N6160Z

Part: BATTERY — DISCHARGED (MAIN)

WEAK. REPLACED WITH SERVICEABLE BATTERY.

Part: BATTERY — DISCHARGED (MAIN)

WEAK. REPLACED WITH SERVICEABLE BATTERY.

Part: ACTUATOR — INOPERATIVE (ENGINE) · airframe 10,690 hrs

ACTUATOR INOPERATIVE.

Part: RESTRAINT — STUCK (MAIN ROTOR) · airframe 10,639 hrs

STICKING. REPLACED WITH SERVICEABLE PART.

Part: INDICATOR — FAILED (TOT) · airframe 10,612 hrs

DURING START TOT INDICATOR DID NOT INDICATE TEMPERATURE. SENDING TO VENDOR FOR REPAIR.

Part: TRANSPONDER — MALFUNCTIONED (OSILLATOR)

TRANSCEIVER'S I.D. LIGHT STAYS ON.

Part: TRANSPONDER — MALFUNCTIONED (COCKPIT)

TRANSCEIVER IDENT LIGHT STAYS ON.

Part: GYRO — PRECESSING (COCKPIT)

ATTITUDE GYRO PRECESSES 4 DEGREES DURING CLIMB AND DIVE ERECTION RATES.

Part: FILTER — MALFUNCTIONED (ENGINE OIL)

FILTER NOT BYPASS.

Part: FUEL CELL — DAMAGED (FUSELAGE)

FUEL CELL HAS BLISTERS INSIDE AND OUTSIDE OF CELL.

Part: INDICATOR — FAILED (ENGINE OIL)

INDICATOR WAS REMOVED FROM BOWL AND CLEANED. INSTALLED INDICATOR BACK ON BOWL, TESTED AND INDICATOR STILL DIDN'T WORK.

Part: INDICATOR — FLUCTUATES (GAS PRODUCER)

TACHOMETER NEEDLE FLUCTUATES AND DROPS OFF.

Part: POWER SUPPLY — FAILED (STROBE)

STROBE INOPERATIVE.

Part: POWER SUPPLY — FAILED (STROBE)

STROBE INOPERATIVE.

Part: GPS — FAILED (COCKPIT)

GPS BATTERY LOW INDICATED.

Part: STOP — DETERIORATED (MAIN ROTOR)

RUBBER STOP DETERIORATED.

Part: VOLT REGULATOR — FAILED (DC SYS)

VOLTAGE REGULATOR FAILED GENERATOR WONT COME ON LINE.

Part: TRANSMITTER — INTERMITTENT (FUEL QTY)

INTERMITTENT FUEL QUANTITY FLUCTUATION.

Part: TRANSDUCER — ERRATIC (FUEL PRESS)

TRANSDUCER READS ERRATIC.

Part: YOKE — MIS MFG (T/R)

THE POSITION OF THE FLAPPING RELIEF ARE MISMACHINED IN CENTER BORE OF YOKE. THE RELIEF ARE 90 DEGREES OFF FROM PROPER POSITION. (MISMANUFACTURED)

Part: TACH GEN — WORN SPLINE (ROTOR)

TACH GEN WORN DRIVE SPLINE.

Part: TRANSMITTER — ERRATIC (FUEL QTY)

FUEL QUANTITY READING ERRATIC.

Part: LORAN — FAULTY (COCKPIT)

LORAN INTERMITTENT.

Part: TRANSCEIVER — DEFECTIVE (COCKPIT)

TAKES AWHILE FOR DISPLAY TO COME ON AND A LOT OF BACKGROUND NOISE WHEN TRANSMITTING. VERIFIED DISPLAY HAD MISSING SEGMENTS. REPLACED DISPLAY DS901 P/N 037-5060-01. REPAIRED PROBLEM. BENCH CHECK GOOD.

Part: CROSSTUBE — PAD SLIPPING (SKIDS)

PADS SLIPPING. ASB NO. 94046 WAS COMPLIED WITH 1-13-95 BY PHI SHEETMETAL SHOP.

Part: INDICATOR — DEFECTIVE (DUAL TACH)

TURBINE NEEDLE DROPS 20 RPM WHEN AIRCRAFT IS AT 100 RPM. TIME SINCE REPAIR 16:45.

Part: INDICATOR — DEFECTIVE (DUAL TACH)

LOW ROTOR WARNING HORN WILL NOT MUTE WHEN REDUCED TO IDLE.

Part: HOUSING — LEAKING (TRANSMISSION)

INPUT SEAL LEAKING ON TRANSMISSION. INSTALLED SERVICEABLE SEAL ASSY.

Part: GOVERNOR — DEFECTIVE (ENGINE)

ON TAKEOFF, N1, N2 AND ROTOR FLUCTUATIONS -- OVERTORQUE EXCEEDING 120%. REPLACED WITH SERVICEABLE GOVERNOR AND PERFORMED OVERTORQUE INSPECTION.

Part: PUMP — LEAKING (INNER SEAL)

OIL PUMP INNER SEAL LEAKING. REPLACED WITH SERVICEABLE OIL PUMP.

Part: TRANSCEIVER — INOPERATIVE (COCKPIT)

INOPERATIVE. REPLACED BURNT F401 FUSE, INSTALLED Q415 HEAT SINK. REPAIRED CONNECTION AT LOCAL OSCILLATOR. RETURNED TO SERVICE.

Part: NOZZLE — DEFECTIVE (4TH STAGE)

ENGINE REMOVED DUE TO N2 DRAG. UPON INSPECTION OF TURBINE PARTS NOTED THE FOLLOWING: LIFTING AND FLAKING PLASMA IN 4TH STAGE NOZZLE #4 TIP PATH. INSTALLED SERVICEABLE 4TH STAGE NOZZLE.