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.
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
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 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 PISDR 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 SDR 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.SDR CA130603019Shaft · damaged(CAN) IN FLIGHT SURGE ON NR 1 ENGINE DURING MAINTENANCE OPERATIONS, THE FCU WAS REMOVED AND FOUND INPUT SHAFT DAMAGED.SDR 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 RSDR 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 NOTICEDSDR UALA2013051503372Fmu · faultyAFTER ENG SHUTDOWN EICAS MESSAGE FUEL VALVE RT SHOWED. REPLACED RT ENG FMU IAW AMM.SDR 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.SDR 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 RETURNSDR 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 SSDR 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 AIRCRASDR 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.SDR 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 ASDR 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 SDR 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 ESDR CA130409004Fcu · damaged(CAN) DURING DAILY INSPECTION FOUND MINOR FUEL SEEP FROM FCU BETWEEN FLANGES OF PNEUMATIC SECTION AND MAIN BODY ON LOWER LT SIDE.SDR 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.SDR 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 SDR 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 ISSUESDR 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 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.SDR 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.SDR 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.SDR UALA2013032001704Fcu · malfunctionedLEFT ENGINE ROLLED BACK AFTER START. FLAMES REPORTED. REPLACED LEFT ENGINE FUEL PUMP, FUEL CONTROL UNIT AND EEC.SDR 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.SDR 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 SDR 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 MESDR 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 STICSDR 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 WASDR 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 MODERSDR 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.SDR 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 TSDR 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 SDR 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.SDR 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 ASDR 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. NONSDR 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 SHSDR 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 GOISDR 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 CONDITSDR 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 TROUBLESHOSDR 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.SDR 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 PESDR 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 SERSDR 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 SDR 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 BSDR 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 SELECTEDSDR 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 LTSDR UALA2012121707264Stator · faultyRIGHT ENGINE EEC C1 STATUS MSG, RTFL. REPLACED NR 2 ENGINE EEC ALTERNATOR STATOR. RAN ENGINE, NO MESSAGES, INDICATIONS NORMAL.SDR 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 RELIGSDR 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 LAY
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