JASC 2213
Service difficulty reports · 148
Reports filed under 2213 · Flight Controller, 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 = '2213' 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 = '2213' 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 2023FA0000798Control Tube · shearedAIRCRAFT WAS IN DECENT, WHEN PILOT INPUTTED 1/4 TO 1/2 INCH MOVEMENT OF THE CONTROL WHEEL, CONTROLS BECAME LIGHT FOLLOWED BY THE AIRCRAFT SHAKING VIOLENTLY. THE CONTROL YOKE FLUCTUATED BETWEEN FULL FORWARD AND FULL AFT REQUIRING BOTH PILOT AND INSTRUCTOR PILOTSDR AALA202207057998Control Unit · noneAIRCRAFT WAS GROUNDED: APPROXIMATELY 30 MINUTES PRIOR TO LANDING AUTO FLIGHT, #1 FLIGHT CONTROL UNIT (FCU) ECAM FAULT. QRH SYSTEM RESET OK BUT ONLY 5 MINUTES THEN FAULT RE-OCCURRED. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED AT DFW SAFELY WITHOUT FURTHSDR OEJA202202150001Control Box · faultedWHILE ATTEMPTING T/O FORM JAX TO BNA. IMMEDIATELY AFTER SELECTING T/O POWER, CASS SYSTEM GENERATED A RED "PRIM TRIM INOP" A YELLOW "SEC TRIM FAIL" AND A WHITE "PRI TRIM FAIL". CREW ABORTED TAKE OFF AND TAXIED BACK TO THE FBO. I WAS NOTIFIED RIGHT AWAY AND WE DSDR HALA2022020300033None · noneSHIP 386 - ATO - DUE TO FMA MALFUNCTION. CORRECTIVE ACTION: NO FAULTS FOUND IN PFR. PERFORMED AUTOLAND TEST. PERFORMED RTO INSPECTION. (8452195)SDR YENA2021111800771Fcu · fault messageFLT 20, LHR-JFK. "AUTO FLT FCU 1 FAULT" ECAM MSG ON DESCENT TROUGH 10,000 FT. ; TROUBLESHOT PER TSM 22-81-00-810-802-A. R/R FCU PER AMM 22-81-12. ALL FUNCTIONAL TESTS PASSED AT THIS TIME. TSI C/W.SDR YENA2021061800376Controller · faultedFLT 150, GND-JFK. WHILE AIRBORNE COMING IN FOR LANDING THERE WAS NO LOCALIZER INFO CORRECT FREQ HAND TUNED STILL NO LOCALIZER GLIDE SLOPE DID DISPLAY BUT NO COURSE GUIDEANCE NO FLAGS, ECAMS OR ANY OTHER MESSAGES ; FOUND FMGC2 FAULT ON PFR, RESET FMGC2 PER TSM SDR DALA2021041302176Autopilot Sys · failedSHIP 695 CRUSING AT FL 380 SAW A MOMENTARY PUFF OF SMOKE (5 SEC) BEHIND AUTOPILOT SWITCHS ON MCP. SIMULTANEOUSLY ALTITUDE WINDOW CHANGED TO FL 35.5. AIRPLANE REMAINED LEVEL. ALL LIGHTS ON MCP AT1/2 BRIGHTNESS. NO.ODOR. CORECTIVE ACTION: R/R MCP REF B757 AMM 22SDR ASAA2021022234191Dfgs · failedMODE CONTROL PANEL ALTITUDE WINDOW FLICKERING. GROUNDED - YES. INITIAL EVALUATION, CONFIRMED DEFECT. REMOVED AND REPLACED DFCS MCP IAW B737-900 AMM 22-11-34-000/400-801, FLICKERING STOPPED. PERFORMED DFCS LRU REPLACEMENT FOR MCP AND LAND VERIFY IAW AMM 22-11-0SDR ASAA2021022234189Dfgs · failedHEADING DISPLAY PANEL MODE CONTROL IS FLICKERING. GROUNDED - YES. INITIAL EVALUATION, CONFIRMED DEFECT. REMOVED AND REPLACED DFCS MCP IAW B737-900 AMM 22-11-34-000/400-801, FLICKERING STOPPED. PERFORMED DFCS LRU REPLACEMENT FOR MCP AND LAND VERIFY IAW AMM 22-1SDR 120B2020041500024Display · inoperative#2 FMS (TIMEOUT) MESSAGE & FMS WOULD NOT AUTO SEQUENCE ON THE POSITION REPORT PAGE.SDR AALA2019081539030Controller · unreliableAIRCRAFT WAS GROUNDED: PILOT REPORTS AT FL 37.0 MANAGED SPEED AT .78, SPEED VAIRIES FROM .76. TO .79 CONTINUOUSLY IN SELECTED SPEED MAINTAIN .78. MAINTENANCE REPLACED FLIGHT CONTROL UNIT IAW AMM-22-81-12. OPS CHECKS GOOD.SDR ASAA2019041172894Sensor · faultedWHILE PERFORMING LAND VERIFY AND FMS TC 78222000 - FOUND LEFT AILERON POSITION SENSOR A FAULTY. GROUNDED - YES. PERFORMED AILERON POSITION SENSOR ADJUSTMENT PER B737-900 AMM 22-11-29-820-801, ADJUSTMENT CK'S GOOD. PERFORMED AILERON POSITION SENSOR TEST PER AMMSDR ASAA2019020728126Control Unit · inoperativeFCU 1 INOP GROUNDED - YES. REMOVED AND REPLACED FCU PER AMM 22-81-12. CAT 3 OPS CHECK OK.SDR IPXA2019020138563Computer · odorINSPECTION TYPE:FUMES / ODOR IN COCK PIT. TECH RECOMMENDS: PERFORM BOW TS MD11-3610-00487 TO INSPECT FOR PNEUMATIC DUCT INTGRITY AND TO ASSURE THERE IS NOT ANY FOREIGN OILS. C/W WAN 2859911. C/W WAN 2859911. R/R #2 FCC PER MM 22-11-01-004-026 AND MM 22-11-01-SDR UIEA2017092001749Servo · no testCENTER AUTOPILOT RUDDER SERVO M278 FAIL DURING TEST. THE SERVO WAS REPLACED.SDR UIEA2017092001751Servo · failedRIGHT AUTOPILOT RUDDER SERVO M279 FAIL DURING TEST. THE SERVO WAS REPLACED.SDR RJEF20160419001Fcu · faultyDURING CLIMB OF FLIGHT TA588, THE PILOT REPORTED FCU ALTITUDE UNABLE TO CHANGE ALTITUDES. DUE THAT SITUATION THE ACFT RETURNED. AFTER AN UNEVENTFUL LANDING, ONCE THE ACFT PARKED AT THE GATE, PERFORMED FAULT ANALYSIS IAW TSM 22-81-00-810-801-A. REPLACED THE SDR CA160222005Computer · malfunctioned(CAN) ON DESCENT A "BURNED INSULATION" ODOR WAS NOTED, THE ODOR PERSISTED, BUT NO SMOKE WAS EVIDENT. ON THE GROUND, TROUBLESHOOTING REVEALED THE RT FLIGHT CONTROL COMPUTER HAS INTERNALLY MALFUNCTIONED, CAUSING THE ODOR. THE FCC WAS REPLACED.SDR A6WA201542983Actuator · failedFLIGHT 3926, WITH AUTOPILOT OFF, RECEIVED UNCOMMANED YAW. COMPLIED WITH IAC & QRH, ISSUE CLEARED WITH YAW DAMPER OFF. INTERROGATED FCC & FOUND NR 2 YAW DAMPER FAILED. R & R NR 2 LINEAR YAW DAMPER ACTUATOR IAW AMM 22-22-01. OPS CHECKED GOOD.SDR CA150112002Fmc · failed(CAN) FMGC 2 AND NAV IR2 FAULT ENROUTE. RESET UNSUCCESSFUL.. FMGC 2 CIRCUIT BREAKER RESET. NO HISTORY. AFS BITE CARRIED OUT THROUGH MCDU NO FAULT. SERV - NAV IR2 RESET. GROUND SCAN AND INTERFACE TEST BITES CARRIED OUT THROUGH MCDU. NO FAULT. CONSIDER SERV.SDR CA150105002Fmc · failed(CAN) AFTER DEPARTING WITH FMGC 2 UNDER MEL THE CREW REPORTED THAT FMCG 1 HAD ALSO FAILED. THE FLIGHT RETURNED TO YVR AND LANDED APPROXIMATELY 3000KG OVERWEIGHT. NO EMERGENCY WAS DECLARED. RESOLUTION NAV DATA SOFTWARE FOUND CORRUPT---LAST MONTHS SOFTWARE RELOSDR CA141229005Power Supply · failed(CAN) AIRCRAFT LOST THE FIRST OFFICER`S FLIGHT DIRECTOR, COMMAND BARS LOST AND AUTOLAND STATUS TO NO LAND 3 THE CREW ALSO HAD A FAINT ELECTRICAL ODOR IN THE COCKPIT. ELECTED TO DIVERT AND DECLARED AN EMERGENCY. RT FCC FOUND TO HAVE A BURNED OUT POWER SUPSDR CA141229004Fmc · failed(CAN) AFTER DEPARTURE, EXPERIENCED NR 1 FMGC FAILURE, A PATCH WAS DONE WITH MOC AND CREW ELECTED TO RETURN TO DEPARTURE. FLIGHT LANDED . NR 1 FMGC WAS REPLACED AND OPS TESTED SERVICEABLE IAW AMM 22-83-34 PB 401.SDR CA140926013Fmc · failed(CAN) INCIDENT DETAILS:PAN PAN DECLARED AT 40W DUE TO LOSS OF 2 FMCS. AUTOPILOT SERVICEABLE.REBOOTED SYSTEM,NOW OK,CANX PAN PAN WITH ATC.CARRYING ON RESOLUTION ON THE MAT FOUND MSG 31-83172 NOT ACTIVE. GRND TEST THROUGH MAT TEST PASS. NO FAULT HISTORY.SDR CA140908025Computer · failed(CAN) NON-COMMANDED CHANGE OF FLIGHT DIRECTOR PASSING FL170 IN DESCENT TO FL120, NOTICED CHANGE OF FLIGHT DIRECTOR MODE FROM NAV/VS TO NAV/ALTSCAP, GREEN, WITH A VARIATION OF PITCH FROM -2 DEGREES TO -8 DEGREES, VERTICAL SPEED GOING FROM -2500 FT/MIN TO -4500 SDR CA140827004Fmc · defective(CAN) INCIDENT DETAILS: JUST BEFORE TOP OF DESCENT FMGC 2 FAILED, FMGC 1 WAS ALREADY UNSERVICEABLE AND ON MEL RELIEF. THE CREW DECLARED PAN PAN AND AN UNEVENTFUL LANDING WAS CARRIED OUT. NIL ADVERSE REACTION WAS REPORTED BY THE CAPTAIN. RESOLUTION FMGC #1 (FLSDR DALA2014072904255Annunciator · failedDIVERTED DUE TO SMOKE IN THE COCKPIT. THE CREW REPORTED THE CAPTAIN`S FLIGHT MODE ANNUNCIATOR SMOKING AND ARCING. MAINTENANCE REPLACED THE CAPTAIN`S FMA ALL RTS WERE GOOD.SDR CA140709004Indicator · failed(CAN) CLIMBING IN SPEED MODE WITH THE SPEED BUG SET AT 250 KNOTS THE SPEED BUG MADE AN UNCOMMANDED CHANGE TO 79 KNOTS. NO VERTICAL SPEED CHANGES HAD BEEN MADE RECENTLY ALTHOUGH WE WERE MAKING LATERAL CHANGES OF HEADING AND ALSO INTERCEPTING AN FMS COURSE AROUNSDR CA140926010Computer · malfunctioned(CAN) DURING CLIMB PASSING FL 140. SPEED 290 KNOT. AUTOPILOT ENGAGED (RIGHT PILOT FLYING). SPEED AND NAV. MODE. UNCOMMANDED SPEED CHANGE OBSERVED. SPEEDBUG, JUMPED FROM 290 TO 60 KNOT. FMA SHOWING PITCH - MODE. SPEED MODE REENGADED AND 290 KNOT SET. EVENT BUTSDR CA140306007Control Panel · failed(CAN) UNCOMMANDED FD CHANGE: A SPEED BUG.SDR CA140306006Control Panel · malfunctioned(CAN) UNCOMMANDED FD CHANGE: A FLIGHT MODE CHANGE.SDR SWIA201436230Circuit Card · failedAUTOPILOT PITCH TRIM CAUTION, AIRCRAFT PITCHED DOWN WHEN AUTOPILOT DISCONNECTED. FLT 2583 REPLACED NR 2 FCC CARD IAW AMM, PN 622-9815-904, SN ON 12TBG & SN OFF 1F3J.SDR CA140207003Director · malfunctioned(CAN) FLIGHT DIRECTOR UNCOMMANDED CHANGE. ON CLIMB, SPEED WENT FROM 280 KTS TO 040 KTS.SDR SWIA201335769Control Panel · failedAIRCRAFT OSCILLATES UP & DOWN WHEN USING AUTOPILOT. AIRCRAFT FLIES NORMALLY WHEN AUTOPILOT SELECTED OFF. FLT 5652 REPLACED FCP IAW AMM & REPLACED BOOTH FCC CARDS IAW AMM. PN1 822-0044-001, SN1 ON 414, SN1 OFF 18G8Y, PN2 822-1308-320, SN2 ON 21H1N, SN2 OFF 3SDR CA131118017Indicator · erratic(CAN) ON GPS APPROACH, VFR CONDITIONS, THE PILOT NOTICED THAT THE FLIGHT COMMAND INDICATOR WAS OSCILLATION VERTICALLY PRIOR TO THE AUTO PILOT DISCONCERTING. THE APPROACH WAS CARRIED OUT MANUALLY WITH OUT INCONTINENT. MAINTENANCE REPLACED THE FLIGHT COMMAND INSDR CA131101010Indicator · inoperative(CAN) ON ENGINE START UP AND TAXI THE PILOT NOTICED THE FLIGHT COMMAND INDICATOR NOT RESPONDING TO THE ACFT MOVEMENT. THE ACFT RETURNED TO THE BLOCKS AND MAINTENANCE REPLACED THE UNIT WITH AN O/H UNIT. THE SYSTEM FUNCTION CHECKED SERVICEABLE.SDR CA130621001Director · failed(CAN) DURING CLIMB THROUGH 31,600 CREW OBSERVED PITCH UP COMMAND ON THE FLT DIRECTOR, WITH SPEED INDICATING 59 KTS. SPEED BUTTON SHOWED. 17 KTS. EVENT BUTTON PUSHED AT 1757Z DEFECT RAISED TO PROVIDE DATA FOR OPERATOR ACTION IAW SL 440-SL-22-014A WITH DEFECT NRSDR SIMA20130309001Controller · malfunctionedON FLIGHT 3570 THE CREW REPORTED AN ELECTRICAL ODOR FROM THE COCKPIT. THE AIRCRAFT WAS REMOVED FROM SERVICE. VERIFIED STRONG ELECTRICAL BURNT SMELL FROM THE FLIGHT GUIDANCE CONTROLLER. REMOVED AND REPLACED THE FLIGHT GUIDANCE CONTROLLER IAW AMM II CH 22-11-SDR SIMA20130303001Controller · faultyON FLIGHT 2830 THE CREW REPORTED AN UNIDENTIFIABLE ODOR IN THE COCKPIT- POSSIBLY ELECTRICAL. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND ODOR TO BE ORIGINATING FROM THE FLIGHT GUIDANCE CONTROLLER. REMOVED AND REPLACED THE FLIGHT GUIDANCE CONTROLLER IAW EMB-SDR SIMA20130211002Controller · malfunctionedON FLIGHT 3307 THE CREW REPORTED THAT ON FINAL APPROACH THEY NOTICED STRONG ELECTRICAL FUMES IN THE COCKPIT. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND ELECTRICAL SMELL COMING FROM AUTOFLIGHT GUISDR CA130118011Control Panel · failed(CAN) AFTER DEPARTURE, THE FLIGHT CREW ENCOUNTERED FAILURES OF BOTH FLIGHT DIRECTORS AND THE AUTOPILOT SYSTEM. THE FLIGHT CREW DIVERTED BACK AND LANDED APPROXIMATELY 3000 KGS OVER THE MAXIMUM STRUCTURAL LANDING WEIGHT. THERE WAS NO EMERGENCY DECLARED AND THERSDR 2013F00012Potentiometer · malfunctionedSMOKE COMING FROM AUTOPILOT CONTROLLER.SDR UALA2012111406557Fcu · malfunctionedFCU DISPLAY MALFUNCTIONING CLIMB-DESCENT. VERTICAL SPEED WINDOW SHOWS ZEROS IN OPEN CLIMB. REPLACED FCU PER MM WITH KNOWN GOOD UNIT FROM ACFT 4019. ACCOMPLISHED OPERATIONAL TEST OF THE AFS PER 22-96-00 AND LAND CAT III CAPABILITY TEST PER MM 22-97-00, OPS SDR GN0A20120930001Control Panel · failedAUO TO (UOX): AFTER TAKEOFF WHILE CLIMBING THROUGH 3500FT THE AUTO-PILOT WAS ENGAGED. WHEN PASSING 5000FT THE LEFT FLIGHT DIRECTOR BARS PITCHED DOWN 2.5° WHICH CAUSED THE AUTO-PILOT TO COMMAND THE AIRCRAFT FOLLOW. THE LEFT AUTO-PILOT WAS DISENGAGED AND AIRCSDR USAA2012032600034Fcu · malfunctionedELECTRICAL & CHEMICAL ODORS DETECTED ON FLIGHT DECK. REMOVED AND REPLACED FLIGHT CONTROL UNIT PER AMM 22-81-400-001. OPS CHECKED GOOD.SDR USAA2012010600001Fcu · defectiveAT GATE IN CLT, SMOKE (PERCEIVED AS ELECTRICAL) WAS COMING FROM MODE CONTROL PANEL. HAD TO SHUT OFF ALL ELECTRICAL TO GET IT TO STOP. MAINTENANCE REMOVED AND REPLACED THE FLIGHT CONTROL UNIT IAW AIRBUS MAINTENANCE MANUAL 22-81-12-0401.SDR UALA2012010400085Servo Valve · no testLEFT AILERON SERVO FAILED OPERATIONAL TEST AND FCC BITE TEST. REMOVED SERVO IAW AMM. INSTALLED LT LCCA SERVO VALVE PER AMM. LEAK CHECKED GOOD, FAILED OPERATIONAL TEST WITH CMCS MESSAGE "AILERON SERVO-L, FCC-L INTERFACE FAIL SERVO POSITION 22055." REPLACED SDR E81R2011122232191Circuit Card · failedFLIGHT CREW REPORTED ACFT STARTED "PORPOISING" +/- 300 FT AT 800 FPM WHILE IN CRUISE FLIGHT AT FL400. COPILOT'S SIDE DISPLAY SIMULTANEOUSLY DISPLAYED "PITCH TRIM FAIL" INDICATION. ACFT DIVERTED. FOUND ELEVATOR CABLES AND ELEVATOR SERVO BRIDLE CABLE TENSIONSSDR SIMA201135503Controller · malfunctionedON FLIGHT 4554 THE CREW REPORTED THAT AT 30,000 FEET IN LIGHT CHOPPY WEATHER HAD AN UNCOMMANDED RIGHT TURN FOLLOWED BY RED "AP" ON PFD AT 2,500 FEET. THE AIRCRAFT YAWED NOSE RIGHT WITH ONLY YAW DAMP ON. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND RESDR HALA2011101000447Computer · faultedETOPS SIGNIFICANT SYS - FLIGHT CONTROL COMPUTER FAULTED. R & R FLIGHT CONTRL COMPUTER IAW AMM 27-93-34. OPS CHECKED & TESTED GOOD IAW AMM 27-93-00.
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