N206FS

Part: FRAME — CORRODED (FUSELAGE) · airframe 12,324 hrs

AFT LOWER FRAME ASSY WAS FOUND TO BE CORRODED. THE AFT LOWER FRAME WILL THEN BE REPAIRED IAW THE FAA-APPROVED REPAIR DATA.

Part: DIFFUSER — SEPARATED (COMPRESSOR) · airframe 12,324 hrs

ENGINE WAS REMOVED DUE TO CYCLED WHEELS. COMPRESSOR DISASSEMBLED DUE TO CRACKED SCROLL. DIFFUSER FOUND TO HAVE SEPARATED PLATE. REPLACED DIFFUSER.

Part: CONTROL TUBE — CRACKED · airframe 12,211 hrs

CORROSION AND CRACKS ON CONTROL TUBE, NEXT TO END AT FIXED CLEVIS. SCRAPPED CONTROL TUBE. NOTE: PREVIOUSLY SUBMITTED ON 10/6/09.

Part: STRUCTURE — CORRODED (STABILIZER) · airframe 12,211 hrs

CORROSION AND CRACKS ON LT STABILIZER SPAR TUBE. SENT TO VENDOR FOR REPAIR. NOTE: PREVIOUSLY SUBMITTED ON 10/6/09.

Part: STRUCTURE — CORRODED (TAILBOOM) · airframe 12,211 hrs

EXCESSIVE CORROSION ON TOP CENTER SURFACE OF HORIZONTAL STABILIZER ASSY. SENT TO VENDOR FOR REPAIR. NOTE: PREVIOUSLY SUBMITTED ON 10/6/09.

Part: BATTERY — DISCHARGED (MAIN)

MAIN BATTERY, NO VOLTS.

Part: BEARING — WORN (BELLCRANK)

MAIN ROTOR BELLCRANK HAS WORN BEARINGS. REPLACED 2 BEARINGS 206001053005. REPAIRED.

Part: SEAT BELT — MISMANUFACTURED (COCKPIT) · airframe 10,070 hrs

SEAT BELT RESTRAINT TOO SHORT.

Part: CHECK VALVE — SMOKE (TURBINE OIL) · airframe 9,968 hrs

TURBINE OIL PRESSURE CHECK VALVE SMOKING ON SHUTDOWN. REPAIRED.

Part: BATTERY — WEAK (MAIN)

MAIN BATTERY WEAK.

Part: SHAFT — SHEARED (STARTER GEN) · airframe 9,957 hrs

STARTER GENERATOR HAS A SHEARED SHAFT.

Part: SPLINE ADAPTER — WORN (TACH GENERATOR) · airframe 10,002 hrs

TACH GENERATOR HAS A WORN DRIVE SPLINE.

Part: GPS — INOPERATIVE (COCKPIT) · airframe 9,940 hrs

GPS RECEIVER INOPERATIVE.

Part: CROSSTUBE — CORRODED (MLG) · airframe 9,562 hrs

CROSSTUBE CORRODED BEYOND LIMITS. REPLACED WITH SERVICEABLE CROSSTUBE.

Part: SKID — CORRODED (MLG) · airframe 9,952 hrs

SKID TUBE CRACKED DUE TO CORROSION EXFOLIATING FROM TUBE AT FORWARD END NEAR HOLD DOWN RING.

Part: CROSSTUBE — CORRODED (MLG) · airframe 9,843 hrs

CORROSION PITS BEYOND LIMITS. REPLACED WITH SERVICEABLE CROSSTUBE.

Part: SKID — CORRODED (MLG) · airframe 8,843 hrs

CORROSION PITS BEYOND LIMITS. REPLACED WITH SERVICEABLE CROSSTUBE.

Part: SKID — CORRODED (MLG) · airframe 8,843 hrs

CORROSION PITS BEYOND LIMITS. REPLACED WITH SERVICEABLE PART.

Part: CROSSTUBE — CORRODED (MLG) · airframe 8,843 hrs

CORROSION PITS BEYOND LIMITS. REPLACED WITH SERVICEABLE CROSSTUBE.

Part: RESTRAINT — WEAK (FLAP) · airframe 809 hrs

SPRINGS WEAK AND STICKING ARMS. REPLACED WITH SERVICEABLE ASSY.

Part: SERVO — LEAKING (MAIN ROTOR) · airframe 8,843 hrs

CAUSING EXCESSIVE INTERNAL LEAKAGE. FOUND DEFECTIVE LAPPING. SENT TO FORTNER ACCESSORY SERVICE CORP. FOR WARRANTY REPAIR.

Part: VALVE — DAMAGED (ENGINE) · airframe 8,843 hrs

THREADS DAMAGED THAT GO INTO COMBUSTION CASE. REPLACED WITH SERVICEABLE PART.

Part: WEB — WORN (SERVO MOUNT) · airframe 8,843 hrs

OUTBOARD FORWARD SERVO MOUNT LUGS ARE BEING WORN BY THE SERVO FORWARD ROD END BEARING DUE TO ROCKING MOTION OF THE SERVO. REPLACED WITH SERVICEABLE PART.

Part: INDICATOR — READS HIGH (OIL PRESSURE)

INDICATOR READS 4 PSI HIGH.

Part: FILTER — MALFUNCTIONED (ENGINE OIL)

FILTER WILL NOT BYPASS.

Part: FLOAT — LEAKING (MLG)

FLOAT BAG ASSEMBLY FAILED 6 HOUR LEAK TEST AFTER 2 HOURS.

Part: FLOAT — LEAKING (MLG)

FLOAT BAG ASSEMBLY FAILED 6 HOUR LEAK TEST AFTER 2 HOURS.

Part: BEARING SEAT — WORN (M/R GEARBOX)

BEARING SEAT WORN BEYOND LIMITS. REPLACED WITH SERVICEABLE CARRIER ASSY.

Part: RECEIVER — MALFUNCTIONED (LORAN)

RIGHT INSIDE KNOB STEM POWER OUT WITH KNOB ON LORAN.

Part: SHAFT — CORRODED (FREEWHEEL)

CORROSION BEYOND LIMITS ON SEAL RIDE. REPLACED WITH SERVICEABLE SHAFT.

Part: TORQUEMETER — STICKING (COCKPIT)

TORQUE NEEDLE STICKS AT 14 PERCENT WHEN DECREASING PRESSURE.

Part: INDICATOR — STICKS (COCKPIT TOT)

TOT INDICATOR INTERMITTENTLY STICKS AT ZERO.

Part: PROBE — FAILED (FUEL QTY)

PROBE PEGS OUT FUEL QUANTITY INDICATOR HIGH SIDE.

Part: INDICATOR — FAILED (COCKPIT TOT)

NO TOT INDICATIONS.

Part: TORQUEMETER — DEFECTIVE (ENGINE)

ENGINE TORQUE GAUGE FLUCTUATES.

Part: GRIP — WORN (M/R)

ASSEMBLY LEAKING GREASE, DUE TO RETAINER SPINNING INSIDE OF GRIP. PRO SEAL UNBONDED. WORN AREA IN GRIP. MIN .007 MAX. .012 DEPTH. REPLACED WITH SERVICEABLE PARTS.

Part: SPLINE ADAPTER — MIS MFG (TURBINE)

RECEIVING INSPECTION OF NEW, NEVER INSTALLED SPLINE ADAPTER INDICATED I.D. MANUFACTURED .0005" OVER MAX B.P. SPECS OF .6565". ADAPTER MEASURES .657. INSTALLED NEW SPLINE ADAPTER. SHIPMENT OF PART AND SUBMITTAL FOR CREDIT ACCOMPLISHED ON AFA# 24444A.

Part: TRANSCEIVER — DEFECTIVE (COCKPIT ATC)

SECOND KNOB WILL NOT TURN INTERNAL NUMBER. REPLACED ONE KNOB SHAFT FROM SPARE. ALSO REPLACED V101 CAVITY OSCILLATOR THAT WAS WEAK. REPAIRED PROBLEM. BENCH CHECK GOOD.

Part: CELL — DEFECTIVE (DC SYS)

TIME. INSPECTED BY ACCESSORY SHOP AND FOUND CELL #14 VOLTAGE READING ZERO AS RECEIVED. CELL REPLACED WITH ONE GIVEN ON CONSIGNMENT.

Part: TRANSCEIVER — MALFUNCTION (COCKPIT)

SWITCHES CHANNELS BY ITSELF AND HARD TO CHANGE FREQUENCY.

Part: BEARING — CRACKED (T/R)

BEARINGS CRACKED. ALSO REPLACED 4 EACH SLEEVES P/N 206-010-733-003. BEARINGS SCRAPPED LOCALLY. SEE MMIR'S # 4831 THROUGH # 4844 FOR ADDITIONAL BEARINGS.

Part: SHAFT — CORRODED (FREEWHEEL)

CORROSION BEYOND LIMITS ON SEAL RIDE.