GE CF34-8E5

Service difficulty reports · 549

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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 engine_model_key = 'CF348E5'
  ORDER BY difficulty_date DESC"

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SDR 200805141Fmu · faultyFLIGHT 7544 DEN TO IND CREW REPORTED E2 HAD LP VIBE TO 4.0 (IN AMBER) ON CLIMBOUT, PROCEEDED TO PULL POWER BACK UNTIL VIBE STABILIZED. ABOUT 15 MINS LATER IN CRUISE N1 DROPPED TO 25% AND RECEIVED AN E2 CNTRL FAULT. COULD NOT REGAIN CONTROL OF ENGINE AND PERFMay 11, 2008 · N634RW · Emb ERJ170100SE · Fuel Control/Turbine EnginesSDR R61A200800005Uplock Sensor · failedCREW REPORTS THUMPING NOISE UNDER FEET DURING CLIMB OUT. NO EICAS MESSAGES NOTED. CREW FOLLOWED QRH, DIVERTED AND LANDED WITHOUT INCIDENT. MAINT TROUBLESHOT AIRCRAFT AND FOUND RT NR1 MLG UPLOCK SENSOR AND NR1 PSEM MODULE FAILED. REMOVED AND REPLACED UPLOCK SENMay 6, 2008 · N803MD · Emb ERJ170100SU · Landing Gear Position and WarningSDR 200805071Flap System · malfunctionedFLIGHT 7533, ON DESCENT, CREW SELECTED FLAPS (1) AND GOT SLAT FAIL MESSAGE FOLLOWED BY SPOILER FAULT AND SHAKER ANTICIPATED. RECYCLED TO ZERO AND MESSAGES WENT AWAY. ON SECOND RECYCLE SLAT FAIL MESSAGE REMAINED. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INMay 5, 2008 · N636RW · Emb ERJ170100SE · Leading Edge Slat Control SystemSDR 20080306Shroud · damagedFLIGHT 6451 ATL TO MSY ON DESCENT NR 1 ENGINE N1 WAS AT APPROX 25-28%, THE ITT WENT TO AMBER THEN RETURNED TO NORMAL FOR A MOMENT ONLY TO RETURN TO AMBER AND THEN RED. CREW SHUT DOWN NR 1 ENGINE AND LANDED WITHOUT INCIDENT. ENGINE BORESCOPE REVEALED 3RD STAGMar 2, 2008 · N861RW · Emb ERJ170100SE · Turbine SectionSDR 15528Actuator · defectiveSLAT FAIL MESSAGE ON EICAS AFTER TAKEOFF. PILOTS PERFORMED QRH MESSAGE DID NOT CLEAR. PEFORMING TROUBLESHOOTING.Feb 6, 2008 · N606CZ · Emb ERJ170200LR · Leading Edge Slat ActuatorSDR C77A200800005Slat Track · obstructedDURING FLIGHT INBOUND, PILOT SENT ACARS MESSAGE OF SLAT FAIL. A/C PERFORMED A ZERO FLAP LANDING, AND THE PILOT AS NOTED THE BRAKES HAVING A HIGH TEMP. AC PROCEEDED TO GATE UNDER ITS OWN POWER. MAINT THEN PERFORMED THE SLAT-ACE 1 AND 2 TESTS. ALL TESTS COMPLETEJan 27, 2008 · N606CZ · Emb ERJ170200LR · Leading Edge DevicesSDR 200801231Actuator · failedON APPROACH CREW RECEIVED ENGINE 1 CONTROL FAULT EICAS MESSAGE AND A LOW/ABNORMAL N1 INDICATION. SHORTLY THEREAFTER ENGINE 1 ITT ROSE RAPIDLY AND PEAKED AT ABOUT 970 DEGREES. CREW SHUT ENGINE NR 1 DOWN INFLIGHT, DECLARED AN EMERGENCY, AND MADE A NORMAL LANDIJan 20, 2008 · N640RW · Emb ERJ170100SE · Compressor Bleed ControlSDR 200801091Connector · dirtyFLIGHT 9405 DSM TO ATL ON FINAL APPROACH THE CREW EXPERIENCED AN UN-COMMANDED MAXIMUM THRUST ON ENGINE NR 1 LASTING FOR APPROXIMATELY 5 TO 10 SECONDS AND THEN THE THRUST ON THE ENGINE RETURNED TO NORMAL. THE CREW DISENGAGED THE AUTO THROTTLES AND CONTINUED THJan 6, 2008 · N645RW · Emb ERJ170100SE · Engine Fuel System WiringSDR CA070409001Engine · malfunctioned(CAN) ON TAKEOFF ROLL, 1ST OFFICER NOTICE A MOMENTARY FLUCTUATION OF ABOUT 2% ON NR 1 N1 GAGE JUST AFTER THE 80 KNOTS CALL. N1 THEN STABILIZED UNTIL REACHING JUST OVER 100 KNOTS, FLUCTUATED AGAIN. DID NOT HEAR OR FEEL ANY CHANGES IN ENGINE. THERE WERE NO EIMar 30, 2007 · Cndair CL6002D24 · Engine (Turbine/Turboprop)SDR 200703261Accelerometer · defectiveFLIGHT 7542 IAD TO YUL - DURING CLIMBOUT AND DURING CRUISE CREW REPORTED AN NR 2 ENG LP SPOOL VIBE 4.1 DURING CLIMB AND WENT TO 4.0 AT CRUISE. PERFORMED QRH PROCEDURE AND RETURNED TO FIELD. OCM REMOVED AND REPLACED FWD ACCELEROMETER. PERFORMED ENGINE RUNS Mar 22, 2007 · N635RW · Emb ERJ170100SE · Engine Vibration AnalyzerSDR ECI10514Asymmetry Switch · misalignedFLAPS WOULD NOT RETRACT DURING TAXI. FLAP ASYMMETRY FOUND TO BE OUT OF ADJUSTMENT. REMOVED AND REPLACED RT FLAP ASYMMETRY SWITCH WITH NEWLY OVERHAULED SWITCH. REALIGNED ASYMMETRY SWITCHES.Jan 29, 2007 · N919CT · Gulstm GIV · Trailing Edge Flap Control SystemSDR R61A20070002Unknown · unknownDURING A/C DECENT SETTING UP FOR APPROACH CREW REPORTED A SLAT FAIL MESSAGE ON EICAS. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE WAS DISPATCHED TO THE A/C. MAINTENANCE CLEARED SF-ACE INHIBITS, SYSTEM OPERATIONAL CHECK GOOD AND A/C WASJan 26, 2007 · N809MD · Emb ERJ170100 · Leading Edge Slat Control SystemSDR R61A20070001Pump · crackedCREW REPORTED ON APPROACH THEY HAD AN EICAS MESSAGE HYDRAULIC QUANTITY 2 LOW. THEY FOLLOWED QRH AND LANDED WITHOUT INCIDENT TAXIED TO THE GATE. MAINTENANCE WAS DISPATCHED TO THE AC AND FOUND NUMBER 2 ENGINE HYDRAULIC PUMP LEAKING. MAINTENANCE REPLACED PUMP ANDJan 25, 2007 · N828MD · Emb ERJ170100 · Hydraulic Pump (Electric/Engine), MainSDR ECI10513Switch · misalignedFLAPS WILL NOT RETRACT AFTER LANDING. FLAP ASYMMETRY SWITCHES FOUND TO BE OUT OF ADJUSTMENT.Jan 21, 2007 · N919CT · Gulstm GIV · Trailing Flap Position Indicating SystemSDR 200701121Engine · vibrationFLIGHT 7717 MSP TO IAD ON CLIMB CREW NOTICED HIGH LP VIBRATIONS IN ENGINE TWO. RAN THE QRH AND REDUCED POWER TO THE ENGINE. THE VIBRATIONS REMAINED WITHIN LIMITS AT THE REDUCED POWER. COULD NOT RETURN TO NORMAL POWER WITHOUT THE VIBRATIONS GOING OUT OF LIMJan 8, 2007 · N634RW · Emb ERJ170100SE · Engine (Turbine/Turboprop)SDR R61A20060024Control Valve · failedDURING TAKEOFF ROLL FLIGHT CREW RECEIVED PACK 2 FAIL MESSAGE. CREW ABORTED TAKE OFF RETURNED TO GATE MAINTENANCE PLACED SYSTEM ON MEL AND AIRCRAFT WAS RETURNED TO SERVICE. MAINTENANCE CLEARED THE MEL BY REPLACING THE FLOW CONTROL VALVE.Dec 19, 2006 · N823MD · Emb ERJ170100 · Cabin Cooling SystemSDR CA061120005Fan Blade · bent(CAN) ON APPROACH CREW SAW LARGE WHITE BIRD , FELT AND HEARD THUMP ON LEFT SIDE OF AIRCRAFT. MAINTENANCE INSPECTION FOUND #1 ENGINE INLET BYPASS FAN BLADES POSITIONS 1 THRU 5 DAMAGED AND BENT. BORESCOPE OF ENGINE COMPRESSOR FOUND NO OTHER DAMAGE. AIRCRAFT WILLNov 19, 2006 · Cndair CL600* · Turbine Engine Compressor SectionSDR 20060023Skin · crackedDURING HEAVY MAINTENANCE INSPECTION A CRACK WAS FOUND ON THE RT VERTICAL STABILIZER SKIN. THE CRACK IS 7.5 INCH LONG AND IS 4.5 INCH FROM THE REAR SPAR RIVET LINE.Oct 19, 2006 · N822MD · Emb ERJ170100 · Vertical Stabilizer, Plate/SkinSDR R61A200060021Pump · crackedCREW REPORTED NR 2 SYSTEM HYDRAULIC SYSTEM QUANTITY AND PRESSURE WENT TO ZERO. CREW DECLARED AN EMERGENCY DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE REPORTS NR 2 ENGINE HYDRAULIC PUMP IS LEAKING. REMOVED AND REPLACED NR 2 ENGINE HYDRAULIC PUMP OPERATIONOct 18, 2006 · N820MD · Emb ERJ170100 · Hydraulic Pump (Electric/Engine), MainSDR R61A0019Warning Message · illuminatedCREW REPORTED DURING TAKEOFF ROLL ENGINE 2 BLEED OVER PRESSURE MESSAGE ON EICAS. CREW ABORTED TAKE OFF AND RETURNED TO THE GATE. MAINTENANCE INSPECTED AND CHECKED FOR CMC FOUND NO RECORDED MESSAGES SYSTEM OPERATIONAL CHECK NORMAL AND RETURNED THE A/C TO SERVICOct 7, 2006 · N812MD · Emb ERJ170100 · Engine Bleed Air SystemSDR 200610052Bleed Air Sys · warning lightFLIGHT 6443, AT 15 KTS REJECTED TAKEOFF FOR BLEED OVER PRESSURE. MEL`D BLEED NR 1.Oct 3, 2006 · N857RW · Emb ERJ170100SE · Engine Bleed Air SystemSDR 200610051Display · failedFLIGHT 6470, F/O PFD CRACKLED, WENT BLANK, FOLLOWED BY AN INCREASING ELECTRICAL ODOR. REMOVED AND REPLACED F/O PFD.Oct 3, 2006 · N862RW · Emb ERJ170100SE · Central DisplaySDR R61A20060020Warning Message · false activationDURING A/C DECENT SETTING UP FOR APPROACH CREW HAD A SLAT FAIL MESSAGE ON EICAS. CREW DECLARED AN EMERGENCY AND LANDED WITH OUT INCIDENT. MAINTENANCE WAS DISPATCHED TO THE A/C. MAINTENANCE CLEARED S/F ACE INHIBITS SYSTEM OPERATIONAL CHECK GOOD AND AIRCRAFT WASSep 24, 2006 · N828MD · Emb ERJ170100 · Central WarningSDR 200609261Apu · odorCREW NOTICED SMOKE IN THE CABIN AFTER APU STARTED. ORD MX WAS THEN ABLE TO DUPLICATE PROBLEM BUT IT WAS NOT SMOKE LIKE THE CREW CALLED, BUT A STRONG ODOR IN THE CABIN DURING APU START. WHEN APU WAS SHUTDOWN THE ODOR WENT AWAY. APU WAS CAUSING ODOR IN CABIN DUSep 22, 2006 · N647RW · Emb ERJ170100SE · Airborne Auxiliary Power Unit (APU) SystemSDR 200608221Fan Blade · bentFLIGHT 6484 GPT ON TAKEOFF ROLL, APPROXIMATELY 50 KNOTS, CREW EXPERIENCED UNKNOWN AND CONSTANT HUMMING NOISE, NO SIGNIFICANT VIBRATION ASSOCIATED WITH IT. ACCOMPLISHED RTO. OCM DISCOVERED A BENT FAN BLADE IN THE NR 2 ENGINE. FURTHER INVESTIGATION REVEALED NAug 21, 2006 · N863RW · Emb ERJ170100 · Turbine Engine Compressor SectionSDR 28481680Actuator · faultyFLIGHT 7516 ORD TO YUL DURING LANDING CREW RECEIVED MESSAGE ON EICAS ENG 2 FAIL. A/C LANDED WITHOUT INCIDENT, CREW PULLED OFF RUNWAY AND RAN THROUGH QRH NO ABNORMAL SPIKE IN ITT OR ABNORMAL FUEL FLOW NOTED. CREW REPORTS NO OBVIOUS INDICATIONS OF WHY THE ENGINAug 3, 2006 · N860RW · Emb ERJ170100 · Compressor Bleed ControlSDR 200608071Actuator · faultyFLIGHT 7516 ORD TO YUL DURING LANDING CREW RECEIVED MESSAGE ON EICAS ENG 2 FAIL. A/C LANDED WITHOUT INCIDENT, CREW PULLED OFF RUNWAY AND RAN THROUGH QRH NO ABNORMAL SPIKE IN ITT OR ABNORMAL FUEL FLOW NOTED. CREW REPORTS NO OBVIOUS INDICATIONS OF WHY THE ENGINAug 3, 2006 · N860RW · Emb ERJ170100 · Compressor Bleed ControlSDR R61A20060017O-Ring · leakingDURING CRUISE FLIGHT CREW REPORTED NR 2 ENGINE LOST OIL QUANTITY FOLLOWED BY LOW OIL PRESSURE INDICATION WARNING. FLIGHT CREW FOLLOWED QRH PROCEDURES AND SHUTDOWN NR 2 ENGINE IN CRUISE FLIGHT AND DECLARED AN EMERGENCY. DIVERTED TO CLE AND LANDED WITHOUT INCIJul 14, 2006 · N802MD · Emb ERJ170100 · Turbine Engine Oil SystemSDR CA060705001Transducer · malfunctioned(CAN) DURING RIGHT ENGINE WINDMILL RELIGHT, RIGHT ENGINE OIL PRESSURE AT 0 PSI UNTIL 24% N2. AT 34% N2, RIGHT OIL PRESSURE AT 3 PSI. ENGINE SHUT DOWN AND RTB SINGLE ENGINE. NOTE: DURING CRUISE PRIOR TO ENGINE SHUTDOWN, RIGHT ENGINE OIL PRESSURE WAS CONSTANTLY Jul 2, 2006 · Cndair CL6002D24 · Engine Oil PressureSDR R61A20060013Engine · bird ingestionDURING TAKEOFF ROLL CREW VISUALLY NOTED THAT ENGINE NR 1 INGESTED A BIRD, ABORTED TAKEOFF AND RETURNED TO THE GATE WITHOUT INCIDENT. MAINTENANCE PERFORMED INSPECTION AND REPLACED 3 BLADE PAIRS.Jun 1, 2006 · N824MD · Emb ERJ170100 · Engine (Turbine/Turboprop)SDR R61A20060010Pump · crackedCREW REPORTED LOSS OF NR 1 HYDRAULIC QAUNTITY AND PRESSURE. CONTINUED ON TO DESTINATION. DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NR 1 ENGINE DRIVEN HYDRAULIC PUMP CRACKED. REPLACED NR 1 ENGINE HYDRUALIC PUMP AND RETURNED A/C TOMay 10, 2006 · N827MD · Emb ERJ170100 · Hydraulic Pump (Electric/Engine), MainSDR R61A20060009Coupling · misinstalledDURING CLIMBOUT AT 4500 FEET FLIGHT CREW HAD A NR 1 ENGINE FIRE MESSAGE. CREW FOLLOWED QRH PROCEDURES SHUT DOWN ENGINE AND FIRE INDICATION MESSAGE EXTINGUISHED RETURNED TO THE FIELD WITHOUT INCIDENT. EMERGENCY WAS NOT DECLARED. UPON FURTHER INVESTIGATION FOMay 9, 2006 · N803MD · Emb ERJ170100 · Engine Bleed Air SystemSDR 200605082Fmu · malfunctionedFLIGHT 7718 ORF TO ORD CAPTAIN REPORTS ON SHORT FINAL, RECEIVED AMBER -FAIL- BOX ACROSS N1 INDICATOR. DISCONNECTED AUTO THROTTLE; ENGINE INDICATIONS WERE N1 AND N2 SPOOL DOWN, DECREASE IN ITT AND FUEL FLOW. WML INDICATION APPEARED INDICATING RELIGHT ATTEMPT.May 7, 2006 · N652RW · Emb ERJ170100 · Fuel Controlling SystemSDR 200604102Fadec · malfunctionedFLT NR 6491 ORD TO SLC, ON DESCENT AUTO THROTTLES STARTED TO CREATE A SPLIT IN PWR SETTING. CREW CYCLED AUTO THROTTLES, WHEN RE-ENGAGED AUTO THROTTLE SPLIT REOCCURRED. CREW DISENGAGED AUTO THROTTLES AGAIN AND REALIZED THAT N1, FUEL AND N2 WERE ALL SURGING. Apr 7, 2006 · N859RW · Emb ERJ170100 · Fuel Controlling SystemSDR R61A200600005Warning Light · activatedAS SOON AS THE POWER WAS SET TO GO, ADS1 FAIL EICAS AND ASSOCIATED MASTER CAUTION ILLUMINATED. AIRCRAFT WAS UNDER 40 KTS. T/O WAS ABORTED. MESSAGES WERE CLEARED. AIRCRAFT TAXIED BACK FOR A SECOND ATTEMPT. THE SECOND ATTEMPT, BEFORE THE POWER WAS SET, TAT1 FFeb 26, 2006 · N824MD · Emb ERJ170100LR · Flight Environment DataSDR 200602171Turnbuckle · brokenFLT 7631 IAD TO IND, NR 1 ENG FALLING SHORT OF COMMANDED POWER WITH A LAG IN THROTTLE RESPONSE. SHUT DOWN ENGINE, DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. ON INSPECTION, FOUND VARIABLE GUIDE VANE ACTUATOR TURNBUCKLE FAILED. REMOVED AND REPLACED NR 1 ENGFeb 17, 2006 · N653RW · Emb ERJ170100 · Fuel Controlling SystemSDR EMB06002Fadec · unknownMAINTENANCE - COMPLIED WITH TECH SERVICE ITEM DUE TO RECENT HISTORY. REMOVED AND REPLACED NR 2 ENGINE FADEC.Jan 31, 2006 · N818 · Emb ERJ170100 · Fuel Controlling SystemSDR R61A20060003Line · chafedDURING INBOUND FLIGHT 3345 PITTSBURG TO INDIANAPOLIS, HYDRAULIC SYSTEM 2 QUANTITY WENT TO 0. CREW DECLARED AN EMERGENCY LANDED WITHOUT INCIDENT.Jan 16, 2006 · N829MD · Emb ERJ170100 · Hydraulic System, MainSDR R61A200600002Bleed Valve · unknownDURING TAKEOFF ROLL CREW RECEIVED E2 FAIL MESSAGE AND ENGINE SHUTDOWN. CREW ABORTED TAKEOFF AND RETURNED TO THE GATE.Jan 12, 2006 · N810MD · Emb ERJ170100 · Compressor Bleed ValveSDR 200512111Warning System · activatedON CLIMB CREW REPORTED ENGINE 11 AND ENGINE 2 BLEED LEAK INDICATION.Dec 11, 2005 · N646RW · Emb ERJ170100 · Pneumatic Indicating SystemSDR 200512101Bleed Valve · failedCREW REPORTED ENGINE 1 AND ENGINE 2 BLEED LEAK MESSAGE. VERIFIED THAT ENGINE BLEED VALVE FAILED OPEN DURING TAKEOFF.Dec 10, 2005 · N651RW · Emb ERJ170100 · Pneumatic Distribution SystemSDR 200512041Pump · crackedCREW REPORTED LOSS OF PRESSURE IN NR 2 HYDRAULIC SYSTEM DURING CRUISE FLIGHT. FOUND ENGINE 2 ENGINE DRIVEN PUMP WITH CRACK CAUSING LEAK. REMOVED AND REPLACED PUMP.Dec 4, 2005 · N637RW · Emb ERJ170100 · Hydraulic Pump (Electric/Engine), MainSDR EMB05017Control Quadrant · unknownENGINE NR 2 WOULD NOT START. AIRFLOW APPEARS NORMAL FOR START CONFIGURATION, NO N2 OR N1 ROTATION. AIRCRAFT RELEASED ON MEL. 11/23/05 - TROUBLESHOT SYSTEM, REMOVED AND REPLACED THRUST CONTROL QUADRANT W/AUTO. OPERATIONAL CHECK IS GOOD ON GROUND RUN UP.Nov 21, 2005 · N813MA · Emb ERJ170100 · Engine (Turbine/Turboprop)SDR EM05012Engine · shutdownON APPROACH, NR 2 ENGINE AUTO SHUTDOWN. CREW DECLARED AN EMERGENCY & LANDED WITHOUT FURTHER INCIDENT. AS ACFT TAXIED TO GATE, NR 2 ENGINE HAD AN AUTO RESTART. MX BORESCOPED NR 2 ENGINE HPT, NO FAULTS FOUND. DOWNLOADED NR 2 ENGINE FADEC INFO FORWARDED TO GE. Sep 20, 2005 · N802MD · Emb ERJ170100 · Engine (Turbine/Turboprop)SDR EM05004Pump · unserviceableENGINE NR 1 NO DISPATCH FAULT MESSAGE. MAINTENANCE, TROUBLESHOT SYSTEM IAW GE EM 72-00-00 FAULT CODES. REMOVED AND REPLACED FADEC, FAULT REMAINED. REMOVED AND REPLACED FUEL METERING UNIT, FAULT REMAINED. REMOVED AND REPLACED FUEL PUMP, FAULT CLEARED. SYSTMar 6, 2005 · N802MD · Emb ERJ170100 · Engine Fuel PumpSDR EM05005Fadec · malfunctionedFLIGHT 1818, DCA TO CLE - ENGINE ONE NO DISPATCH FAULT MESSAGE. MAINTENANCE TROUBLESHOT SYSTEM IAW GE, EMB FAULT CODES. REMOVED AND REPLACED FADEC AND FUEL METERING UNIT, FAULT REMAINED.Mar 6, 2005 · N802MD · Emb ERJ170100 · Fuel Controlling SystemSDR EM05006Fmu · malfunctionedFLIGHT 1818, DCA TO CLE - ENGINE ONE NO DISPATCH FAULT MESSAGE. MAINTENANCE TROUBLESHOT SYSTEM IAW GE, EMB FAULT CODES. REMOVED AND REPLACED FUEL METERING UNIT AND FADEC, FAULT REMAINED. REMOVED AND REPLACED FUEL PUMP, FAULT CLEARED.Mar 6, 2005 · N802MD · Emb ERJ170100 · Fuel Control/Turbine EnginesSDR CHQA200500026Retaining Ring · missingFLIGHT FROM CURACAO CUR TO FLL FOR AIRCRAFT DELIVERY - AFTER DEPARTING CUR AND CLIMBING TO 38,000 FEET, THE CREW NOTICED THE OIL QUANTITY WAS DIMINISHING ON ENGINE 2. THE OIL PRESSURE BEGAN TO DROP SOON AFTER. THE RIGHT ENGINE WAS SHUTDOWN AND THE AIRCRAFT RFeb 4, 2005 · N645RW · Emb ERJ170100LR · Turbine SectionSDR EM04024Fmu · malfunctionedREMOVED NR 1 ENGINE FADEC FOR TROUBLESHOOTING, NO HELP. REINSTALLED FADEC ON NR 1 ENGINE. REMOVED AND REPLACED NR 1 ENGINE FUEL METERING UNIT. FAULT CLEARED, GROUND POWER ASSURANCE RUN CHECK IS NORMAL.Dec 7, 2004 · N804MD · Emb ERJ170100 · Fuel Controlling System
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