JASC 7320

Service difficulty reports · 4,393

Reports filed under 7320 · Fuel Controlling System, newest first.

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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 jasc_code = '7320'
  ORDER BY difficulty_date DESC"

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SDR CA090109005Line · broken(CAN) AIRCRAFT TOOK OFF WITH NORMAL POWER. SHORTLY AFTER TAKEOFF NR 1 ENG TORQUE ROLLED BACK TO 45-50 PERCENT, ECU MANUAL ON OR OFF NO CHANGE. AIRCRAFT CONTINUED TO DESTINATION FOR NORMAL LANDING. MAINTENANCE INSPECTION FOUND `P3` LINE FAILED/BROKEN AT END Jan 7, 2009 · Dhav DHC8102SDR 2009FA0000025Metering Unit · malfunctionedWHILE ON A TRAINING MISSION, THE PILOT NOTICED THE FUEL FLOW WAS 18 GPH DURING CLIMB, PILOT REPORTED FUEL FLOW WAS NORMAL ON TAKEOFF. ON TROUBLESHOOTING, THE MX FOUND THE ARM ON THE MIXTURE SIDE WAS VERY ROUGH. FUEL METERING UNIT WAS REPLACED AND RUN-UP WAS Jan 7, 2009 · N5581T · Beech F33ASDR HNAA200911200393Bypass Switch · failedNR 1 FUEL FILTER BYPASS CAUTION LIGHT ILLUMINATED WHEN SETTING TAKE OFF POWER THEN EXTINGUISHED WHEN POWER REDUCED TO FLIGHT IDLE. R&R NR 1 HIGH PRESSURE FILTER AND BYPASS SWITCH. INSPECTED OLD FILTER NO DEBRIS FOUND. GROUND RUN ACFT OPS CHECK GOOD. LOW PREJan 7, 2009 · N982HA · Dhav DHC8102SDR HEEA123017Hmu · malfunctionedAIRCRAFT YAWED LEFT SUDDENLY FOLLOWED IMMEDIATELY BY DECREASE IN ENGINE NOISE, LOSS IN ALTITUDE, ACTIVATION OF LOW RPM AUDIO AND FADEC FAIL AUDIO. CAUTION LIGHTS THAT ILLUMINATED WERE FADEC FAIL, FADEC DEGRADED, RESTART FAULT, AUTO RELIGHT AND RPM, FADEC MODEJan 5, 2009 · N401PH · Bell 407SDR ASAA0954159Hmu · contaminatedON CLIMBOUT (FUEL FILTER BYPASS) NR1 ENG ILLUMINATED. AFTER INITIATING RETURN TO BASE, FUEL FITER BYPASS LT EXTINGUISHED AND REMAINED SO FOR REST OF FLIGHT. ALL ENG PARAMETERS NORMAL. FUEL TEMP NEVER BELOW +8 DEG CELSIUS, GROUNDED, YES. BITE TEST ENG NR1 NO RJan 5, 2009 · N585AS · Boeing 737890SDR U2RA872LP2993Cable · out of rigNR 1 ENGINE FLAMED OUT AT IDLE AT 30,000 FT. BEGAN PERFORMING ENGINE FLAMEOUT ABNORMAL CK LIST. ENGINE RELITE AND PERFORMED NORMALLY AFTER IGNITION TURNED ON. FINISHED ABNORMAL CK LIST. WEATHER VMC. PERFORMED PULL, TRAVEL AND RIGGING CHECKS OF VBV AND VSV Dec 25, 2008 · N872SJ · Doug DC871FSDR Q2SA753005Sensor · failedON TAKE-OFF FROM LEIGE, BELGIUM (EBLG), NR 2 ENGINE FLAMED OUT. LOUD NOISE HEARD AND AIRCRAFT YAWED LEFT. IGNITION AND ENGINE ANTI-ICE IN USE. ENGINE RELIGHT AT 3000' AGL, ALL PARAMETERS NORMAL. AIRCRAFT CONTINUED TO DESTINATION AT DOHA, QATAR (OTBD). NO Dec 25, 2008 · N753SA · Boeing 747228FSDR SWAA087303Sensor · faultyAIR TURNBACK - BETWEEN 10K & 15K FT ON CLIMB NR 1 N1 WAS 80 PERCENT OR 12 LESS THAN NR 2 N1. MOVED NR 1 THRUST LEVER TO STOP, NO DIFFERENCE, TURNED PMC NR 1 OFF NO DIFFERENCE. REMOVED AND REPLACED NR 1 ENGINE CIT SENSOR PER MM.Dec 23, 2008 · N528SW · Boeing 7375H4SDR ZESA2008015Fuel Control · intermittentON 12/12/08 THE "FUEL BOOST PUMP ON R" AMBER CAS MESSAGE DISPLAYED IN FLIGHT. THE MOTIVE FLOW PRESSURE SWITCH WAS REMOVED AND REPLACED AND THE SYS CHECKED OUT. ON 12/13/08 THE SAME INDICATION CAME ON. THE RT BLEED VALVE SOLENOID WAS REMOVED AND REPLACED ANDDec 12, 2008 · N44M · Cessna 680SOVSDR CA081212003Plug · loose(CAN) DURING A ROUTINE CHECK, A FUEL LEAK WAS DISCOVERED COMING FROM THE NR 2 ENGINE MFC. UPON FURTHER INVESTIGATION A PLUG WAS FOUND LOOSE. THE PLUG WAS REMOVED, THE O-RING REPLACED AND THE PLUG RE-INSTALLED. A LEAK CHECK WAS CARRIED OUT WITH NO LEAKS NOTEDec 12, 2008 · Cndair CL6002B19SDR DL75E081675Eec · malfunctionedL ENG SEC CONT STATUS MESSAGE DISPLAYED, UNABLE TO CLEAR OUT RAN NR 1 ENG SEVERAL TIMES AND SELECT EEC TO ALTN POSITION NO MSG ARE NOTED. PERFORMED VISUAL INSPECTION ALL WIRING CHECK OK FOUND LOOSE CONNECTOR AT TCA AND J1 CONNECTOR ON EEC, AS PRECAUTION AND DNov 30, 2008 · N718TW · Boeing 757231SDR ASAA0853880Gasket · leakingRIGHT ENGINE HAS FUEL LEAK FOUND FUEL TUBE GASKET CONNECTING TO HMU LEAKING. VERIFIED FUEL LEAK DURING IDLE LEAK CHECK. REMOVED & REPLACED GASKET REF MM 73 21 10 400 801 F00 (ITEM 34) FIG 401. IDLE LEAK CHECK GOOD.Nov 23, 2008 · N587AS · Boeing 737890SDR DXTA200811223366Computer · malfunctionedNR 1 COMPUTER LIGHT ILLUMINATED ON TAKEOFF ROLL AT APPROX 60KTS. ABORTED TAKEOFF. DOWNLOAD DEEC AND FOUND ECTM DATA BUFFERS FULL. CLEANED ECTM DATA. PERFORMED IDLE RUN AND OPS CHECKS IAW MM.Nov 22, 2008 · N893QS · Raythn HAWKER800XPSDR ASAA0853877Hmu · leakingDURING LEAK CK OF REPLACEMENT OF NR 2 ENGINE NOTED HMU TO BE LEAKING AT THE TOP SURFACE FITTING/ADJUSTING SCREW CAP JUST AFT OF THE SUPPLY FUEL LINE. LEAK IS COMING FROM THE PARTING LINE BETWEEN HMU AND CAP REPLACED NR 2 ENGINE HMU PER AMM73 21 10 400. OPS ANov 21, 2008 · N587AS · Boeing 737890SDR HALA2008112000865Eec · failedETOPS SIGNIFICANT SYSTEM, STATUS MESSAGE LT ENG EEC C1 DISPLAYED. PIMU BITE SHOWS EEC CH-A/B B25 FD-BK FAIL. PERFORMED CORRECTIVE ACTION PIMU MSG INDEX AND FIM 73-21-00. REMOVED CONNECTOR FROM 2.5 BLEED VALVE AND CHECKED PINS NO TROUBLE FOUND. RESEATED CONNov 20, 2008 · N591HA · Boeing 76733ASDR M7KA1006084142Actuator · intermittentGOVENOR LIGHT ILLUMINATES INTERMITTENTLY WITH THIS EMERGENCY BACKUP CONTROL. ACTUATOR INSTALLED.Nov 17, 2008 · N822MH · Urocop EC130B4SDR DL76L081591Stator · damagedDURING ACCOMPLISHMENT OF EA 51-470869-12 REV H MAINTENACE FOUND PMA STATOR HAD INTERNAL DAMAGE AND REPLACED THE STATOR, STATOR PN 2710540-1 WITH DEPT 335 AS PRIME SHOP. FAA HAS REQUESTED SDR AND QA FOLLOW-UP WITH VENDOR TO CONFIRM DAMAGE AND DETERMINE IT'S SONov 14, 2008 · N197DN · Boeing 767332SDR FJT08116572Bellows · collapsedENROUTE, DURING CLIMBOUT, RT ENGINE BECAME UNRESPONSIVE TO POWER LEVER INPUT. INDICATED TORQUE WAS 100 PERCENT. CREW SHUTDOWN RT ENGINE PRIOR TO LANDING. ACFT LANDED WITHOUT FURTHER EVENT. R & R P2T2 SENSOR DUE TO COMPLETELY COLLAPSED BELLOWS AT INPUT TO FNov 13, 2008 · N657BA · Bag JETSTM3101SDR DXTA200811123352Flow Divider · misriggedRT ENGINE QUIT ON LANDING ROLL OUT. ENGINE QUIT WHEN RT THROTTLE WAS BROUGHT TO IDLE. RT THROTTLE SEEMS TO HAVE AN EXCESSIVE AMOUNT OF SLOP WHEN BROUGHT BACK TO IDLE THRUST. VERIFIED DISCREPANCY, FOUND RT ENGINE CONTROLS AT FCU AND FUEL FLOW DIVIDER IMPROPERNov 12, 2008 · N302QS · Cessna 560CESSNASDR FJT08116571Restrictor · obstructedENROUTE, DURING CLIMBOUT, RT ENGINE BECAME UNRESPONSIVE TO POWER LEVER INPUT. INDICATED TORQUE WAS 100 PERCENT. CREW SHUTDOWN RT ENGINE PRIOR TO LANDING. ACFT LANDED WITHOUT FURTHER EVENT. OPERATED ENGINE APPROX 3 HOURS LATER AND NO DEFECTS NOTED. INSPECTNov 11, 2008 · N657BA · Bag JETSTM3101SDR HAEA200800205APump · failedENGINE RPM ROLLED BACK FL430 PLUS 30 MINUTES. AIRCRAFT DESCENDED TO FL 150 AND DIVERTED TO GSP. MAINTENANCE DISCOVERED ENGINE DRIVEN FUEL PUMP FAILED. REPLACED FUEL CONTROL/FUEL PUMP ASSY. NO FURTHER DEFECTS.Nov 10, 2008 · N525TW · Lear 25SDR ASAA0853708Probe · malfunctionedNR 2 ENG N1 FLUCTUATION RAPIDLY FORM 91.2 TO 100.1 BETWEEN ABOUT 2500FT TO 6000FT ON CLIMBOUT, AUTOTHROTTLE WAS FOLLOWING. ALL OTHER ENGINE PARAMETERS APPEAR NORMAL. ABOVE 6KFT ALL NORMAL. NR 2 ENG EEC LOGGED FAULTS 73-30902-T12 SIGNALS DISAGREE 73-21702 ADINov 7, 2008 · N586AS · Boeing 737890SDR DL75E081362Shutoff Valve · fodDURING PREFLT FOR FUEL CONTROL CHANGE HAD LOW AIR FROM NR 1 ENG AFTER REMOVING HPSOV FOUND METAL STRIPS INSIDE VALVE. CONSULTED ENGINE SHOP AND DETERMINED TO BE AIRSEAL FROM 12TH TO 13 STG COMPRESSOR SECTION. REPLACED NR 1 ENGINE PER TRANS 6T103.Oct 14, 2008 · N722TW · Boeing 757231SDR CA081025002Bracket · broken(CAN) ENGINE AUTO IFSD, ACFT DIVERTED TO ATL UNEVENTFUL LANDING. FSO CABLE RELEASE, PIECES FOUND IN THE TAILPIPE. LPT3 SCUFFED AND NICKED CONSISTENT WITH CABLE DAMAGE. NO EVIDENCE OF A TURBINE FAILURE. LP SYSTEM FREE TO TURN SMOOTHLY. ENGINE IN RRC FOR INVESTIOct 10, 2008 · Boeing 717200SDR CA081007001Fadec · malfunctioned(CAN) DURING PUSH-BACK FROM THE GATE WITH BOTH ENGINES RUNNING (PROPS FEATHERED), THE NR 2 ENGINE HAD AN UN-COMMANDED SHUTDOWN WITH AN ASSOCIATED NR 2 ENG FADEC FAIL WARNING LIGHT AND POWERPLANT MSG. INTERROGATION OF THE CDS REVEALED THE FOLLOWING FAULT CODESOct 3, 2008 · Bombdr DHC8400SDR 2008UALA05956Eec · faultedENG LOW IDLE L DURING DESCENT. REPLACED ELECTRICAL ENGINE CONTROL. REPLACED IDLE SOLENOID RELAY K434, AIR-GRD BAT RELAY K167, AND RELAY K785. CLEANED CONNECTORS ON FCU. OKAY FOR SERVICE.Sep 30, 2008 · N643UA · Boeing 767322SDR DL76L081206Eec · malfunctionedAFTER LEFT ENG START, LT ENG CONTROL STATUS MSG APPEARED FOLLOWED BY LT ENG C2 STATUS MSG. PERFORMED LT ENG PIMU READOUT. FOUND BITE MSG CH-A LOST POWER AND CH-B UNIT FAIL. CYCLED EEC C/B AND PIMU RESET. ALL MESSAGES CLEARED. RAN LT ENG IN DLE AND NO FAULSep 21, 2008 · N180DN · Boeing 767332SDR DL76L081207Rotor · damagedRT ENG EEC MSG, AUTO THROTTLES INOP, RT CTR FUEL PUMP, NO RT ENG N2 DISPLAY. ALL OCCURRED INFLT EN ROUTE TO CVG. FOUND PMA ROTOR DAMAGED DUE TO DRIVE ASSY FAILURE. BEARING PIECES MISSING AND PRESUMED TO HAVE ENTERED THE GEARBOX WHEN BEARING FAILED. METAL OSep 20, 2008 · N198DN · Boeing 767332SDR FDEA200808293646Hmu · failedNR 1 ENGINE N1 INDICATION BECAME UNSTABLE DURING CLIMB. REPEAT WRITE-UP. THEN EGT EXCEEDED LIMITS AT 952 DEG THEN FUEL FLOW INDICATION BECAME UNSTABLE WITH SURGING AND YAW. PULLED TO IDLE N-1 AND FF INDICATION REMAINED UNSTABLE BUT SURGING STOPPED. PERFORMAug 29, 2008 · N661FE · Airbus A300F4605RSDR FDEA200808293645Ecu · failedDURING CLIMB NR 2 ENG N1, FF, EGT BECAME UNSTABLE, ASSOCIATED WITH ENGINE SURGING. FADEC GRD TEST, FOUND FAULT CODE 352-21 ON CH A. N1 SPEED SENSOR PERFORMED TSM PROCEDURE 73-21-30 352-21 FIG 102 SHEET 28. CHECKED BOTH CH A AND B SYS GOOD. SPEED SENSOR IS Aug 29, 2008 · N681FE · Airbus A300F4605RSDR 08FDEA03646Hmu · failedNR 1 ENGINE N1 INDICATION BECAME UNSTABLE DURING CLIMB. REPEAT WRITE-UP. THEN EGT EXCEEDED LIMITS AT 952 DEG. THEN FUEL FLOW INDICATION BECAME UNSTABLE WITH SURGING AND YAW. PULLED TO IDLE N-1 AND FF INDICATION REMAINED UNSTABLE BUT SURGING STOPPED. PERFORAug 29, 2008 · N661FE · Airbus A300B4605RSDR 08FDEA03645Ecu · failedDURING CLIMB NR 2 ENG N1, FF, EGT BECAME UNSTABLE, ASSOCIATED WITH ENGINE SURGING. FOLLOWING NR 2 ENG FADEC BITE DISPLAY: BITE CHA CHB 270 84120 84120 271 99080 99080 272 20000 20000 273 274 ON 350-354. FADEC GROUND TEST: FOUND FAULT CODE 352-21 Aug 29, 2008 · N681FE · Airbus A300B4605RSDR CA080912002Hmu · malfunctioned(CAN) ACFT EXPERIENCED LOSS OF POWER TO FLIGHT IDLE (FI) ON LT ENGINE DURING FLIGHT WHICH LEAD TO A COMMANDED ENGINE IN-FLIGHT SHUTDOWN + RESTART WITH INABILITY TO GO ABOVE FI. FLIGHT WAS DIVERTED WHERE THE A/C LANDED WITH THE LT ENGINE AT FI POWER. EXTENSIVE Aug 26, 2008 · Beech 400ASDR SIMA200824101Fmu · malfunctionedON FLIGHT 3576 CREW REPORTED ENGINE 1 POWER FLUX N1 ITT, N2, IGNITION A&B AUTO RELIGHT AND FADEC TRANSFER IN FLIGHT FOR ABOUT 39 SECONDS. THRUST SURGED UP/DOWN CONTINUED FROM ABOVE TRUST LEVERS AT FLT IDLE. ENGINE 1 STABILIZED. NO ABNORMAL INDICATIONS AFTERAug 26, 2008 · N240DS · Saab 340BSDR 08FDEA03600Sensor · failedNR 1 ENGINE N1 INDICATION BECAME UNSTABLE DURING CLIMB. REPEAT WRITE-UP. THEN EGT EXCEEDED LIMITS AT 952 DEG THEN FUEL FLOW INDICATION BECAME UNSTABLE WITH SURGING AND YAW. REMOVED AND REPLACED THE FUEL FILTER AND THE TEMP INLET SENSOR (T 1.2). REF AMM 73-Aug 26, 2008 · N661FE · Airbus A300F4605RSDR K2D2008F00000Pressure Switch · leakingON OR AROUND 5:00 PM, WEDNESDAY, 6 AUGUST, 2008, WHILE CONDUCTING A POST FLIGHT INSP, DISCOVERED SOME OIL LEAKAGE IN ENGINE COMPARTMENT. AS HE WAS INVESTIGATING LEAKAGE, NOTICED THAT THE FUEL FILTER PRESSURE SWITCH HAD PLAYED BETWEEN TWO BODY HALVES AND HAD SAug 6, 2008 · N500PH · Hughes 369ESDR 08FDEA03093Hmu · failedAPPROACHING CRUISE ALTITUDE GOT A LEVEL 2 'ENG 2 N2 LOW' FOLLOWED BY A ROLL BACK ON ENG 2. ALL INDICATIONS INDICATED FLAME OUT. ACCOMPLISHED QRH PROCEDURES AND LANDED WITHOUT INCIDENT. DID NOT ATTEMPT A RESTART. PERFORMED ENGINE POST-WINDMILLING INSPECTIONJul 26, 2008 · N576FE · Doug MD11FSDR CIE2008F00003Fcu · malfunctionedWHILE PERFORMING ENGINE RUN UP AT RUNWAY 36R RUN UP, LT ENGINE WAS FOUND TO BE UNRESPONSIVE AFTER LT ENGINE PROP GOVERNOR CHECK WAS COMPLETE. N1 DROPPED BELOW 50 PERCENT AND CONTINUED TO DROP. FUEL FLOW ALSO DROPPED AND CONTINUED TO DROP. ENG WAS THEN SHUTDJul 17, 2008 · N60PD · Beech 200BEECHSDR SWAA084048Mec · faultyDURING DESCENT NR 1 ENGINE HANG UP AT 50% FOR TWO TO THREE MINUTES, THEN ROLLS BACK. R&R NR 1 MEC PER MM.Jul 17, 2008 · N686SW · Boeing 737317SDR SWIA200819956Line · chafedLEFT ENGINE FUEL CONTROL AMBIENT SENSE LINE IS CHAFED THROUGH AT SUPPORT CLAMP. FOUND AT C-CHECK. REPLACED LEFT ENGINE FUEL CONTROL AMBIENT SENSE LINE AS PER CRJ200 AMM 73-21-15-400-803. Jul 16, 2008 · N442SW · Cndair CL6002B19SDR C2X2008F00010Fcu · inoperativeFLIGHT 2245 - OKC - FLIGHT CREW REPORTED VENTRAL TANK FAIL MESSAGE ON EICAS. CREW DIVERTED FLIGHT AND LANDED WITHOUT INCIDENT. MX REMOVED AND REPLACED VENTRAL FUEL CONDITIONING UNIT AND PERFORMED OPERATIONAL SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO Jul 13, 2008 · N12157 · Emb EMB145XRSDR C2XAA08ON158Fadec · inoperativeFLT 0417 - SAT - FLIGHT CREW REPORTED E1 FLUCTUATIONS IN FUEL FLOW-N1-ITT FL270. MX PERSONNEL REMOVED AND REPLACED E1 FADEC 1B AND FPMU. OPERATIONALLY CHECKED SATISFACTORY AND AIRCRAFT WAS RELEASED TO RETURN FOR SERVICE. FADEC 1B: P/N 23078837, S/N BX 16159Jul 12, 2008 · N17196 · Emb EMB145XRSDR E302008F00000Eec · malfunctionedON JULY 11, 2008 AT APPROX 1050AM THE AC LIFTED OFF AND AT APPROXIMATELY 25 TO 30 FT BOTH ENGINES LOST POWER. PILOT INITIATED A RIGHT PEDAL TURN AND ATTEMPTED TO LAND AT THE TAKEOFF POINT, THE AIRCRAFT LANDED IN THE GRASS SHORT OF THE PAD ON TOP OF THE GUARD Jul 11, 2008 · N108DU · Gulstm GIVSDR 2008FA0000485Flow Divider · failedDURING CLIMB OUT AFTER TAKEOFF, NR 1 ENGINE COULD ONLY PRODUCE 85 PERCENT N1. WHILE RETURNING TO BASE , ENGINE SHUT ITSELF DOWN ON 2 MILE FINAL. TROUBLESHOOTING FOUND THAT FUEL FLOW DIVIDER HAD MALFUNCTIONED. FUEL FLOW DIVIDER WAS REMOVED FROM SERVICE, AND Jul 9, 2008 · N6001L · Cessna 550SDR CA080709001Eec · malfunctioned(CAN) ON TAKE OFF, THROUGH 400 FT WITH BLEEDS ON AND CLIMB POWER SET 90% NH + 900 RPM, ENGINE LT EXPERIENCED A SURGE. LT NH WENT 110%, THEN DROPPED TO 70%. RESTABILIZED AT 90%. REDUCED POWER TO BOTH ENGINES. RETURNED FOR LANDING. GROUND RUNS WERE COMPLETED COUJul 6, 2008 · Dhav DHC8315SDR ZESA2008010Fmu · faultyCREW WROTE UP THE LT ENGINE FOR ACCELERATING MUCH SLOWER THAN THE RT ENGINE. TROUBLESHOT TO THE HMU. REMOVED AND REPLACED WITH AN OVERHAULED UNIT. RAN ACFT AND COMPLETED A MAINT CHECK FLIGHT. ALL CHECKED OK. TWO FLIGHTS LATER, CREW WROTE UP LT ENGINE NOT MJul 4, 2008 · N889B · Cessna 550SDR 2008UALA03627Eec · malfunctionedNR 2 ENG UNCOMMANDED ROLLBACK FOR 30 SECONDS. RTFL. POSSIBLE INTERNAL EEC ISSUE. REPLACED EEC AND PMA STATOR AS PRECAUTIONARY, NO REPEATS.Jun 29, 2008 · N513UA · Boeing 757222SDR ASAA0853107Hydromech Unit · faultyENG NR 2 SHORT TERM FAULT MSG NO. FAULT CODE NR 73 20342. THE FMV POSITION SIGNAL OUT OF RANGE. PERFORMED TEST 12 ACTUATORS TEST CONFIRMED FAULT. VERIFIED ROTABLE COMPONENT MFG NR 442369 S/N NR 3219 REF IPC 73 21 10 01 ITEM 25T. REPLACED HMU REF MM 73 21Jun 23, 2008 · N584AS · Boeing 737890SDR AALA200801602B-Nut · looseDEN INFLIGHT T225/13JUN BOS TO SAN. CREW REPORTED ENGINE PRESSURE RATIO INDICATION FOR NR ONE ENGINE. LANDED DEN WITHOUT INCIDENT. SECURED B-NUT ON P1 LINE FORWARD OF NR ONE ENGINE FUEL FLOW GOVERNOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)Jun 13, 2008 · N613AA · Boeing 757223SDR C2XA08TY060Module · malfunctionedACFT GOES TO ET10 RSV POWER ON ITS OWN UNCOMMANDED IN FLIGHT. WILL NOT STAY IN ANY OTHER THRUST RATING. REMOVED AND REPLACED RESISTOR MODULE IAW EMB 145 AMM 73-22-02. OPS CHECK GOOD. (S)Jun 12, 2008 · N13202 · Emb EMB145XR
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