N202LF

Part: SHIELD — BROKEN (MAIN ROTOR) · airframe 4,794 hrs

SHIELD, BROKEN AND REPLACED.

Part: SHIELD — BROKEN (MAIN ROTOR) · airframe 4,794 hrs

SHIELD, BROKEN AND REPLACED.

Part: SHIELD — BROKEN (MAIN ROTOR) · airframe 4,794 hrs

SHIELD, BROKEN AND REPLACED.

Part: HYDRAULIC SYSTEM — LEAKING · airframe 4,790 hrs

LEAKING HYDRAULIC UNIT.

Part: CONTROL UNIT — UNSERVICEABLE (FLT CONTROLS) · airframe 4,790 hrs

CONTROL UNIT IS CAUSING AN UNCONTROLLABLE LATERAL INPUT.

Part: METER — UNSERVICEABLE (TORQUE) · airframe 4,771 hrs

TORQUE KEEPS FLUCTUATING.

Part: SWITCH — STUCK (HYD SYS TEST)

WHEN PERFORMING THE FUNCTIONAL TEST OF THE HYDRAULIC SYSTEM, CHAPTER 43-14, PG 24 OF THE MM. UNABLE TO GET THE HYDRAULIC UNIT TO SWITCH OVER TO THE NR 2 POSITION. DURING THE INVESTIGATION, IT WAS OBSERVED THAT THE HYDRAULIC TEST SWITCH WAS STUCK IN THE RESET POSITION. THE RESULT WAS WHEN FAILING THE NR 1 SYSTEM THE HYDRAULIC PAC SHOULD SWITCH OVER TO THE NR 2 SYSTEM, IT WAS TRYING TO RESET TO THE NR 1 POSITION. ADJUSTING THE SWITCH AND THE GUARD YIELDED NO SUCCESS. REPLACING THE SWITCH AND THE SWITCH GUARD YIELDED A POSITIVE RESULT. (K)

Part: FIREWALL — DAMAGED (ENGINE BAY) · airframe 4,719 hrs

FIREWALL REPAIRED TOO MANY TIMES AND NOW IS UNSAFE.

Part: CLUTCH — UNSERVICEABLE (M/R XMSN) · airframe 4,719 hrs

CLUTCH WORN BEYOND LIMITS.

Part: FIREWALL — CRACKED (NACELLE) · airframe 4,719 hrs

FIREWALL IS CRACKED BY FASTNERS AND HAS BEEN REPAIRED SEVERAL TIMES BEFORE. INTEGRITY IS COMPROMISED AND DO NOT WANT ENGINE TO INGEST FOD.

Part: SKID — UNSERVICEABLE (MLG) · airframe 4,719 hrs

RIVETS PULLED AND GOUGES IN BOTTOM OF TUBE.

Part: STARTER GEN — UNSERVICEABLE (NR 2 ENGINE) · airframe 4,413 hrs

NR 2 ENG FAILED TO START. STARTER GENERATOR UNSERVICEABLE.

Part: TORQUEMETER — UNSERVICEABLE (ENGINE) · airframe 4,668 hrs

FLUCTUATING OVER 40 PERCENT WITH NO CHANGE IN N1 OR TOT.

Part: CONTROL UNIT — UNSERVICEABLE (FLT CONTROLS) · airframe 4,555 hrs

CAUSING UNCONTROLLED INPUT IN LATERAL AXIS OF FLIGHT CONTROLS.

Part: BEARING — WORN (BELLCRANK) · airframe 4,632 hrs

BEARINGS ARE WORN CAUSING EXCESSIVE PLAY.

Part: SEAT — TORN (COCKPIT) · airframe 4,599 hrs

SEAT TORN, CUSHION HAS NO SUPPORT.

Part: SEAT — CRUSHED (COCKPIT) · airframe 4,599 hrs

CRUSHABLE SEATS WERE CRUSHED.

Part: PRESSURE SWITCH — UNSERVICEABLE (OIL PRESSURE) · airframe 4,581 hrs

PRESSURE SWITCH FAILED AND REPLACED.

Part: NEEDLE — STUCK (TRIPLE TACH) · airframe 4,479 hrs

TRIPLE TACH NEEDLES WERE STICKING REPLACED TRIPLE TACH

Part: NEEDLE — DEFECTIVE (TRIPLE TACH) · airframe 4,479 hrs

TRIPLE TACH NEEDLES WERE STICKING REPLACED TRIPLE TACH

Part: ACTUATOR — DEFECTIVE (PITCH) · airframe 4,474 hrs

PITCH CSAS FAILED REPLACED ACTUATOR.

Part: POWERPACK — DEFECTIVE (HYD SYSTEM) · airframe 4,466 hrs

HYDRAULIC PACK LEAKING, REPLACED.

Part: IGNITER BOX — DEFECTIVE (NR 1 ENGINE) · airframe 4,439 hrs

NR 1 ENGINE WOULD NOT START, EXCITER BOX WAS NOT PUTTING OUT REPLACED

Part: SKIN — CRACKED (VERTICAL STAB)

FOUND FATIGUE CRACK IN RIGHT VERTICAL STABILIZER FIN DURING PREFLIGHT. CRACK STARTED AT FORWARD AND TOP ATTACH POINTS AND RAN AFT FOR APPROXIMATELY 8 INCHES. CRACK WAS ON INSIDE SURFACE AT MOUNTING POINTS TO HORIZONTAL STABILIZER.

Part: SWITCH — INOPERATIVE (ROTOR OIL SYSTEM)

SWITCH INOPERATIVE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.

Part: SWITCH — INOPERATIVE (ROTOR OIL SYSTEM)

SWITCH INOPERATIVE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.

Part: SWITCH — INOPERATIAVE (GEARBOX)

SWITCH INOPERATIVE. FAILS TO ILLUMINATE PRESSURE LIGHT. LIGHT FLICKERS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.

Part: SWITCH — INOPERATIVE (OIL PRESSURE)

OIL PRESSURE WARNING SWITCH INOPERATIVE. WILL NOT TURN OFF MAIN TRANSMISSION PRESSURE WARNING LIGHT. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.

Part: SHAFT — DEFECTIVE (M/R DRIVE)

RECEIVED UNIT IN NEW CONDITION AND FOUND THE PLATING WAS PEELING OFF. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.

Part: SHAFT — DEFECTIVE (M/R DRIVE)

RECEIVED SHAFT UNIT IN NEW CONDITION AND FOUND THE PLATING WAS PEELING OFF. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.

Part: CONTROL UNIT — MALFUNCTIONED (AUTOFLIGHT)

CONTROL MALFUNCTION, ROLL FEEDBACK DURING FLIGHT AND PITCH INOPERATIVE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.

Part: BUSHING — WORN (ENGINE MOUNT)

ENGINE MOUNT BUSHING'S ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.

Part: INDICATOR — STICKS (DUAL TORQUE)

DUAL TORQUE INDICATOR NEEDLES STICK. REPLACES WITH NEW UNIT, CORRECTED PROBLEM.

Part: BEARING — WORN (T/R)

BEARING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.

Part: SWITCH — FAILED (OIL PRESS WARN)

OIL PRESSURE WARNING SWITCH INOPERATIVE. LOW PRESSURE LIGHT 'ON' IN-FLIGHT AND AT GROUND IDLE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.

Part: BUSHING — WORN (ENGINE MOUNT)

ENGINE MOUNT BUSHING'S ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.

Part: GEARSHAFT — WORN (SPUR ADAPTER)

SPUR ADAPTER GEARSHAFT HAD EXCESSIVE SPLINE WEAR. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.

Part: SWITCH — FAILED (OIL PRESSURE)

TRANSMISSION OIL PRESSURE LIGHT ILLUMINATES DURING FLIGHT. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.

Part: SWITCH — FAILED (OIL PRESSURE)

TRANSMISSION LIGHT ILLUMINATES DURING FLIGHT. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.

Part: CONTROL UNIT — INOPERATIVE (AUTOFLIGHT)

CONTROL UNIT INOPERATIVE. AIRCRAFT EXPERIENCED PITCH AND ROLL HARD OVERS UPON TAKEOFF. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.

Part: BEARING — WORN (T/R)

BEARING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS, CORRECTED PROBLEM.

Part: SWITCH — INOPERATIVE (OIL PRESS WARN)

OIL PRESS WARN SWITCH INOPERATIVE. LIGHT CAME ON DURING FLIGHT THEN WENT OUT. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.

Part: BELLOWS — TORN (M/R)

BELLOWS IS TORN AROUND CLAMP AND FOLD AREAS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.

Part: BEARING — WORN (T/R)

BEARING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS. CORRECTED PROBLEM.

Part: BELLOWS — TORN (M/R MAST)

BELLOWS IS TORN AROUND CLAMP AND FOLD AREAS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.

Part: BUSHING — WORN (T/R)

TEFLON LINERS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS, CORRECTED PROBLEM.

Part: BUSHING — WORN (T/R)

TEFLON LINERS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS, CORRECTED PROBLEM.

Part: BLADE PIN — WORN (M/R)

BLADE PIN WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.

Part: INDICATOR — INOPERATIVE (ENG TQ)

INDICATOR UNIT INOPERATIVE UPON INSTALL. GAUGE READS APPROXIMATELY 20 PERCENT TQ ON BOTH ENGINES WITH JUST ELECTRICAL POWER APPLIED. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.

Part: SWITCH — DEFECTIVE (OIL PRESS WARN)

OIL PRESS WARN CAUSES LIGHT TO COME ON TOO SOON.

Part: HYD PACK — WORN (NR 1 SYS)

LATERAL PLAY ON #1 SYSTEM. LONGITUDINAL AND COLLECTIVE INPUT LEVERS EXCEEDED .5MM.