JASC 3460
Service difficulty reports · 4,692
Reports filed under 3460 · Flight Management Computing Hardware 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 = '3460' 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 = '3460' 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 VNAA0206003Control Unit · malfunctionedDURING THE TAKEOFF, THE CREW RECEIVED A FLIGHT GUIDANCE CONTROL UNIT LAT MODE FAIL CAS MESSAGE AND ABORTED TAKEOFF. AFTER EXITING THE RUNWAY THE MESSAGE CLEARED ITSELF AND FLIGHT WAS CLEARED FOR ANOTHER TAKEOFF ATTEMPT. FLIGHT 4097 THEN DEPARTED WITH NO FURTSDR GTIA020629Computer · inoperativeACY - FLT 259 - AUTO PILOT DOES NOT HOLD SELECTED VERTICAL SPD IN VERTICAL SPPED MODE OR SELECTED IAS MODE WHEN DESCENDING. FOUND INOPERATIVE DFGC COMPUTER NR 1 REMOVED AND REPLACED DFGC NR 1 AND RAN RETURN TO SERVICE TEST NO FAULT NOTED CHECKED GOOD. (M)SDR 2002F00532Fmc · failedFLIGHT NUMBER 710, RIGHT FMC FAILED ON TAXI OUT. AIRCRAFT RETURNED TO THE GATE. MAINTENANCE REMOVED AND REPLACED THE RIGHT FMC COMPUTER IN ACCORDANCE WITH MM 34-61-01-024, OPERATIONAL CHECKS GOOD.SDR MALA020299Computer · failedEN ROUTE FROM TYS TO DTW, FGC1 LIGHT ILLUMINATED. MAINTENANCE REPLACED FGC IAW 22/10-11. OPS CHECK GOOD.SDR 02142421Computer · faultyDURING APPROACH OF THE FLIGHT FROM CVG TO ALB, THE CREW REPORTED UNCOMMANDED ROLL AND YAW MOVEMENT OF THE AIRCRAFT. AN EMERGENCY WAS DECLARED WITH THE ALB TOWER AND THE AIRCRAFT WAS LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE PERSONNEL REMOVED AND REPLACED SDR 2002F00507Computer · failedFLIGHT NUMBER 925, DURING CRUISE RECEIVED EICAS MSG L FMC FAIL. OTHER CDU DISPLAYS SINGLE FMC OPERATION MESSAGE. MAINTENANCE REMOVED AND REPLACED THE LEFT FMC COMPUTER IN ACCORDANCE WITH MM 34-61-01-4. OPERATIONAL CHECKS GOOD.SDR GTIA020514Computer · failedLGA - FLT 1381 - NR 1 AUTO PILOT CLICK OFF ON THE DESCENT, AT THE SAME TIME AUTO THROTTLES CLICK OFF. BOTH FMAS AND DFG PANELS WENT BLANK FOLLOWED QRH PROCEDURES SWITCH TO AUTO PILOT NR 2 AND SYSTEM WORKED FOR REMAINDER OF FLIGHT. REMOVED AND REPLACED NR 1 DSDR GTIA020513Computer · failedFLT 709 - LAX - AUTO THROTTLES AND AUTO PILOT CAME OFF ON DESCENT THROUGH 21,000 MASTER CAUTION. FOUND NR 1 DFGC BAD. REMOVED AND REPLACED NR 1 DFGC, RTS CHECKS GOOD. (M)SDR HEEA078934Transducer · failedYAW DROPS OFF LINE AND HAS NO RESISTANCE MOVEMENT.SDR RAIA00205148Screen · backed out5590-STL- FO FLIGHT INFORMATION SYS SCREEN WENT BLANK. MAINTENANCE REMOVED AND REPLACED THE FO ELECTRONIC FLIGHT INFORMATION SYSTEM TUBE.SDR CALA2000267Fmc · malfunctionedAIRCRAFT LOST ALL NAVIGATION DATA; BOTH CAPT AND F/O DEU DISPLAYS ARE BLANK. REMOVED AND REPLACED NR 1 FLIGHT MANAGEMENT COMPUTER.SDR AALA20020709Fmc · failedLEFT FMC FAILED MIDWAY THROUGH THE FLIGHT. SELECTING ALTERNATE FMC RESTORED FUNCTION. INSTALLED LOADED PART FMC AND CROSSLOAD CARRIED OUT IAW MM 34-61-00-21 AND 34-6-01-4, SYSTEM NORMAL. (M)SDR GTIA020488Computer · failedFTW - FOUND DFGS 1 AND 2 RTS FAIL TEST WITH FOLLOWING FAULTS, NOTED AIL MECH TORQUE 1 FAIL, AIL MECH TORQUE 2 FAIL, SPOILER POSITION FAIL. NR 18 PER POSITION XMITTER. ADJUSTED FLAP POSITION TRANSMITTERS FOR AIL MECH. TORQUE 1 FAIL AND AIL MECH TORQUE 2 FAILSDR 2002UALA00801Cdu · failedCAPT CDU WENT INOP AFTER TAKEOFF. CREW WAS UNABLE TO RESTORE THE SYSTEM. DUAL CDU REQUIRED PRIOR TO ENTERING CLASS 2 RNP-10 AIRSPACE. AT JFK, THE CENTER CDU WAS SWAPPED WITH THE INOPED CAPTAIN'S ONE AND DEFFERED. DEFECTIVE CDU WAS REPLACED AT LHR.SDR MEX2002121Computer · failedFLT 935 - MTY-MEX - BOTH FMA'S OUT OF SERVICE WITH THE DFGC SWITCH IN THE NR 2 POSITION. PERFORMED A RESET TO THE ELECTRIC BARS, DFGC 1 DID NOT PERFORM THE POWER UP UNTIL THE DFGC SWITCH WAS CHANGED. THE COPILOT ADI WAS CHANGED BUT DID NOT CORRECT THE PROBLESDR AALA20020515Fmc · malfunctionedLAX - FLT 297 - EN ROUTE LAX-HNL - BOTH FMC'S FAILED TO PERFORM NAVIGATION CALCULATIONS FOLLOWING TAKEOFF. RESET PER OPERATIONS MANUAL. RETURNED AND LANDED LAX WITHOUT INCIDENT. VERIFIED SOFTWARE FOR FMC: OPC, OPS, FDO, AMI ALL GOOD PER MAINTENANCE MANUAL. SDR 2002F00504Cdu · inoperativeFLIGHT NUMBER 273, DURING CRUISE FIRST OFFICERS CDU WENT BLANK. SELECTING ALTERNATE FMC DID NOT CORRECT FAULT. MAINTENANCE REMOVED AND REPLACED THE FLIGHT MANAGEMENT COMPUTER CONTROL DISPLAY UNIT PER MM 34-61-02. OPERATIONAL CHECKS GOOD.SDR VNAA0204005Fmc · malfunctionedDURING TAKEOFF, THE HEADING MODE OF THE FLIGHT MANAGEMENT SYSTEM FAILED AND THE CREW ABORTED TAKEOFF. THE CREW CALLED MAINTENANCE CONTROL AND RESET THE SYSTEM. FLIGHT 4032 ATTEMPTED A SECOND TAKEOFF AND DEPARTED WITHOUT ANY OTHER INCIDENTS.SDR P2EA2002M019Computer · malfunctionedNR 1 & NR 2 FLT GUIDANCE COMPUTER WENT BLANK DURING FLIGHT. AIRCRAFT LANDED AND RETURNED TO GATE WITH NO INCIDENT. PERFORMED RETURN TO SERVICE TEST ON BOTH DIGITAL FLIGHT GUIDANCE COMPUTER IAW MM 22-01-05. OPERATIONAL CHECKED GOOD.SDR VNAA0203037Computer · malfunctionedDURING TAKEOFF, THE CREW RECEIVED A FLIGHT GUIDANCE COMPUTER FAIL CAS MESSAGE AND ABORTED TAKEOFF. AFTER EXITING THE RUNWAY THE MESSAGE CLEARED AND FLIGHT 4099 WAS CLEARED FOR ANOTHER TAKEOFF ATTEMPT. FLIGHT 4099 THEN DEPARTED WITH NO FURTHER INCIDENTS.SDR SIMA200207702Computer · faultyOKC - FLT 3602 - CREW REPORTED AT APPROXIMATELY 4000 FT FIRST OFFICER LOST HEADING AND ATTITUDE FOLLOWED BY THE CAPTAIN LOSING HIS HEADING AND ATTITUDE. EMERGENCY WAS DECLARED AND AIRCRAFT WAS LANDED SAFELY. DURING RETURN TO FIELD CAPTAIN SIDE CAME BACK ON LSDR VNAA0203025Computer · malfunctionedTHE FLIGHT WAS ON THE TAKEOFF ROLL WHEN THE FLIGHT CREW RECEIVED A FLIGHT GUIDANCE COMPUTER FAIL WARNING MESSAGE ON THE EICAS DISPLAY. THE FLIGHT CREW ABORTED THE TAKEOFF AND EXITED THE RUNWAY. ONCE CLEARING THE RUNWAY THE WARNING MESSAGE CLEARED ITSELF WITHSDR AWXA200200225Fmc · failedTAKEOFF FL 180 FMGC NR 1 & 2 FAILED DUMPING PRIMARY & SECONDARY FLT PLANS. AUTOPILOT WOULD NOT EXCEED 5 DEG TURN RATE, RADIO NAV HARD TUNED TO 109.9. VERTICAL RATE OF DESCENT AT TOUCHDOWN 100 FPM. R&R NR 1 & 2 FMGC. OPS CHECK, AUTO-LAND TEST GOOD & NAV DATSDR GTIA020141Computer · failedRSW - NR 1 DFGS WENT INOPERATIVE ON SHORT FINAL. NR 2 DFGS WORKS OK. REMOVED AND REPLACED NR 1 DIGITAL FLIGHT GUIDANCE COMPUTER AS REQUIRED IAW MD80 MM CH 22-01-05. PERFORMED RETURN TO SERVICE TEST. RTS CHECK GOOD. (M)SDR 2002F00377Fmc · faultyWHILE EN ROUTE, FL370, SMOOTH AIR, AIRSPEED ORANGE BUG SLOWED TO 220 KT, THEN RETURNED TO NORMAL SPEED FOLLOWED BY AUTOPILOT AND AUTOTHROTTLE DISCONNECT. AUTOPILOT RECONNECTED OK, AUTOTHROTTLE DIFFICULT TO RECONNECT. MAINTENANCE REPLACED LEFT FMC. (M)SDR VNAA0202016Computer · malfunctionedDURING THE TAKEOFF ROLL, THE CREW RECEIVED A FLIGHT GUIDANCE COMPUTER FAIL INDICATION AND ABORTED TAKEOFF. THE CREW WAS TAXIING TO THE GATE AND THE MESSAGE CLEARED BY ITSELF. MAINTENANCE CONTROL MEL'D THE FLIGHT GUIDANCE COMPUTER AND THE FLIGHT DEPARTED WITHSDR MEX2002033Computer · failedFLT 907 - MTY-MEX - PILOT REPORTED AHRS NR 2 OUT OF SERVICE.. (M)SDR MEX2002029Computer · failedFLT 403 - MEX-NYC - AIRCRAFT RETURNED TO MEX AS CONSEQUENCE OF NAVIGATIONAL INSTRUMENTS FAIL. DURING CLIMBING THE NR 2 SYMBOL GENERATOR MALFUNCTIONED. BOTH EFIS WERE SWAPPED, OPERATION REESTABLISHED, BUT AFTER BOTH SYMBOL GENERATORS AND BOTH FMA OUT OF SERVICSDR CA020221012Adc · out of adjust(CAN) AIRCRAFT RETURNED AFTER TAKEOFF WITH MULTIPLE FLIGHT ENVELOPE AND SPEED PROTECTION FAULTS. MAINTENANCE FOUND LOADED FLIGHT PLAN DATA NOT IN AGREEMENT . IRS(INERTIAL REFERENCE SYSTEM) WERE REALIGNED , FLIGHT PLAN DATA REINSERTED AND ALL FMS (FLIGHT MANAGESDR AWXA200200099Fmc · out of adjustBUR - ABORTED TAKEOFF - FLT 0536 - C - DURING TAKEOFF ROLL OUT OF BUR EN ROUTE TO PHX WHEN ADVANCING THROTTLE IN BLUE FLEX TEMPERATURE DROPPED OUT OF FMGC CAUSING THE MASTER CAUTION LIGHT TO ILLUMINATE AT APPROXIMATELY 40-50 KNOTS. TAKEOFF WAS ABORTED AND AIRSDR 2002UALA00172Cdu · failedRT FMC OVERHEATED SHORTLY AFTER DEPARTURE. A HOT PLASTIC SMELL WAS VERY EVIDENT IN THE COCKPIT. CAPT ELECTED TO RETURN TO IAD. RT FMC HMCDU OVERHEATED, HOT PLASTIC SMELL WAS VERY EVIDENT IN THE COCKPIT. RT HMCDU BECAME INOPERATIVE AND WAS VERY HOT TO TOUCSDR USAABB01139Fmc · failedPHL - FLT 42 - EN ROUTE PHL-AMS, CREW NOTED THAT THE RIGHT FMC HAD FAILED. FLIGHT RETURNED TO PHL. MAINTENANCE REPLACED THE FMC. (M)SDR CA011210006Display · overheated(CAN) SMELL OF SMOKE. FMS CDU WAS HOT TO TOUCH AND LOSS OF COLORS ON SCREEN.SDR SWIA200110362Computer · malfunctionedSMELL OF SMOKE. FMS UNIT WAS HOT TO TOUCH AND LOSS OF COLORS ON SCREEN. REMOVED AND REPLACED FMS UNIT PER CRJ MM 34-16-01.SDR AUS20011168Capacitor · burned out(AUS) NAVCOM CAPACITOR C491 BURNT.SDR GTIA011012Computer · failedACY - AUTO PILOT INOPERATIVE IN CMP NR 1. REMOVED AND REPLACED NR 1 DFGC, OPS CHECK NORMAL. (M)SDR GTIA011137Computer · faultyFTW - NR 2 DFGC P/N 4034241-971, S/N 88081643 WILL NOT ALLOW AUTO PILOT TO ENGAGE. ALSO, NR 2 FLIGHT DIRECTOR FLAG IN VIEW. REMOVED NR 2 DFGC IAW MD80 MM 22-01-01. INSTALLED NR 2 DFGC IAW MD80 MM 22-01-01. (M)SDR GTIA010972Computer · faultyFLL - FLT 171 - AUTO THROTTLES WOULD NOT REMAIN ENGAGED WITH DFGC NR 1 SELECTED. WORKED NORMAL ON DFGC NR 2. REMOVED AND REPLACED NR 1 DFGC RTS CHECK GOOD. (M)SDR QXEA0101607Computer · faultyRDD- ELECTRICAL SMELL IN COCKPIT BELIEVED TO BE COMING FROM NR 2 FMS. WHEN FMS IS TURNED OFF THERE IS NO SMOKE. REMOVED AND REPLACED NR 2 FMS. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.SDR 2001UALA02074Computer · malfunctionedON CLIMBOUT FELT STRONG VIBRATION IN RUDDER PEDALS. STRONG VIBRATION WAS FELT IN THE REAR OF THE CABIN. THE VIBRATION WAS REPORTED AS BEING A SIDE-TO-SIDE MOTION. FAC (FLIGHT AUGMENTATION COMPUTER) WAS REPLACED.SDR VNAA0109010Computer · malfunctionedDURING TAKEOFF, THE CREW RECEIVED A FLIGHT GUIDANCE COMPUTER FAIL MESSAGE AND ABORTED TAKEOFF. AS FLIGHT 4065 EXITED THE RUNWAY THE MESSAGE CLEARED. THE CREW CONTACTED MAINTENANCE CONTROL AND CLEARED FOR ANOTHER TAKEOFF ATTEMPT. FLIGHT 4065 THEN DEPARTED WISDR MALAL010680Computer · faultyDURING ROTATION RECEIVED FTC, EL TRIM WITH LOUD BUZZING NOISE OVER OVERHEAD SPEAKER, WINDSHR AMBER AND RED FLASHED ON AND OFF, YD ALSO FAILED AND ASSOCIATED YD WHITE LIGHT. FGC 1 WHITE ILLUMINATED, TRP FAILED, FD FAILED, CONTINUOUSLY REC'D WDSHR WARNING LIGHTSDR GTIA010847Control Panel · faultyFLL - FLT 139 - SPD/MACH BUTTON WILL NOT SWITCH WHEN PUSHED. REMOVED AND REPLACED FLIGHT GUIDANCE CONTROL PANEL. (M)SDR 2001F00456Fmc · malfunctionedRIGHT AFTER TAKEOFF IN A LEFT TURN EXPERIENCED A DUAL FMC FAILURE. BOTH SYSTEMS RETURNED TO NORMAL WHEN WINGS LEVEL. PERFORMED BITE CHECK OF LEFT AND RIGHT FMC'S. NO FAULTS FOUND. SYSTEM OPS CHECK NORMAL ON GROUND. REF MM 34-61-00 AND FIM 34-61-00. RETURSDR GTIA010841Computer · malfunctionedACY - FLT 138 - SELECTING CLIMB POWER ON TRP AFTER TAKEOFF CAUSED RIGHT THROTTLE TO MOVE BACK TO CORRECT POSITION MANUALLY WORKED OK REST OF FLIGHT DFGC NR 1. REMOVED NR 1 DFGC CLEANED CONTACTS AND REINSTALLED SAME UNIT PERFORMED RTS CHECK OF NR 1 DFGC IAW MMSDR CA011026004Computer · malfunctioned(CAN) PILOT REPORTED THE INABILITY TO CANCEL THE 'FD' FLIGHT DIRECTOR ANNUNCIATOR LIGHT ON THE AUTOPILOT ANNUNCIATOR PANEL. COMMAND BARS ON ADI WOULD NOT DROP OUT OF VIEW. FLIGHT DIRECTOR COMPUTER REMOVED AND REPAIR.SDR AUS20010931Wire · transposed(AUS) FLIGHT CONTROL COMPUTER TO STABILISER POSITION SENSOR WIRES TOPIN 22 AND PIN 23ON CONNECTOR D4079 CROSSED.SDR GTIA010834Computer · faultyFLT 1572 - NR 2 DFGC ALT PRE-SELECT BLANK. REMOVED AND REPLACED NR 2 DFGC IAW MD80 MM 22-01-01 RAN RTS TEST MD MM 22-01-05, ALL OPS CHECK OK. (M)SDR GTIA010942Computer · faultyFTW - ALTITUDE SELECTOR ON DFGCP IS INTERMITTENT. REMOVED DFGCP IAW MD80 MM 22-01-02. INSTALLED DFGCP IAW MD80 MM 22-01-02. DFGS RTS WILL BE ACCOMPLISHED ON C-CHECK CARD B16-09R-01. (M)SDR VNAA0108011Computer · malfunctionedDURING THE TAKEOFF ROLL, THE CREW RECEIVED A FLIGHT GUIDANCE COMPUTER FAIL MESSAGE AND ABORTED TAKEOFF. THE MESSAGE CLEARED BY ITSELF AND THE CREW CALLED MAINTENANCE CONTROL WHO ADVISED THE CREW TO ATTEMPT ANOTHER TAKEOFF. FLIGHT 4094 THEN DEPARTED WITH NO F
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