Swearingen SA226TC

Service difficulty reports · 565

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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 aircraft_model_key = 'SA226TC'
  ORDER BY difficulty_date DESC"

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SDR CA080609005Tube · leaking(CAN) THE CREW OF THE ACFT REPORTED LOW POWER FROM THE NR 1 ENGINE. DURING THE COURSE OF TROUBLESHOOTING MX SUSPECTED A BLEED AIR LEAK CAUSED BY A CRACK IN THE BELLOWS FOR THE BLEED AIR LINE. THIS FLEXIBLE JOINT IS COVERED IN A WIRE HEAT SHIELD AND UPON CUTTINJun 5, 2008 · Swrngn SA226TC · Engine Bleed Air SystemSDR CA080609004Actuator · unresponsive(CAN) SHORTLY AFTER DEPARTING, AND ACCELERATING THROUGH 200KTS, THE PITCH TRIM STOPPED RESPONDING. TRIM SONALERT WAS SOUNDING WHENEVER THE TRIM SWITCH WAS USED, HOWEVER THE TRIM GAUGE WAS NOT MOVING AND THE ACFT CERTAINLY WAS NOT TRIMMING. THIS WAS ATTEMPTED OJun 3, 2008 · Swrngn SA226TC · Stabilizer ActuatorSDR CA080609006Duct · cracked(CAN) DURING A ROUTINE INSP IT WAS DISCOVERED VISUALLY THAT A BLEED AIR LINE TO THE HEAT EXCHANGER OF THE AIR CYCLE MACHINE HAD CRACKED 2 INCHES, ABOUT ONE THIRD THE CIRCUMFERENCE OF THE TUBE.May 31, 2008 · Swrngn SA226TC · Air Distribution SystemSDR CA080415005Windshield · crackedDURING THE RETURN LEG TO MAIN BASE THE AIRCRAFT EXPERIENCED A RT HEATED WINDSHIELD CRACK IN A SPIDER WEB FASHION. THE AIRCRAFT DESCENDED THE CABIN DIFF WAS LOWERED AND AIRSPEED REDUCED. UPON WINDOW REMOVAL NO DISCREPANCIES WERE NOTED WITH THE PREVIOUS INSTALLApr 12, 2008 · Swrngn SA226TC · Flight Compartment WindowsSDR CA080404002Shaft · failedDURING A ROUTINE INSPECTION OF THE HYDRAULIC PUMP, THE RETAINING BOLT WHICH HOLDS THE SPLINE DRIVE INTO THE HYDRAULIC PUMP HAD SHEARED.Mar 26, 2008 · Swrngn SA226TC · Hydraulic Pump (Electric/Engine), MainSDR CA080326002Exhaust Duct · cracked(CAN) WHEN THE ENG WAS UNDERGOING A PHASE 6 INSP, A CRACK APPROX 3 INCH LONG WAS DISCOVERED IN THE ENGINE EXHAUST DUCT NEAR THE EGT PROBE BOSSES. IT APPEARED TO BE ON A PREVIOUS WELD. REMOVED AND REPLACED THE DUCT. (TC NR 20080326002)Mar 24, 2008 · Swrngn SA226TC · Engine Collector/Tailpipe/NozzleSDR CA080320003Frame · crackedDURING AN AGING AIRCRAFT INSPECTION A CRACK WAS DETECTED VISUALLY EXTENDING FROM THE LOWER AFT LATCH (POSITION 8). WHEN THE DOOR WAS REMOVED FOR REPAIR FURTHER CRACKS WERE DISCOVERED TO THE ATTACHING STRUCTURE FOR BOTH LOWER LATCHES (POSITIONS 7 AND 8). THISMar 12, 2008 · Swrngn SA226TC · Cargo/Baggage DoorsSDR CA080304009Fuel Control · failed(CAN) ENGINE HAD BEEN REMOVED IN RUNNING CONDITION FOR SCHEDULED HOT SECTION/GEARBOX INSP. ENG SENT TO ENGINE SHOP. UPON INITIAL START UP FOR THE TEST CELL RUN, THE ENGINE WOULD NOT START. FUEL CAME OUT THE DRAINS AND THE BACK OF THE ENGINE. THE FUEL PUMP PRESMar 3, 2008 · Swrngn SA226TC · Fuel Control/Turbine EnginesSDR CA080220002Windshield · delaminated(CAN) DURING THE CRUISE PORTION OF FLIGHT, THE CREW WITNESSED THE RT SIDE COCKPIT HEATED WINDSHIELD PHYSICALLY DELAMINATING . THE CREW INDICATED THE AC WAS OPERATING AT A 6.0 PSI DIFFERENTIAL WHICH IS WITHIN THE MAXIMUM 7.25 PSI DIFFERENTIAL FOR THE AC. NO ACTFeb 18, 2008 · Swrngn SA226TC · Flight Compartment WindowsSDR CA080214002Drive Shaft · failed(CAN) TROUBLESHOT NO RPM INDICATION. REMOVED TACH GENERATOR FROM RT ENGINE, DRIVE SHAFT WAS STILL STUCK IN THE ENGINE. IT APPEARS THAT THE SHAFT SEPARATED FROM THE ARMATURE INSIDE. REMOVED THE SHAFT, NO DAMAGE TO THE ENGINE DRIVE. INSTALLED SERVICEABLE PART ANFeb 13, 2008 · Swrngn SA226TC · Engine RPM Indicating SystemSDR CA080124005Nut · backed out(CAN) A/C CAME IN TO THE MAINT HANGER DUE TO HAVING A CHIP LIGHT COME ON IN THE COCKPIT. INSP FROM MAINT NOTICED THAT THERE WAS METAL ON THE CHIP DETECTOR OF ENGINE P-54121. AT THAT TIME THE ENGINE WAS FORWARDED TO THE ENGINE SHOP FOR FURTHER INSP. THE ENGINE Jan 22, 2008 · Swrngn SA226TC · Turbine Engine Accessory DriveSDR CA080117005Adapter · cracked(CAN) DURING THE DAILY INSPECTION IT WAS NOTICED THAT THERE WAS OIL IN THE BOTTOM OF THE COWLING. FURTHER INSP REVEALED THAT THE (3) OF THE (4) TANGS FOR THE STUDS WHICH HOLD DOWN THE OIL FILTER ADAPTER WERE CRACKED. TOTAL TIME ON THIS PART IS UNDETERMINED BECJan 11, 2008 · Swrngn SA226TC · Turbine Engine Oil SystemSDR CA071218006Windshield · cracked(CAN) UPON ENGINE START AND TAXI THE F/O HEATED WINDSCREEN CRACKED. THE GLASS CRACKED FROM THE BOTTOM UP. THE CREW TURNED AROUND AND SHUTDOWN. MAINT REMOVED AND REPLACED THE WINDOW. OUR COMPANY CONTINUES TO HAVE PROBLEMS WITH THESE HEATED WINDSHIELDS AND IN SPDec 14, 2007 · Swrngn SA226TC · Flight Compartment WindowsSDR CA071116001Sensor · overheated(CAN) THE FOLLOWING WAS REPORTED BY THE FLIGHT CREW FOLLOWING THE CO-PILOTS HEATED WINDSHIELD FAILURE: (WHILE ON THE ILS FO MENTIONED A BURNING SMELL, AND NOTICED IT AS WELL.) TOOK MY FLASHLIGHT OUT BUT COULD NOT NOTICE ANY DETECTABLE SMOKE IN THE CABIN OR COCNov 14, 2007 · Swrngn SA226TC · Windshield/Door Rain/Ice RemovalSDR 2007FA0000790Pipe · damagedNOTE: AIRCRAFT HAS BEEN PARKED FOR 2 YEARS AFTER BEING DAMAGED IN HURRICANE. AIRCRAFT WAS BEING DISASSEMBLED FOR SALVAGE. IB OF RT NACELLE, BLEED AIR PIPE, PN: 27-84187-015, HAS CHAFED/BURNED THROUGH THE ASBESTOS SLEEVE SURROUNDING THE STARTER RELAY WIRING ASep 1, 2007 · N226AM · Swrngn SA226TC · Pneumatic Distribution SystemSDR CA070720005Actuator · malfunctioned(CAN) AFTER FLAP RETRACTION, FLIGHT CREW DISCOVERED THAT THEY HAD NO CONTROL OF PITCH TRIM USING PRIMARY OR SECONDARY CIRCUITS. AFTER DISCUSSION WITH MAINTENANCE, FLIGHT CONTINUED TO MAINTENANCE BASE WHERE MAINTENANCE REPLACED TRIM ACTUATOR. (TC NR 20070720005Jul 19, 2007 · Swrngn SA226TC · Stabilizer ActuatorSDR CA070727008Master Cylinder · faulted(CAN) AIRCRAFT ABORTED TAKEOFF DUE TO A DRAGGING BRAKE. UPON MAINTENANCE INSPECTION THE RT BRAKE MASTER CYLINDERS WERE FOUND AT FAULT. BRAKE PRESSURE COULD NOT BE RELEASED BY THE AFFECTED MASTER CYLINDERS. BOTH NR 2 AND NR 4 BRAKE MASTER CYLINDERS WERE REPLAJul 17, 2007 · Swrngn SA226TC · Master Cylinder/Brake ValveSDR 2007FA0000731Pipe · arcedIB OF RT NACELLE, BLEED AIR PIPE (PN 2784187019), CHAFED OR BURNED THROUGH THE ASBESTOS SLEEVE SURROUNDING THE STARTER RELAY WIRING, WHICH THEN ARCED A HOLE IN THE BLEED PIPE, WHICH THEN BURNED THE SHIELDING FROM THE STARTER RELAY WIRES, WHICH THEN ARCED A HOLJun 25, 2007 · N160WA · Swrngn SA226TC · Air Distribution SystemSDR CA070614003Line · cracked(CAN) CREW NOTICED A LARGE PUDDLE OF HYDRAULIC FLUID COMING FROM THE NOSE WHEEL WELL AREA. DETERMINED TO BE A CRACKED LINE ON A BEND RADIUS, WHICH WAS THE SUPPLY LINE TO THE NWS SYSTEM. THE SYSTEM WAS DISABLED AND PLACED ON AN MEL DEFERRAL, CLEANED AND LEAK Jun 13, 2007 · Swrngn SA226TC · Hydraulic System, MainSDR CA070503010Control Cable · failed(CAN) CONTROL CABLE FAILED WHERE IT MAKES A BEND COMING OUT OF THE CENTER PEDESTAL. COMMON FAILURE POINT. REPLACED WITH NEW PART, REPLACED OTHER SIDE AS A PRECAUTION AS WELL. (TC NR 20070503010)Apr 23, 2007 · Swrngn SA226TC · Power LeverSDR CA070417001Valve · stuck(CAN) THE AC RT MLG TIRES WERE BLOWN UPON LANDING. DURING INSPECTION IT WAS FOUND THAT THE RT BRAKE ASSY WERE DRAGGING AND OVERHEATED CAUSING THE WHEELS NOT TO TURN FREELY UPON TOUCHDOWN. TIRES, BRAKES AND AFFECTED BRAKE MASTER CYLINDERS WERE REPLACED. AN INIApr 12, 2007 · Swrngn SA226TC · BrakeSDR CA070208005Windshield · cracked(CAN) DURING TAXI WITH THE WINDSHEILD HEAT SELECTED ON THE RT COCKPIT HEATED WINDSHEILD CRACKED. THE FLIGHTCREW RETURNED TO THE TERMINAL AND THE AIRCRAFT WINDOW HAS BEEN REPALCED BY MAINTENANCE. NO CAUSE OF THE CRACKED GLASS COULD BE DETERMINED. THIS IS THE THFeb 5, 2007 · Swrngn SA226TC · Flight Compartment WindowsSDR CA070117003Windshield · delaminated(CAN) DURING FLIGHT THE FLIGHT CREW HEARD A LOUD CRACK FROM THE RT HEATED WINDSHIELD. THEY IMMEDIATELY NOTICED THE WINDOW PANES BEGIN TO DELAMINATE. NO OBJECT WAS WITNESSED HITTING THE AIRCRAFT OR WINDSHIELD. THE AIRCRAFT LANDED SAFELY AND THEN RETURNED TO BASJan 15, 2007 · Swrngn SA226TC · Flight Compartment WindowsSDR CA070112003Windshield · cracked(CAN) UPON LANDING THE FLIGHT CREW WITNESSED THE LT HEATED WINDSHIELD CRACK FROM THE LOWER RT CORNER TO THE UPPER CENTER PORTION OF THE WINDOW. THE LANDING WAS REPORTED AS NORMAL AND NO ABNORMAL INDICATIONS WERE NOTICED PRIOR TO FAILURE OF THE WINDOW. UPON INJan 11, 2007 · Swrngn SA226TC · Flight Compartment WindowsSDR CA061219027Windshield · failed(CAN) DURING FLIGHT THE RT COCKPIT HEATED WINDSHEILD SHATTERED BUT REMAINED INTACT. THE FLIGHT CREW DECALRED AN EMERGENCY AND RETURNED TO THE AIRPORT UNEVENTFULLY. THE WINDOW WAS REPLACED BY MAINTENANCE. THE CREW EXPLAINED THAT PRIOR TO THE WINDOW SHATTERING ADec 15, 2006 · Swrngn SA226TC · Flight Compartment WindowsSDR CA061124005Channel · cracked(CAN) DURING OVERHAUL OF THE RT FLAP ASSY, THE CENTER HINGE CHANNEL WAS REMOVED FOR REPLACEMENT AND WAS FOUND CRACKED BETWEEN (2) RIVET HOLES. THE CHANNEL HAS BEEN REPLACED. (TC NR 20061124005)Nov 21, 2006 · Swrngn SA226TC · Trailing Edge FlapsSDR CA061219025Windshield · failed(CAN) DURING FLIGHT THE LT COCKPIT HEATED WINDSHEILD SHATTERED BUT REMAINED INTACT. THE AIRCRAFT IMMEDIATLY RETURNED TO THE AIRPORT AND THE WINDOW WAS REPLACED BY MAINTENANCE. NO CAUSE COULD BE DETERMINED AS TO WHY THIS WINDOW SHATTERED. (TC NR 20061219025)Nov 20, 2006 · Swrngn SA226TC · Flight Compartment WindowsSDR 2006FA0001074Servo · malfunctionedAIRCRAFT PULLS TO THE RT. OPERATOR REMOVED AND REPLACED NOSE STEERING SERVO, FLUSHED OUT LINES AND REPLACED FILTER. OPS CHECK GOOD IAW MFG MM. (K)Oct 31, 2006 · N247ML · Swrngn SA226TC · Landing Gear Steering SystemSDR CA061027003Torque Sensor · damaged(CAN) UPON TAXI INTO AIRPORT, THE RT ENGINE SHUT DOWN DUE TO THE CENTER GEAR ON THE TORQUE SENSOR SHAFT & WHERE NUT HOLDS THE GEAR ON BROKE OFF. AT THIS TIME THE A/C WAS AT THE TERMINAL AND NO PROBLEMS AROSE DUE TO THIS INCIDENT. SUSPECT THE NUT ON THE SHAFT WOct 14, 2006 · Swrngn SA226TC · Engine BMEP/Torque IndicatingSDR CA060905007Wire · damaged(CAN) AIRCRAFT HAD EXPERIENCED PROBLEMS WITH BATTERY DISCONNECTING INTERMITTENTLY. FIRST TIME WAS CIRCUIT BREAKER POPPED. NEXT TIME FOUND CORROSION ON BATTERY RELAY, REPLACED RELAY. THIS IS A COMMON DEFECT WITH THESE TYPE OF RELAYS. THIRD INSTANCE WAS ON NEAug 31, 2006 · Swrngn SA226TC · Electrical Power System WiringSDR CA060901006Switch · odor(CAN) CREW NOTED BEFORE TAKEOFF A BURNING SMELL IN THE COCKPIT PRIOR TO TAKEOFF. NO SYSTEM FAULTS WERE NOTED OR BREAKERS POPPED AND THE SMELL WENT AWAY, SO THE FLIGHT CONTINUED IT`S LAST LEG. NO FAULTS NOTED IN FLIGHT. IT WAS LATER DISCOVERED A SPEED SWITCHAug 31, 2006 · Swrngn SA226TC · Fuel Controlling SystemSDR CA060824004Line · leaking(CAN) AIRCRAFT WAS IN CRUISE, CREW NOTED HYDRAULIC LEAKAGE ON THE COCKPIT FLOOR. CONDUCTED A NORMAL LANDING, NOSE GEAR UP LINE IN COKPIT WAS LEAKING. REPLACED LINE, ON NEXT LEG, A LINE FAILED IN THE LH GEAR WELL, CREW ACTIVATED EMERGENCY EXTENSION AND NORMAL Aug 22, 2006 · Swrngn SA226TC · Hydraulic System, MainSDR CA060824003Fuel Control · malfunctioned(CAN) UPON LANDING, CREW APPLIED REVERSE THRUST. BELOW 70 KIAS, THE RPM LEVER WAS SELECTED TO (LOW). ON THE TAXIWAY, THE CREW NOTED VERY LOW ENGINE RPM, LOW OIL PRESSURE LIGHT, AND LOW EGT. THEY DETERMINED THE ENGINE HAD FLAMED OUT AND PARTIALLY RESTARTED. Aug 18, 2006 · Swrngn SA226TC · Fuel Control/Reciprocating EnginesSDR CA060627004Bearing · failed(CAN) THE FRONT SCAVENGE PUMP DRIVE GEAR SHAFT SHEARED IN THE SCAVENGE PUMP, DUE TO THE SCAVENGE PUMP BUSHING THAT SEIZED FROM OIL STARVATION AND METAL CONTAMINATION CAUSED BY THE TORQUE SENSOR BEARING. THE OIL PRESSURE PUMP SHAFT AND BUSHING ALSO HAVE WEAR ONJun 27, 2006 · Swrngn SA226TC · Turbine Engine Accessory DriveSDR CA060530007Carrier Assy · making metal(CAN) OIL SAMPLE RECEIVED FROM WEAR CHECK INDICATING HIGH OIL FILTER WEIGHT W/MAJOR ALUMINUM, MINOR CARBON STEEL IN SAMPLE. ENG REMOVED FOR INSP. DURING TEARDOWN: PLANETARY CARRIER SPLINE LOCKS STRIPPED/DESTROYED. CARRIER WORN DUE TO EXCESS PIN LOADING. ALL May 15, 2006 · Swrngn SA226TC · Engine (Turbine/Turboprop)SDR CA060428001Oil Filter · broken(CAN) DURING A ROUTINE DAILY INSPECTION THE OIL FILTER BYPASS PIN WAS FOUND POPPED INDICATING AN OBSTRUCTED OIL FILTER. UPON INSPECTION OF THE FILTER IT WAS FOUND TO BE BROKEN AT THE OIL INLET MOUNTING FLANGE. PREVIOUS SDR'S HAVE BEEN ISSUED FOR THIS PROBLEM, Apr 27, 2006 · Swrngn SA226TC · Turbine Engine Oil SystemSDR SAI040601Annunciator · false indication12 MINUTES AFTER TAKE OFF THE RIGHT WING (250* ON LEADING EDGE WIRING) OVERHEAT FLASHING WARNING LIGHT CAME ON. PILOT PERFORMED AFM PROCEDURES DECLARED A EMERGENCY AND RETURNED TO CASPER, WY. AIRCRAFT WAS TROUBLESHOT AND DETERMINED THAT A FAILURE IN THE ANNUApr 5, 2006 · N235BA · Swrngn SA226TC · Overheat DetectionSDR CA060321004Cable · broken(CAN) FLIGHT CREW REPORTED THAT DURING START THE RPM WAS UNCONTROLLABLE AND INITIATED A MANUAL SHUT DOWN. MAINTENANCE DISCOVERED THE POWER LEVER BROKEN APPROX. 4 INCHES FROM THE END JUST SHORT OF THE QUICK DISCONNECT FITTING. DUE TO THE FACT THAT THE TELE-FLEMar 17, 2006 · Swrngn SA226TC · Engine Fuel System WiringSDR CA060221009Control Cable · failedCREW ATTEMPTED TO START THE ENGINE ON 4TH LEG OF THE DAY. ENGINE ACCELERATED TO 30 PERCENT AND TEMPERATURE INCREASED. ENGINE WAS SHUT DOWN. MAINTENANCE DISCOVERED THE POWER LEVER CABLE HAD SEVERED IN THE PEDASTAL AND THE ENGINE WAS STUCK IN FULL REVERSE. (Feb 13, 2006 · Swrngn SA226TC · Power LeverSDR CA060221006Panel · crackedWHILE UN-COWLING, RT ENGINE MAINTEANCE FOUND A PIECE OF STAINLESS STEEL IN THE LOWER SECTION OF COWL. INVESTIGATION REVEALED A HOLE IN THE LT SIDE OF ASPIRATOR ASSEMBLY ABOVE THE OIL COOLER. THE ASPIRATOR WAS REPLACED AND AIRCRAFT SINCE RETURNED TO SERVICE. Feb 11, 2006 · Swrngn SA226TC · Nacelle/Pylon, Main FrameSDR CA060126007Blade · damaged(CAN) DISCOVERED WARPED TRAILING EDGE OF PROPELLER BY MAINTENANCE. UNIT HAD BEEN OVERHAULED FEB 2003 THEN RETURNED FOR THIN TRAILING EDGE APRIL 2003. REPAIRED BY SAME FACILITY. TRAILING EDGE WAS SIGNIFICANTLY THINNER THAN SIMILAR IN FLEET. REMOVED PROPELLEJan 20, 2006 · Swrngn SA226TC · Propeller Blade SectionSDR CA060112005Door · jammedDURING APPROACH, CREW ATTEMPTED TO EXTEND L/G AND NOTICED RT MAIN WAS NOT DOWN AND LOCKED. IT WAS DETERMINED LANDING GEAR WAS NOT COMING OUT OF RT W/W. IT TOOK SEVEN ATTEMPTS TO GET LANDING GEAR TO COME DOWN AND LOCK INTO POSITION. INSPECTION REVEALED RT I/Jan 10, 2006 · Swrngn SA226TC · Landing Gear DoorsSDR AU510001635Wire Harness · deterioratedFUEL BOOST PUMP WIRING HARNESSES PN 27-82015-810 AND PN 27-82015-811 DETERIORATED. FOUND DURING INSPECTION IAW AD/SWA226/51 AND SB226-28-011.Dec 12, 2005 · Swrngn SA226TC · Fuel System WiringSDR CA051027009Web · cracked(CAN) DURING INSPECTION, MAINTENANCE FOUND SEVERAL FATIGUE CRACKS IN THE CENTER AISLE FLOORBOARD WEBS AND FLOOR FRAMES BETWEEN STATIONS 174 AND 427. THESE CRACKS WERE FOUND ON BOTH THE LT AND RT SIDES OF THE AISLE. BOTH WEBS WERE REPLACED.Oct 25, 2005 · Swrngn SA226TC · Fuselage Miscellaneous StructureSDR CA050804010Release Cable · sheared(CAN) WHEN COMPLYING WITH AN UNRELATED INSPECTION UNDER THE COCKPIT FLOOR, MAINTENANCE DISCOVERED THE NOSE LANDING GEAR EMERGENCY RELEASE CABLE WAS SHEARED AT THE CLEVIS WHERE IT ATTACHES TO THE HANDLE BELLCRANK. THIS AIRCAFT HAD RECENTLY (WITHIN 50 HOURS) UNAug 2, 2005 · Swrngn SA226TC · Landing Gear Retraction/Extension SystemSDR TCA005Transceiver · inoperativeDOCUMENTED ON FL241 BY PILOT, LOST ALL RADIO CONTACT SHORTLY AFTER DEPARTURE, NR 1 AND NR 2 COMM NO AUDIO FROM ANY RADIOS. PILOT RETURNED TO TOL WITHOUT INCIDENT AFTER DECLARING EMERGENCY WITH TOL TOWER.Aug 1, 2005 · N629E · Swrngn SA226TC · VHF Communications SystemSDR CA050725007Fcu · leaking(CAN) UPON LANDING AND SHUTDOWN OF THE LT ENGINE IT WAS NOTICED THAT THE OVERBOARD ENGINE DRAIN FOR THE FUEL CONTROL UNIT WAS LEAKING FUEL. THE FUEL CONTROL WAS REPLACED. THE LAST TIME THIS FCU WAS REPAIRED IT WAS FOR THE SAME FUEL LEAK PROBLEM IN MARCH OF 200Jul 21, 2005 · Swrngn SA226TC · Fuel Control/Turbine EnginesSDR CA050725003Carrier Assy · cracked(CAN) DURING ENGINE TREND RECORDING BY THE FLIGHT CREW IT WAS NOTICED THAT THE LH ENGINE OIL PRESSURE INDICTION HAD DECREASED 15 PSI WITHIN A WEEK OF OPERATION. UPON ARRIVAL MAINTENACE WAS ADVISED AND ELECTED TO REMOVE THE ENGINE FOR INSPECTION. UPON INSPECTIOJul 20, 2005 · Swrngn SA226TC · Turbine Engine Reduction GearSDR CA050623004Torque Tube · chafedDURING AN INSPECTION, IT WAS DISCOVERED THAT THE RIGHT ELEVATOR TORQUE TUBE HORN WAS CHAFFED. THE CAUSE OF THE CHAFF WAS A SCREW, WHICH ATTACHES A CLOSING PANEL ON THE VERTICAL STAB. THE TORQUE TUBE WAS REPLACED AND A SHORTER SCREW INSTALLED.Jun 21, 2005 · Swrngn SA226TC · Stabilizer Control SystemSDR TCA004Engine · overservicedTHE PILOT REPORTED THAT INBOUND FLIGHT TO LRD THERE WAS A SMELL OF OIL IN THE COCKPIT. SHUT DOWN THE BLEED AIR AND THE SMELL DISAPPEARED. DID NOT DECLARE AN EMERGENCY AND LANDED WITHOUT INCIDENT. AFTER LANDING, WAS INSTRUCTED BY BASE MX IN TOL TO CHECK ALL Jun 5, 2005 · N629EK · Swrngn SA226TC · Turbine Engine Oil System
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