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 CA111005004Control Unit · failed(CAN) FLIGHT CONTROL UNIT (FCU) NAVIGATION EQUIPMENT, (AUTO PILOT, FLIGHT DIRECTOR, AUTO-THRUST, ALTIMETER) FAILURE IN DESCENT. CFR ON STANDBY FOR ARRIVAL. FCU REPLACED IAW AMM 22-81-12 PB401. AFS AND LAND TEST OK.SDR JJBA20110909002Control Unit · intermittentFLIGHT CREW REPORTED F/O NAVIGATION SOURCE SWITCHES FROM V LOC TO AUX RANDOMLY IN FLIGHT. MX R & R THE AFCS CONTROL. PERFORMED OPS CHECK AND WAS SATISFACTORY.SDR IXXA110054OController · malfunctionedDURING CRUISE, 30 MIN INTO FLIGHT, AUTOPILOT DISCONNECTED AND WOULD NOT RECONNECT. THE CREW RETURNED . MX REPLACED AUTOPILOT CONTROLLER. OPS CHECKED GOOD IAW MM 22-10-2. ACFT RETURNED TO SERVICE.SDR E81RJT230313Circuit Card · faultyFLIGHT CREW REPORTED RECEIVING A RED "AP PITCH TRIM FAIL" INDICATION ON CLIMBOUT. VERIFIED FAULT IN NR 1 AUTOPILOT SYS FCC-4007 FLIGHT CONTROL COMPUTER CARD. REPLACED FCC-4007 CARD WITH AN O/H CARD, AUTOPILOT/ FLIGHT DIRECTOR, AND PITCH TRIM OPS CHECK NORMALSDR CA110124005Electronic Unit · unserviceableGOING THROUGH 15000 UNCONTROLLED TAIL OSCILLATION BACK AND FORTH - DISCONNECTED AUTOPILOT STILL OSCILLATIONS - CALL FROM F/A - VERY VIOLENT IN TAIL- SLOWED ACFT & STOPPED - NO WARNING LIGHTS. ON INVESTIGATION FOUND RT YAW DAMPER CHANNEL FAILING TEST, WITH INOSDR YENA20110103174Computer · faultyFLT 735 JFK-BQN AIR RETURN JFK AUTO FLT FAC 1 FAULT ECAM WITH SMOKE SMELL IN COCKPIT. ACCOMPLISHED INSPECTION FOR BURNING SMELL IAW 24-00-00-810-823. IDENTIFIED SMELL AS FAC 1 COMPUTER, REMOVED AND REPLACED FAC 1 COMPUTER IAW 22-66-34-04. OPS CHECK GOOD IAWSDR C2XA10IA325Controller · overheatedIAH - FLIGHT 3026, DURING PREFLIGHT INSPECTION THE CREW REPORTED A BURNING SMELL COMING IN THE COCKPIT. MAINTENANCE INSPECTED THE COCKPIT, REMOVED AND REPLACED THE GUIDANCE CONTROLLER, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RESDR UALA2010120604465Servo · faultyNO LAND 3 MESSAGE DISPLAYED INFLT. EFI NO LUCK. CAPT INST SOURCE SEL C CLEARED MESSAGE. LAST FLT FAULT RUDDER SERVO FCC L CODE 111481. REPLACED LT AUTOPILOT ROLLOUT GUIDANCE SERVO ACTUATOR. OP CHECKED GOOD. LEAK CHECKED GOOD.SDR GTIA1000085Autopilot Sys · burnedFAC 1 & 2 FAULTS ALSO HAD BURNED ODOR IN COCKPIT.SDR YENA20100811112Fcu · failedFLT 271 LAS-BUR, CREW REPORTED UNCOMMANDED RUDDER DEFLECT OF 1 DEGREE AT 8K FEET NAV/AP ON. NO LOSS OF CONTROL ON AIRCRAFT. REMOVED AND REPLACED FCU PER AMM 22-81-12-04. OPS CHECK GOOD. NO FAULTS PRESENT A/P 1&2.SDR F3LA2009080300124Control Unit · defectiveCREW MADE AN AIR RETURN, DUE TO THE ALTITUDE SELECTOR KNOB ON THE FLIGHT CONTROL UNIT BEING STUCK ON AN ALTITUDE, RENDERING THE AUTO-PILOT, AUTO-THRUST AND FLIGHT DIRECTORS TO AN UNAVAILABLE STATE. MX REMOVED AND REPLACED THE FLIGHT CONTROL UNIT AND PERFORMED SDR VNAA2009060900003Computer · failedCREW REPORTED A FD 2 STATUS MSG AND RETURNED TO CLT WITHOUT INCIDENT. MAINTENANCE INTERROGATED MDC AND FOUND FCC NR 22 DASHED OUT. MAINTENANCE REMOVED AND REPLACED FCC NR 2, PERFORMED OPS CHECK PER AIRCRAFT MAINTENANCE MANUAL AND AIRCRAFT WAS RELEASED FOR SESDR USAA2009052891311Transformer · burnedFLT 1729-LGA - SMOKE - FLIGHT CREW REPORTEDLY OBSERVED SMOKE COMING OUT THE FLIGHT CONTROL UNIT. MAINTENANCE REMOVED AND REPLACED THE FCU PER AIRBUS MAINTENANCE MANUAL 22-81-12-991-002. VENDOR TEARDOWN REPORT INDICATES THE T1 AND T2 TRANSFORMERS IN THE FCU SDR CA090421011Computer · malfunctioned(CAN) AT 130 KTS, RUDDER KICK ACFT VEERED LT ON TAKEOFF. ACFT CONTROLLER AND NO PROBLEMS AIRBORNE. REMOVED UNITS: YAW DAMPER ACTUATOR, PN SC4700-3, SN 435, INSTALLED 2007-05-08. IT HAD 53994 FH, 6796 FH TSI. FLT AUGMENTATION COMPUTER, PN B397BAM0513, SN 56SDR ASAA0954699Computer · malfunctionedAFTER ENG START W/ENG GENERATORS ON THE BUSSES FLT CONTROL MASTER CAUTION LIGHT ILLUMINATED ON RECALL. SPD TRIM FAIL AND MACH TRIM FAIL LIGHTS ILLUMINATED ON OVERHEAD FD FLAG ILLUMINATED ON CAPTAIN'S EADI. AFCS SYS A WARN LIGHT (BAT) C/B POPPED ON P18 PANEL.SDR AALA2009021501033Computer · malfunctionedMIA - EMERGENCY DECLARED ON ACCOUNT OF FLIGHT CONTROL PROBLEMS. RETURNED MIA WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. AIRCRAFT HAD UNCOMMANDED PITCH TRIM INPUTS WITH AUTO PILOT OFF. REPLACED FLIGHT CONTROL COMPUTER AND ANGLE OF ATTACK SENSOR 0861FLSDR USAA920081832Fcu · defectiveFLT 1180 PDX-PHL, APPROXIMATELY 5 MINUTES AFTER TAKEOFF, SMOKE STARTED COMING OUT OF CENTER GLARESHIELD PANEL (AUTOPILOT PANEL). WE TURNED OFF BACKGROUND LIGHTS AND RETURNED TO PDX. SMOKE STOPPED SHORTLY AFTER TURNING OFF BACKGROUND LIGHTS. MX R&R THE FLT CSDR AALA200801181Control Module · inoperativeSJU INFLIGHT T660/02MAY SXM TO JFK - WITH CENTER AUTO PILOT ON CREW REPORTED A PITCH UP. FOLLOWED BY EICAS MESSAGE AND MASTER CAUTION LIGHT. AUTO PILOT WENT OFF. REPLACED CENTER FLIGHT CONTROL COMPUTER AND LEFT AND RIGHT STABILIZER TRIM AILERON CONTROL MODUSDR QMLA7216Computer · burnedTHE AIRCRAFT ROLLED VERY SLIGHTLY TO THE RT AND THEN TO THE LT. THE ROLL RATE WAS CASUAL, AND SINCE WE WERE FLYING IN SLIGHTLY GUSTY CONDITIONS I TOOK ALMOST NO NOTICE OF IT. THEN THE AIRCRAFT DID IT AGAIN. THIS TIME THE ROLLS WERE ACCOMPANIED BY THE STRONG ODSDR C2XA07IA224Controller · malfunctionedIAH - FLIGHT 2170, THE CREW REPORTED THAT THE COCKPIT HAD A TOXIC ODOR. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE FLIGHT GUIDANCE CONTROLLER TO BE BURNT. MAINTENANCE REMOVED AND REPLACED THE FLIGHT GUIDANCE CONTROLLER, OPERATIONALLY CHECKED WITH NO DESDR UPS07150638Controller · failedINSPECTION TYPE:N/A DIV - CREW EXPERIENCED MULTIPLE AUTOPILOT AND FLIGHT DIRECTOR FAILURES WHILE EN ROUTE TO DFW. FLIGHT DIVERTED TO DEN. REMOVED AND REPLACED FLIGHT CONTROL UNIT PER A300 MM 22-15-12-04 BY CAT QUALIFIED TECH. ALL SYSTEMS CHECKS OK.SDR 2007UALA00377Fcu · malfunctionedAUTO FLT -FCU 1 FAULT- DISPLAYED ON UPPER ECAM SCREEN. CREW COMMENTS, WITH SMOKE FROM FCU. [SUP 05-08-07] REPLACED FCU AFTER VERIFYING THAT FCU WAS FAULTY AND WAS SOURCE OF SMOKE. FURTHER FAULT TRACING DETERMINED THAT THE PSU WAS DEFECTIVE.SDR A6WA200640345Actuator · unknownAFTER DISCONNECTION AUTOPILOT ON APPROACH UNABLE TO MOVE CONTROL COLUMN FORWARD AND AFT, EVENTUALLY FIXED ITSELF. REMOVED AND REPLACED ELEVATOR SERVO SERV N/R OFF 13VYD. (M)SDR 2006FA0000603Servo · intermittentFLIGHT CREW REPORTED PILOTS CONTROL WHEEL TRIM INTERRUPT/AUTOPILOT DISENGAGE SWITCH NOT DISCONNECTING YAW DAMPER ON FINAL APPROACH. FOUND CONTROL WHEEL SWITCH OPERATIONS NORMAL. REPLACED SVO-85C YAW DAMPER SERVO WITH OVERHAULED UNIT. ALSO, REPLACED NR 1 FCCSDR 2006FA0000602Circuit Card · intermittentFLIGHT CREW REPORTED AUTOPILOT PITCH TRIM FAILURE ANNUNCIATION CAME ON DURING CLIMB WITH AUTO PILOT DISCONNECTED. AIRCRAFT REPPORTED TO HAVE PITCH-UP MOVEMENT. FOUND NR 1 FCC-850 CARD INTERMITTENTLY NOT CROSS-TALKING TO NR 2 FCC-850 CARD. REPLACED NR 1 FCC SDR DJFA2006232Controller · burnedTRIP ID NR 995418 DURING INITIAL CLIMB TO ALTITUDE WHILE PASSING FL 260, THE CREW HEARD A SINGLE (POP) SOUND FOLLOWED SHORTLY BY A BURNING ELECTRICAL ODOR AND LIGHT SMOKE COMING FROM THE CO-PILOTS WINDSCREEN BASE NEAR THE GLARE SHIELD. AN EMERGENCY WAS DECLASDR CBR2006F00001Autopilot Sys · malfunctionedFLIGHT DIVERTED WHILE ON LT BASE, DESCENDING THROUGH 1600 FT, AUTO PILOT DISENGAGED ITSELF, F/O WAS FLYING, WHEN HE TRIED TO HAND FLY, FLIGHT CONTROLS WERE JAMMED. HE CALLED PITCH ASSIST, DID MEMORY ITEMS FOR PITCH YAW CAPTAIN SIDE AND REGAINED CONTROL, DIVERSDR AWXA200501615Control Panel · malfunctionedPHX - AIR TURN BACK - FLT 478 - CREW REPORTED THAT ON INITIAL TAKEOFF AT HEADING SELECT, THE AIRCRAFT LOST HEADING BUG, AIRSPEED BUG, F/O COURSE INDICATOR, STEERING BARS ON FLT DIRECTOR, AND AUTOPILOT. CREW RETURNED TO PHX AND LANDED WITHOUT FURTHER INCIDENT.SDR P5CA0501339Yaw Damper · malfunctionedCREW REPORTED ON TAXI OUT UPPER RUDDER SHOWED 5 DEGREES LEFT AND LOWER RUDDER WAS CENTERED. AFTER TAXI IN, RUDDER POSITIONS WERE CONFIRMED BY MAINTENANCE. REPLACED YAW DAMPER COMPUTER AS PER MM 22-16-02. OPS CHECK PASSED ON GROUND.SDR DL757050183Computer · failedSMOKE SMELL NOTICED BY FLIGHT AND CABIN CREW. REPLACED CENTER FCC.SDR CA050303006Computer · wrong part(CAN) ON OCTOBER 15, 2004 A FLIGHT COMPUTER (FC) WAS REPLACED ON AIRCRAFT. THE REMOVED FC WAS THEN SENT FOR REPAIR. IT WAS DETERMINED THAT THE FC PN WAS NOT RECOGNIZED. IT WAS THEN SENT TO THE MFG FOR FURTHER INVESTIGATION. MFG CONFIRMED THAT THE INSTALLED IDSDR ALG2005F00009Amplifier · smokeLANDING, ON DOWN WIND APPROACH SMELLED ODOR, ON FINAL THE ODOR BECAME STRONGER, ON LANDING SMOKE CAME FROM OVERHEAD CIRCUIT BREAKER PANEL AREA. THE NR 2 PITCH AMP BREAKER POPPED. MAINTENANCE PULLED OVERHEAD AND AFCS CIRCUIT BREAKER PANEL, FOUND NO EVIDENCE OSDR 2004UALA01242Computer · malfunctionedALL FMGC 1 FUNCTIONS LOST. AUTOPILOTS DISENGAGED. SUPPLEMENTAL DATA UPDATE FMGC 1 WAS FAULTED BY THE CFDS TEST. REPLACED THE NR 1 FMGC. SHOP TEST FOUND SOLDER CRACKS ON THE U10 OF A51 CARD.SDR SWIA200414243Computer · malfunctionedSTAB CH 1 INOPERATIVE. STATUS AP PITCH TRIM CAUTION, STAB TRIM/MACH TRIM CAUTION. REMOVED AND REPLACED HSTCU AND FCC. OPERATIONAL CHECK GOOD PN 7060-9, SN OFF 1057.SDR SIMA200427201Computer · malfunctionedON TAXI OUT RUDDER PEDALS JAMMED. REPLACED NR 1 INTEGRATED COMPUTER. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)SDR AWXA200400887Computer · malfunctionedEN ROUTE, FLT MANAGEMENT GUIDANCE COMPUTER NR 1 FAILED AND FMGC NR 2 FAULTED, FIRST OFFICER LOST MAP DISPLAY 3 TIMES, DIVERTED TO CMH & LANDED WITHOUT FURTHER DIFFICULTY. MX R & R FMGC NR 1 IAW T/C R2A22302, PERFORMED OPS TEST OF FMGC NR 1 & 2, BOTH CHECK GOOSDR P8UF200400002Computer · failedDURING CLIMB LOWER YAW DAMPER B-CHANNEL BECOMES INOPERATIVE.SDR 04139633Computer · intermittentDURING AIRCRAFT OPERATION THE CREW REPORTED AN INTERMITTENT UNCOMMANDED YAW MOVEMENT. THE FLIGHT LANDED UNEVENTFULLY. THE FLIGHT CONTROL COMPUTER WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE.SDR 0400469960Control Panel · shortedCOCKPIT CREW REPORTED HEAVY SMOKE AND SPARKS COMING FROM THE CENTER CONSOLE WHILE AT CRUISE. FLIGHT DIVERTED TO AN UNEVENTFUL SAFE LANDING AT GRR. NO FIRE EXTINGUISHER WAS USED AND SOURCE OF THE SMOKE STAYED RESTRICTED TO THE AUTOPILOT CONTROL PANEL LIGHTINGSDR AUS20040199Panel · faulty(AUS) AUTOPILOT MODE CONTROL PANEL FAULTY.SDR MALA040218Computer · malfunctionedJUST AFTER AIRBORNE LIGHTS ON ADVISORY PANEL FTC, EL TRIM, YD ILLUMINATED. AIR RETURN TO MSP. RERACKED DFGC. DFGS OP CHECKS GOOD IAW RJ-85 M/M CHAP 22. EXCEPT FOR AUTOTHROTTLE.SDR AUS20040292Controller · faulty(AUS) AUTOPILOT BURNED OUT. ROLL SERVO ALSO BURNED OUT.SDR RAIA00401056Control Unit · malfunctionedSTL - YAW DAMPER INOP INDICATION. MAINTENANCE DEFERRED PER MEL. SUBSEQUENTLY CLEARING DMI BY REMOVING AND REPLACING FLIGHT GUIDANCE CONTROL UNIT.SDR AWXA200400002Control Unit · malfunctionedAFTER TAKEOFF AT DTW EN ROUTE FOR PHX RECEIVED ECAM MESSAGE AUTO FLIGHT FCU 1 & 2 FAULT. ALTIMETER FLIGHT CONTROL UNIT (FCU) WINDOWS WENT BLACK, AND HAD LOSS OF AUTO THRUST & HEADING SELECT, TURNED BACK TO DTW AND LANDED WITHOUT EVENT. MAINTENANCE REMOVED ANSDR 03313655Circuit Board · faultyDURING FINAL APPROACH THE CREW REPORTED RECEIVING AUTOPILOT PITCH TRIM MESSAGES. FLIGHT LANDED UNEVENTFULLY. FAULT WAS TROUBLESHOT TO THE NR 2 FCC CARD AND UNIT WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTISDR 03309643Circuit Card · faultyDURING FLIGHT THE AIRCRAFT EXPERIENCED EXCESSIVE YAW WITH NO YAW DAMPER FAIL INDICATIONS. THE NR 2 FCC CARD WAS REPLACED.SDR AWXA200301055Control Panel · failedDURING CRUISE EN ROUTE FROM PHX TO MSY AT 33000 FT AUTOPILOT DISCONNECTED DUE TO MODE CONTROL PANEL (MCP) FAILURE, FLIGHT DIRECTORS AND AUTOPILOT INOPERATIVE. ONLY WINDOW WORKING ON MCP WAS THE FIRST OFFICERS COARSE SELECTOR, FLIGHT INSTRUMENTS AND RADIO MAGNESDR SWIA200312269Control Panel · malfunctionedALTITUDE PRESELECT NOT HOLDING ALTITUDE/DEPARTED PRESELECT AND RAN UP AND DOWN UNCONTROLLABLE. PRESELECT KNOB WOULD NOT CONTROL. DISENGAGED AP AND HAND FLEW PLANE. REMOVED AND REPLACED FCP IAW MM 22-10-07. FCP & AP OPS CHECK GOOD IAW MM 22-11-07.SDR U30A200300033Computer · malfunctionedAFTER PUSHBACK FOR FLT 326 IN BWI, CREW RECEIVED ECAM MESSAGE FOR AUTO FLT YAW DAMPER FAULT, AFTER ENGINE START. AIRCRAFT RETURNED TO GATE. MAINTENANCE RESET THE NR 2 FAC (FLIGHT AUGMENTATION COMPUTER) IAW CAATS TASK 22-63-00-810-815. SYSTEM OPS CK'D OK. AIRCRSDR AWXA200300111Computer · failedLAS - ABORTED TAKEOFF - FLT 0532 - ON TAKEOFF ROLL IN LAS EN ROUTE FOR RNO AT 85 TO 90 KTS BOTH NAV DISPLAYS AND FLIGHT MANAGEMENT GUIDANCE COMPUTERS (FMGC) TIMED OUT, SCREEN NOT DISPLAYING MAPS. REJECTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE RESET FMGC CI
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