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 ASAA12511453Control Panel · inoperativeF/O COURSE WINDOW INOPERATIVE, ACFT GROUNDED. CYCLED MCP NR 1 DC CIRUCIT BREAKER, DISPLAY CAME UP NORMALLY FOR A FEW SECONDS AND WENT BACK OUT AGAIN. REPLACED MCP REF MM 22-11-34, OPS CHECKED NORMAL. ACCOMPLISHED ALL MCP LWMP CHECKS PER CHECKLIST MM 22-0-01 SDR ASAA12511434Autopilot Sys · malfunctionedF/O COURSE SELECTOR WINDOW ON MCP INOPERATIVE. ON SUBSEQUENT FLIGHT TOGA BUTTON DOES NOT ACTIVATE 'PITCH GUIDANCE' UNTIL AIRBORNE. NR 1 CMD A/P WILL NOT ENGAGE. F/O CMD A/P WILL ENGAGE. DUPLICATED PROBLEMS FOUND MCP NR 1 DC C/B OUT. INSPECTED C/B & PANEL ARESDR UALA2012042002351Computer · failedRT FLIGHT CONTROL COMPUTER FAILED GROUND TEST 1 AND LOG 7 FLIGHT FAULT "NO INFC FCC R MCDP". REPLACED RT FCC.SDR ASAA12511420Actuator · failedFCC A FAILS SELF TEST. MESSAGE 22-11339 'R SENSOR EXC INV'. ACFT GROUNDED. REPLACED A/P AILERON A ACTUATOR IAW AMM 22-11-25-400-801, LEAK CHECKED GOOD IAW AMM 22-11-25-710-801. OPS CHECKED GOOD IAW AMM 22-11-25-710-801.SDR CA120522017Servo · malfunctioned(CAN) DURING CLIMB WITH AUTOPILOT ON, UNCOMMANDED PITCH CHANGES OF 3-4 DEGREES. AP SELECTED OFF AND PITCH CHANGES STOPPED. MAINTENANCE REPLACED AUTOPILOT PITCH SERVO.SDR ASAA12511397Computer · malfunctionedMCP INOPERATIVE. ACFT GROUNDED. REBOOTED MCP REF. MM 22 11 34. MCP POWERED NORMALLY. TESTED REF MM 22-11-34 AND 22-11-00 BITE GRP. NR 32 AND NR 49. TESTS OK. TESTED HGS REF SMM 34-36-00. TESTED OK.SDR 2012FA0000199Autopilot Sys · malfunctionedDISCONNECTED AUTOPILOT AND HAND FLEW ACFT FOR SEVERAL MINUTES. SHORTLY AFTER INITIATING DESCENT TO LAND, AILERONS BEGAN TO "SEIZE." ELEVATOR STILL HAD FULL MOVEMENT, THEN IT ALSO BEGAN TO SEIZE. IT TOOK ABOUT FIVE TO TEN SECONDS TO LOSE AILERON AUTHORITY, TSDR SWIA201230355Servo · failedFLT 6445, AUTO PILOT UNCOMMANDED ROLL. REPLACED THE AILERON SERVO IN REFERENCE TO MM.SDR COMA2012040950028Actuator · failedON CLIMBOUT, RECEIVED YAW DAMP 1 STATUS MESSAGE. EMERGENCY DECLARED, ACFT RETURNED TO DEPARTURE AND LANDED SAFELY. REMOVED AND REPLACED NR 1 YAW DAMPER LINEAR ACTUATOR. OPS CHECKED GOOD.SDR SIMA201203300013Button · unsecureON FLIGHT 3529 THE CREW REPORTED THEY WERE UNABLE TO ENGAGE AN LATERAL FLT DIR MODE ROLL, HDG, NAV VSI & SPD MODES WORKED INTERMITTENTLY AL HOLD WORKED. THE CREW ELECTED TO RETURN TO MIA. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SESDR ASAA12511301Control Panel · faultyAIRSPEED KNOB WORKS INTERMITTENTLY. REMOVED AND REPLACED DFCS MODE CONTROL PANEL REF MM 22 11 34. INSTALLATION TEST PASSED.SDR SIMA201208602Actuator · inoperativeON FLIGHT 3869 THE CREW REPORTED THAT ON THE CLIMBOUT AT 290 KNOTS THE RUDDER STARTED TO OCILLATE RIGHT AND LEFT. AUTOPILOT WAS IMMEDIATELY DISCONNECTED, OCILLATIONS CONTINUED LEFT AND RIGHT. YD#1 INOP STATUS MSG APPEARED, TRIED TO DISCONNECT YD#2. WOULD NSDR ASAA12511265Control Panel · malfunctionedVNAV SWITCH LIGHT OUT WHEN SELECTED AND ON LIGHTS TEST. VNAV WORKS NORMAL. REPLACED MCP PANEL REF MM 22 11 34. ACCOMPLISHED LWMP TEST BITE NR 32 AND BITE NR 49 AND HGS SENSOR TEST FCC/AT REF LWMP CHECKLIST MM 22 00 01 AND SMM 34 36 00. ALL TEST GOOD.SDR ASAA12511244Light · malfunctionedVNAV LIGHT ON MODE CONTROL PANEL INOP. V NAV LIGHT OPERATES NORMAL ON GRND. NO HISTORY FOR 30 DAYS.SDR UALA2012031501715Circuit Breaker · trippedCREW NOTICED CB 10 (CTR BUS POWER) OUT ON P6 ELECTRICAL PANEL. CREW COULD NOT ENGAGE CTR AUTO PILOT REF TO WDM24-51-31 SHEET 1, PAGE 1. UNABLE TO DUPLICATE FAULT CENTER BUS POWER CB STAYS IN WITH CENTER AUTOPILOT ENGAGED CHECKED TB16 AND RELAY K107 FOR PROPESDR HNAA2012031200684Computer · malfunctionedAIRSPEED EXCEEDED 45 DEGREE BANK WITH AUTOPILOT AND FLIGHT DIRECTOR ENGAGED. INDICATED AIRSPEED 180 KTS. FLAPS AT ZERO. GEAR UP. NO FULL FLIGHT CONTROL DEFLECTION. COULD NOT DUPLICATE. R & R NR 1 FGC AS PRECAUTION. OPS CHECKED GOOD IAW MM 20-10-01.SDR UALA2012031201610Autopilot Sys · malfunctionedWHEN USING AUTOPILOT 1FMGC DROPS OUT OF MNGD SPEED AND NAV. REVERTS TO SLCTD SPD AND HDNG TBLSHT & SUSPECT FAC NR 1. FAC 1 & 2 SWAPPPED FOR T-S, A-C REMOVE FROM CAT II & III UNTIL SATISFACTORY AUTOLAND TEST ACCPD. A-C IS DOWNGRADED TO CAT I STATUS. ACCOMPLISDR ASAA12511211Unknown · malfunctionedAFTER T/O VNAV SELECTED A/S BUG ON BOTH PILOT FLT DISPLAYS INDICATED UP INSTEAD OF 250 KTS. FLAPS WERE FULLY RETRACTED. THIS PROBLEM CONTINUED TO LEVEL OFF AT 34 000FT WITH MULTIPLE ATTEMPTS AT VNAV & LVL CHANGE. LVL CHG WAS OK. CLIMB PAGE ANNUNCIATED 212 SDR ASAA12511148Unknown · malfunctionedGROUND POWER WAS INTERUPTED AND THEN RE ESTABLISHED. AFTERWARD MCP PANEL LIGHTS ALL WENT OUT. REPOWERED MCP REF MM 22 11 34 400 801. MCP POWERED UP NORMALLY. CBS PULLED AND RESET : P18 1 D 1 D 2 D 3 D 5 E 1 E 3. P6 2 B 1 B 3 B 4 C 3. POWER RESTORED TO MCP.SDR AXSA20120219001Module · not seatedCREW REPORTED THAT ON CLIMBOUT, NOTED RMI NR 1 HAD A NAV FLAG, CREW BRIEFLY TUNED IN GDM VOR. ONCE GDM WAS TUNED IN THEY NOTED THAT NAV NR 1 ALSO PRESENTED A NAV FLAG AND NAV NR 2 WAS FULLY OPERATIONAL. ON LEVEL OFF, CREW DECIDED TO ENGAGE AUTOPILOT. ONCSDR USAA2012022000023Adiru · faultedIN AUTOPILOT ONE, AIRCRAFT STARTED AN UNCOMMANDED CLIMB AT CRUISE. AUTOPILOT 2 WAS OK. POST FLIGHT REPORT SHOWED ADIRU1 FAULTED. BITE TEST AND GROUND SCAN OF ADIRU 1 CHECKED GOOD IAW AIRBUS MAINTENANCE MANUAL 34-13-00. PERFORMED AUTOMATIC FLIGHT SYSTEM TESSDR ASAA12511080Circuit Breaker · trippedAFCS INTLK 2 CIRCUIT BREAKER FOUND IN THE OPEN POS DURING PREFLT. RESET C/B A/P TESTS GOOD REF 22 00 01 730 801.SDR ASAA12511067Unknown · malfunctionedON APPROACH AT ABOUT 1500 AGL "APPROACH MODE" AUTOPILOT "B" ENGAGED AUTOPILOT B DISENGAGED ITSELF. DID NOT TRY TO RE-ENGAGE AUTOPILOT. ACCOMPLISHED FIM 22 11 TASK 801. LOC BEAM ANOMOLY DET FAULT LOGGED ON LEG 1. LAND VERIFY TEST PASSED. GROUND VERIFICATIOSDR ASAA12511016Control Panel · faultyTHE FIRST DIGIT ON THE GLARE SHIELD HEADING SELECTOR "FLUTTERS" (CONTINUALLY BLINKS VERY FAST) NO OTHER DIGITS ON GLARE SHIELD SELECTORS "FLUTTER". REPLACED MCP REF MM 22 11 34 OPS CHECK NORMAL. ACCOMPLISHED ALL MCP LWMP CHECKS REF LWMP CHECKLIST MM 22 00 01SDR ASAA12511014Unknown · malfunctionedPILOT REPORTS C/B OUT (OPEN) AT P6 2 ROW A3 AFCS INTLK 2. OPEN P6 2 PNL ACCOMP GVI OF PNL NO DEFECTS NOTED CLOSED PNL & CLOSED C/B AT P6 2 ROW A3 REF WDM 22 11 12 & MM 20 60 01 860 801. PERFORMED DFCS LRU REPLACEMENT TEST FOR FCC BG 35 PER MM 22 11 37 TEST PSDR UALA2012012700562Control Panel · faultyCREW REPORT STAB TRIM 2 & 3 AND STAB. AUTOPILOT MODE CONTROL PANEL REPLACED DUE TO STAB TRIM PROBLEM. REPLACED MCP.SDR 5APR20120117105Controller · faultyTHE FLIGHT CREW REPORTED THE AUTO PILOT SYSTEM AS BEING INOP. THE AUTO PILOT MODE CONTROLLER, PN 065-00086-0017 WAS FOUND TO BE FAULTY. IT WAS R & R USING A SERVICEABLE UNIT OF THE SAME PN IAW AMM 12-A-22-10-05-00A-920A-A. THE SYS OPERATIONALLY TESTED GOOD SDR CA120126004Servo · failed(CAN) AP SHOWS TOO SLOW REACTION TO PITCH DEMANDS OF FD. CANNOT FOLLOW FD PITCH BAR. SIGNIFICANT PROBLEMS ARE MARKED DURING CLIMB WITH EVENT BUTTON OF FDR AT 1338 UTC PASSING FL160. SECOND FDR BUTTON PUSH AT 14:18 ALT HOLD FAIL. CORRECTIVE MAINTENANCE ACTSDR UALA2012010900174Transducer · intermittentNO LAND 3 DISP ON ASA WITH SYS ENGAGED IN CMD. SOURCE SELECT IN 2 (1=L ,2=C, 3=R) POS. CREW COMMENTS: LEFT AP SAME THING. FOUND FAULT FEEL POS-FCC C. FLIGHT FAULT CODES ARE FLT 5-132221,122221, FLT 22-132221, FLT 30-132221, FLT 40-122221, CARRIED OUT TRANSDR UALA2012010900214Actuator · leakingFOUND RT YAW DAMPER ACTUATOR M509 LEAKING DURING OPERATION. INSTALLED NEW ACTUATOR PER MM.SDR UALA2012010500109Computer · faultedFMGC 2 FAULT. REPLACED NR 2 FMCG PER MM. AUTOLAND CAT III TEST.SDR REXA201101030Panel · malfunctionedYAW DAMPER 1 IS JAMMED, WILL NOT DISCONNECT. REMOVED AND REPLACED YAW DAMPER PANEL PER AMM 22-22-04. OPS CK GOOD. OK FOR SERVICE.SDR ASAA11510848Unknown · malfunctionedCAPT FD AMBER FLAG DISPLAYS. FOUND FCC A DC C/B OUT. INSPECTED & RESET C/B REF MM 20 60 01 FCC A OPS CK OK REF MM 22 11 33.SDR NACA20110053Light · overheatedRETURNED TO ANCHORAGE DUE TO STRONG ELECTRICAL SMELL. FOUND ALTITUDE ALERT (A)-1 LIGHT ASSEMBLY DARKENED FROM OVERHEATING OR SMOKING. FOUND C/B C318 TRIPPED. MASTER DIM BUS INDICATOR SECT 6 INCHES REPLACED KORRY LIGHT ASSEMBLY & RESET C/B. OP CHECK GOOD RESDR ASAA11510806Unknown · malfunctionedSPEED TRIM FAIL LT ON RECALL. PERFORMED LAND VERIFY TESTS SYS TESTS GOOD. REF MM 22 00 01 730 801.SDR AALA20111210TUL13Circuit Breaker · defectiveEWR - CREW REPORTED NUMBER 2 AUTO THROTTLES WOULD NOT ENGAGE. ONCE AIRBORNE SELECTED NUMBER 1 DFGS AND YAW DAMPER OFF LIGHT ILLUMINATED. FLIGHT RETURNED EWR LANDED WITHOUT INCIDENT. REPLACED NUMBER 1 YAW DAMPER FAULTY CIRCUIT BREAKER. SYSTEM GROUND CHECK NSDR CA120103020Computer · failed(CAN) UNCOMMANDED AUTOPILOT CHANGE. LT AILERONS INPUT DURING LT TURN. REPLACED FCC1, FCC2 & AILERON SERVO.SDR 2011FA0000778Bracket · crackedDURING A ROUTINE PHASE A/B INSPECTION, TECHS DISCOVERED THAT THE AUTOPILOT RUDDER CABLE BRACKET LOCATED AFT OF THE CANTED BULKHEAD HAS A 1" CRACK AT THE BASE OF THE BRACKET PASSING THROUGH THE TOP MOUNT HOLE.SDR ASAA11510768Unknown · malfunctionedSTAB OUT OF TRIM LIGHT ILLUMINATED IN FLIGHT. FOLLOWED CHECKLIST AND FOUND AUTOPILOT NOT TRIMMING. MANUAL TRIMMED REMAINDER OF FLIGHT. ACCOMPLISHED FIM TASK 22 11 00 810 801, ACCOMPLISHED DFCS BITE PROCEDURES. ALL FAULTS CLEARED & DFCS BITE TEST PASSED. DSDR AALA20111206LAX01Unknown · unknownLAX - CREW REPORTED AIRCRAFT BECAME DIFFICULT TO CONTROL. AUTOPILOT AND AUTOTHROTTLES BOTH POPPED OFF. DURING THIS TIME THE MACH TRIM INOP LIGHT WAS FLASHING OFF. EMERGENCY DECLARED FLIGHT RETURNED LAX LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICESDR CWQR2011120531Cable Assy · wornDURING AN INSPECTION, FOUND CABLE SAWING INTO THE RUDDER SERVO BRACKET GUARD. THE CABLE WAS FLATTENED AND HAD BROKEN STRANDS. THE CABLE GUARD WAS GROOVED. THE CABLE GUARD AND THE CABLE WERE REPLACED.SDR A6WA201141074Control Cable · out of limitsABNORMAL LEFT TURN OF CONTROL WHEEL DURING FLIGHT OPS. ALL TRIMS CENTERED. INSPECTED AUTOPILOT CONTROL CABLE TENSION 4 FOUND OUT OF LIMITS, ADJUSTED AUTOPILOT CONTROL CABLE TO BE WITHIN LIMITS.SDR CA111214003Autopilot Sys · malfunctioned(CAN) AFTER PASSING TURBULENT CONDITIONS OVER MOUNTAINS AND APPROACHING DESTINATION, DURING CRUISE AT FL30, THE PILOT ENGAGED THE ALT AND HDG UPPER MODES AND APPROXIMATELY 2 MIN. LATER IN CALM CONDITIONS, THE HELO ABRUPTLY ROLLED RT AT 90 FOLLOWED BY A DIVE SDR AALA20111127TUL07Circuit Breaker · defectiveABQ - INFLIGHT DFW-SJC. CREW REPORTED BOTH AUTOPILOTS, YAW DAMPER AND MACH TRIM FAILED. EMERGENCY DECLARED FLIGHT DIVERTED ABQ LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. SWAPPED OUT CIRCUIT BREAKER C17 WITH C15 DUE TO DFGS SWITCH A THAT WAS DESDR 9JLA201112152012Controller · defectiveTHE CREW REPORTED THAT THEY EXPERIENCED AN INTERMITTENT FLIGHT CONTOLLER CHANNEL B FAILURE DURING CRUISE FLIGHT. THE FLIGHT CONTROLLER WAS FOUND TO BE DEFECTIVE. REMOVED THE DEFECTIVE CONTROLLER SN 1112. INSTALLED A MODIFIED UNIT. FUNCTIONAL CHECKS WERE SASDR REXA201100862Autopilot Sys · malfunctionedAP TRIM IS LWD CAUTION MSG IN FLIGHT FOLLOWED BY AP DISCONNECTING. RETRIMMED RE ENGAGED AP AND 1 MIN LATER IT DISCONNECTED AGAIN. PERFORMED OPS CHECK OF AUTOPILOT IAW AMM 22-11-00. ALL OPS CHECKS NORMAL. NO CODES STORED IN FCC. OK FOR SERVICE.SDR ASOA11IA004Warning Message · false activationDURING CLIMB, THE CREW RECEIVED AN AUTOPILOT FAIL MESSAGE ON THE EICAS DISPLAY. THE ACFT RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED SYS AND OPS CHECKS, HOWEVER THE CONDITION COULD NOT BE DUPLICATED NOR DID THE INDICATION ILLUMINASDR 9JLA201112211874Computer · defectiveCREW REPORTED THAT THE AUTO-PILOT PITCH TRIM FAIL ANNUNCIATOR ILLUMINATED WITH THE AUTO-PILOT ENGAGED. TROUBLESHOOTING FOUND THE NR 1 FCC, PN 822-1019-313, SN 262Y DEFECTIVE. INSTALLED A MODIFIED FCC. FUNCTIONAL CHECKS SATISFACTORY.SDR UALA2011112106398Yaw Damper · inoperativeYAW DAMPER UPPER STATUS MSG. UPPER YAW DAMPER INOP, MAYBE DUE TO MODULE FAULT, ACTUATOR FAULT, IRU'S OFF OR IN ALIGN, ENGAGE SW OFF, OR MODULE POWER OFF. CHRONIC ITEM NO TIME. PERFORMED GND TEST PER MEL. INBOUND FAULT 22601. NEED TO ACCOMPLISH FIM 22-21 TSDR UALA2011111606281Control Panel · faultyHEADING SELECT 1ST DIGITS SOMETIMES STICK (WILL NOT MOVE). REPLACED MODE CONTROL PANEL PER MM.
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