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 SWIA201438457Autopilot Sys · malfunctionedUNCOMMANDED STAB TRIM MOVEMENT WITH AUTOPILOT ENGAGED.SDR ASAA2014062908387Selector Panel · failedTHE ALTITUDE SELECTOR ON THE MCP WILL NOT CHANGE ALTITUDES. ACFT GROUNDED. CONFIRMED FAULT, MCP ALTITUDE NUMBERS FROZEN. PULLED AND RESET "MCP DC2" CIRCUIT BREAKER AT P6-2 PANEL, MCP ALTITUED SELECTOR WILL FUNCTION FOR A WHILE THEN FREEZES UP. REPLACED DFCSDR HALA2014062500094Control Panel · failedALT WINDOW ON MCP PANEL INOPERATIVE FROZEN. REPLACED MODE CONTROL PANEL PERMORMED TESTS 1-4-30-40 MCP OPS NORMAL ACFT REMAINS LAND 3 STATUS.SDR CALA2014062791338Autopilot Sys · malfunctionedALL AUTO PILOTS DISCONNECTED & NO LAND 3 STATUS MSG. CMC FAULT DOWNLINKED AUTOPILOT BACKDRIVE RT. BACKDRIVE SYS INOPERATIVE OR DEGRADED DUE TO FAILURE IN RT COLUMN. CREW CYCLED CB AS NO AUTOPILOTS WOULD ENGAGE. THE CYCLING OF THE BREAKER ALLOWED THE AUTOPISDR ASAA2014062508352Autoland Sys · malfunctionedHGS AUTOLAND FAILED. LANDED TO FAR RT OF CETER LINE HALFWAY BETWEEN CENTER LINE AND RUNWAY EDGE. ACFT GROUNDED. PERFORMED FIM 22-11, TASK 825, PERFORMED LAND VERIFY TEST, AMM TASK 22-11-00-700-801. NO FAULTS. NO HISTORY LAST 30 DAYS. PERFORMED HGS SYS TESTSDR SIMA20140624005Autopilot Sys · malfunctionedIN CRUISE AT FL190 AUTO PILOT ENGAGED. AUTO PILOT LAGGED FLIGHT DIRECTOR RESULTING IN 400 FPM CLIMB & 500 FPM OSCILLATIONS, FROM CAPTURED ALTITUDE, 1/8 INCH GAP BETWEEN FLIGHT DIRECTOR & ACFT SYMBOL. LEVELED AT 2100 FT ON APPROACH & AGAIN WITH GLIDESLOPE CAPSDR ASAA2014062208309Warning Message · illuminatedAT 150 FEET RA ON ILS 34R, BOTH PITCH AND TEERING BARS DISAPPERED FROM CAPT AND F/O'S PFDS. ACFT GROUNDED. NR 1 AND NR 2 DFCS LOGGED NO FAULTS, REF FIM 22-11, TASK 801. PERFORMED LAND VERIFY TEST REF MM 22-11-00/201, BITE GROUP 49 ALL TESTS PASSED. ACFT REMSDR CALA2014062491332Warning System · false activationYAW DAMPER 2 FAULT AFTER ENG START. CYCLED 2 FAC SWITCH & RESET CB FAULT CLEARED & BITE CHECKED OK IAW AMM22-96-00.SDR ASAA2014061908290Selector · malfunctionedMCP ALTITUDE SELECTOR INOPERATIVE, NUMBERS IN ALTITUDE WINDOW FROZEN. ACFT GROUNDED. MCP CHECKED NORMAL IAW FIM 22-11TASK 80, ALT SELECTOR. OPS CHECKED NORMAL.SDR HAEA2014061900228Amplifier · failedNEARING THE END OF CRUISE FLT EN ROUTE TO RFD CREW REPORTED AN ELEC SMELL IN THE COCKPIT. THE AUTOPILOT AMP HAD FAILED & WAS THE PROBABLE SOURCE OF THE SMELL. REPLACED AUTOPILOT AMP & TESTED THE SYS NO DEFECTS NOTED OR SMELLS.SDR USAA2014061900004Actuator · leakingON DESCENT THRU 12,000 FT TO 9,000 FT, A DISTINCT METALLIC DIRTY SOCK ODOR IN COCKPIT. ODOR DISSIPATED AT 9,000 FT. THE YAW DAMPER LEAKING. R & R YELLOW SYS YAW DAMPER ACTUATOR IAW AMM 27-26-51. OPERATIONS & LEAK CHECKED GOOD. ALSO, R & R YELLOW RESERVOIR SDR ASAA2014061608231Control Panel · failedHEADING SELECT BUG WILL NOT MOVE WHEN HEADING SELECT KNOB IS TURNED. ACFT GROUNDED. REPLACED MODE CONTROL PANEL IAW AMM 22-11-34-00-801 AND 22-11-34-400-801. ACCOMPLISHED MCP INSTALLATION TEST IAW AMM 22-11-34-740-801. ALL TESTS PASSED.SDR CA140611002Autopilot Sys · failed(CAN) CREW DISCOVERED AN UNUSUAL PITCH UP MOVEMENT AND CHECKED THE SPEED BUG WHICH HAD MOVED FROM 252 KNOTS TO AROUND 50 KNOTS.SDR ASAA2014060208020Circuit Breaker · trippedMCP DC1 CIRCUIT BREAKER IS OUT. ACFT GROUNDED. VERIFIED CIRCUIT BREAKER IS OPEN. ACCESSED P18-1 AND ACCOMP G.V.I. OF CIRCUIT BREAKERS NO DEFECTS NOTED. CLOSED P18-1 AND CLOSED CIRCUIT BREAKER. ACCOMPLISHED MCP INST TEST, TEST PASSED IAW MM 22-11-34-740-80SDR ASAA2014052807962Computer · faultedAUTOPILOT B DISENGAGED DURING DESCENDING TURN FOR NO APPARENT REASON. ENGAGED AND HAD TO DO IT AGAIN IN DESCENDING TURN. ACFT GROUNDED. CYCLED SMYD 2 CMPTR DC "SPD LIM" FLAG OUT, MSG 27-32000 GONE. R & R NR 2 SMYD REF MM 27-32-42-400-801. ACCOMPLISHED LANDSDR USAA2014052700039Relay · defectiveTHREE DIFFERENT TIMES, AT CRUISE, AT INITIAL DESCENT & LEVEL ON APPROACH, GOT SHARP QUICK UNCOMMANDED RUDDER INPUTS. RUDDER PEDALS DID NOT MOVE & NO RUDDER TRIM MOVEMENT OBSERVED. SHUT OFF FAC 1 & IT APPEARED TO CORRECT. REPLACED RELAY RTL SYS 1, 13CC1 IAW SDR ASAA2014052107892Annunciator · no testWHILE ACCOMPLISHING EMG, FOUND AUTOFLIGHT STATUS ANNUNCIATOR PANEL ON F/O'S SIDE, AUTOPILOT WILL NOT TEST IN RED. ACFT GROUNDED. REPLACED F/O'S ANNUNCIATOR PANEL. TEST PASSED IAW MM 22-11-32-400-801.SDR ASAA2014051707864Control Panel · failedBANK SELECTOR KNOB, MODE CONTROL PANEL 25 & 30 ONLY. ACFT GROUNDED. REPLACED MCP IAW MM 22-11-34, OPS CHECKED NORMAL. ACCOMPLISHED DFCS LRU MCP NR 32 TEST, LAND VERIFY NR 49, & HGS FCC/AT SENSOR TEST, ALL TEST NORMAL IAW MM 22-11-34, 22-11-00, & SMM:34-36-SDR USAA2014051900007Fcu · malfunctionedSMOKE IN COCKPIT FROM FCU AREA. CREW DECLARED AN EMERGENCY & RETURNED TO FIELD. FLIGHT LANDED WITHOUT INCIDENT & TAXIED TO THE GATE UNDER ITS OWN POWER. R & R FCU IAW AMM 22-81-12-0401. OPERATIONS CHECKED OK IAW AMM 22-10-00-0501. PERFORMED AFS & LAND TESSDR AALA20140514004Circuit Breaker · poppedTUL INFLIGHT LIT DFW. CREW REPORTED AUTOPILOT & AUTO-THROTTLE DISCONNECTED FOLLOWED BY UN COMMANDED OSCILLATION IN YAW. ALSO GEAR UNSAFE LIGHT ILLUMINATED. EMERGENCY DECLARED FLIGHT DIVERTED TUL LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACEDSDR CALA2014051391019Status Message · activatedNO LAND 3 STATUS, LT FCC FAIL. IAW MM 22-10-00 ACCOMPLISHED MCP & FCC TESTS ACFT DOWNGRADED TO CAT 1 STATUS IAW SEQ 5576 001. NEED TO ACCOMPLISH GND RECERTIFICATION TO RESTORE ACFT TO FULL CAT 2 - 3 CAPABILITY STATUS.SDR CA140730017Tube · worn(CAN) DURING A TRIM SERVO REPLACEMENT. THE TRIM TUBE ASSEMBLY WAS RUBBING ON A RIVET LOCATED ON THE ELT SHELF IN THE TAIL OF THE AIRCRAFT. THE TUBE HAS A WALL OF 0.035" OF THICKNESS. TUBE WAS WORN TO A WALL THICKNESS OF APPROX 0.10" THICK. TRIM TUBE WAS REPLACSDR SWIA201437520Servo · failedAUTO PILOT DISCONNECTED ON ILS APPROACH MODE AFTER MAKING UNCOMMANDED TURN TO THE RIGHT. R & R AILERON SERVO AND FCC 2 22-12-14. PN ON/OFF 622-4404-101, SN ON 267TH, SN OFF D93V, PN ON/OFF 622-9815-904, SN ON 10NRV, SN OFF 17GN.SDR ASAA2014050607713Computer · failedSPEED TRIM FAILED, MACH TRIM FAILED SINGLE CHANNEL ONLY. ACFT GROUNDED. TROUBLESHOT IAW FIM 22-11, TASK 801. REPLACED FCC "A" IAW MM 22-11-33. FCC A BITE 35 NORMAL. PERFORMED SPEED TRIM BITE 60.32 & MACH TRIM BITE 60.33. BOTH TEST NORMAL. PERFORMED LAND SDR QXEA2014050500394Module · malfunctionedWITH AUTOPILOT ENGAGED AND NAVIGATING DIRECTLY TO FMG VOR, AND DESCENDING AT APROXIMATELY 1700 FT PER MINUTE, A MOMENTARY AILERON MISTRIM MESSAGE APPEARED AND THE AIRPLANE BEGAN TO GO INTO A 15-20 DEGREE RT BANK AND PROCEED OFF COURSE. AFTER DISCONECTING THE SDR CA140502003Autopilot Sys · failed(CAN) SHORTLY AFTER TAKEOFF, FLIGHT CREW UNABLE TO ENGAGE AUTO-PILOT. FLIGHT HAD DEPARTED WITH 1 INOPERATIVE ON MEL, BUT APPARENT FAILURE OF ALL 3 OCCURRED. WORKED WITH MOC FOR POSSIBLE RE-SETS, BUT UNABLE. RETURNING TO STATION, AND IS EXPECTED TO LAND APPROXSDR CA140501002Autopilot Sys · failed(CAN) AFTER TAKEOFF, AUTO FLT YAW DAMPER 2 ECAM. ALSO, LOST FD2 AND HAVE NO AUTOPILOT 1 OR AUTOPILOT 2. CONVERSED WITH MOC FOR POSSIBLE RESETS. UNABLE RESET. ELECTED TO DIVERT AND WILL LAND APPROXIMATELY 5.0 TONES OVERWEIGHT. PERFORMED RESET OF FAC 1 AND 2SDR ASAA2014043007652Autoland Sys · malfunctionedAUTOLAND TEST UNSATISFACTORY, ACFT TOUCHDOWN WELL OF CENTERLINE. ACFT GROUNDED. PERFORMED FCS FLIGHT FAULT REVIEW IAW FIM 22-11, TASK 801 AND HGS FLIGHT FAULT REVIEW IAW 34-36-00, NO FAULTS NOTED. PERFORMED LANDING, VERIFY 22-11-00/201 AND MMR/ILS DFCS TESTSDR ASAA2014042907643Display · inoperativeAFTER GPU POWER FAILURE, THE AFDS PANEL WAS BLANK. ACFT GROUNDED. CYCLED MCP POWER 1 & 2 MCP LIGHTS, OPS NORMAL, REF DFCS LRU REPLACEMENT TEST MM 22-11-00. ACFT REMAINS CAT 3 AUTOLAND & HGS, SCREW REFLECTS SAME.SDR QXEA2014042700335Autopilot Sys · malfunctionedTHE ACFT FAILED TO FOLLOW AN FMS RIGHT TURN TO DOWNWIND AT SEA. ONE SECOND LATER THE AUTOPILOT DISCONNECT WARNING SOUNDED WITH ASSOCIATED LIGHTS. A/P DISCONNECT BUTTON WAS PUSHED TO SILENCE THE WARNING WHILE AN ATTEMPT TO FLY THE ACFT BACK ON COARSE BY HAND SDR FDEA201404260901Unknown · malfunctionedAUTOPILOT FAILED TO CAPTURE ALT SEVERAL TIMES DURING CLIMB OUT IN PROFILE. RATE OF CLIMB WAS BETWEEN 3000 & 4000 FT PER MIN. ALSO, CAPTURES ALT VERY SLUGGISH, TENDS TO FLUCTUATE - 500 FEET FOR ABOUT A MIN BEFORE FINALLY CAPTURING ALT. DURING DESCENT IN PROFSDR ASAA2014042507571Warning Message · false activationAUTOLAND UNSATISFACTORY. FLARED HIGH, BALLOONED, DRIFTED RT OF CENTERLINE, LANDED LONG, AROUND 2500' FROM RUNWAY END. ACFT GROUNDED. NO HISTORY 30 DAYS. ACCOMPLISHED DFCS FLIGHT FAULT REVIEW IAW FIM 22-11-801 & HGS FAULT ISOLATION IAW SMM 34-36-00, ONLY FAUSDR ASAA2014042307565Control Panel · failedAUOPILOT COMMAND B BUTTON WILL NOT ILLUMINATE. ACFT GROUNDED. REPLACED MODE CONTROL PANEL IAW AMM 22-11-34-000-801 AND 22-11-34-400-801, OPS CHECKED GOOD.SDR HALA2014042200053Autopilot Sys · malfunctionedLOSS OF LEFT FLT DIRECTOR AUTO PILOT DISCONNECT, SELECTED "R", OPS NORMAL. ACCOMPLISHED MCDP GROUND TEST 40 IAW FIM 22-02-00. NO FAULT NOTED ON TEST. CAPTAIN'S INSTRUMENT SOURCE SELECTOR RETURNED TO NORMAL POSITION. LMP STATUS REMAINS "LAND 3". OK FOR SERVISDR HALA2014042100049Warning Message · false activationADVANCING THROTTLES DURING TAKE OFF, ECAM AUTO THRUST FAULT. RETURN TO GATE. RTO 10 KTS. PERFORMED AFS AND LAND TEST IAW AMM 22-96 AND 22-97. SYSTEM OPS NORMAL. OK FOR SERVICE.SDR SWIA201437133Actuator · failedYAW DAMPER NR 2 KEEPS DISCONNECTING AND WHEN ENGAGED CAUSES UNCOMMANDED RUDDER MOVEMENT. R & R YAW DAMPER NR 2 LINEAR ACTUATOR IAW AMM, PN ON/OFF: 622-9968-001, SN ON: 2497, SN OFF: 2561.SDR ASAA2014040907494Switch · out of positionAUTOPILOT AB WOULD NOT ENGAGE AFTER TAKE OFF. FOUND AUTOPILOT STAB TRIM SWITCH IN CUTOUT POSITION, WORK NORMAL WITH SWITCH IN NORMAL. ACFT GROUNDED. PERFORMED DFCS LAND VERIFY GRP 49, IAW MM 22-11-00 AND HGS SYS TEST, IAW SMM 34-36-0. GROUND VERIFICATION SUSDR N6WA201404003001Yaw Damper · faultedYAW DAMPER NR 2 INOPERATIVE STATUS MESSAGE. DEFERRED YAW DAMP NR 2 IAW MEL 22-22-01 CAT C.SDR ASAA2014033107379Control Panel · malfunctionedMODE CONTROL PANEL IS BLANK. ACFT GROUNDED. CYCLED MCP DC1 AND DC2 CIRCUIT BREAKERS. MCP RETURNED TO NORMAL. NO HISTORY. MODE CONTROL PANEL BITES NORMAL IAW GRP 32-22-11-34/501. LAND VERIFY TESTS NORMAL BITE GRP 49 22-11-00/201. HGS SENSOR TEST NORMAL RESDR ASAA2014032607322Autoland Sys · malfunctionedDURING AUTOLAND & HGS AP, ACFT LANDED OVER 36' RT OF CENTERLINE. HGS SYSTEM LOOKED ACCEPTABLE. ACFT GROUNDED. PERFORMED DFCS FAULT REVIEW IAW FIM 22-11, TASK 801, NO FAULTS. PERFORMED LWMP TESTS IAW MM 22-00-01: DFCS LAND VERIFY BITE GP NR 49 AND HGS SYSTESDR CALA2014032690696Autopilot Sys · malfunctionedDIVERT TO LAX DUE TO AUTO FLIGHT CONTROL ISSUE.SDR WX0A071895Control Panel · faulty15 MIN FROM DESTINATION LEAVING 15000' WE LOST BOTH CAPTAIN'S & FLIGHT OFFICER'S FLIGHT DIRECTORS, AUTOPILOTS & AUTO THROTTLES DISENGAGED. WE RAN QRH & SWITCHED TO NR 1 DFGS. ALL SYS WERE NORMAL UNTIL WE GOT ONTO THE APPROACH. ABOUT 15 MILES OUT ON THE APPRSDR ASAA2014032007258Computer · malfunctionedTHE SPEED LIMIT LIGHT ON THE PFD CAPTAIN SIDE, AUTO SLAT FAIL LIGHT AND MACH TRIM LIGHT ON RECALL. ACFT GROUNDED. PERFORMED FCC INSTALLATION TEST REF AMM 22-11-33. ALL TEST PASSED. NO HISTORY PAST 30 DAYS. CYCLED ACFT POWER.SDR CHQA20140314084Switch · faultyCREW REPORTED THAT THEY RECEIVED A PITCH TRIM MAIN INOPERATIVE MSG IN FLIGHT. THE CREW RETURNED TO FIELD & LANDED WITHOUT INCIDENT. MX REPLACED THE AUTO PILOT DISCONNECT SWITCH. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.SDR UIEA2014031400104Unknown · malfunctionedNON-COMMANDED AILERON INPUT, NON-COMMANDED RT AUTOPILOT ENGAGEMENT, NON-COMMANDED VS ENGAGEMENT, NON-COMMANDED HEADING HOLD & NON-COMMANDED STAB TRIM RUNAWAY FULL NOSE UP. FOUND FAULT INDICATION ON RT AILERON STAB TRIM MOSUDE, RESET & ALL INDICATIONS RETURNEDSDR ASAA2014030907122Warning Light · illuminatedSPEED TRIM FAIL LIGHT ON AFTER ENGINE START. ACFT GROUNDED. WHEN PERFORMING FIM TASK 22-11, TASK 801, DFCS SYSTEM BITE, UNABLE TO ENTER BITE TEST DO TO CODE 22-11363. PULLED FCC-A DC CIRCUIT BREAKER & RAN BITE FOR "B" CHANNEL ONLY. RESET FCC-A DC C/B & OPENSDR HYTA2014F00084Servo · failedSERVO, FAILURE OF THE TACH GENERATOR.SDR YENA20140305049Computer · failedAIRCRAFT DIVERTED, LOSS OF GPS DATABASE 180 DEGREES OFF IN FLIGHT. ACCOMPLISHED AFS TEST AND FOUND FMGC NR 2 FAILED. R & R NR 2 FMGC IAW MM 22-83-34. AFS TEST NORMAL.SDR O2JA2014F00092Computer · failedPILOTS REPORTED THAT THE YAW DAMPER, WHEN ENGAGED, THE BALL WAS WAY OUT TO THE LEFT, WHEN DISENGAGED HAD TO RETRIM ACFT, WHEN ENGAGED SECONDARY YAW DAMPER WITH SAME RESULTS, DISENGAGED AGAIN TRIMMED ACFT AND ENGAGED AUTO PILOT WITH THE AUTO PILOT AND NOTICESDR ASAA2014030307060Control Panel · failedENGAGE LIGHT FOR THE VNAV SWITCH ON THE MCP IS INTERMITTENT. ACFT GROUNDED. REPLACED MCP, REF AMM 22-11-34/401. INSTALLATION TEST, LRU REPLACEMENT TEST FOR MCP BITE GROUP NR 32, LAND VERIFY BITE GROUP NR 49, AND HGS SENSOR TEST FOR FCC/AT ALL PASS. ACFT REM
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