N2014K

Part: BLADE — DAMAGED (MAIN ROTOR) · airframe 17,733 hrs

OUTBOARD ABRASION STRIP HAS SEVERAL HOLES AND SEPARATION ON TRIM TABS.

Part: BLADE — DAMAGED (MAIN ROTOR) · airframe 17,733 hrs

OUTBOARD ABRASION STRIP HAS SEVERAL HOLES AND SEPARATION ON TRIM TABS.

Part: FLOAT — FAILED (MLG) · airframe 16,912 hrs

AFTER ELECTRICAL INFLATION OF FLOAT SYSTEM, A LEAK AT THE REAR POP OFF VALVE WAS NOTED. VALVE THREADS WERE STRIPPED. VALVE WOULD ONLY ROTATE.

Part: COMPENSATOR — CORRODED (COCKPIT)

COMPENSATOR CORRODED.

Part: INDICATOR — INOPERATIVE (COCKPIT)

RATE OF TURN NEEDLE INOPERATIVE.

Part: INDICATOR — FAILED (COCKPIT)

ATTITUDE INDICATOR TUMBLING.

Part: INVERTER — INOPERATIVE (DC SYSTEM)

INVERTER HAD NO OUTPUT.

Part: DUAL AMMETER — STICKING (COCKPIT)

NR 1 POINTER STICKS.

Part: INVERTER — INOPERATIVE (AC SYSTEM)

INVERTER INOPERATIVE.

Part: STROBE — FAILED (FUSELAGE)

STROBE LIGHT DOES NOT FLASH, INOPERATIVE.

Part: DETECTOR — INOPERATIVE (RPM LIMIT)

RPM LIMIT DETECTOR INOPERATIVE.

Part: INDICATOR — STUCK (FUEL QUANTITY)

INDICATOR IS PEGGED PAST ZERO.

Part: INDICATOR — INOPERATIVE (COCKPIT)

INDICATOR HAS NO DISPLAY.

Part: BLADE — MALFUNCTIONED (MAIN ROTOR)

BLADE CLIMBS EXCESSIVELY.

Part: BLADE — WON'T TRACK (MAIN ROTOR)

BLADE WILL NOT TRACK.

Part: BLADE — HEAVY (MAIN ROTOR)

BLADE CLIMBS EXCESSIVELY IN FLIGHT AND IS HEAVY.

Part: ABRASION STRIP — DAMAGED (M/R BLADE)

OUTBOARD ABRASION STRIP ON BLADE HAS PIN HOLE PENETRATED.

Part: ABRASION STRIP — DAMAGED (M/R BLADE)

OUTBOARD ABRASION STRIP ON BLADE HAS PIN HOLE PENETRATED.

Part: ABRASION STRIP — DAMAGED (M/R BLADE)

OUTBOARD ABRASION STRIP ON BLADE HAS PIN HOLE PENETRATED.

Part: ABRASION STRIP — DAMAGED (M/R BLADE)

OUTBOARD ABRASION STRIP ON BLADE HAS PIN HOLE PENETRATED.

Part: COMPUTER — MALFUNCTIONED (AFCS)

COMPUTER WILL NOT TEST IN YAW POSITION.

Part: COMBINING GRBOX — MAKING METAL (ENGINE)

COMBINING GEAR BOX MAKING METAL.

Part: INDICATOR — STICKS (TRIPLE TACH)

NR 1 NEEDLE STICKS AND INDICATES LOW OUT OF TOLERANCE.

Part: TARSYN — FAILED (COCKPIT)

HSI INOPERATIVE. STAYS AT 270 DEGREES AND NR2 PITCH HARD OVER. TIME SINCE REPAIR 50:30.

Part: TARSYN — SEIZED (AUTO FLIGHT)

TARSYN HSI FROZEN IN PLACE.

Part: TRANSCEIVER — FAILED (COCKPIT)

TRANSCEIVER WILL NOT WORK. FOUND Q103 TRANSISTOR, C106 CAPACITOR AND CR104 DIODE INOPERATIVE AND F1 FUSE BURNT. REPLACED ALL THESE COMPONENTS. UNIT FIRED UP AND ADJUSTED POWER OUT AND PULSE WIDTH. BENCH CHECK GOOD.

Part: BLADE — DEFECTIVE (M/R)

UNABLE TO TRACK AND BALANCE BLADE.

Part: SERVO ASSY — STUCK (M/R)

NR2 ACTUATOR STUCK HARD OVER.

Part: COMPUTER — MALFUNCTION (AFCS)

FAILED 31.2 AND FOLLOWING TEST ON SST.

Part: COMPUTER — MALFUNCTION (AFCS)

AFCS COMPUTER INTERMITTENT KICK IN YAW. FAILED TEST 242 AND 243 IN ROLL.

Part: COMPUTER — FAILS TEST (AFCS)

AFCS COMPUTER FAILS 31.2 AND FOLLOWING TEST ON SST.

Part: CAP ASSY — CRACKED (SKID FWD)

SKID ASSY MOUNT PADS CRACKED.

Part: CAP ASSY — PADS CRACKED (SKID)

SKID ASSY MOUNT PADS CRACKED.

Part: CONTROL ROD — FAILED (T/R)

NR1 PITCH ADI WON'T MOVE.

Part: COMPUTER — FAILED TEST (AFCS)

FAILED TEST 242 AND 243 IN ROLL + 35.3 IN YAW.

Part: INDICATOR — ERROR (TRIPLE TACH)

3% SPLIT IN ENGINE RPMS.

Part: ACTUATOR — FAILED (STEP)

STEP ACTUATOR CAUSES CIRCUIT BREAKER TO POP WHEN ACTIVATED.

Part: DETECTOR — MALFUNCTION (RPM LIMIT)

#1 ENGINE OUT AND PARTICAL SEPARATOR. LIGHT INTERMITTENT.

Part: RECEIVER — DEFECTIVE (COCKPIT ADF)

ADF AUDIO SCRATCHY ON ALL FREQUENCIES.

Part: YAW CONTROL — FAILED (T/R CONTROL)

ACTUATOR FULLY EXTEND WILL NOT RETRACT.

Part: BATTERY PACK — FAILED (CABIN)

BATTERY PACK FAILED CAPACITY TEST.

Part: EJECTOR — CRACKED (LT EXHAUST)

EJECTOR IS CRACKED. AFT HAT BAND CRACKED BEYOND LIMITS APP. 2" LONG.

Part: TRANSCEIVER — DEFECTIVE (COCKPIT)

NO AUDIO. SENT TO DALLAS AVIONICS FOR WARRANTY REPAIR. RECEIVED IN JULY 95.

Part: BLADE — CRACKED (M/R)

BLADE IS CRACKED. (TWO CHORDWISE CRACKS ON THE OUTBOARD LEADING EDGE STRIP. THE FIRST CRACK IS AT STATION 180" WHICH IS COMPLETELY CHORDWISE. THE SECOND CRACK IS AT STATION 199.5 WHICH IS ONLY A PARTIAL CHORDWISE CRACK.

Part: CROSSTUBE — DAMAGED (CROSSTUBE)

CUT MARKS AROUND MOUNTING PADS. NO DAMAGE ALLOWED IN THIS AREA.

Part: ALTIMETER — READS LOW (COCKPIT)

NEEDLE INDICATES 140 FEET LOW AT 18,000 FEET. SENT TO B.F. GOODRICH AEROSPACE FOR INSPECTION AND REPAIR.

Part: ELEVATOR ASSY — FLANGE CRACKED (SPAR)

MOUNTING FLANGE THATS BONDED TO SPAR IS CRACKED FROM SPAR TOWARDS OUTER FLANGE. SCRAPPED ELEVATOR ASSEMBLY.

Part: TRANSCEIVR — DEFECTIVE (COCKPIT COMM)

TRANSMITS AND RECEIVES WEAK.

Part: CONTROL UNIT — FAILED (DC SYS)

CONTROL UNIT FAILED. #2 DC GENERATOR INOPERATIVE.

Part: CVR — WONT TEST (COCKPIT)

CVR WILL NOT TEST.

Part: ACCUMULATOR — LEAKING (HYD)

LEAKING FROM WEEP HOLE. REPLACED WITH SERVICEABLE ACCUMULATOR.

Part: CVR — WONT TEST (COCKPIT)

CVR WILL NOT TEST.

Part: CVR — WONT TEST (COCKPIT)

CVR WILL NOT TEST; RATTLE INSIDE. TIME SINCE REPAIR 0:00.

Part: SKYNAV 5000 — INOPERATIVE (COCKPIT)

SKY NAV 5000 INOPERATIVE.

Part: RECEIVER — INOPERATIVE (COCKPIT ADF)

INOPERATIVE.

Part: GOVERNOR — DEFECTIVE (TURBINE)

UNABLE TO GET NG TOPPING SET.