N3207Q

Part: BATTERY — WEAK (MAIN) · airframe 10,296 hrs

MAIN BATTERY WEAK.

Part: HOUSING — LOOSE (BLEED VALVE)

BLEED VALVE HOUSING IS LOOSE. REPAIRED.

Part: CHECK VALVE — MALFUNCTIONED (FUEL SYSTEM) · airframe 10,148 hrs

POPPET BROKEN IN FUEL SYSTEM CHECK VALVE. SCRAPPED.

Part: INDICATOR — MALFUNCTIONED (ATTITUDE) · airframe 10,247 hrs

ATTITUDE INDICATOR WOULD NOT CAGE. REPAIRED.

Part: SOLENOID VALVE — DAMAGED (ANTI- ICE SYSTEM) · airframe 10,285 hrs

SOLENOID VALVE CAUSING CIRCUIT BREAKER TO POP AND SMOKE. REPLACED WITH SERVICEABLE PART.

Part: BATTERY — WEAK (MAIN) · airframe 10,287 hrs

MAIN BATTERY WEAK.

Part: AMPLIFIER — DAMAGED (ICS) · airframe 10,256 hrs

CABIN ICS AMP UNABLE TO ADJUST VOLUME. SHOP REPAIR.

Part: SEAT BELT — MISMANUFACTURED (COCKPIT) · airframe 9,316 hrs

BELTS (SHOULDER HARNESS) WAS SEWN WRONG SIDE OUT. SHOULDER STRAP ADJUSTMENT ARE ON THE INSIDE (WRONG SIDE).

Part: RELIEF VALVE — LEAKING (EMERGENCY FLOATS) · airframe 10,148 hrs

EMERGENCY FLOAT RELIEF VALVE LEAKING. REPAIRED.

Part: BEARING — WORN (DRIVE LINK) · airframe 10,148 hrs

TAIL ROTOR HEAD DRIVE LINK HAS WORN BEARINGS. REPAIRED.

Part: BEARING — WORN (PITCH LINK ASSY) · airframe 9,975 hrs

TAIL ROTOR HEAD PITCH CONTROL LINK HAS WORN BEARINGS. SCRAPPED.

Part: EXHAUST PIPE — CRACKED (ENGINE) · airframe 10,104 hrs

EXHAUST ASSY CRACKED. REPAIRED.

Part: TRANSDUCER — INOPERATIVE (FUEL PRESSURE) · airframe 10,138 hrs

TRANSDUCER SHOWING NO FUEL PRESSURE INDICATIION. SCRAPPED.

Part: BEARING — WORN (T/R CONTROL ROD) · airframe 10,025 hrs

TAIL ROTOR HEAD CONTROL ROD WORN BEARING. SCRAPPED.

Part: BEARING — WORN (PITCH LINK) · airframe 9,954 hrs

TAIL ROTOR HEAD PITCH CONTROL LINK HAS WORN BEARINGS. REPAIRED.

Part: DUCT — TORN (COMPRESSOR) · airframe 10,025 hrs

ENGINE COMPRESSOR INDUCER BLEED DUCT TORN. SCRAPPED.

Part: GPS — MALFUNCTIONED (COCKPIT) · airframe 9,925 hrs

GPS RECEIVER CARD NEEDS ALIGNMENT.

Part: VOLT REGULATOR — FAILED (DC SYSTEM)

VOLTAGE REGULATAOR DROPS OFF-LINE WHEN RADIO IS KEYED.

Part: TRANSCEIVER — MALFUNCTIONED (COCKPIT)

TRANSCEIVER'S REPLY LIGHT BLINKS CONSTANTLY.

Part: CYLINDER — LEAKING (CYCLIC)

ACTUATOR VALVE BOOT TORN (LEAKING).

Part: COVER — TORN (FLOAT)

FLOAT COVER WORN AND TORN.

Part: FUEL CELL — LEAKING (FUSELAGE)

LEAKAGE THROUGH FABRIC AND BLISTERS INSIDE OF CELL.

Part: INDICATOR — FAILED (TOT)

TOT INDICATOR HAS NO INDICATION ON UNIT.

Part: COVER — TORN (FLOAT)

FLOAT COVER WORN AND TORN.

Part: FREEWHEEL — CRACKED (CAP)

CAP ASSEMBLY HAS CORROSION PITS IN SEAL HOUSING.

Part: SKIN — DENTED (HORIZ STAB)

STABILIZER ASSEMBLY HAS EXCESSIVE DENTS.

Part: POWER SUPPLY — FAILED (STROBE SYSTEM)

STROBE LIGHT POWER SUPPLY HAS NO POWER OUTPUT.

Part: POWER SUPPLY — FAILED (STROBE)

POWER SUPPLY INOPERATIVE AND HAS NO OUTPUT.

Part: POWER SUPPLY — FAILED (STROBE)

POWER SUPPLY HAS NO OUTPUT.

Part: ALT ENCODER — FAILED (COCKPIT)

ENCODER HAS NO VALID OUTPUT.

Part: CYLINDER — LEAKING (M/R SERVO)

M/R SERVO LEAKING, CYLINDER SCORED.

Part: EXHAUST COLLECTO — CRACKED (ENGINE)

ENGINE REMOVED DUE TO NR3 & NR4 WHEEL CYCLES. UPON INSPECTION OF TURBINE PARTS NOTED: COATING FLAKING FROM EXHAUST COLLECTOR LAB SEAL FLANGE AND CRACKED BEYOND SERVICEABLE LIMITS. INSTALLED A STANDARD AERO OVERHAULED EXHAUST COLLECTOR.

Part: ACTUATOR — FAILED (M/R CONTROL)

ACTUATOR ARM DOES NOT EXTEND OR RETRACT.

Part: POWER SUPPLY — FAILED (STROBE)

STROBE DOES NOT FLASH.

Part: REGULATOR — FAILED (ENGINE)

GENERATOR DOES NOT COME ON LINE.

Part: FIN ASSY — MIS DRILLED (TAILBOOM)

FIN ASSY MIS-DRILLED HOLES.

Part: TRANSCEIVER — FAILED (COCKPIT ATC)

TRANSPONDER WILL NOT SQUAK IDENT 6033. PERFORMED PRELIMINARY INSPECTION. FOUND UNIT NOT RECEIVING AT ALL. REPLACED V101 CAVITY TUBE P/N C2080A. REPAIRED, ADJUSTED POWER OUT, PULSE WIDTH AND FREQUENCY. BENCH CHECK GOOD.

Part: RESTRAINT — BEARING UNSTAKED (XMSN)

TRANSMISSION RESTRAINT BEARINGS UNSTAKED.

Part: ENGINE — MALFUNCTION (POWER RPM)

PILOT REPORTED THAT AIRCRAFT YAWED IN CRUISE FLIGHT AND THE ROTOR RPM DROPPED AND RECOVERED TO 96 PERCENT. RETURNED TO OFFSHORE PLATFORM WITH 96 PERCENT ROTOR RPM. AFTER LANDING AND EXERCISING COLLECTIVE, THE ROTOR RPM RETURNED TO 100 PERCENT. MAINTENANCE C/W A PRESSURE AND VACUUM FUEL SYSTEM CHECK. COULD NOT FIND ANY PROBLEMS. REPLACED FUEL CONTROL, GOVERNOR, AND FUEL NOZZLE FOR PRECAUTION.

Part: LORAN — DEFECTIVE (COCKPIT)

SOME BUTTONS HAVE INTERMITTENT BACKLIGHTING.

Part: PUMP — DAMAGED (M/R GR BOX)

PUMP HOUSING DAMAGED AND SHAFT WORN IN SEAL AREA.

Part: SPLINE ADAPTER — STEPWEAR (COMPRESSOR)

ENGINE REMOVED DUE TO TURBINE CYCLED OUT #2 WHEEL AND CRACKED SCROLL. UPON INSPECTION OF COMPRESSOR PARTS NOTED THE FOLLOWING: STEP WEAR BEYOND SERVICEABLE LIMITS ON SPLINE ADAPTER INTERNAL SPLINES. REPLACED DISCREPANT PARTS.

Part: CARBON SEAL — WORN (COMPRESSOR)

ENGINE REMOVED DUE TO TURBINE CYCLED OUT #2 WHEEL AND CRACKED SCROLL. UPON INSPECTION OF COMPRESSOR PARTS NOTED THE FOLLOWING: WORN BEYOND SERVICEABLE LIMITS ON CARBON SEAL ASSY. TANGS AND TANG SLOTS. REPLACED DISCREPANT PARTS.

Part: GEARSHAFT — STEPWEAR (SPUR ADAPTER)

ENGINE REMOVED DUE TO TURBINE CYCLED OUT #2 WHEEL AND CRACKED SCROLL. UPON INSPECTION OF COMPRESSOR PARTS NOTED THE FOLLOWING: STEP WEAR BEYOND SERVICEABLE LIMITS ON SPUR ADAPTER GEARSHAFT FORWARD SPLINES. REPLACED DISCREPANT PARTS.

Part: INDICATOR — INOPERATIVE (DUAL TACH)

TURBINE NEEDLE INOPERATIVE AND PLUGS REVERSED.

Part: TRANSCEIVER — DEFECTIVE (COCKPIT VHF)

LOSES MEMORY; VHF RADIO DISPLAY FLICKERS. FREQUENCIES ARE NOT ALL ACCESSIBLE AND WILL NOT RECEIVE.

Part: TRANSCEIVER — INTERMITTENT (COCKPIT ATC)

INTERMITTENT INOPERATIVE. REPLACED CAVITY OSCILLATOR V101 DUE TO LOW POWER OUT. REPAIRED. REPLACED PHOTOCELL V301 DUE TO WEAK REPLY LIGHT. REPAIRED. ALIGNED RECEIVER. ADJUSTED FREQUENCY AND PULSE WIDTH. CLEANED CONTACTS ON ALL WAFER SWITCHES. BENCH CHECK GOOD.

Part: RESTRAINT — WORN (TRANSMISSION)

BEARINGS IN RESTRAINT WERE WORN AND THE BEARING ON R/H SIDE OF RESTRAINT WAS UNSTAKED.

Part: ELT — MALFUNCTION (COCKPIT)

TRIGGERED AND WOULD NOT RESET. TIME SINCE REPAIR 741:30.