N8199J

Part: HUB — DAMAGED (TAIL ROTOR)

TAIL ROTOR HEAD AND BLADES ARE DAMAGED.

Part: TURBINE WHEEL — CRACKED (ENGINE) · airframe 3,868 hrs

TURBINE REMOVED FOR HIGH CYCLED WHEELS. UPON INSPECTION OF PARTS NOTED SULFIDATION AND CRACKED NR 1 WHEEL BLADES. SCRAPPED WHEEL.

Part: BLEED VALVE — FAILED (ENGINE) · airframe 4,125 hrs

FAILED BLEED VALVE ALLOWING ENGINE TO PRODUCE HIGH TOT.

Part: DOOR — DEPARTED (HYD PACK)

WHILE IN FLIGHT, THE HYDRAULIC PACK INSPECTION DOOR ON THE LT SIDE OF TRANSMISSION COWL DEPARTED AIRCRAFT. NO ADDITIONAL DAMAGE TO AIRCRAFT. REPLACED COVER.

Part: BLADE — FLAKING (TAIL ROTOR)

PAINT ON TAIL ROTOR BLADE FLAKING.

Part: BLADE — FLAKING (TAIL ROTOR)

PAINT ON TAIL ROTOR BLADE FLAKING.

Part: TUBE — MISMANUFACTURED (ENGINE OIL)

FAILED DIMENSIONAL REQUIREMENTS OF CEB1307 ON OIL FILTER INLET TUBE ASSY. INSTALLED NEW PART.

Part: INDICATOR — LAGGING (TRIPLE TACH)

TRIPLE RPM INDICATOR'S NR 1 NEEDLE LAGGING.

Part: CLOCK — DAMAGED (COCKPIT)

CLOCK HARD TO WIND.

Part: INDICATOR — READS HIGH (COCKPIT)

RPM INDICATOR'S NR 1 NEEDLE 3 PERCENT HIGHER THAN THE OTHER TWO THROUGHOUT RANGE ALL THE TIME.

Part: AUDIO SELECTOR — MALFUNCTIONED (DUAL CHANNEL)

CABIN ICS SYSTEM HAS BACKGROUND NOISE WHILE IN-FLIGHT AND AFTER START WITH VOX OFF.

Part: NAV COMM — INTERMITTENT (COCKPIT)

VOLUME CONTROL IS WEAK AND INTERMITTENT.

Part: BLADE — DAMAGED (TAIL ROTOR)

TIP OF TAIL ROTOR BLADE DAMAGED.

Part: FLOAT — LEAKING (MLG)

FLOAT BAGS LEAKING.

Part: INDICATOR — FLUCTUATED (TRIPLE TACH)

RPM ROTOR NEEDLE FLUCTUATES, COULD NOT VERIFY COMPLAINT, HOWEVER, NR 1 AND NR 2 NEEDLES HAVE ABOUT 2 PERCENT SPLIT IN MOVEMENT.

Part: INDICATOR — INOPERATIVE (TRIPLE TACH)

TRIPLE RPM INDICATION, NEEDLES INOPERATIVE.

Part: REGULATOR — FAILED (AC SYSTEM)

NR 1 GENERATOR WILL NOT COME ON-LINE.

Part: BEARING — SPALLED (2.5 BEARING)

ENGINE REMOVED DUE TO METAL. UPON INSPECTION OF GEARBOX PARTS NOTED: SPALLED ON NR 2 1/2 BEARING OUTER RACE AND ROLLERS. INSTALLE D A NEW BEARING.

Part: GYRO — MALFUNCTIONED (COCKPIT)

CIRCUIT BREAKER TRIPS ON GYRO.

Part: STARTER — FAILED (START/GEN)

STARTER/GENERATOR INTERMITTENTLY WILL NOT ENGAGE ON START.

Part: TRANSMITTER — MALFUNCTIONED (FUEL SYSTEM)

FUEL PRESSURE FLUCTUATES. FUNCTION CHECK BAD, TRANSMITTER OUTPUT PEGS OUT AT 15 PSI.

Part: ICS — INOPERATIVE (DUAL CHANNEL)

ICS INOPERATIVE-PERFORMED TEST AND ALIGNMENT.

Part: TUBE ASSY — WORN (ENG GR BOX)

ENGINE REMOVED DUE TO METAL. INSPECTION OF GEARBOX PARTS REVEALED: TUBE ASSY. FAILED DIMENSIONAL CHECK PER CEB1307. INSTALLED A NEW TUBE.

Part: TURBINE WHEEL — DEFECTIVE (3RD STAGE)

ENGINE REMOVED DUE TO TURBINE 1750 HOUR INSPECTION. UPON INSPECTION OF TURBINE PARTS NOTED: SEVERE SULFIDATION ON ALL NR3 WHEEL BLADES. SCRAPPED NR3 WHEEL AND REPLACED WITH SERVICEABLE PART.

Part: TURBINE WHEEL — DEFECTIVE (1ST STAGE)

ENGINE REMOVED DUE TO TURBINE 1750 HOUR INSPECTION. UPON INSPECTION OF TURBINE PARTS NOTED: CATASTROPHIC SULFIDATION ON ALL NR1 WHEEL BLADES. SCRAPPED NR1 WHEEL AND REPLACED WITH SERVICEABLE PART.

Part: TRANSMITTER — FAILED (MAST MOMENT)

TORQUE TRANSMITTER INOPERATIVE.

Part: INDICATOR — FAILED (MAST MOMENT)

INDICATOR INOPERATIVE.

Part: WARNING SYS — FAILED (OIL PRESS)

OIL PRESS WARN WOULD NOT ILLUMINATE "T" OIL LIGHT.

Part: GPS — FAILED (COCKPIT)

GPS INOPERATIVE.

Part: INDICATOR — ERRATIC (FUEL)

NR2 NEEDLE ERRATIC BELOW 30%.

Part: VALVE — FAILED (OIL SOV)

VALVE WILL NOT OPEN.

Part: VALVE — INOPERATIVE (OIL SOV)

VALVE INOPERATIVE; WILL NOT OPEN.