Garrett TFE731 series

Service difficulty reports · 742

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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 engine_model_key = 'TFE731'
  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 DJSR20080125Pressure Valve · malfunctionedNR 1 BLEED OVERHEAT LIGHT ILLUMINATED PASSING 15,000 WITH CORRESPONDING CABIN PRESSURE FLUCTUATIONS.Jan 25, 2008 · N531FL · Amd FALCON20C5 · Pneumatic Distribution SystemSDR 2008FA0000304Control Head · burnedDURING NORMAL DESCENT, AT JUST PRIOR TO 18000 FT, CREW NOTICED DISTINCT BURNING ELECTRICAL ODOR, OXY MASK PULLED AND THE SMOKE CHECKLIST WAS RUN. EMERGENCY PRIORITY REQUESTED UPON ARRIVAL, POSSIBLE LIGHT SMOKE IN COCKPIT ONLY WITH NONE IN THE CABIN. IN LESS Jan 25, 2008 · N970S · Amd FALCON50MYST · Communications SystemSDR 080048Starter Gen · malfunctionedLEFT STARTER GENERATOR DROPPED OFF LINE.Jan 18, 2008 · N9999V · Braero HS125700A · Starter-GeneratorSDR 2008FA0000053Pressure Sensor · malfunctionedLOSS OF CABIN PRESSURE AT 25K FT. PRESSURE SENSOR MALFUNCTIONEDJan 17, 2008 · N55FN · Lear 35A · Cabin Pressure SensorSDR CIEA200800001Fire Loop · deterioratedTHE MASTER CAUTION SYSTEM AND RT ENGINE FIRE WARNING LIGHTS ILLUMINATED NEAR THE TOP OF THE CLIMB. THRUST REDUCTION EXTINGUISHED THE LIGHTS. AFTER SOME CONSIDERATION, THRUST WAS THEN SLOWLY ADDED TO AN APPROXIMATE CRUISE SETTING. AFTER ONE MINUTE AT THE CRUJan 2, 2008 · N717EB · Lear 55LEAR · Fire DetectionSDR CIEA200700011Gasket · failedDURING CRUISE FLIGHT THE RT ENGINE FIRE WARNING CAME ON. THE FLIGHT CREW REDUCE THE ENGINE POWER AND THE LIGHT WENT OUT AND REMAINED OUT UNTIL LANDING. DURING MAINTENANCE INSPECTION, THE RT ENGINE BLEED AIR LINE GASKET IN THE PYLON WAS FOUND TO BE DEFECTIVE Dec 27, 2007 · N717EB · Lear 55LEAR · Engine Bleed Air SystemSDR ODAA121907001Access Panel · out of adjustPILOT REPORTED RUDDER PEDALS BINDING FOUND DURING PREFLIGHT, WITH RT PEDAL FORWARD AND LT PEDAL AFT. AFTER APPLYING PRESSURE TO PEDALS WITH FEET, PEDALS BECAME UNBOUND WITH POPPING NOISE HEARD. INSPECTED RUDDER SYSTEM. FOUND RUDDER BINDING AT PANEL SCREW FODec 19, 2007 · N2G · Raythn HAWKER800XP · Horizontal Stabilizer StructureSDR VQMA121807001Bottle · leakingEMERGENCY GEAR PNEUMATIC BOTTLE HAS TO BE SERVICED REPEATEDLY.Dec 18, 2007 · N650Z · Cessna 650 · Landing Gear Retraction/Extension SystemSDR UVV2007F00000Hose · delaminatedTHE LT OB SLAT ANTIICING HOSE (PN FAL 1007) WAS INSTALLED ON 9/8/2005 WHILE COMPLYING WITH AD 2005-07-23 AND SB F10-313. AD 2007-18-08 HAS SUPERSEDED AD 2005-07-23. IAW REQURIEMENTS OF THE MOST RECENT AD 2007-18-08, THE SLAT ANTI-ICE HOSES BEARING PN FAL 100Dec 10, 2007 · N222MU · Amd FALCON10 · Airfoil Anti/De-ice SystemSDR B8M2007F00000Windscreen · incorrectRECEIVED NEW WINDSCREEN RT (B) SCREEN PN NH24016-92, SN L366293. WHILE DOING OUR INCOMING PARTS INSPECTION WE DISCOVERED THAT THE TERMINAL BLOCK LAYOUT PLACARD FOR THE WINDOW WAS INCORRECT. IT WAS LAYED OUT FOR THE LT WINDOW ASSY PN NH24016-81 OR NH24016-91.Dec 7, 2007 · N890SP · Raythn HAWKER800XP · Flight Compartment WindowsSDR DXTA200702659Computer · faultyON TAKEOFF AT APPROXIMATELY 60KTS, THE STALL IDENT 3 ANN LIGHTS ILLUMINATED. TAKEOFF ABORTED, LIGHT EXTINGUISHED. REMOVED FAULTY THIRD CHANNEL IDENT STALL CAN P/N - 10201-1 S/N F469 INSTALLED REPAIRED STALL CAN P/N - 10201-1 S/N F415. SYSTEM OPS CHECKS FUNCTIDec 7, 2007 · N895QS · Raythn HAWKER800XP · Attitude and Direction Data SystemSDR DXTA200702660Downlock Switch · intermittentDURING T/O AS THE NLG LEAVES THE GRD, A NOSE LIKE SHIMMY OR A TIRE IMBALANCE IS HEARD FOR APPROX. 3 SEC. THEN DURING RETRACTION THE NLG LIGHTS DIMLY FLICKER (BOTH RED & GREEN) UNTIL THE GEAR IS RETRACTED FULLY. MLG LIGHT ARE NORMAL. ALSO AT APPROX 20 MIN INTO Dec 7, 2007 · N893QS · Raythn HAWKER800XP · Landing Gear Position and WarningSDR SH073532Inverter · failedAFTER ENGINE START THE PILOT ATTEMPTED TO TURN ON THE NR2 A/C INVERTER WITH NO RESULTS. AFTER SEVERAL ATTEMPTS SMOKE COULD BE SMELLED IN THE AIRPLANE, AT THAT TIME THE ENGINES WHERE SHUTDOWN AND MAIN BATTERY POWER TURNED OFF. A LINE SERVICE ASSISTANT NOTIFIEDDec 4, 2007 · N314SG · Lear 31A · AC InverterSDR 2GBearing · lack of lubePILOT REPORTED NOSE WHEEL VIBRATION AFTER TAKEOFF ROTATION DURING CLIMBOUT. AIRCRAFT DIVERTED TO HOME BASE. NO REPORTED VIBRATION DURING TAKEOFF OR LANDING ROLL OUT. REMOVED LT AND RT NOSE WHEEL ASSEMBLIES. BALANCED LT AND RT NOSE WHEELS, INSPECTED AND REPACKENov 29, 2007 · N2G · Raythn HAWKER800XP · Wheel/Ski/FloatSDR JM02007F00000Tube · leakingAPPROX 2 MINUTES AFTER THE LANDING GEAR WAS DEPLOYED AND A FEW SECONDS BEFORE LANDING, FLIGHT CREW REPORTED AN (UNUSUAL SMELL) ON THE FLIGHT DECK. NO OTHER WARNING OR INDICATOR WAS NOTED. LANDING PROCEEDED AS USUAL. ON POST FLIGHT INSPECTION, HYDRAULIC RESENov 29, 2007 · N407W · Israel 1124A · Hydraulic System, MainSDR VUC2007F00000Fire Warning · false activationDURING CLIMB, RT ENGINE FIRE WARNING LIGHT ILLUMINATED. FLT CREW RETARDED POWER PACK ON RT ENGINE (WHICH WAS AT MAX CONTINUOUS ITT INDICATION), REQUESTED CLEARANCE TO FL 390 AND DECLARED AN EMERGENCY. UPON PULLING POWER BACK THE FIRE WARNING LIGHT EXTINGUISHNov 26, 2007 · N35TJ · Lear 35A · Fire DetectionSDR VUC2007F00001Fire Warning · false activationUPON TAKEOFF, AC CLEARED TO FL410 AND THEN REQUESTED, AND WAS APPROVED FOR FL430. DURING CLIMB TO FL430, RT ENGINE FIRE WARNING LIGHT ILLUMINATED. FLIGHT CREW SLIGHTLY RETARDED THE POWER BACK ON THE RT ENGINE (WHICH WAS AT MAX CONTINUOUS ITT INDICATION) REQUNov 26, 2007 · N35TJ · Lear 35A · Fire DetectionSDR V6N2007F00000Fuel · contaminatedDURING CRUISE AFTER DEPARTMENT, CREW NOTICED A REDUCTION IN FUEL FLOW TO BOTH ENGINES. UNEVENTFUL LANDING MADE. UPON DEPARTURE, NEITHER ENGINE WAS ABLE TO MAKE TARGET N1. FUEL WAS SUMPED AND CHECKED FOR CONTAMINATION, NO SIGNIFICATE RESULTS NOTED. POWER ASNov 18, 2007 · N556HJ · Lear 55LEAR · Fuel StorageSDR DJFA2007132Master Cylinder · weakCREW REPORTED BRAKES FELT SPONGY AND TRAVELED A GREAT DISTANCE BEFORE BRAKING WAS FELT ON LANDING. THE BRAKE MASTER CYLINDERS WERE BLED. THE MAIN AND EMERGENCY SYSTEMS WERE BLED. THE MAIN HYDRAULIC SYSTEM WAS SERVICED TO FULL.Nov 14, 2007 · N791TA · Raythn HAWKER800XP · Master Cylinder/Brake ValveSDR 2007FA0001000Power Supply · burnedDISCREPANCY WAS CABIN INDIRECT LIGHTING IS INTERMITTENT. FOUND SHORTED WIRING AT AFT LT SIDE VALANCE, 2 BURNED POWER SUPPLIES AND SEVERAL CRACKED LAMP FIXTURES. CUSTOMER STATED THIS IS THE 3RD TIME THE POWER SUPPLIES WERE FOUND BURNED.Nov 8, 2007 · N107LT · Hawker BAE125700B · Passenger Compartment LightingSDR DJFA2007125Skin · corrodedDURING POST FLIGHT INSPECTION CREW NOTED EVIDENCE OF CORROSION ON THE ELEVATOR LEADING EDGES. MAINTENANCE DISCOVERED THE CORROSION TO BE MODERATE AND OUT OF REPAIRABLE LIMITS. MAINTENANCE REPLACED THE LEADING EDGE.Nov 8, 2007 · N831LX · Raythn HAWKER800XP · Elevator, Plate/SkinSDR DXTA200702586Engine · fodUPON START-UP, LT ENGINE BEGAN TO VIBRATE AND SHUDDER. LT ENGINE START ABORTED. REMOVED RAG FROM FAN. CLEANED FAN BLADES AND INLET OF TOWEL DEBRIS. A VISUAL INSPECTION OF INLET/BYPASS STATOR AND FAN ASSY. NO DAMAGE VISIBLE. BOROSCOPE OF 1ST STAGE L.P.C. ROTORNov 1, 2007 · N858QS · Raythn HAWKER800XP · Engine (Turbine/Turboprop)SDR 2007FA0001018Control Unit · leakingFUEL LEAKING FROM CENTRAL LB CROSSFEED UNIT AND DRAIN TUBE CAP BROKEN. REF MFG SERVICE ADVISORY FSA900EX-EASY-28-10-03-R1. (K)Oct 24, 2007 · N47EG · Amd FALCON900EX · Aircraft Fuel Distribution SystemSDR EWCR200700003Oil System · leakingTHE AIRCRAFT WAS A CRUISE ALTITUDE 37,000 WHEN THE PILOTS NOTICED FIRST BLUE, AND THEN WHITE SMOKE FILLING THE FLIGHT DECK AND CABIN. REDUCED POWER, DECLARED AN EMERGENCY, AND LANDED AT LAGRANGE, GA. THERE WAS STILL SOME SMOKE IN THE AIRCRAFT UPON LANDING. Oct 18, 2007 · N750CK · Cessna 650 · Turbine Engine Oil SystemSDR DELA200720009Indication Sys · intermittentLOW FUEL LIGHT ILLUMINATED WITH 4000 LBS TOTAL FUEL ON AIRPLANE AND 1200 LBS FUEL IN THE WINGS. FUEL READER GAUGE INDICATED 400 LBS OF FUEL ON RT WING. LATER ON WENT BACK TO INDICATE 1200 LBS ON THE WINGS. TAKEOFF (SIC) WITH 4000 LBS TOTAL LANDING WEIGHT WAS 1Oct 5, 2007 · N773DL · Lear 35A · Fuel Indicating SystemSDR DELA200700008Warning Light · false indicationLOW FUEL LIGHT ILLUMINATED WITH 4000 LBS TOTAL FUEL ON AIRPLANE AND 1200 LBS FUEL IN THE WINGS. FUEL READER GAUGE INDICATED 400 LBS OF FUEL ON RT WING. LATER ON WENT BACK TO INDICATE 1200 LBS ON THE WINGS. TAKE OF (SIC) WITH 4000 LBS TOTAL LANDING WEIGHT WAS 1Oct 5, 2007 · N773DL · Lear 35A · Fuel Indicating SystemSDR DELA200720008Indication Sys · false indicationLOW FUEL LIGHT ILLUMINATED WITH 4000 LBS TOTAL FUEL ON AIRPLANE AND 1200 LBS FUEL IN THE WINGS. FUEL READER GAUGE INDICATED 400 LBS OF FUEL ON RT WING. LATER ON WENT BACK TO INDICATE 1200 LBS ON THE WINGS. TAKE OF (SIC) WITH 4000 LBS TOTAL LANDING WEIGHT WAS 1Oct 5, 2007 · N773DL · Lear 35A · Fuel Indicating SystemSDR DJFA2007112Connector · burnedCREW REPORTED SMELL OF SMOKE FROM THE LAV AND BAGGAGE FIRE ILLUMINTATED. AIRCRAFT LANDED SAFELY. MAINTENANCE DISCOVERED A BURNED PIN IN THE LAV WATER TANK CONNECTOR BURNED. THE BURNED PIN WAS REPLACED. NO OTHER FAULTS WERE DETECTED.Oct 1, 2007 · N733TA · Raythn HAWKER800XP · Water/Waste System WiringSDR IJO2007F00000Warning Light · false indicationAFTER TAKEOFF, LANDING GEAR SELECTED UP. AT ABOUT 1,000 FT AGL, NOSE & RT MLG RED TRANSITION LIGHTS WERE STILL ILLUMINATED. SELECTED LANDING GEAR DOWN, AT WHICH TIME ALL 3 GREEN SAFE LIGHTS ILLUMINATED, ALONG WITH AN INCREASED WIND NOISE LEVEL FROM THE EXTENSep 30, 2007 · N150SB · Braero BAE125800A · Landing Gear Position and WarningSDR DELA200720007Connector · dirtyNOSE GEAR UNSAFE LIGHT ILLUMINATED ON APPROACH. FLY BY TOWER INDICATED GEAR WAS DOWN. LANDED UNEVENTFULLY. TROUBLESHOT WIRING TO NLG DOWNLOCK SWITCH, FOUND CONTACTS AT CONNECTOR PLUG NEEDED CLEANING. CLEANED AND REATTACHED. CONDUCTED GEAR SWING, OPS CHECKSep 27, 2007 · N431AS · Lear 35A · Landing Gear System WiringSDR 2007FA0000885Vane · corrodedLT IB FLAP VANE, UPPER SKIN CORRODED BEYOND LIMITS. POSSIBLE CAUSE: DISSIMILAR METAL CORROSION AS TRAILING EDGE IS MAGNESIUM AND SKIN IS ALUMINUM OR ENVIRONMENT IN WHICH THE VANE OPERATES. IT IS LOCATED BEHIND THE MLG. ASSURE THE SKIN IS PROPERLY TREATED IAWSep 10, 2007 · N150SB · Braero BAE125800A · Trailing Edge FlapsSDR A9J2007F00000Sensor · failedALL SENSORS ON A NEW WINDSHIELD FAILED. THERE ARE A TOTAL OF 400 HRS SINCE NEW. (K)Aug 26, 2007 · N3VJ · Lear 31A · Windshield/Door Rain/Ice RemovalSDR M000999Static Port · leakingSPLIT IN ALTIMETERS (RT ALTIMETER INDICATES 400 FOOT HIGHER THAN LT ALTIMETER AT 41,000 FT MSL) VERIFIED SPLITS IN ALTIMETERS AND PILOTS PITOT/STATIC SYS. INSTALLED NEW CO-PILOTS STATIC PORT FITTING P/N CM2933-7. LEAK CHECK, SAND, FILLED, PRIMED, PAINTED AND Aug 24, 2007 · N650Z · Cessna 650 · Pitot/Static SystemSDR DELA200700006Downlock Sensor · false indicationON APPROACH, LOWERED LANDING GEAR AND HAD RED LIGHT ON RT MLG. RECYCLED GEAR, SAME RESULT. PERFORMED ELECTRICAL MALFUNCTION ALTERNATE GEAR EXTENSION, SAME RESULT. CHANGED LANDING LOCATION; LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED MALFUNCTIONING RT MLG Aug 20, 2007 · N431AS · Lear 35A · Landing Gear Position and WarningSDR 2007FA0000827Manifold · damagedLT PYLON OVERHEAT INDICATION OCCURRED IN FLIGHT. FOUND HIGH PRESSURE BLEED AIR MANIFOLD MATING FLANGE DEFORMED. REPLACED ASSY 4536102150V43-1 WITH NAV ASSY 45361020228-001. CAUSE MAY BE AGE OR REPEATED CLAMPING. ORIGINAL PART HAS BEEN SUPERSEDED BY THE MFGAug 14, 2007 · N858MK · Lear 45LEAR · Engine Bleed Air SystemSDR VQMA081907001Bottle · leakingGEAR PNEUMATIC BLOWDOWN BOTTLE IS LEAKING.Aug 9, 2007 · N650Z · Cessna 650 · Landing Gear Retraction/Extension SystemSDR 2007FA0000703Static Line · misinstalledTHIS RVSM AIRCRAFT HAD AN ALTIMETRY SYSTEM SPLIT. CONTACTED STC GROUP HOLDER FOR PROPER ROUTING OF STATIC SYSTEM PLUMBING. FOUND CO-PILOTS STATIC SYSTEM INSTALLATION WAS NOT CROSS-COUPLED WITH PILOTS SYSTEM. INSTALLED FABRICATED HOSES TO THE CO-PILOTS SYSTEM TAug 6, 2007 · N621RB · Lear 35A · Pitot/Static SystemSDR 2007FA0000836Static System · misinstalledTHIS RVSM AIRCRAFT HAD AN ALTIMETRY SYSTEM SPLIT. CONTACTED STC GROUP HOLDER FOR PROPER ROUTING OF STATIC SYSTEM PLUMBING. FOUND CO-PILOTS SYSTEM WAS NOT CROSS COUPLED WITH PILOTS SYSTEM. INSTALLED FABRICATED HOSES TO THE CO-PILOTS SYSTEM TO MEET STC NR ST Aug 6, 2007 · N621RB · Lear 35A · Pitot/Static SystemSDR BSYA200700014Tube · bentAIRCRAFT ON IT'S WAY FROM DAL TO LCK WHEN THE PILOT NOTICED THE OIL PRESSURE DROPPING, HE THEN ELECTED TO SHUT THE ENG DOWN AND DIVERTED INTO MEM. ENGINE SHOP FOUND OIL TUBES BENT AND GASKET BAD. REPLACED ALL TUBES AND ONE GASKET AT THE N1 MONOPOLE.Jul 31, 2007 · N813AS · Lear 35A · Turbine Engine Oil SystemSDR 2007FA0000701Rod · cracked(REF CNTRL NR WW1045) RECOVERED AIRCRAFT FROM TAXI WAY AFTER A LANDING WITH NO MLG GREEN LIGHTS. LT GEAR STARTED RETRACTING DURING TAXI. FOUND LT AFT GEAR RETRACT ACTUATOR PISTON ROD BROKEN INSIDE PISTON WHICH HAD CAUSED A MIS-DIRECT OF GEAR DOWN FLOW TO ROJul 9, 2007 · N40TA · Israel 1124 · Landing Gear ActuatorSDR 2007FA0000593Support Fitting · damagedAFTER REMOVAL OF AILERON AND SERVICE SUPPORT FITTING AT BL 9R FUSELAGE STATION 199.579. FOUND SEVERAL MISSED DRILLED/ELONGATED /FILLED FASTENER HOLES IN T CASTING P/N:25W17124, ANGLE P/N:25W171126 AND AILERON AND SERVICES SUPPORT FITTING CASTING P/N:25W35321Jul 3, 2007 · N49MN · Israel 1125 · AileronsSDR 2007FA0000594Support Fitting · mismanufacturedAFTER REMOVAL OF AILERON AND SERVICE SUPPORT FITTING AT BL 9R FUSELAGE STATION 199.579. FOUND SEVERAL MISSED DRILLED/ELONGATED /FILLED FASTENER HOLES IN T CASTING P/N:25W17124, ANGLE P/N:25W171126 AND AILERON AND SERVICES SUPPORT FITTING CASTING P/N:25W353216Jul 3, 2007 · N49MN · Israel 1125 · AileronsSDR 2007FA0000632Link Rod · crackedPERFORMED EDDY CURRENT INSPECTION OF 8 EA THRUST REVERSER LINK ROD. FOUND A CRACK IN (1) LINK ROD. VERIFIED FINDING USING MAGNETIC PARTICLE INSP METHOD. DURING MP INSP, NOTED ANOTHER CRACK, NOT DETECTED USING EDDY CURRENT. DECIDED TO PERFORM MP INSP OF ALLJun 29, 2007 · N245SM · Raythn HAWKER800XP · Engine Thrust ReverserSDR 2007FA0000878Transponder · failedON 6/27/2007 WHILE ENROUTE, THE PRIMARY TRANSPONDER FAILED WHILE THE AIRCRAFT WAS OPERATING IN AIRSPACE. THE CREW WAS ABLE TO SWITCH TO THE SECONDARY TRANSPONDER AND CONTINUE THEIR FLIGHT TO LOCK WITHOUT FURTHER INCIDENT. UPON ARRIVAL, THE PRIMARY TRANSPONDEJun 29, 2007 · N56EM · Automatic Direction Finder (ADF) SystemSDR DELA200700005Wire Harness · damagedLT ENGINE N1 LAGGED BEHIND RT ENGINE N1 ON TAKEOFF ROLL, AND ALSO LT ENGINE COMPUTER LIGHT CAME ON. FOUND (B) SOLENOID OF SERVO VALVE CONNECTOR HAD EXPOSED WIRE. RE-TERMINATED PINS (A) AND (B) OF CONNECTOR PLUG. CREW CONDUCTED HIGH POWER RUN AND HIGH SPEED Jun 27, 2007 · N431AS · Lear 35A · Turbine Engine System WiringSDR DELA200700004Uplock Switch · malfunctionedLT GEAR UNSAFE LIGHT STAYED ON AFTER TAKEOFF. REMOVED AND REPLACED UPLOCK SWITCH.Jun 2, 2007 · N1324P · Lear 55LEAR · Landing Gear Position and WarningSDR 2007FA0000486Actuator · misalignedINSTALLED REBUILT FLAP ACTUATOR IN RT OB POSITION; PN 1391T100-8, SN 387AB. FLAP OPERATION WAS NORMAL. WHILE CHECKING AILERON TRAVELS IT WAS DISCOVERED THAT AILERON TRAVELS WERE LIMITED BY THE REBUILT FLAP ACTUATOR. A COVER PLATE ON THE FLAP ACTUATOR HAD BEMay 30, 2007 · N27TZ · Israel 1124 · Trailing Edge Flap ActuatorSDR 2007FA0000487Actuator · misalignedINSTALLED REBUILT FLAP ACTUATOR IN RT OB POSITION; PN 1391T100-8, SN 387AB. FLAP OPERATION WAS NORMAL. WHILE CHECKING AILERON TRAVELS IT WAS DISCOVERED THAT AILERON TRAVELS WERE LIMITED BY THE REBUILT FLAP ACTUATOR. A COVER PLATE ON THE FLAP ACTUATOR HAD BEMay 30, 2007 · N27TZ · Israel 1124 · Trailing Edge Flap ActuatorSDR 2007FA0000539Actuator · misalignedINSTALLED REBUILT FLAP ACTUATOR IN RT OB POSITION; PN 1391T1008, SN 387AB. FLAP OPERATION WAS NORMAL. WHILE CHECKING AILERON TRAVELS IT WAS DISCOVERED THAT AILERON TRAVELS WERE LIMITED BY THE REBUILT FLAP ACTUATOR. A COVER PLATE ON THE FLAP ACTUATOR HAD BEEMay 30, 2007 · N27TZ · Israel 1124 · Trailing Edge Flap ActuatorSDR 2007FA0000465Pitot Line · looseWHILE TROUBLESHOOTING A LEAK IN NR 2 STATIC SYSTEM, THE RT SIDE STATIC PLATE HAD TO BE TAKEN LOOSE. UPON REMOVAL OF THE PLATE, SILICONE RTV WAS FOUND ON THE FITTING FOR THE NR 1 STATIC SYSTE. WHEN THE FITTING WAS LOOSENED, FOUND A LAGRE AOUNT OF TEFLON PIPE May 9, 2007 · N160FJ · Amd FALCON10 · Pitot/Static System
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