THE DISCONNECT BUTTOSDR UALA2012052402911Computer · faultyCENTER AUTOPILOT WILL NOT ENGAGE AND FIRST OFFICER FLT DIRECTOR BARS LOST WHEN CENTER FLT DIRECTOR ENGAGED. CENTER FCC INOPERATIVE. REPLACED CENTER FLIGHT CONTROL COMPUTER AS PER AMM. OPS CHECKED NORMAL. ALSO ACCOMPLISHED AUTOPILOT FLIGHT CONTROL TEST AS PSDR ASAA12511571Autoland Sys · unknownAUTOLAND & HEADINGS, LANDED LEFT OF CTR LINE OVER LEFT RUNWAY CENTER LIGHTS AT 1000FT AND CONTINUED TO DIVERGE TO THE LEFT DISCONNECTED AUTO PILOT AND RETURNED TO CENTER LINE. ACFT GROUNDED. PERFORMED SUCCESSFUL LAND VERIFY TEST IAW AMM 22-11-00-700-801. DISDR AALA20120515015Control Panel · malfunctionedIAD - INFLIGHT JFK-PAP. CREW REPORTED FLIGHT DIRECTOR FAILED, FOLLOWED BY FAILURE OF AUTO THROTTLES AND VERTICAL NAVIGATION. EMERGENCY DECLARED FLIGHT DIVERTED IAD LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED MODE CONTROL PANEL. SYSTEMSDR ASAA12511556Control Panel · inoperativeF/O WINDOW IS BLANK ON MODE CONTROL PANEL. ACFT GROUNDED. REPLACED DFCS MODE CONTROL PANEL REF MM 22-11-34-400 801. OPS NORMAL. PERFORMED ADDITIONAL TEST REF LAMP CHECK LIST MM 22-00-01-730-801, BG 32 DFCS LRU FOR MCP BG 49 LAND VERIFY TEST & HGS SENSOR FOR SDR SWIA201230711Actuator · failedUNCOMMANDED RUDDER CHANGE. (FLT 6223) REPLACED NR 2 YAW DAMPER LINEAR ACTUATOR AND NR 2 AHRS IN REFERENCE TO AMM. PN ON 622-9968-001 SN OFF 3038.SDR UIEA2012051000209Control Panel · malfunctionedCAPTAINS COMMAND AIRSPEED BUG OUT OF VIEW. L AND C FLT DIR INOPERATIVE IAS, HEADING AND ALT ON MCP COULD NOT BE CHANGED. IAS AND HEADING DID CHANGE ON HSI. FOUND MULTIPLE FAULTS IN REF TO MODE CONTROL PANEL. R & R MCP IAW AMM ALL OPS CHECK NORMAL AT THIS TISDR UALA2012051002679Display · inoperativeBOTH PFD'S ON SAME FAC AP 1&2 INOPERATIVE, CAT2 LISTED ON INOPERATIVE SYS. DID COMPLETE REBOOT OF AIRCRAFT. COMPLETED FAC 1 TEST AND AFS TEST. ACCOMPLISHED CAT 3 TEST WITH GOOD RESULTS AMM 22-97-00-710-001. ALL MESSAGES CLEARED.SDR ASAA12511508Unknown · unknownF/O COURSE WINDOW BLANK. ACFT GROUNDED. PULLED AND RESET CB AFCS MCP DC 2. REF FIM 22-11-00. F/O COURSE INDICATION NORMAL. PERFORMED LAND VERIFY REF MM 22-00-01. BITE TEST 32. TESTS OK. PERFORMED HGS TEST REF MM 34-36-00. TESTS OK.SDR ASAA12511507Unknown · unknownAFTER 3 HRS OF FLIGHT A AUTOPILOT DISENGAGED SMOOTH AIR. RE-ENGAGED AND WORKED NORMALLY FOR DURATION OF FLIGHT. ACFT GROUNDED. DFCS A LOGGED MSG 22-11-607 MCP DATA INVALID. FOLLOWED FIM 22-11, TASK 817. ALL TEST PASSED. ACCOMPLISHED LWMP CHECKS REF CHECKLISDR ASAA12511573Sensor · failedWHILE ATTEMPTING TO ACCOMPLISH TASK CARD 78222000, TEST FAILED, BITE GROUP 31. ACFT GROUNDED. FAULTS SPOILER 9 POS SENSOR 2 (FAULT MESSAGE 22-11160) TROUBLESHOT IAW FIM REF 22-12-00-810-802, ADJUSTED SPOILER 9 POSITION SENSOR IAW AMM REF TASK 22-11-27-820-80SDR UALA2012043002534Computer · malfunctionedAUTO FLT 'FCU 1 FAULT' DISPLAYED ON UPPER ECAM SCREEN. ATTEMPTED RESET PERFORM 13.50.3 CYCLED FCU1 FCU2 CB`S, NO FIX. PERFORMED FULL RESET OF FCU CB`S B5-M21. FCU 1 FAULT CLEARED.SDR SIMA20120429002Autopilot Sys · malfunctionedON FLIGHT 3822 THE CREW REPORTED THAT AT 400 FEET DISCONNECTED THE AUTOPILOT - AUTOPILOT THEN PUSHED THE NOSE DOWN FOUGHT AIRCRAFT UNTIL AN UNBINDING FEELING HAPPENED AND REGAINED CONTROL OF A/C. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THSDR REXA2012042700576Yaw Damper · disengagedYD NR 1 DISENGAGED IN FLIGHT MULTIPLE TIMES. REMOVED AND REPLACED NR 1 YAW DAMPNER IAW AMM 22-22-01. OP/C GOOD.SDR ASAA12511447Autoland Sys · malfunctionedPRACTICE AUTOLAND KOAK WITH HGS MONITOR GOT APPROACH WARNING IN FLARE. HAD 12KTS X WIND. CHECKED FAULT REVIEW FCC B HAD NUMEROUS MMR FAULTS ON PERVIOUS LEG NOTHING BEFORE THAT. RESET BOTH SYS MMR2 CHECKED GOOD IAW AMM 34-31-42-400-801, LAND VERIFY TESTED GO
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