JASC 7321

Service difficulty reports · 2,878

Reports filed under 7321 · Fuel Control/Turbine Engines, 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 = '7321'
  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.

SDR CA130612006Ecu · failed(CAN) 11 PM LOCAL TIME. THE PILOT MADE A NORMAL OUTBOUND FLIGHT AND SHUTDOWN AT A TRAUMA SCENE. 5 MINUTES INTO A 10 MINUTE RETURN FLIGHT THE FADEC DEGRADE LIGHT, AUTO RELIGHT LIGHT CAME ON WITH ALL OTHER INDICATIONS NORMAL FADEC REMAINED IN AUTO MODE. THE PIJun 5, 2013 · Bell 407SDR VNAA2013053100018Fuel Control · failedCREW REPORTED RIGHT ENGINE OVERSPEED MASTER WARNING MESSAGE BELOW 80 KNOTS ON TAKEOFF. CREW REJECTED TAKEOFF AND SAFELY RETURNED TO GATE. MAINTENANCE INSPECTED, PERFORMED POWER ASSURANCE RUN AND FOUND RIGHT ENGINE EXCEEDED MAXIMUM PERMITTED N2. MAINTENANCE May 31, 2013 · N215PS · Cndair CL6002B19SDR CA130626002Bellows · distorted(CAN) ENGINE WOULD NOT DEVELOP POWER FROM IDLE. FCU REPAIRED BY REPAIR FACILITY. FCU REINSTALLED AFTER REPAIR, MAINTENANCE UNABLE TO ADJUST IDLE, MIN FLOW. ENGINE WOULD NOT DEVELOP TAKEOFF POWER. UNIT RETURNED AND DISTORTED BELLOWS ASSY FOUND.May 25, 2013 · Dhav DHC3SDR CA130603019Shaft · damaged(CAN) IN FLIGHT SURGE ON NR 1 ENGINE DURING MAINTENANCE OPERATIONS, THE FCU WAS REMOVED AND FOUND INPUT SHAFT DAMAGED.May 23, 2013 · Aerosp AS355F2SDR SIMA20130522003Fadec · malfunctionedTHE CREW REPORTED THAT DURING CRUISE FLIGHT, NR 2 ENGINE (N1) SMOOTHLY ROLLED BACK ABOUT 25-30 PERCENT AND THEN SMOOTHLY CAME BACK UP, IT DID THIS 3 TIMES IN ABOUT 15 MINUTES AND THEN RETURNED TO NORMAL. ON LANDING, GOT E1 EXCEEDANCE ON EICAS. THE ACFT WAS RMay 22, 2013 · N606AE · Emb EMB145LRSDR CA130530003Fuel Control · malfunctioned(CAN) DURING A CROP DUSTING RUN, THE ENGINE TORQUE DROPPED FROM 45PSI DOWN TO 30PSI. THE PILOT ADVANCED THE POWER LEVER BUT THE ENGINE TORQUE SURGED AND WAS UNSTABLE. A FORCED LANDING WAS MADE AT A REMOTE AIRSTRIP. THE A/C WAS NOT DAMAGED AND THE PILOT NOTICEDMay 20, 2013SDR UALA2013051503372Fmu · faultyAFTER ENG SHUTDOWN EICAS MESSAGE FUEL VALVE RT SHOWED. REPLACED RT ENG FMU IAW AMM.May 14, 2013 · N222UA · Boeing 777222SDR CA130516005Fcu · contaminated(CAN) METAL WAS FOUND IN THE FCU FILTER. UPON INSPECTION OF THE CFP EXTENSIVE RUBBING WAS FOUND. THIS CFP HAD ONLY BEEN INSTALLED FOR 26.7 HRS.May 9, 2013 · Skrsky S61NSDR PCSA2013051001Fuel Control · faultyENGINER 2 FLAMEOUT AT CRUISE. ALL PARAMETERS NORMAL. ENG WINDMILL FOR ABOUT 15 MIN. 20 PSI OIL PRESS. THE NR 2 ENGINE OIL FILTER WAS CHECKED, FOUND NORMAL, THE NR 2 FUEL PUMP AND FUEL CONTROL UNIT REPLACED AND TESTED PER THE B727 AMM AND THE AIRCRAFT RETURNMay 6, 2013 · N598AJ · Boeing 727212SDR UALA2013050103047Relay · failedON SHUTDOWN NR 2 ENGINE HAD A LOT OF WHITE SMOKE AND ON STATUS PAGE HAD ENGINE FUEL VALVE R MSG. MAINT TEXT: CORRECTION THIS WAS FUEL VAPOR AND NOT SMOKE. FOUND MAINT MSG 73-60212 LATCHED. ACCOMPLISHED FIM TASK 73-22 802 ITEM E ENGINE FUEL CONT FAILED TO SApr 30, 2013 · N218UA · Boeing 777222SDR VNAA2013042800021Fadec · failedCREW REPORTED THE RIGHT ENGINE FLAMED OUT. AIRCRAFT RETURNED TO AIRPORT LANDING WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED THE RIGHT ENGINE FADEC PER AIRCRAFT MANUALS. OPERATION CHECKS WERE ACCOMPLISHED USING AIRCRAFT MANUALS AND AIRCRAApr 28, 2013 · N712PS · Cndair CL6002C10SDR YENA20130424085Fmu · failedFLT 706, ABORTED TAKEOFF FOR ENGINE FAILURE. TOWER NOTIFIED CAPTAIN THAT NR 1 ENGINE WAS SMOKING. REMOVED AND REPLACED NR 1 FMU IAW AMM 73-22-57-04. OPS AND LEAK CHECKED GOOD.Apr 24, 2013 · N594JB · Airbus A320232SDR ZESA2013F00107Fcu · malfunctionedAIRCRAFT WAS REPORTED AS HAVING A YAW ON APPROACH WHEN REDUCING POWER ON THE ENGINES. THE ROOT CAUSE WAS THE RT ENGINE FUEL CONTROL UNIT (FCU). THE FCU WOULD FLUCTUATE WHEN THE ACFT WAS ON APPROACH WHEN THE ENGINE POWER WAS BEING REDUCED. FCU REPLACED AND AApr 24, 2013 · N5AE · Beech 200BEECHSDR CA130417007Seal · leaking(CAN) WHEN BOOST PUMPS WERE ACTIVATED, FUEL WAS SEEN COMING OUT OF THE ACFT ENGINE DRAIN. ONCE THE ACFT STARTED, THE LEAK WOULD STOP. ENGINE MFG KNOWS ABOUT THIS ISSUE AND SAYS THAT THE SEALS ARE POOR. WE HAVE HAD THIS ISSUE WITH THIS FCU AND 2 OTHERS WITH Apr 15, 2013 · Snias AS350B2SDR UALA2013040802314Eec · failedLEFT ENG FAILURE ON TAXI IN. MAINT TEXT: DEBRIEFED CREW, AFTER ROLL OUT ON TO TAXI WAY UPPER EICAS FAILURE MSGS RELATED TO NR 1 ENGINE ROTATION DECREASING AND EGT RISING RAPIDLY, CAPT SHUT DOWN ENGINE. BOTH S SVA OR FCU-EEC AND P SVC OR FCU-EEC MESSAGES ON EApr 6, 2013 · N551UA · Boeing 757222SDR CA130409004Fcu · damaged(CAN) DURING DAILY INSPECTION FOUND MINOR FUEL SEEP FROM FCU BETWEEN FLANGES OF PNEUMATIC SECTION AND MAIN BODY ON LOWER LT SIDE.Apr 5, 2013 · Cessna 208BSDR UALA2013040802309Warning Light · false activationEIGHT HOURS INTO FLIGHT, STATUS LIGHTS LT ENG EEC C1-L ENG A-O VALVE DISPLAYED. PERFORMED AMM FIM TASK 73 -21-00. NO PROBLEMS FOUND. OK TO CONTINUE.Apr 5, 2013 · N668UA · Boeing 767322SDR USAA2013040800010Eec · faultyENGINE 2 FAIL MSG JUST PRIOR TO TAKEOFF, SHUTDOWN COMPLIED WITH ECAM. REMOVED AND REPLACED NUMBER TWO ENGINE INTERFACE UNIT P/N 3957985205 S/N 2851 PER AIRBUS MAINTENANCE MANUAL 73-75-34-400-041-A AND REMOVED AND REPLACED NUMBER TWO ELECTRONIC ENGINE CONTROL Apr 5, 2013 · N659AW · Airbus A320232SDR CA130701002Fuel Control · malfunctioned(CAN) DURING THE SHORT FINAL LANDING, THE ENGINE NR 2 POWER STAY AT FLIGHT IDLE EVENT IF THE PLA WAS MOVED. THE PILOT SHUTDOWN THE ENGINE AND PERFORMED AN UNEVENTFUL SINGLE ENGINE LANDING. DURING THE ON GROUND INVESTIGATION THE FCU WAS REPLACED AND THE ISSUEApr 3, 2013SDR CA130403008Hmu · malfunctioned(CAN) DURING CRUISE AT FLIGHT LEVEL 360 EXPERIENCED SOME TURBULENCE AND AIRSPEED DECREASED. PUSHED TRUST LEVERS FORWARD AND THE NR 1 ENGINE N1 SPEED WHITE NEEDLE FLUCTUATED AND DROPPED - 5 PERCENT. SECOND TIME PUSHED TRUST LEVERS FORWARD AGGRESSIVELY AND NR Apr 2, 2013 · Boeing 737*SDR UALA2013032701954Eec · faultyCREW REPORTS: AT FLAP RETRACTION AFTER TAKEOFF, GOT STATUS MSG ON LOWER ECAM, WHEN SLATS OUT. ENGINE 2 AT IDLE ON GROUND. ENGINE 2 MAX PWR-IDLE. INOP SYS SHOWS REV 2 AND ENGINE 2 THR. REPLACED NR 2 ENGINE EEC REFERENCE MM 73-22-34, OPS CHECK NORMAL.Mar 25, 2013 · N815UA · Airbus A319131SDR KC8A20130325001Fcu · faultyRIGHT ENGINE TORQUE DECREASED AFTER TAKEOFF. AIRCRAFT RETURNED TO BASE (KYIP). TROUBLESHOT PROBLEM AND DETERMINED IT TO BE THE FUEL CONTROL UNIT. FUEL CONTROL UNIT REMOVED TO BE SENT OUT FOR REPAIR.Mar 22, 2013 · N241CK · Beech 200BEECHSDR UALA2013032001725Fcu · failedNR 1ENG FLAME OUT. REMOVED AND REPLACED FUEL PUMP AS PER AMM, FUEL CONTROL AS PER AMM AND ALSO EEC AS PER MM 73-21-04.Mar 19, 2013 · N536UA · Boeing 757222SDR UALA2013032001704Fcu · malfunctionedLEFT ENGINE ROLLED BACK AFTER START. FLAMES REPORTED. REPLACED LEFT ENGINE FUEL PUMP, FUEL CONTROL UNIT AND EEC.Mar 18, 2013 · N536UA · Boeing 757222SDR USAA2013031800006Eec · inoperativeON GROUND ENGINE NUMBER 2 FAILED 1 MINUTE AFTER START (AT IDLE). NO ACTION WAS TAKEN BY CREW TO INDUCE FAILURE. REMOVED AND REPLACED NUMBER 2 ENGINE ELECTRONIC ENGINE CONTROL IN ACCORDANCE WITH JOB CARD 26L40073002.Mar 15, 2013 · N659AW · Airbus A320232SDR CA130502003Fuel Control · malfunctioned(CAN) WHEN TOP OF CLIMB TO FSPP ABOUT TO SET CRUISE POWER, 40PSI, CLIMB AT 45 PSI, 76 PERCENT RPM, THE NR 2 ENGINE SHOWED AN OVER TORQUE TO 65PSI AND THE ITT REACHED APPROXIMATELY 900 DEGREES C. THE PILOT POWERED BACK TO IDLE THE NR 2 ENGINE. THE ENGINE DID Mar 8, 2013SDR USAA2013031100008Fmu · failedCAPTAIN REPORTED THAT DURING TAXI, STARTED ENGINE 2 AND EVERYTHING APPEARED NORMAL, BUT AFTER ADDING POWER ABOVE IDLE, RECEIVED 'ENG 2 FAIL' MESSAGE. ATTEMPTED CROSS BLEED HUNG START. APU BLEED START ALSO FAILED. MAINTENANCE REMOVED AND REPLACED NR 2 FUEL MEMar 8, 2013 · N659AW · Airbus A320232SDR CA130416001Fuel Control · malfunctioned(CAN) AFTER T/O, THE ENGINE POWER COULD NOT BE REDUCED AND THERE WAS NO RESPONSE FROM THE POWER LEVER. THE PILOT PUT THE ACFT IN CLIMB MODE TO CONTROL SPEED AND RETURNED TO THE AIRPORT WHERE, DURING SHORT FINAL, SHUT THE ENGINE DOWN. AN UNEVENTFUL DEAD STICMar 5, 2013 · Fltchr FU24AIRPTSSDR CA130306004Fuel Control · disconnected(CAN) FUEL LEVER WAS DISCONNECTED AT LINKAGE. LEVER POSITIONED IN OPEN POSITION DURING RIGGING REQUIREMENTS. LINKAGE RECONNECTED. AT NO TIME WAS THE FUEL SYSTEM FUEL LINES OPENED. THE NEXT ENGINE START ATTEMPT RESULTED IN FAILED START ATTEMPT. THE SYSTEM WAMar 4, 2013 · Snias AS350BASDR ASAA2013030294045Hmu · unstableWHILE CLIMBING THROUGH HIGH 20S AT 3201/.792 COST INDEX 45, FUEL HAD DEVELOPED A 600 LBS IMBALANCE WITH LT SIDE HEAVY. TURNED LT CENTER PUMP OFF, CROSSFEED CLOSED AND ALL OTHER BOOST PUMPS ON. ABOUT 4 MINUTES LATER AT ABOUT 33,000 LEFT ENGINE VARIED AT MODERMar 2, 2013 · N587AS · Boeing 737890SDR HALA2013030200028Fmu · failedLT ENGINE NO FUEL FLOW. TWO STARTS ATTEMPTED. R & R FUEL FLOW TRANSMITTER IAW AMM 73-31-01. LEAK CHECKED OK. CONDITION SAME. R & R FMU FOR NR 1 ENGINE IAW 73-21-01. LEAK CHECKED GOOD. OPS CHECKED GOOD. GROUND IDLE RUN CHK OK.Mar 2, 2013 · N580HA · Boeing 76733ASDR KY7A20130304001Fcu · intermittentFLIGHT CREW REPORTED THAT AFTER DEPARTING, THEY EXPERIENCED A MOMNENTARY "SURGE" OF E1 TORQUE ON CLIMBOUT AT 12000 FT MSL, FOLLOWED BY STABILIZATION OF ENGINE OPERATION. MX ADVISED PILOT TO RETURN TO DEPARTURE. RE-ROUTED. ON FINAL APPROACH, PILOT WAS UNABLE TFeb 27, 2013 · N276CA · Swrngn SA226TCSDR SIMA20130223003Fmu · inoperativeON FLIGHT 2827 THE CREW REPORTED AN ENGINE 1 OUT EICAS MESSAGE ALONG WITH NR 1 ENGINE FAILURE. SHUTDOWN AFTER TOUCHDOWN WHILE IN REVERSE THRUST. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED NR 1 ENGINE FUEL PUMP METERING UNIT IAW ROLLS ROYCE Feb 23, 2013 · N831AE · Emb EMB135KLSDR CA130318002Fuel Control · failed(CAN) DURING LANDING ROLLOUT THE ENGINE MADE AN UNCOMMANDED POWER INCREASE, TORQUE LIMITER CUT IN. THE PILOT SHUT THE ENGINE DOWN. TROUBLESHOOTING FOUND A FAULTY FUEL CONTROL WHICH WAS REPLACED BEFORE THE ACFT WAS RETURNED TO SERVICE.Feb 18, 2013 · Beech B200CSDR CA130311005Fuel Control · failed(CAN) DURING T/O ROLL THE NR 1 ENGINE TORQUE OVERSHOT TO 92 PERCENT WHILE THE POWER MANAGEMENT WAS SET AT THE T/O POSITION FOR 90 PERCENT. THE PILOT ELECTED TO ABORT T/O PROCEDURE AT LESS THAN 60 KNOTS. INVESTIGATION LED TO THE REPLACEMENT OF THE FUEL PUMP AFeb 18, 2013 · Aerosp ATR72212ASDR USAA2013021900007Eec · faultyAPPROXIMATELY 30 MINUTES INTO FLIGHT, CREW REPORTED AN ENGINE 1 EPR MODE FAULT. FLIGHT RETURNED TO FIELD AT PHX AND LANDED WITHOUT INCIDENT. NO EMERGENCY WAS DECLARED. FADEC 1A FLT DATA "EPRINI" P/F P5/EEC1. INSPECTED NR 1 EPR TUBES FOR VISIBLE DAMAGE. NONFeb 17, 2013 · N802AW · Airbus A319132SDR UALA2013021400882Eec · malfunctionedRIGHT ENGINE PRI CONT EICAS MESSAGE AFTER START. CREW CONTACTED TOMC. EPCS PAGE SHOWED P PMA-EEC. FAULT WAS ERASED PER TOMC DIRECTION AND DID NOT RETURN WITH ALTERNATE POWER APPLIED TO EEC. UNABLE TO RESTART ENGINE DUE TO APU BLEED ISSUE. NO FAULTS NOW SHFeb 14, 2013 · N550UA · Boeing 757222SDR QMLA2013021313034Fuel Control · malfunctionedAT APPROX 1030 AM WHILE STARTING AN APPROACH INTO THE HOSPITAL. HAD A PRONOUNCED YAW FOLLOWED BY THE NR 2 ENGINE LOW LIGHT COMING ON, OBSERVED THE ENGINE RPM CLIMB TO 110 PERCENT AND DROP OFF, ENGINE RPM FELL BELOW 20 PERCENT AS WELL. AUDIBLE WARNING WAS GOIFeb 13, 2013 · N211SL · Bolkms BK117B2SDR AWHA20130306001Fuel Control · faultyFLIGHT 8662, THE CONDITION LEVER WAS ADVANCED AND THE ENGINE ACCELERATED TO TAKEOFF POWER WITH NO POWER LEVER INPUT. WHEN THE PILOT WENT INTO BETA AND BRAKING WHICH RESULTED IN A CHANGE OF NOISE/PITCH WITH NO NOTICEABLE POWER REDUCTION. PILOT RETURNED CONDITFeb 13, 2013 · N846FE · Cessna 208BSDR CA130130008Fuel Control · malfunctioned(CAN) UPON START UP THE ENGINE DECELERATED FROM 61 PERCENT N1 TO 50 PERCENT N1 WITHOUT PILOT INPUT. THE PILOT TRIED TO ROLL THE THROTTLE UP FURTHER WITH NO N1 REACTION. THE START WAS THEN ABORTED. A LICENSE ENGINEER WAS DISPATCHED TO THE SITE FOR TROUBLESHOJan 25, 2013 · Bell 206BSDR UALA2013012500476Probe · failedLT ENGINE EEC MODE ILLUMINATED, FLT DIVERTED. REPLACED PT2 TT2 PROBE REF MM 73-21-03 ACCOMPLISHED PT2 SYSTEM LEAK TEST NO14 REF MM 71-0 0-00 AND EEC IDLE TEST NO6 REF MM 71-00-00 ALL CHECKED OK.Jan 25, 2013 · N652UA · Boeing 767322SDR KY7A20130128001Fcu · failedON CLIMB THROUGH 14000, FLIGHT CREW NOTED ENGINE TEMPERATURE INCREASING AND TTL BYPASS SYSTEM ACTIVATION. POWER LEVER MOVEMENT HAD NO EFFECT ON ENGINE AND FLIGHT CREW PULLED THE STOP AND FEATHER CONTROL DUE TO OVER-TEMPERATURE CONDITION. ACFT DIVERTED. MX PEJan 24, 2013 · N882DC · Frchld SA227DCSDR REXA2013012300177Fuel Control · out of rigDURING START TO TAKE AIRCRAFT TO THE GATE RECEIVED HOT ICON, NO FUEL APPLIED, FLAMES COMING OUT OF ENGINE AND ENGINE FIRE BOTTLES WERE DISCHARGED. REMOVED AND REPLACED NR 2 FIRE BOTTLE IAW AMM 26-21-10. RIGGED RIGHT FUEL CONTROL IAW AMM 76-10-00. OK FOR SERJan 23, 2013 · N826AY · Cndair CL6002B19SDR CALA2014011590157Eec · faultyLT ENG EEC C1 STATUS MESSAGE ON CONTINUOUS. PLACED ON MEL DF849, HAS HISTORY. BITE OF PIMU FOR LEG 5 SHOWS EEC CH AB FAULT CAT 1. FMU CROSS CHECK FAIL BOTH CHANNELS. NEED TO CHECK FMU & HARNESS IAW 71-PIMU INDEX PG 62V & 62W. TROUBLE SHOT IAW FIM 71-PIMU Jan 12, 2013 · N662UA · Boeing 767322SDR CA130110005Governor · malfunctioned(CAN) PREFLIGHT INSPECTION OF ACFT REVEALED GOVERNOR BIASING SHAFT, PN 206-062-717-1, ON TRANSMISSION DECK TWISTED AT SHEAR POINT. LINEAR ACTUATOR ARM REMOVED AT GOVERNOR ARM, PN 206-061-107-3, TO INSPECT FOR BINDING. GOVERNOR ARM/SHAFT SEIZED. SERVICEABLE BJan 9, 2013 · Bell 206BSDR YENA20130109006Fadec · failedFLT 525 EWR-MCO, AT THE GATE NR 1 ENGINE ONLY OPERATING-GROUND PWR ADDED BUT NOT SELECTED-ELEC DID NOT DISPLAY PROPERLY- THEN THRUST LEVERS REMAINS AT IDLE ENGINE NR 1 INCREASED N1 FROM 20.1 N1 TO 30.1 N1 NO PILOT INPUT- START/ STOP SELECTION SWITCHES SELECTEDJan 9, 2013 · N339JB · Emb ERJ190100IGWSDR DXTA2013020505270Fuel Control · malfunctionedDURING TAXI, AFTER NORMAL ENGINE START, NR 1 ENGINE SHUTDOWN ON ITS OWN. BEFORE SECOND ENGINE START ATTEMPT, EXECUTED SHUTDOWN AND START CHECKLIST, BUT THE NR 1 ENGINE N2 NEVER WENT ABOVE 41 PERCENT. REMOVED DEFECTIVE LT FUEL CONTROL. INSTALLED REPAIRED LTJan 2, 2013 · N102QS · Beech 400ASDR UALA2012121707264Stator · faultyRIGHT ENGINE EEC C1 STATUS MSG, RTFL. REPLACED NR 2 ENGINE EEC ALTERNATOR STATOR. RAN ENGINE, NO MESSAGES, INDICATIONS NORMAL.Dec 17, 2012 · N663UA · Boeing 767322SDR YENA20121216670Fadec · failedFLT 117 JFK-MSY, CREW DECLARED EMERGENCY DUE TO TLA COMP FAIL FOLLOWED SHORTLY AFTER BY ENGINE 1 FAIL. FOLLOWED BY NORMAL SINGLE ENGINE LANDING AT MSY. NO ABNORMAL SIGNS PRIOR TO ENGINE FLAMEOUT ENGINE WINDMILLED THROUGHOUT LANDING ROLL AUTO AND MANUAL RELIGDec 16, 2012 · N292JB · Emb ERJ190100IGWSDR CA121228007Fuel Control · malfunctioned(CAN) THE PILOT REPORTED THAT DURING CLIMB THE NR 2 ENGINE POWER STARTED TO ROLL BACK TO IDLE. THE PILOT ATTEMPTED TO RECOVER POWER BY MOVING THE THROTTLE, WITH NO RESPONSE. THE CREW ELECTED TO LEVEL OFF AND RETURN TO HOME BASE. WHEN THEY ENTERED A CLOUD LAYDec 12, 2012 · Cessna 550
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