JASC 7320
Service difficulty reports · 4,393
Reports filed under 7320 · Fuel Controlling 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 = '7320' 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 = '7320' 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 CA140130009Hmu · malfunctioned(CAN) ON TAXI OUT OF AC102, FIN456 HAD NR 2 ENGINE FLAMEOUT, THE FLIGHT CONTINUED TO YYZ WITHOUT FURTHER INCIDENT. MOC HAS REQUESTED THAT THE DFDR BE PULLED AND SENT TO YUL FOR PLAYBACK. HMU REPLACED IAW AMM 73-21-10, PB401 CONF 06.SDR ASAA2014012612499Warning Message · false activationAFTER START, ENGINE LIGHT STAYED ILLUMINATED ON FIRST OFFICER`S BOTH ALT MODE LIGHTS ON ENGINE ELECTRONIC CONTROL PANEL CAPTAIN`S IAS DISAGREE. ACFT GROUNDED. PERFORMED EEC BITE TEST REF FIM 73-00, TASK 801, NO FAULTS FOUND, PERFORMED EEC GROUND TEST REF AMMSDR ASAA2014011512397Hmu · malfunctionedWHILE ACCOMPLISHED, FOUND NR 1 ENG WITH FAULT 73-10351, FMV POS SIGNALS DISAGREE - SHORT TIME FAULT. ACFT GROUNDED. PERFORMED ACTUATORS TEST REF MM 71-00-00-700-807-F00 AND EEC TEST REF MM 73-21-00-700-804-F00 BOTH TESTS PASSED. ACCOMPLISHED RESISTANCE CHECKSSDR IPXA4201401171352Hmu · faultedNR 1 ENGINE FAILURE AFTER TAKEOFF, APPROXIMATELY 1000 FT, PRECEEDED BY COMPRESSOR STALL. FUEL JETTISON ACCOMPLISHED BEFORE RETURN TO DEPARTURE. STATUS MESSAGE 71574, TROUBLESHOT IAW FIM 71-00 TASK A09, FOUND HMU FAULTY . R & R HMU IAW AMM 73-21-14 AND CHECKSDR ASAA2014010612335Computer · malfunctionedMAGENTA XB DISPLAYED INTERMITTENTLY IN CLB/DESCENT ADJACENT TO ENGINE NR 2 N2 INDICATION. ALL ENGINE PARAMETERS NORMAL. ACFT GROUNDED. COULD NOT DUPLICATE MALFUNCTION. EEC LOGGED 76-31362 & 73-21352. START LEVER SIG DISAGREE & APL VOLTAGE TO EEC. ACCOMPLSDR HNAA2014010300651Ecu · failedNR 2 ECU FAILED AFTER TAKEOFF. ACFT RETURNED TO, NR 2 ECU FAILED AND WEATHER CONDITIONS TO BAD TO CONTINUE.SDR YENA20140102002Ecu · failedAIRCRAFT DIVERTED, IN FLIGHT WITH NO ASSOCIATED ECAM, STATUS PAGE SAID THE FOLLOWING: WHEN SLAT OUT - ENGINE 2 AT IDLE, ON GROUND, ENG 2 MAXPOWER IDLE. INOP SYSTEMS: REVERSER 2, ENGINE 2 THRUST. THE TECH FOUND FAULTS ASSOCIATED W/ ELECTRONIC ENGINE CONTROL (ESDR CALA2014010290010Probe · malfunctionedENG 1 TT2 & PT2 PROBE HEAT FAIL MESSAGE IS ACTIVE. REPLACED NR 1 ENG PT2 &TT2 PROBE. IDLE RUN TEST NR 6 & NR 7 ZIA 42332.SDR CALA2013123094034Flex Line · damagedNR 2 ENG P5 FLEXIBLE TUBE TO EEC DAMAGED. R & R P5 FLEX LINE IAW MM.SDR IPXA2013123001171Ecu · intermittentEMERGENCY DECLARED - NR 3 ENG BECAME UNRESPONSIVE DURING APPROACH, PHASE OF FLIGHT. ENG CONTINUED TO RUN BUT THROTTLE MOVEMENT DIDN'T CONTROL ENGINE NO CURRENT FAULT ON CFDS. VISUAL CHECK NR 3 ENG NO ABNORMAL FOUND. T/S P IAW FIM 76-11-01-03, FIG 103 SUSPECTSDR HALA2013122400182Fmu · malfunctionedRIGHT ENGINE N1 VARIES INFLIGHT DURING CRUISE. N1 CONTINUALLY OSCILLATES .5 PERCENT AT CONSTANT THROTTLE SETTING. RIGHT ENGINE EPR CHANGES IN RELATION TO N1 CHANGES. REMOVED NR 2 ENGINE FMU REF AMM 73-21-01. INSTALLED SERVICEABLE FMU ON NR 2 ENGINE IAW AMM 7SDR ASAA2013122112205Hmu · malfunctionedAFTER NR 2 ENGINE START, ENGINE CONTROL LIGHT ILLUMINATED. ACFT GROUNDED. ACCOMPLISHED FIM TEST TASK 73-06-801 FOUND FAULT NR 2-75-20582. PERFORMED ACTUATORS TEST IAW 8-732-AMM 71-00-00. ACTUATORS TEST, OPS CHECKED GOOD. NO OTHER FAULTS FOUND. OK FOR SERVISDR DXTA2013122005601Hmu · defectiveON TAXI OUT RT ENG SHUT DOWN, POWER WAS AT IDLE. THE RED ENG FAIL RT MESSAGE POSTED. FOUND RT ENG HMU TO BE CAUSING FUEL DELIVERY DISRUPTION WHEN TRANSFERRING FROM MOTIVE FLOW FUEL SUPPLY TO BOOST PUMP FUEL SUPPLY. R & R RT ENG HMU WITH OVERHAULED HMU. PERSDR VQI2014F00012Hmu · malfunctionedDURING CRUISE, CREW RECEIVED NR 1 ENGINE, NR 2 ENGINE OVER LIMIT ECAM EMESSAGE WITH ASSOCIATED FUEL CONTROL FAULT AND HMU, FMV, ENGINE 1A, 1B, CREW FOLLOWED SHUTDOWN PROCEDURE FOR NR 1 ENGINE AND SENT ACARS MESSAGE TO DISPATCH WITH MSG " ENGINE 1 PRECAUTION SHSDR L2QR201312120001Tube · misinstalledDURING HOT SECTION INSPECTION, FUEL MANIFOLD TUBE ASSEMBLIES WERE INSTALLED INCORRECTLY. TUBES WERE INSTALLED IN REVERSE POSITION AS CALLED OUT IN MM, PN 30B1402, SECTION 73-10-04, PARA B (9). LAST DOCUMENTED REPAIR EVENT ACCESSING THIS LOCATION WAS IN 30 JSDR CALA2013121293627Sense Line · crackedON INBD SIDE OF NR 1 ENG FOUND CRACKED LINE FOR 4.9 AIR SENSING, REPLACED LINE.SDR REXA2013120902224Shaft · shearedAFTER LANDING, RECEIVED A LT ENGINE BLEED CAUTION, THEN LT ENGINE DEGRADED. CAUTION FOLLOWED WITHIN 30 SECONDS BY LT ENGINE FLAMEOUT. DURING THIS WHOLE EVENT, ALL ENGINE GAUGES SHOWED NORMAL. INSPECTED LT ENGINE & FOUND OTBD VG SHAFT SHEARED. R & R VGV SSDR DCGA2013FA0000717Seal · leakingDURING PREFLIGHT CHECKS, PILOT TURNED ON FUEL BOOST PUMPS. NOTICE FUEL COMING FROM THE ENGINE DECK DRAINS. MAINTENANCE DETERMINED THAT THE ENGINE FUEL CONTROL GOVERNOR DRIVE FUEL SEAL WAS LEAKING. THE FUEL CONTROL UNIT WAS REPLACED.SDR SWAA2013121223250Hmu · faultyAIR TURN BACK CLIMBING FROM 12000 TO 15000 NR 2 ENG STARTING SURGING FROM 62% N1 TO 79% N1 WITH AUTO THROTTLES ENGAGED INITIALLY. SURGE CONTINUED WITH AUTO THROTTLES OFF. R & R NR 2 ENG HMU & FUEL PUMP PACKAGE IAW MT.SDR WAIA2014121600012Hmu · faultyFLIGHT CREW REPORTED THAT DURING TAXI OPERATION TOWARDS THE RUNWAY, THE NR 1 ENGINE BEGIN TO SURGE. CREW THEN RETURNED BACK TO FBO. MAINTENANCE TROUBLESHOT THE SYSTEM TO A FAULTY HMU. MX TEAM INSTALLED A REPAIRED HMU, AND NOTICED THAT DURING ENGINE GROUND RSDR CALA2013120993551Sense Line · unsecureENG 3 EEC EICAS CAME ON DEPARTURE. ALL EEC IN ALT MODE IAW PROCEDURE. FOUND EEC SENSE LINE ADRIFT AT NOSE COWL BULKHEAD, DUE TO FLEX LINE ADAPTOR FITTING MISSING. CF CREATED FOR SUBSTITUTE CONNECTION.SDR SWAA2013121123169Hmu · faultyAIR RETURN ON TAKEOFF NR 1 ENG WOULD NOT GO ABOVE APPROXIMATELY 62%. R & R NR 1 ENG HMU MT.SDR XV6A2013112500009Shutoff Valve · stuckLEFT ENGINE FIRE BOTTLE FIRED DUE TO FIRE INDICATION DURING VENT. 1C EMERGENCY EXIT REMOVED FOR POSSIBLE GROUND EVAC. ENGINE VENT WAS DUE TO ABORTED START, LEFT ENGINE HUNG AT 32-33 PERCENT, NO TEMP LIMIT REACHED - 60 SECONDS. DURING TROUBLESHOOTING OF NR 3SDR UIEA2013112200566Hmu · malfunctionedDURING LT TURN INTO PARKING ADDED POWER FOR TURN, NR 4 ENG NO RESPONSE. R & R 4 ENGINE HMU IAW MM 72-21-14. RAN ENGINE AND PERFORMED MM 71-00-00 TEST 3, 12 AND 2 ENGINE RESPONSE NORMAL.SDR CA131202018Governor · malfunctioned(CAN) GOVERNOR CAUSING LOW ENGINE RPM. GOVERNOR REPLACED.SDR ASAA2013111896413Controller · faultedNR 2 ENGINE HAS FAULT CODES 75-10362 HPTACC POSITION SIGNAL IS OUT OF RANGE, 75-20412 HPTACC POSITION SIGNAL DISAGREE, 75-10412 HPTACC POSITION SIGNAL DISAGREE. ACFT GROUNDED. CONFIRMED FAULT, NR 2 EEC BITE FAULT HISTORY SHOW FAULT CODES 75-10362, 75-20412,SDR QMLA2013111413167Sense Line · crackedIN CRUISE FLIGHT WHILE ON A SCENE STANDBY, THE ENG OIL PRESS LIGHT ILLUMINATED WITH CORRESPONDING OIL PRESS GAGE INDICATION OF ABOUT 1.2 BAR. WE ANNOUNCED A PRECAUTIONARY LANDING, SIMULTANEOUSLY COMMENCED AN IMMEDIATE POWER ON LANDING, TOUCHING DOWN APPROXIMASDR SIMA20131111001Fadec · malfunctionedCREW REPORTED DURING CLIMB ABOVE FL270, NR 1 ENGINE ROLLED BACK TWICE LOSING 10 PERCENT N1, WOULD NOT ACCELERATE AT CRUISE ALTITUDE. THRUST WAS IN DETENT AND AT FULL POWER, THRUST LEVERS WERE NOT LOOSE, CRUISE ALT FL 370. ALL ENGINE INDICATIONS REMAINED INSDR CA131101002Drain Line · chafed(CAN) DURING REPLACEMENT OF THE NR 1 HYDRAULIC EDP, IT WAS NOTICED THAT THE ECS FUEL DRAIN LINE WAS CHAFED. LT ENGINE ECS FUEL DRAIN LINE, PN CN627-8035-001, AIPC 71-71-03, FIG 5-35, REPLACED. ENGINE, PN CF34-8C5, SN 194345, TSN 15594, CSN 8288, TSR 2303, CSSDR CA131105001Module · malfunctioned(CAN) DURING GROUND CHECKS, IT WAS FOUND THAT THE ENGINE CONTROLS DID NOT RESPOND TO POWER LEVER MOVEMENTS WHEN THE GOVERNOR SWITCH WAS SELECTED TO MANUAL MODE. FUEL MANAGEMENT MODULE REPLACEMENT RECTIFIED THE PROBLEM.SDR CALA2013101191973Eec · failedLEFT ENGINE EEC MALFUNCTIONED. REPLACED EEC IAW MM 73-21-04 AND ACCOMPLISHED NR 1 ENGINE RUN. NO STATUS MESSAGE ON SHUTDOWN.SDR QMLA2013101013141Valve · failedFOUND FUEL PRESSURIZING VALVE ON NR 2 ENGINE INOPERATIVE, ALLOWING TOO MUCH FUEL TO ENTER ENGINE AT START. RAW FUEL WAS BEING PUSHED THROUGH THE ENGINE ON START AND FLOWING INTO THE COWLINGS OF ACFT. IN FLIGHT THE TRAPPED FUEL WAS SEEPING OUT OF THE COWLINGSSDR DJFA20131009001Fdu · low pressureDURING INITIAL DESCENT FROM CRUISE, CREW NOTED SLIGHT (200LBS) FUEL IMBALANCE. CROSSFEED FROM RT TANK WAS ACTIVATED MANUALLY. WITHIN 15 TO 30 SECONDS CREW NOTED INDICATIONS OF UNCOMMANDED LT ENGINE SHUTDOWN. ENGINE RESTART PROCEDURE WAS INITIATED WITH SUCESSDR CALA2013100991885Probe · faultyON TAXI OUT LT ENG EEC MODE EICAS MESSAGE. ITEM ROLLED FORWARD. REPLACED PT2 TT2 PROBE IAW 73-21-03 PN 0154ED2. RAN ENG, OPERATIONS CHECKED GOOD. NO FAULTS FOUNDSDR ABXA20131008576Gpu · malfunctionedLEFT ENGINE VERY SLOW TO RESPOND WITH THROTTLE ADVANCEMENT. ON BLOCK IN, LT ENGINE ADVANCED UNCOMMANDED, THROTTLE IN IDLE POSITION, TO APPROXIMATELY 80 PERCENT, N2. PERFORMED ENGINE RUN IAW 74-00-00-2, NO DEFECTS NOTED. AS FAR AS ENGINE GOING TO FLIGHT IDLESDR CALA2013093091538Knob · faultyFCU ALTITUDE SELECT KNOB HAS NO SPRING. ENTERS OPEN DESCENT MODE AT A TOUCH. BUTTON HAS NO RESISTANCE WHEN SELECTING ALTITUDE IT WILL ENGAGE OPEN DESCENT EASILY. R & R FCU BORROWED FROM JETBLUE, FUNCTIONALLY CHECKED GOOD, IAW 22 81 12 400 001A, OPERATIONS TESDR AALA20130916006Valve · leakingIND CREW REPORTED RT ENGINE LOSS OF POWER. CREW ACCOMPLISHED IN-FLIGHT SHUT-DOWN OF RT ENGINE. EMERGENCY DECLARED FLIGHT RETURNED IND LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND FUEL PRESSURIZING & DUMP VALVE LEAKING. REPLACED RT NR 2 P &SDR ASAA2013091295970Valve · faultedWHILE PERFORMING T/C 78273000, FOUND NR 2 ENGINE FAULT 75-20462 HPTACC DEMAND & POSITION DISAGREE. ACFT GROUNDED. ACCOMPLISHED TASK CARD 78273000 AGAIN, NR 2 ENGINE FAULT REMAINS ACTIVE. REPLACED HPTACC IAW AMM 75-21-01 SYSTEM OPS CHECKED GOOD IAW AMM 71-00SDR CA130916005Fadec · malfunctioned(CAN) DURING CRUISE, THE ACFT ENCOUNTERED A NR 2 ENGINE SHUTDOWN. AS A PRECAUTION, THE FLIGHT CREW DECLARED A PAN PAN FOR PRIORITY TO DESCEND. INTERROGATED CMC, ENGINE NR 2 NO DISPATCH EICAS MESSAGE AND FADEC NR 2 FAULT ADVISORY. FADEC NR 2 REPLACED IAW AMMSDR CALA2013090991143Interface Unit · faultyNR 2 ENGINE APPROXIMATELY IDLE RPM HIGH, NR 2 READS 75. REPLACED NR 2 PDIU. ACCOMPLISHED SUCCESSFUL BITE TEST & ENGINE APPLIED IDLE TEST IAW JRH 2-500-2. ALL PARAMETERS NORMAL.SDR IPXA3580134Eec · malfunctionedRT ENGINE INFLIGHT SHUTDOWN, DUE TO HIGH OIL TEMP. COMPLIED WITH HIGH OIL TEMP PER MM 72-00-00-206-547-P00. COMPLETED INSPECTION PER MM 72-00-00-206-547-P00. EEC REPLACED. RAN ENGINE AT MULTIPLE THROTTLE SETTINGS FOR 30 MINUTES. ALL ENGINE PARAMTERS NORMALSDR Z5FA2013090643001Fuel Control · failedENGINE FLAMED OUT ON SLOW DESCENT BELOW 37,000 FT. LOW PRESSURE FUEL LIGHT FLASHED THEN BOOST PUMP AS ENGINE FLAMED OUT. ENGINE WAS RESTARTED ON FIRST TRY IAW PROCEDURES AT 10,000 FT. NO EMERGENCY WAS DECLARED. ACFT LANDED SAFELY. ENGINE WAS INSPECTED AND FUSDR UIEA2013083000490Filter · failedSTATUS MESSAGE RT ENG FUEL FILTER. R & R FUEL FILTER IAW AMM 73-11-02/401, LEAK CHECK OK. MESSAGE ERASED.SDR UIEA2013083000484Eec · failedLT ENGINE CONTROL STATUS MESSAGE, REPLACED LT ENGINE EEC, ECU IAW AMM 73-21-15, OPS CHECK NORMAL.SDR ASAA2013082795892Hmu · malfunctionedCLIMBING THOUGH 17,000 FT, NR 2 ENGINE SURGED CONTINUALLY. RAN SURGE CHECKLIST, THROTTLE ALMOST CLOSE WHEN ENGINE STALLED, ENGINE THEN FAILED. COMPLETED CHECKLIST AND RETURNED DEPARTURE. ACFT GROUNDED. ACCOMPLISHED EA 700-72EA-10951. NR 2 ENGINE HMU REPLSDR HNAA2013082200474Eec · failedNR 2 TORQUE SLOW TO ADVANCE DURING TAKEOFF ROLL. TORQUE READS 0 PERCENT AT FLIGHT IDLE. R & R NR 2 EEC PERFORMED ENG RIG WC 70-00-02Q. OPS CHECKED GOOD.SDR CA130822007Fmu · malfunctioned(CAN) AFTER AN UNEVENTFUL CLIMB, THE CHECKS WERE NORMAL BUT LESS THAN A MINUTE LATER THE NR WAS NOTED AT 101 PERCENT SHORTLY FOLLOWED BY 102 PERCENT. THE CREW REPORTED AS THE DESCENT WAS IMMINENT, THE POWER RESPONSE AND ON LOWERING THE COLLECTIVE THE NR INCRESDR CA130822001Flow Divider · leaking(CAN) DURING REVENUE FLIGHT AFTER TAKEOFF REACHING 9,000 FT, THE MASTER AND CAUTION LIGHT ILLUMINATED INDICATING FIRE ON THE LT ENGINE. EMERGENCY PROCEDURES WERE FOLLOWED AND AFTER 6 TO 7 MINUTES THE FIRE EXTINGUISHED, BOTH FIRE BOTTLES WERE USED. ACFT RETURSDR USAA2013081600002Eec · faultyDURING CRUISE, STS PAGE SHOWED INOPERATIVE SYSTEMS REVERSER 2 AND ENG 2 THRUST. ENGINE PARAMETERS NORMAL WITH AUTO THRUST ENGAGED. AT LANDING, NR 2 THRUST REVERSER WORKED AND ENGINE RESPONDED NORMAL. AN EMERGENCY WAS DECLARED BY THE CAPTAIN. MX R & R THE NR SDR CALA2013081390426Packing · leakingNR 2 ENGINE FUEL PUMP LINE TO FCOC LEAKING AT FUEL PUMP. REPLACED PACKING. NO LEAK PRESENT ON ENGINE RUN.
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