N8045T

Part: WIRE — BROKEN (WARNING LIGHT) · airframe 14,995 hrs

IN FLIGHT, NR 2 FUEL VALVE CAUTION LIGHT ILLUMINATED. DEVIATED TO HOUMA AND NOTIFIED MAINTENANCE. MAINTENANCE FOUND BROKEN WIRE BEHIND INSTRUMENT PANEL APPROXIMATELY 8.

Part: HOSE — RUPTURED (HYD SYSTEM) · airframe 13,240 hrs

NR 1 HYDRAULIC SYSTEM FAILED IN FLIGHT. LANDED WITHOUT INCIDENT. MAINTENANCE FOUND A HOSE RUPTURED. REPLACED HOSE. ALSO REPLACED PUMP DUE TO RUNNING DRY.

Part: PACKING — LEAKING (HYD PUMP) · airframe 13,211 hrs

THE OIL COOLER WARNING LIGHT ILLUMINATED. RETURNED. FOUND A CUT PACKING ON FITTING ON UTILITY HYDRAULIC PUMP ALLOWING ALL FLUID TO LEAK OUT. REPLACED PACKING.

Part: COUPLING — CRACKED (HYD PUMP) · airframe 13,211 hrs

OIL COOLER CAUTION LIGHT ILLUMINATED IN FLIGHT. REPLACED CRACKED UNION ON THE UTILITY HYDRAULIC PUMP.

Part: BEARING — DAMAGED (MAIN ROTOR)

WHEN BEARING GREASED, BLACK GREASE COMES OUT.

Part: BATTERY — DISCHARGED (MASTER) · airframe 12,704 hrs

MASTER BATTERY DEAD.

Part: BATTERY — WEAK (MASTER) · airframe 12,684 hrs

BATTERY WEAK.

Part: BATTERY — WEAK (MASTER) · airframe 12,684 hrs

BATTERY WEAK.

Part: STARTER — MALFUNCTIONED (ENGINE) · airframe 12,684 hrs

STARTER KICKS OFF DURING START.

Part: BLOWER — INOPERATIVE (NR 2 ENGINE) · airframe 12,499 hrs

NR 2 ENGINE BLOWER OFF CAUTION LIGHT ILLUMINATED IN FLIGHT. TO BE SENT TO VENDOR FOR REPAIR.

Part: BATTERY — WEAK (MAIN) · airframe 12,544 hrs

BATTERY HAS WEAK VOLTAGE.

Part: BATTERY — WEAK (MAIN) · airframe 12,544 hrs

BATTERY HAS WEAK VOLTAGE.

Part: RELAY — FAILED (ELECTRICAL)

NR 2 BATTERY WILL NOT GO INTO SERIES.

Part: IGNITER — FAILED (ENGINE) · airframe 12,243 hrs

ENGINE HARD TO START. REPLACED IGNITERS.

Part: BATTERY — WEAK (MAIN)

MAIN BATTERY WEAK. BATTERY SCRAPPED AT VENDOR 1/17/03.

Part: BATTERY — WEAK (MAIN)

MAIN BATTERY WEAK. BATTERY SCRAPPED AT VENDOR 1/17/03.

Part: BATTERY — WEAK (MAIN)

MAIN BATTERY WEAK.

Part: BATTERY — WEAK (MAIN)

MAIN BATTERY WEAK.

Part: DISPLAY — FAILED (WX RADAR SYS) · airframe 12,159 hrs

WEATHER RADAR DISPLAY FAILED IN FLIGHT.

Part: COMPUTER — FAILED (WX RADAR SYSTEM) · airframe 12,159 hrs

WX RADAR COMPUTER FAILED IN FLIGHT.

Part: BEARING — WORN (MOUNT FITTING)

ENGINE MOUNT FITTING HAS WORN BEARINGS. REPLACED BEARING P/N VTB03500 AND P/N VTB03490 DUE TO WORN. REPAIRED.

Part: BEARING — WORN (MOUNT FITTING)

ENGINE MOUNT FITTING HAS WORN BEARINGS. REPLACED BEARING PN VTB03500 AND PN VTB03490 DUE TO WORN. REPAIRED.

Part: INDICATOR — WEAK (WX RADAR SYS) · airframe 12,107 hrs

WEATHER RADAR SYSTEM HAS WEAK AND SCRATCHY RECEPTION.

Part: SEAL — LOOSE (T/R HEAD)

TAIL ROTOR HEAD GREASE SEAL LOOSE. REPAIRED.

Part: HANGER ASSY — VIBRATION (TAIL ROTOR)

HANGER ASSY HAS VIBRATION - AVMS. REPAIRED. REPLACED BEARING DUE TO WORN AND BOLT DUE TO CORROSION.

Part: BATTERY — WEAK (MAIN)

MAIN BATTERY WEAK.

Part: COUNTERWEIGHT — WORN (TAIL ROTOR)

TAIL ROTOR COUNTERWEIGHT WORN. REPAIRED.

Part: HANGER ASSY — WORN (TAIL ROTOR)

HIGH IPS READING FROM AVMS. REPAIRED. REPLACED WORN BEARING.

Part: IDLER GEAR — WORN (MAIN ROTOR)

MAIN ROTOR HAS WORN BEARINGS. REPAIRED AND REPLACED BEARINGS.

Part: BATTERY — WEAK (MAIN)

MAIN BATTERY WEAK.

Part: BLOWER — DAMAGED (ENGINE) · airframe 12,026 hrs

BLOWER ASSY PARTICLE SEPERATOR LIGHT CAME ON. FOUND SHAFT SHEARED. TO BE SENT TO VENDOR FOR REPAIR.

Part: AMPLIFIER — INOPERATIVE (ADF SYSTEM)

ADF AMPLIFIER INOPERATIVE.

Part: BEARING — WORN (M/R SUPPORT)

MAIN ROTOR SUPPORT HAS WORN BEARINGS. REPAIRED.

Part: WIRE HARNESS — DAMAGED (ENGINE) · airframe 7,438 hrs

ENGINE YELLOW ELECTRICAL HARNESS PRODUCING MGT FLUCTUATION ON GAUGE IN COCKPIT. TO BE SENT TO VENDOR.

Part: TRANSCEIVER — MALFUNCTIONED (VHF SYSTEM) · airframe 11,306 hrs

VHF TRANSCEIVER UNRELIABLE, TRANSMIT LIGHT COMES ON WITH SQUELCH. ADJUSTED MIC GAIN AND SIDETONE. FOUND Q102, Q109 AND Q110 TRANSISTORS BAD AND Q110 SOCKET BAD DUE TO CORROSION. ALSO FOUND Q102, Q104 AND Q106 TRANSISTORS BAD. REPLACED. REPAIRED. BENCH CHECK GOOD.

Part: TRANSCEIVER — INTERMITTENT (VHF SYSTEM) · airframe 11,157 hrs

RECEIVES AND TRANSMITS INTERMITTENT. FOUND WHEN UNIT STOPPED RECEIVING THAT VCO VOLTAGE WAS FAR OUT OF SPECS. FOUND C/N SQUELCH HARD TO ADJUST TO SPECS AND RECEIVER HAS MOTORBOATING AND HIGH PITCH NOISE. ADJUSTED VCO AND ALIGNED RECEIVER SEVERAL TIMES. RESOLDERED COMPONENTS IN VCO SECTION AND RECEIVER WAS NO LONGER INTERMITTENT BUT STILL HAD MOTORBOATING AND HIGH PITCH NOISE AND HARD TO ADJUST C/N SQUELCH. REPLACED Q304, Q305, AND Q309 CAPACITOR. REPLACED C368 AND C372 CAPACITORS AND L310 COIL. REPLACED C370 CAPACITOR. REPAIRED. BENCH CHECK GOOD.

Part: CONTROL CABLE — BENT (ENG CONTROLS) · airframe 11,360 hrs

CABLE IMPOSSIBLE TO MOVE. FOUND THREADED PORTION OF CABLE TO BE BENT. REPLACED WITH SERVICEABLE CABLE.

Part: ACTUATOR — FAILED (AIRSTAIR STEP) · airframe 11,450 hrs

RT PASSENGER STEP WILL NOT STOW.

Part: BATTERY — WEAK (MAIN)

BATTERY WEAK.

Part: ACTUATOR — FAILED (AIRSTAIR STEP) · airframe 11,450 hrs

RT PASSENGER STEP WILL NOT STOW.

Part: BATTERY — WEAK (MAIN)

BATTERY WEAK.

Part: HANGER ASSY — DAMAGED (T/R DRIVESHAFT) · airframe 11,069 hrs

HIGH VIBRATION READING FROM RDA SYSTEM. REPLACED TAIL ROTOR DRIVESHAFT HANGER.

Part: INTERPHONE — DAMAGED (COCKPIT) · airframe 10,769 hrs

FACEPLATE WORN. FOUND SWITCHES S1, S4, S7, S8, S9, S10, S11, TRANSMIT KNOB, RESISTOR R36 AND LIGHT PANEL BAD. REPLACED. REPAIRED. BENCH CHECK GOOD.

Part: BLEED VALVE — INOPERATIVE (COMPRESSOR) · airframe 11,475 hrs

COMPRESSOR BLEED VALVE INOPERATIVE - VALVE WON'T OPEN.

Part: WIRE HARNESS — DAMAGED (ENG TEMP IND) · airframe 11,531 hrs

NR 2 ENGINE TEMPERATURE CONNECTOR ON GREEN HARNESS IS CAUSING THE ENGINE TEMPERATURE INDICATOR TO PEG OUT AT VARIOUS TIMES.

Part: SEAL — CRACKED (M/R DRIVESHAFT)

FOUND BOOTS CRACKED, CORRODED AND DAMAGED ON 250 HOUR COUPLING LUBE INSPECTION. REPLACED WITH SERVICEABLE PARTS.

Part: STARTER — MALFUNCTIONED (ENGINE) · airframe 10,751 hrs

STARTER WON'T STAY ENGAGED.

Part: COVER — MISSING (MLG FLOAT)

AFTER SHUTDOWN AT HELIPORT, FOUND AFT PORTION OF RIGHT HAND FLOAT COVER MISSING. REPLACED FLOAT COVER.

Part: BLOWER — FAILED (SHAFT) · airframe 11,034 hrs

THE #1 PARTICLE SEPARATOR CAUTION LIGHT CAME ON. MAINTENANCE FOUND PARTICLE SEPARATOR BLOWER SHAFT SHEARED.

Part: BATTERY — DISCHARGED (MAIN)

WEAK. WOULD NOT TAKE A CHARGE.

Part: BATTERY — DISCHARGED (MAIN)

WEAK.

Part: BATTERY — DISCHARGED (MAIN)

WEAK. WOULD NOT TAKE A CHARGE.

Part: BATTERY — DISCHARGED (MAIN)

WEAK.

Part: BATTERY — DISCHARGED (MAIN)

WEAK.

Part: BATTERY — DISCHARGED (BATTERY BAY) · airframe 10,720 hrs

BATTERY WEAK. WON'T HOLD A CHARGE.

Part: STARTER — FAILED (ENGINE) · airframe 10,751 hrs

FUNCTIONAL CHECKED GOOD AND FOUND STARTER WOULD NOT STAY ENGAGED. IT WOULD KICK OFF AFTER APPROX. 5 TO 6 SECONDS. SENDING TO VENDOR FOR REPAIR.

Part: BATTERY — DISCHARGED (BATTERY BAY) · airframe 10,720 hrs

BATTERY WEAK. WON'T HOLD A CHARGE.

Part: CLIP — BROKEN (M/R GEARBOX)

METAL IN OIL . BROKEN CLIP ON MAIN CASE CHIP PLUG. REPAIRED. REPLACED 2 EACH CLIPS.

Part: STARTER — FAILED (ENGINE)

STARTER SPINS, BUT WILL NOT ENGAGE ENGINE.

Part: INDICATOR — STICKING (COCKPIT)

TEMPERATURE NEEDLE STICKS AT 625 DEGREES PERIODICALLY.

Part: ACTUATOR — FAILED (FBW ELEVATOR)

BRAKE NOT RELEASING, WILL NOT TEST.

Part: ACTUATOR — FAILED (FBW ELEVATOR)

ELEVATOR SYSTEM WILL NOT MONITOR TEST.

Part: ACTUATOR — FAILED (FBW ELEVATOR)

ACTUATOR ASSY WOULD NOT MONITOR TEST. S

Part: ACTUATOR — FAILED (FBW ELEVATOR)

BRAKE NOT RELEASING TO PERMIT OTHER ACTUATOR TO TEST.

Part: AMPLIFIER — FAILED (FBW ELEVATOR)

WILL NOT DRIVE THE ACTUATORS.

Part: CONNECTOR — BROKEN (VS INDICATOR)

CANNON PLUG SOCKET BROKEN.

Part: REGULATOR — FAILED (DC SYSTEM)

VOLTAGE REGULATOR DROPS OFF-LINE DURING CROSS START.

Part: INDICATOR — ERRATIC (FUEL QUANTITY)

FUEL QUANTITY INDICATOR READING ERRATIC.

Part: ACTUATOR — FAILED (M/R CONTROL)

WILL NOT ALLOW THE ACTUATOR TO MONITOR TEST; BRAKE WOULD NOT RELEASE; LOUD GRINDING NOISE DURING OPERATION WAS HEARD FROM INTERNAL OF THE UNIT.

Part: RNAV — MALFUNCTIONED (COCKPIT)

PHOTOCELL CAUSES DISPLAY TO FLICKER. PERFORMED PRELIMINARY INSPECTION. FOUND DISPLAY TO BE BAD, REPAIRED, ALIGNED CONVERTER CARD, FOUND UNIT IS NOT TRANSMITTING O.B.I. DATA TO KTS-143. FOUND O.B.I. SYNC. LINE BAD.

Part: STARTER — MALFUNCTIONED (ENGINE)

STARTER KICKS OFF AROUND 5 SECONDS DURING FIRST START ATTEMPT.

Part: AMPLIFIER — MALFUNCTIONED (FBW ELEVATOR)

A/S 3 LIGHT DIM WHEN ELEVATOR IS TESTED.

Part: STARTER — INOPERATIVE (ENGINE)

STARTER INOPERATIVE.

Part: SHAFT — FAILED (T/R GEARBOX)

FAILURE IN THREAD AREA OF OUTPUT SHAFT. REPLACED WITH SERVICEABLE OUTPUT SHAFT.

Part: SOLENOID VALVE — MALFUNCITONED (VACUUM SYSTEM)

SOLENOID VALVE ACTIVATED AND PREMATURELY INFLATED FLOATS.

Part: TRANSCEIVER — MALFUNCTIONED (COCKPIT)

DME DISPLAYS DASHES.

Part: COMPUTER — FAILED (AIR DATA)

COMPUTER SHOWS FAIL 5.

Part: STARTER — FAILED (START/GENERATOR)

STARTER KICKED OFF LINE AT 10 PERCENT NG.

Part: PUMP — DAMAGED (ENGINE FUEL)

BOLT HOLES TOO LARGE FOR REQUIRED BOLTS.

Part: CONTROL UNIT — MALFUNCTIONED (COCKPIT)

CONTROL UNIT NOT CHANNELING CORRECTLY AND DISPLAY HAD HOT SPOTS.

Part: GYRO — FAILED (COCKPIT)

COPILOT'S HSI WOULD NOT SLAVE. TIME SINCE REPAIR 101:25 HOURS.

Part: PROBE — FAILED TEST (FUEL QUANTITY)

PROBE DID NOT PASS CALIBRATION CHECK PER M&O.

Part: FITTING — BROKEN (STATIC SYSTEM)

STATIC SYSTEM FITTING BROKE UNDER PRESSURE DURING TEST (NEEDLE NOT ZERO).

Part: CAUTION PANEL — MALFUNCTIONED (COCKPIT)

90 DEGREE CHIP AND NR 2 FUEL TRANSFER LIGHTS INOPERATIVE.

Part: GEARBOX — CORRODED (COMBINING)

EXCESSIVE CORROSION AND WEAR BENEATH P/N 214-040-160-105 TRIPOD ENGINE MOUNT AND P/N 214-040-151-103 BIPOD ENGINE MOUNT (BEYOND ALLOWABLE LIMITS) CASE ASSY P/N 214-040-991-109, S/N A518, T.T. UNK T.S.O. 283:00 HOURS.

Part: STARTER — MALFUNCTIONED (ENGINE)

STARTER SWITCH DID NOT DISENGAGE AND START ENGINE ENGAGE LIGHT STAYED ILLUMINATED.

Part: CONTROL UNIT — DAMAGED (E/E BAY)

CVR CONTROL HAS TRANSISTOR LOOSE INSIDE UNIT.

Part: CHARGER — MALFUNCTIONED (BATTERY BAY)

BATTERY CHARGER WILL NOT TOP CHARGE BATTERY.

Part: CAUTION PANEL — DAMAGED (COCKPIT)

BAGGAGE AND BRAKE SEGMENTS DAMAGED ON CAUTION PANEL.

Part: INDICATOR — MALFUNCTIONED (COCKPIT)

INDICATOR GOES INTO WAIT MODE AFTER ONE HOUR OF USE.

Part: ACTUATOR — INOPERATIVE (YAW CHANNEL)

ACTUATOR ASSY INOPERATIVE.

Part: FLOAT — LEAKING (AFT)

AFT FLOAT LEAKING AT SEAMS.

Part: REGULATOR — INOP (AC SYSTEM)

VOLTAGE REGULATOR INOPERATIVE.

Part: CHARGER — MALFUNCTIONED (E/E BAY)

BATTERY CHARGER WILL NOT TOP CHARGE BATTERY.

Part: AMPLIFIER — MALFUNCTIONED (AUTOFLIGHT)

COULD NOT ADJUST ROLL CHANNEL TO PROPER VOLTAGE, PITCH WILL NOT ENGAGE.

Part: PUMP — FLUCTUATING (HYDRAULIC SYS)

HYDRAULIC PUMP FLUCTUATING PRESSURE WITH CONTROL MOVEMENT.

Part: INDICATOR — PRECESSING (COCKPIT)

ATTITUDE INDICATOR PRECESSES AND IS SLOW TO ERECT.

Part: CONVERTER — INOPERATIVE (WIPER MOTOR)

CONVERTER INOPERATIVE.

Part: RELAY — FAILED (DC SYSTEM)

RELAY WILL NOT ENGAGE.

Part: STARTER — FAILED (START/GEN)

STARTER WILL NOT MOTOR OR ENGAGE.

Part: INVERTER — INOPERATIVE (AC SYSTEM)

INVERTER INOPERATIVE.

Part: CHIP DETECTOR — LEAKING (ENGINE)

LEAKS FROM ELECTRIC POST, CRIMPED TO DETECTOR BODY.

Part: FUEL CONTROL — DAMAGED (ENGINE)

FUEL CONTROL ASSEMBLY HAS FLAT SPOTS NEAR CUT OFF.

Part: SIGHT GLASS — BROKEN (HYDRAULIC SYS)

GLASS BROKEN ON SIGHT GLASS.

Part: VALVE — FAILED (FUEL SYSTEM)

VALVE DOES NOT OPEN.

Part: POWER SUPPLY — DISCHARGED (CABIN)

POWER SUPPLY WILL NOT HOLD CHARGE.

Part: FUEL CONTROL — WORN (ENGINE)

FUEL CONTROL WORN.

Part: PLATE ASSY — WORN (M/R TRANSMISSION)

TRANSMISSION PLATE ASSEMBLY HAS WORN RUBBER.

Part: PLATE ASSY — WORN (M/R TRANSMISSION)

TRANSMISSION PLATE ASSEMBLY HAS WORN RUBBER.

Part: ACTUATOR — INOPERATIVE (MAIN ROTOR)

ACTUATOR WILL NOT ROTATE.

Part: TRANSDUCER — FAILED (AIRSPEED)

TRANSDUCER FAILED 5 ON ADC.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

POWER SUPPLY FAILED 5 CODES, INOPERATIVE.

Part: STARTER — FAILED (START/GEN)

STARTER KICKS OUT IN START, INTERMITTENT WILL NOT MOTOR.

Part: INDICATOR — STICKING (COCKPIT)

FUEL QUANTITY INDICATOR'S RIGHT NEEDLE STICKS.

Part: ACTUATOR — FAILED (MAIN ROTOR)

ACTUATOR WILL NOT MONITOR TEST AND WILL NOT WORK WITH OTHER ACTUATORS.

Part: TRANSPONDER — FAILED (AIRSPEED)

AIRSPEED TRANSPONDER CAUSING FAIL 5 CODE.

Part: POWER SUPPLY — INOPERATIVE (STROBE)

STROBE LIGHT INOPERATIVE.

Part: STRAP ASSY — UNBONDED (MLG)

RUBBER IS UNBONDED ON STRAP ASSY.

Part: INDICATOR — FAILED (COCKPIT)

RPM INDICATOR FAILED IN FLIGHT.

Part: INDICATOR — INOPERATIVE (TRIPLE TACH)

TRIPLE TACHOMETER'S NR 1 NEEDLE IS INOPERATIVE.

Part: SENSOR DUALRATE — MALFUNCTIONED (SCAS SYSTEM)

SCAS SENSOR ROLL WILL NOT STAY ON LINE.

Part: CONNECTOR — BROKEN (TRANSMITTER)

CONNECTOR BROKEN.

Part: PUMP — MAKING METAL (HYDRAULC SYS)

HYDRAULIC PUMP MAKING METAL.

Part: SPINDLE — CRACKED (M/R)

EAR CRACKED IN MOUNT AREA APPROX. 2 INCHES ON BOTH SIDES, ON LOWER SIDE OF TRAILING EDGE OF WHITE BLADE. SCRAPPED PART.

Part: STARTER — FAILED (ENGINE)

DURING 250 HOUR INSPECTION FOUND CLUTCH FAILED TORQUE SLIPPAGE TEST WAS AT 250 IN. LBS. AND END PLAY WAS AT .014 LIMITS ARE .004-.010.

Part: SPINDLE — CRACKED (M/R HUB)

THE MAIN ROTOR SPINDLE WAS CRACKED AT THE TRAILING EDGE TANGS. BOTH LOWER AND UPPER TANGS WERE CRACKED. THE CRACK WAS DETECTED DURING A DAILY VISUAL INSPECTION BY A COMPANY TECHNICIAN. SUBMITTER STATED FAILURE OF THIS SPINDLE WOULD HAVE CERTAINLY LED TO A CATASTROPHIC ACCIDENT.

Part: SHAFT ASSY — CORRODED (T/R)

EXCESSIVE CORROSION. SCRAPPED LOCALLY.

Part: SHAFT ASSY — CORRODED (T/R)

EXCESSIVE CORROSION. SCRAPPED LOCALLY.

Part: SHAFT ASSY — CORRODED (T/R)

EXCESSIVE CORROSION. SCRAPPED LOCALLY.

Part: SHAFT ASSY — CORRODED (T/R)

EXCESSIVE CORROSION. SCRAPPED LOCALLY.

Part: SWASHPLATE — LOOSE (M/R)

SWASHPLATE LOWER HUB NUT FOUND UNDER TORQUE.

Part: CLOCK — FAILED (COCKPIT)

CLOCK INOPERATIVE.

Part: CIRCUIT BREAKER — FAILED (DC SYS)

CIRCUIT BREAKER INOPERATIVE.

Part: CIRCUIT BREAKER — FAILED (DC SYS)

CHARGES MOTION OUTPUT NOT CHARGING BATTERY.

Part: ACTUATOR ASSY — FAILED (M/R)

ACTUATOR INOPERATIVE.

Part: CONTROL UNIT — FAILED (WINDSHIELD)

WINDSHIELD HEAT INOPERATIVE; DOES NOT COME ON.

Part: INDICATOR — FAILED (COCKPIT)

ATTITUDE INDICATOR INOPERATIVE.

Part: RELAY — FAILED (DC SYS)

CONTACT BALL NR2 TO 24V OPEN IN REST POSITION.

Part: BLOWER — FAILED (AIR DIST)

BLOWER POPS CIRCUIT BREAKER.

Part: CHARGER — FAILED (BATTERY)

CHARGER INOPERATIVE. BATTERY NEVER SHOWS TOP CHARGE.

Part: ACTUATOR — FAILED (M/R)

ACTUATOR MOTOR WEAK.

Part: CIRCUIT BREAKER — OPEN (ELECT SYS)

RELAY IS STUCK OPEN.

Part: POWER SUPPLY — FAILED (LIGHTS)

POWER SUPPLY UPPER AND LOWER LIGHT WILL NOT ILLUMINATE.

Part: RELAY — FAILED (BATTERY SYS)

CAUSING VOLTAGE TO DROP DURING ENGINE START.

Part: BATTERY CHARGER — MALFUNCTION (DC SYS)

BATTERY SWITCH LIGHT REMAINS ON.

Part: RELAY — FAILED (DC SYS)

BATTERY VOLTAGE DROPS DURING START.

Part: CONTROL — FAILED (NAV UNIT)

DISPLAY IS NOT CHANNELING CORRECTLY. PERFORMED PRELIMINARY INSPECTION. FOUND PHOTOCELL LENS MISSING. INSTALLED PHOTOCELL LENS P/N 088-0548-00. REPAIRED. BENCH CHECK GOOD.

Part: STARTER — FAILED (ENGINE)

ENGINE WILL NOT BATTERY START DUE TO HIGH VOLTAGE DRAW.

Part: LIFE RAFT — MIS MFG (ACFT ROOF)

RUNNERS ON LIFE RAFT ASSEMBLY DO NOT LINE UP WITH RAISED CHANNELS ON AIRCRAFT ROOF. UNABLE TO INSTALL RAFT ASSEMBLY.

Part: STARTER — FAILED (ENGINE)

STARTED WILL NOT TURN. INSPECTED BY ACCESSORY OVERHAUL SHOP AND FOUND ARMATURE WAS FROZEN AND WOULD NOT TURN.

Part: CHARGER — FAILED (BATTERY)

BATTERY WILL NOT STAY CHARGED.

Part: CLEVIS ARM ASSY — SEPARATED (M/R XMSN)

CLEVIS ARM ASSY RUBBER SEPARATED.

Part: RELAY — FAILED (DC SYS)

FORWARD START ARM RELAYS WOULD NOT ENERGIZE.

Part: PRESSURE SWITCH — FAILED (ENGINE)

SWITCH INOPERATIVE.

Part: CHARGER — FAILED (BATTERY)

CHARGER WILL NOT CHARGE BATTERY PROPERLY.

Part: WINDOW — FAILED (COPILOT UPPER)

INBOUND TO SHORE BASE, COPILOT'S UPPER 'GREENHOUSE' WINDOW BROKE AND A PORTION OF IT DEPARTED AIRCRAFT. NO PREVIOUS DEFECTS OR REPAIRS PRIOR TO INCIDENT. MAINTENANCE REPLACED WINDOW ASSEMBLY. REF: 214ST IPC, CHAPTER 52-99-00, FIGURE 52-2, ITEM NR 9.

Part: CHARGER — FAILED (BATTERY)

BATTERY CHARGER WILL NOT TOP CHARGE.

Part: STARTER — FAILED (ENGINE)

STARTER WORN BRUSHES AND CLUTCH HOUSING IS CRACKED.

Part: CHARGER — DEFECTIVE (BATT/ CHARGE SYS)

CHARGER NOT TOP CHARGING BATTERY.

Part: PUMP — FAILED (HYDRAULIC SYS)

LOSS OF UTILITY HYD SYSTEM PRESSURE IN-FLIGHT, PUMP FAILED.

Part: GYROSCOPE — FAULTY (COCKPIT)

GYRO SLOW AND ERECT.

Part: REGULATOR — FAILED (DC SYS)

GENERATOR GOES OFF LINE.

Part: TORSION ARM ASSY — FAILURE (M/R XMSN)

BEARINGS TORN AND SPLIT UNDER TWO PLATES.

Part: AMPLIFIER ASSY — FAILED (AUTO FLIGHT)

AUTO PILOT AMP WILL NOT ENGAGE, MONITOR TEST OR ALIGN.

Part: PRESSURE SWITCH — FAILED (ENG SYS)

WARNING LIGHT WILL NOT COME ON RIGHT AWAY AFTER ENGINE SHUTDOWN.

Part: IGNITOR — WORN (ENGINE)

IGNOTOR WORN, INSULATOR BROKEN.

Part: RELAY — FAILED (DC SYS)

CONTACTS BURNT.

Part: OIL TEMP — FLUCTUATES (GR BOX)

GR BOX OIL TEMP FLUCTUATES 70 DEGREES C AT MID RANGE.

Part: CONTROL UNIT — DEFECTIVE (DC SYS)

DC CONTROL UNIT DEFECTIVE. GENERATOR WOULD NOT COME ON LINE. TIME SINCE REPAIR 19:55.

Part: CHARGER — MALFUNCTION (BATTERY)

BATTERY WILL NOT TOP CHARGE.

Part: STARTER — FAILED (ENGINE)

LOSES RPM DURING START THAN HANGS AT 38%. DUE 250 HOUR INSPECTION.

Part: STARTER — MALFUNCTION (NR 1 ENG)

#1 ENGINE SLOW TO START.

Part: INDICATOR — DEFECTIVE (ALTIMETER)

ALTIMETER HAS EXCESSIVE LEAKING AND INDICATES 300 FEET HIGH ON ENCODER.

Part: INDICATOR — READS LOW (COCKPIT)

INDICATES LOW OUT OF TOLERANCE THROUGHOUT SCALE AND NEEDLE FLUCTUATES.

Part: STARTER — FAILED (START/GEN)

STARTER ARMATURE INSULATION CAME OFF.

Part: SWASHPLATE — WORN (M/R)

WORN SLIDER SLEEVE BEARING BORE. ROBBED SUPPORT ASSY FROM THIS SWASHPLATE TO REPAIR SWASHPLATE S/N A467.

Part: SWASHPLATE — BEARING ROUGH (M/R)

THRUST BEARING FOUND ROUGH ON ROTATION; COULD NOT ACHIEVE BREAK-AWAY DUE TO SPHERICAL BEARINGS WORN AND THEN WEARING THE INNER RING BORE WHERE THE SPHERICAL BEARINGS SEAT. THE SUPPORT ASSY WAS ROBBED FROM ASSY TO REPAIR S/N A29, T.T. 3536:20 WHICHHAD A WORN SLIDER SLEEVE BEARING BORE AND WAS TRANSFERRED TO THIS UNIT TO FACILITATE COMPLETING A UNIT

Part: GENERATOR — FAILED (START/GEN)

GENERATOR WILL NOT COME ON LINE.

Part: BEARING — FAILED (SWASHPLATE)

BEARING REMOVED WITH SWASHPLATE ASSEMBLY. SCRAPPED BEARING AT PHI.

Part: SEAL — LEAKING (XMSN)

LEAKING (SEALING LIP LOOKS UNFINISHED) REPLACED WITH NEW SEAL. (BHT TOTAL SUPPORT AIRCRAFT) PARTS AND LABOR WILL BE INVOICED ON WO#9760784.

Part: TRUNNION — BRINELLED (T/R)

T/R TRUNNION BRINELLING.

Part: NUT — WORN (T/R)

T/R WORN.

Part: HOUSING ASSY — COAT MISSING (T/R)

T/R HOUSING BLUE COAT MISSING.

Part: BEARING — WORN (FEATHER)

FEATHER BEARING WORN EXCESSIVELY.

Part: CONTROL — DEFECTIVE (COCKPIT ADF)

ADF CONTROL DISPLAY DIM. PERFORMED PRELIMINARY INSPECTION. FOUND V301 PHOTOCELL BAD. ALSO FOUND SWITCH S305 BAD. REPLACED V301 PHOTOCELL, AND S305 SWITCH. REPAIRED. ALSO REPLACED BROKEN PHOTOCELL LENS P/N 088-0548-00. REPAIRED. BENCH CHECK GOOD.

Part: AMPLIFIER ASSY — FAILED (AUTO FLIGHT)

WILL NOT ENGAGE IN ROLL CHANNEL.

Part: TRIPOD ASSY — BROKE (ENG MT)

TUBE BROKE IN HALF DUE TO RUSTING FROM INSIDE OF TUBE. TUBE BROKE AT END OF BEARING.

Part: HUB — BRINNELED (T/R)

REPLACED THE FOLLOWING PARTS OF T/R HUB ASSEMBLY: 4 EACH, BEARING P/N 214-011-819-101, WORN EXCESSIVELY 1 EACH, TRUNNION P/N 214-011-804-101, BRINELLING. 2 EACH, BEARINGS P/N 214-011-803-101, BRINELLING (SCRAPPED LOCALLY) 2 EACH,SEALS P/N 92-7521, WORN (SCRAPPED LOCALLY) 2 EACH, NUTS P/N MS14145L5, WORN 2 EACH, HOUSINGS P/N 214-011-813-101, BLUE COAT MISSING 2 EACH, THRUST PLUGS P/N 214-011-806-101, WORN (SCRAPPED LOCALLY) PARTS HELD AT PHI FOR CSR SIGNATURE. PARTS AND LABOR WILL BE INVOICED ON PM# 1214.

Part: P500 INDICATOR — MALFUNCTION (RADAR)

RADAR INDICATOR FLASHES "ANTENNA".

Part: RATE GYRO — MALFUNCTION (COCKPIT)

TURN NEEDLE ONLY SHOWS 1/2 STANDARD RATE OF TURN DURING STANDARD RATE TURN.

Part: ACTUATOR — MIS ADJUSTED (M/R)

ACTUATOR STROKE APPEARS TO BE TOO LONG. INTERNAL STOP MAY BE OUT OF ADJUSTMENT.

Part: TRANSCEIVER — MALFUNCTION (COCKPIT)

DOES NOT ALLOW KCU951 CONTROL HEAD TO DISPLAY FREQUENCIES.

Part: SEAL — WORN (ENG/XMSN)

SEAL WORN. REPLACED WITH SERVICEABLE SEAL.

Part: GENERATOR — FAILED (START/GEN)

GENERATOR FAILED AND COULD NOT RESET.

Part: RECEIVER — MALFUNCTION (COCKPIT)

VOR UNIT 25 KHZ CHANNELING NOT WORKING.

Part: SENSOR — MALFUNCTION (M/R)

TORQUE OSCILLATION.

Part: ECU — MALFUNCTION (ENGINE)

ENGINE SURGES DURING POWER TRANSIENTS.

Part: PIN — DEFECTIVE (M/R)

HIGH TIME. REPLACED WITH SERVICEABLE PART. SEE MMIR# HEEA0008821 THROUGH HEEA0008826 FOR ALL PARTS REPLACED.

Part: SUPPORT ASSY — CORRODED (M/R)

SUPPORT ASSY CORRODED. SEE MMIR# HEEA0008821 THROUGH HEEA0008826 FOR ALL PARTS REPLACED.

Part: BEARING — DEFECTIVE (M/R)

TEFLON COAT MISSING ON INNER RACES. SERIAL NUMBERS REMOVED ARE ZN83794, ZN83795, ZN72048, ZN83796. SENT TO BELL HELICOPTER TEXTRON...POWER BY HOUR AIRCRAFT. PARTS AND LABOR WILL BE INVOICED...PM#0596. SEE MMIR# HEEA0008821 THROUGH HEEA0008826 FOR ALL PARTS REPLACED.

Part: YOKE — DEFECTIVE (M/R)

HIGH TIME. REPLACED WITH SERVICEABLE PART. SEE MMIR# HEEA0008821 THROUGH HEEA0008826 FOR ALL PARTS REPLACED.

Part: FITTING — DEFECTIVE

HIGH TIME. REPLACED WITH SERVICEABLE PART. SEE MMIR# HEEA0008821 THROUGH HEEA0008826 FOR ALL PARTS REPLACED.

Part: GRIP — CORRODED (M/R)

CORROSION ON GRIP TANGS. SEE MMIR# HEEA0008821 THROUG HEEA0008826 FOR ALL PARTS REPLACED. S/N A821 & A835

Part: BLADE — SKIN VOID (M/R)

SKIN VOID ON UPPER AND LOWER SURFACES NEAR BLADE STATION 43.5" APPROXIMATELY 2.5" FROM TRAILING EDGE. EACH VOID IS APPROXIMATELY 4" IN DIAMETER.

Part: ACTUATOR ASSY — FROZEN (M/R)

ACTUATOR FROZEN IN PLACE.

Part: ACTUATOR ASSY — DEFECTIVE (M/R)

KICKS OFF LINE AT 100-120 KNOTS.

Part: SWASHPLATE ASSY — OVERSPEED (M/R)

SWASHPLATE OVERSPEED INSPECTION. OVERSPEED TO 112%. (2500 HOUR OVERHAUL DUE)

Part: CONTROL — DEFECTIVE (COCKPIT ATC)

TRANSPONDER INOPERATIVE. PERFORMED PRELIMINARY INSPECTION, FOUND DIODES CR204 & CR205 SHORTED. ALSO FOUND C214 CAPACITOR BAD. REPLACED CR204, CR205, C214. REPAIRED. ALSO REPLACED PHOTOCELL V101 AND PHOTOCELL LENS P/N 088-00548-0000 AND RETAINING RING P/N 090-0036-04.REPAIRED. BENCH CHECK GOOD.

Part: INDICATOR — FAILED (COCKPIT)

INDICATOR INTERMITTENTLY RATCHETS RIGHT 360 DEGREES IN ROLL AXIS AFTER ABOUT AN HOUR OF OPERATION.

Part: PUMP — METAL CONTAM (HYD)

HYD PUMP METAL CONTAMINATION.

Part: MOTOR — SEAL LEAK (BLOWER)

BLOWER MOTOR SHAFT SEAL LEAKING.

Part: AFCS — FAILED (COCKPIT)

ALTITUDE HOLD LIGHT INOPERATIVE.

Part: TRANSCEIVER — DEFECTIVE (COCKPIT)

REMOVED SERVICEABLE. PERFORMED INSPECTION, CLEANED CORROSION FROM UNIT. FOUND RECEIVER SENSITIVITY WEAK IN AM MODE. SENT TO ALLIED SIGNAL AVIONICS FOR INSPECTION AND REPAIR.

Part: SEAL — LEAK (M/R)

I.B. SEAL LEAKING DUE TO DETERIORATION. ONE EACH O.B. SEAL SHOWING MINOR LEAK. REPLACED ALL SEALS AS A SET. PARTS SCRAPPED LOCALLY.

Part: SEAL — LEAK (M/R)

I.B. SEAL LEAKING DUE TO DETERIORATION. ONE EACH O.B. SEAL SHOWING MINOR LEAK. REPLACED ALL SEALS AS A SET. PARTS SCRAPPED LOCALLY.

Part: ANTENNA — DEFECTIVE (LORAN)

LORAN SHOWS NO SIGNAL FROM THIS ANTENNA.

Part: VALVE — LEAKING (FLOAT)

FLOAT VALVE SUSPECT LEAKING.

Part: COMPUTER — INOPERATIVE (AIR DATA)

AIR DATA COMPUTER INOPERATIVE. PART IS BURNT. TIME SINCE REPAIR 15:45.

Part: COMPUTER — INOPERATIVE (COCKPIT)

AIR DATA COMPUTER INOPERATIVE.

Part: RECEIVER — FAILED (COCKPIT ADF)

DOES NOT WORK. REPLACED HEADERS J302, J306, J307 AND APPLIED HUMISEAL TO HEADERS FOR CORROSION CONTROL. REPLACED CRACKED RESISTOR R339 AND CRACKED SPACER FOR BNC. REPLACED BROKEN HEX NUT ON POWER SUPPLY AND INSTALLED MISSING WASHER, NUT AND SPACER. TESTED.BENCH CHECK GOOD.

Part: FUEL CONTR — DEFECTIVE (NR 1 ENG)

#1 ENGINE SURGES. SENT FUEL CONTROL FOR INSPECTION AND REPAIR.

Part: POWER SUPPLY — INOPERATIVE (STROBE)

POWER SUPPLY INOPERATIVE.

Part: POWER SUPPLY — FAILED (LIGHT)

POWER SUPPLY WILL NOT WORK. POPS CIRCUIT BREAKER TIME SINCE REPAIR 39:55.

Part: TRANSCEIVER — FAILED (COCKPIT VHF)

WILL NOT TUNE AND DRAWS EXCESSIVE CURRENT WHEN KEYED. SENT TO ALLIED SIGNAL AVIONICS FOR INSPECTION AND REPAIR.

Part: ACTUATOR ASSY — DEFECTIVE (M/R)

MONITOR TEST MALFUNCTION MOTOR OR MAG BREAK DRAGGING.

Part: ACTUATOR ASSY — DEFECTIVE (M/R)

PISTON HARD TO MOVE WITH BRAKE UNLOCKED. IN MONITOR TEST, PISTON EXTENDS PARTIALLY.

Part: TRANSPONDER — INOPERATIVE (COCKPIT)

TRANSPONDER INOPERATIVE WILL NOT COME ON LINE.

Part: CONTROL — DEFECTIVE (XPONDER)

XPONDER IDENT SWITCH STICKING IN IDENT POSITION.

Part: AMPLIFIER ASSY — FAULTY (AUTO FLIGHT)

ROLL CHANNEL WILLNOT ENGAGE WHEN AMP IS COLD OR HIGH HUMIDITY.

Part: LIFE RAFT — WONT INSTALL (EMERG EQUIP)

COULD NOT INSTALL RAFT. MEASURED OLD RAFT AT APPROX. 9 1/2" AND NEW RAFT MEASURED APPROX. 10 1/2".

Part: POWER SUPPLY — DEFECTIVE (STROBE)

STROBE HAS SLOW FLASH RATE (4 PER MINUTE)

Part: AMPLR ASSY — DEFECTIVE (AUTO FLIGHT)

WILL NOT MONITOR TEST. WILL NOT MOVE ACTUATOR.

Part: GYROSCOPE — FAULTY (COCKPIT)

GYRO WOULD NOT PUT OUT SIGNAL FOR ROLL CHANNEL TO THE AARS AMP.

Part: AMPLIFIER ASSY — DEFECTIVE (AUTO FLIGHT)

ROLL NETWORK VOLTAGES ARE ERRATIC. TIME SINCE REPAIR 470:50.

Part: STARTER — DEFECTIVE (ENGINE)

STARTER DRAGGING. KICKS GENERATOR OFF LINE. COMMUTATOR PITTED.

Part: ACTUATOR ASSY — DEFECTIVE (SAS YAW)

SAS YAW CHANNEL WOULD NOT COME ON LINE UNTIL ACTUATOR LOCK WAS PUSHED INTO OPEN POSITION. WITH ACTUATOR INSTALLED IN AIRCRAFT, LOCK SOLENOID WOULD NOT OPEN LOCK WITHOUT BEING PUSHED. LOCK WOULD STAY OPEN ONCE IT WAS PUSHED THERE.

Part: FLOAT — TORN (FWD LT)

FLOAT UNIT TORN. SENT TO A/C FUEL CELLS FOR GIRT PATTERN FOR P/N 214-052-200-102

Part: FLOAT VALVE — LEAKING (FITTING)

FLOAT VALVE LEAKING OUT OF OUTPORT FITTING AFTER MANUAL INFLATION. S/N 1 &S/N 9

Part: CONTROL SWITCH — DEFECTIVE (COCKPIT NAV)

STANDBY SWITCH HAS NO SPRING TENSION. INSTALLED SWITCH S102. REPAIRED PROBLEM. ALSO INSTALLED HEADER P201. UNIT BENCH CHECK GOOD.

Part: HUB — WONT BALANCE (T/R)

INSPECT AND REPAIR DUE TO UNABLE TO BALANCE.

Part: TRANSCIEVER — LOW POWER (COCKPIT VHF)

TRANSCEIVER LOW OUTPUT POWER. REPLACED TRANSISTORS Q109 AND 110. REPAIRED. INSTALLED MOD 2. REPLACED HEADER J304 AND APPLIED HUMISEAL TO HEADER. REPLACED TRANSMIT HEATSINK DUE TO SCREW BEING BROKEN IN HOLE. FOUND FREQUENCY UNABLE TO ADJUST TO SPECS. REPLACED CRYSTAL Y101.REPAIRED. ADJUSTED C/SQUELCH AND SIDETONE. BENCH CHECK GOOD.

Part: BRACKET — MIS MACHINED (STEP ACTUATOR)

BRACKET IS NOT MACHINED PROPERLY. UNABLE TO INSTALL BEARING BETWEEN BRACKET AS REQUIRED.

Part: BEARING — WORN (T/R FEATHER)

ONE EACH BEARING UNSTAKED IN HUB AND THREE EACH BEARINGS WORN. REPLACED BEARINGS.

Part: FLOAT — INFLATED (SKID)

DURING CRUISE FLIGHT, FLOATS INFLATED. PILOT LANDED ON OFFSHORE PLATFORM WITHOUT INCIDENT. INCIDENT STILL UNDER INVESTIGATION.

Part: FLOAT — INFLATED (EMERGENCY EQUIP)

WHILE IN CRUISE FLIGHT OVER THE GULF OF MEXICO, ACFT EXPERIENCED UNCOMMANDED INFLATION OF EMERGENCY FLOATS. FLIGHT CREW DIVERTED ACFT TO THE NEAREST OFFSHORE HELIPORT AND MADE A SUCCESSFUL LANDING. MAXIMUM ALLOWABLE AIRSPEED FOR FLOAT INFLATION IS 35 KNOTS. AT THE TIME OF INFLATION, ACFT WAS INDICATING APPROX 120 KNOTS. PILOT STATED THEY EXPERIENCED A SLIGHT BUFFETING BEFORE ACFT WAS SLOWED DOWN. PILOT ALSO STATED THE FLOAT SYSTEM WAS NOT ARMED AT THE TIME OF INFLATION. THE CAUSE OF THE UNCOMMANDED IN-FLIGHT INFLATION IS STILL UNDER INVESTIGATION. INFLATION VALVES WERE SENT TO VALVE MFG FOR FURTHER EVALUATION.

Part: FLOAT — INFLATED (EMERGENCY EQUIP)

AIRCRAFT EXPERINCED AN UNCOMMANDED EMERGENCY FLOAT INFLATION WHILE AIRCRAFT WAS ON THE GROUND AND UNATTENDED. THE INFLATION WAS INVESTIGATED BY THE OPERATOR AND A REPRESENTATIVE FROM BELL HELICOPTER. THE MANUFACTURER ATTRIBUTED THE STATIC INFLATION TO DEBRIS FOUND IN THE FLOAT INFLATION VALVES. THE VALVES (BELL PN 214-073-929-105) WERE THE IMPROVED VALVES INSTALLED IAW BELL TB 214ST-95-149.

Part: COMM CONTROL — DEFECTIVE (SBY SWITCH)

"SBY" SWITCH HAS NO SPRING TENSION. REPLACED COMM CONTROL TRANSFER SWITCH S102. REPAIRED. REPLACED HEADER P201 AND APPLIED HUMISEAL TO HEADER FOR CORROSION CONTROL. REPLACED LENS. BENCH CHECK GOOD.

Part: RNAV — INOPERATIVE (COCKPIT GS)

GLIDESLOPE INOPERATIVE. SENT TO THE RADIO SHOP FOR INSPECTION AND REPAIR.

Part: TRANSCEIVER — INOPERATIVE (COCKPIT)

HF INOPERATIVE. WILL NOT TUNE.

Part: TRANSCEIVER — INOPERATIVE (COCKPIT DME)

INOPERATIVE; WON'T COME ON LINE.

Part: SENSOR — FAILED (ENG TORQUE)

NO TORQUE INDICATION.

Part: STARTER — FAILED (START/GEN)

STARTER DROPS OUT AT 10%.

Part: HOSE — LEAKS (ENG SYS)

HOSE LEAKS AT B-NUT FACING.

Part: NOZZLE — DEFECTIVE (ENG FUEL)

FUEL NOZZLE DEFECTIVE. EXCESSIVE DROOLING AND SPITTING. SERIAL NUMBERS REMOVED PKHC4238 & PANO0613 & PKHA8102.

Part: IGNITOR — ERRODED (ENGINE)

TWO EACH IGNITOR PLUGS ERRODED.

Part: VALVE — CORROSION (ENGINE AI)

ANTI ICE VALVE CORROSION.

Part: TRANSDUCER — DEFECTIVE (AUTO FLIGHT)

BODY OF TRANSDUCER BROKEN. PART RECEIVED INSTALLED ON AIRCRAFT.

Part: FITTING — WORN (ENG MOUNT)

#2 ENGINE AFT ENGINE MOUNT BEARING WORN.

Part: CONNECTOR PLATE — DEFECTIVE (ATT INDICATOR)

NOT EQUIPPED WITH A STANDBY ATTITUDE INDICATOR ON/OFF/TEST SWITCH.

Part: BEARING — COVER MISSING (M/R)

DUST COVERS MISSING.

Part: FITTING — WORN (ENG MOUNT)

#1 ENGINE AFT ENGINE MOUNT BEARING WORN.

Part: PANEL — MALFUNCTION (LIGHTING)

INTERNAL LIGHTING INOPERATIVE. PART RECEIVED INSTALLED ON AIRCRAFT.

Part: SEAT BELT — WORN (CABIN)

SEAT BELT WORN BEYOND LIMITS. PART RECEIVED INSTALLED ON AIRCRAFT.

Part: BOLT — WORN (M/R)

WORN BEYOND LIMITS AS PER ASB 214ST-90-51.

Part: BUSHING — PITTED (M/R)

BUSHING PITTED.

Part: BEARING — WORN (T/R)

BEARING WORN AND ROUGH.

Part: FITTING — CRACKED (COWL)

FITTING CRACKED.

Part: CLIP — BROKEN (M/R)

CLIPS BROKEN.

Part: CONTROL CABLE — FRAYED (JETTISON DOOR)

PILOT AND COPILOT'S JETTISON DOOR CABLE FRAYED.

Part: HANDLE — CABLE FRAYED (JETTISON DOOR)

PILOT AND COPILOT'S JETISON DOOR CABLE FRAYED.

Part: STRIKER — WORN (DOOR)

WORN AND ALLOWING DOOR TO OPEN IN FLIGHT.

Part: INDICATOR — STUCK (COCKPIT ALT)

NEEDLE STUCK AT 950 FEET. WHEN TESTED NEEDLE GOES TO 2000 FEET.

Part: TIRE — DEFECTIVE (MLG)

ONE TIRE SPLIT TO THREADS AND ONE TIRE SPLIT WITH PUCTURE.

Part: PILOT RESTRAINT — NOT PROPER (COCKPIT)

PILOT AND COPILOTS RESTRAINTS NOT FAA APPROVED.

Part: CONTROLLER UNIT — INOPERATIVE (WINDSHLD HEAT)

HEATED WINDSHIELD INOPERATIVE.

Part: WASHER — CHAFED (M/R THRUST)

THRUST WASHER CHAFED.

Part: INDICATOR — INOPERATIVE (COCKPIT ENCODER)

ENCODING PORTION OF ALTIMETER INOPERATIVE. WOULD NOT PASS ANNUAL AIRCRAFT INSPECTION.

Part: BEARING — WASHER CHAFED (M/R)

WASHERS CHAFED.

Part: DETECTOR — WONT TEST (SMOKE DET SYS)

INTERMITTENTLY WILL NOT TEST.

Part: ARM ASSY — CRACKED (M/R XMSN MOUNT)

CRACKED AND DETERIORATED PLATE ASSEMBLY. RECEIVED INSTALLED ON AIRCRAFT N8045T.

Part: TORSION ARM — CRACKED (M/R XMSN MOUNT)

CRACKED PLATE ASSEMBLY AND TORSION ARM ELASTOMER. RECEIVED INSTALLED ON AIRCRAFT N8045T.

Part: TRANSCEIVER — DEFECTIVE (COCKPIT)

NO TRANSMIT; WILL NOT TONE.

Part: ANTENNA — DEFECTIVE (VOR LOOP)

VOR NEEDLES WEAK AND ERRATIC. PART RECEIVED INSTALLED ON AIRCRAFT ON 2-1-95. (PREVIOUS AIRCRAFT NUMBER WAS VH-LHQ)

Part: AMPLIFIER — DEFECTIVE (COCKPIT)

IN PITCH MODE, WOULD KICK OFF LINE. PART RECEIVED INSTALLED ON AIRCRAFT ON 2-1-95. (PREVIOUS AIRCRAFT NUMBER WAS VH-LHQ)

Part: CAM FOLLOWER — BEARING WORN (LT SLIDER)

BEARING WORN L/H SLIDING DOOR.. PART RECEIVED INSTALLED ON AIRCRAFT ON 2-1-95. (PREVIOUS AIRCRAFT NUMBER WAS VH-LHQ)

Part: ACTUATOR — INTERMITTENT (M/R CONTROL)

AARS FORE AND AFT SERVO MOTOR INTERMITTENT. PART RECEIVED INSTALLED ON AIRCRAFT ON 2-1-95. (PREVIOUS AIRCRAFT NUMBER WAS VH-LHQ)

Part: BEACON — DEFECTIVE (LOCATOR BEACON)

DUE DATE ON BATTERY ILLEGIBLE. PART RECEIVED INSTALLED ON AIRCRAFT ON 2-1-95. (PREVIOUS AIRCRAFT NUMBER WAS VH-LHQ)

Part: GYRO — DEFECTIVE (COCKPIT HSI)

VALID FLAG ON HSI DOES NOT PULL. PART RECEIVED INSTALLED ON AIRCRAFT ON 2-1-95. (PREVIOUS AIRCRAFT NUMBER WAS VH-LHQ)

Part: INDICATOR — ERROR (COCKPIT VOR)

VOR NEEDLE 10 DEGREES OFF. PART RECEIVED INSTALLED ON AIRCRAFT ON 2-1-95. (PREVIOUS AIRCRAFT NUMBER WAS VH-LHQ)

Part: SENSING ELEMENT — NUT MISSING (FIRE DET)

B NUT MISSING. PART RECEIVED INSTALLED ON AIRCRAFT ON 2-1-95. (PREVIOUS AIRCRAFT NUMBER WAS VH-LHQ)

Part: ANTENNA — WEAK (VOR LOOP)

VOR NEEDLES WEAK AND ERRATIC. PART RECEIVED INSTALLED ON AIRCRAFT ON 2-1-95. (PREVIOUS AIRCRAFT NUMBER WAS VH-LHQ)

Part: INDICATOR — STICKING (COCKPIT)

STICKING. WOULD NOT ADJUST FOR COLLECTIVE UP-DOWN BY-PASS LIGHT. PART RECEIVED INSTALLED ON AIRCRAFT ON 2-1-95. (PREVIOUS AIRCRAFT NUMBER WAS VH-LHQ)

Part: RACE — WORN (M/R)

INNER RACE WORN. PART RECEIVED INSTALLED ON AIRCRAFT ON 2-1-95. (PREVIOUS AIRCRAFT NUMBER WAS VH-LHQ)

Part: LINK ASSY — WRONG PART (M/R)

NOT AN FAA APPROVED COMPONENT. PART RECEIVED INSTALLED ON AIRCRAFT ON 2-1-95. (PREVIOUS AIRCRAFT NUMBER WAS VH-LHQ)

Part: CLEVIS ARM — SEPARATED (ELASTOMER BRG)

ELASTOMER BEARING (TO TORSION ARM) SEPARATED BEYOND LIMITS AS PER 214ST MM. PART RECEIVED INSTALLED ON AIRCRAFT ON 2-1-95. (PREVIOUS AIRCRAFT NUMBER WAS VH-LHQ)

Part: BATTERY — DEFECTIVE (CELL PLATES)

BATTERY WILL NOT TAKE A CHARGE, AND GETS VERY HOT. SUSPECT BREAKDOWN OF INSULATION BETWEEN CELL PLATES. PART RECEIVED INSTALLED ON AIRCRAFT ON 2-1-95. (PREVIOUS AIRCRAFT NUMBER WAS VH-LHQ)

Part: LIGHT ASSY — INOPERATIVE (COCKPIT MARKER)

APPROACH LIGHT WILL NOT ILLUMINATE. PART RECEIVED INSTALLED ON AIRCRAFT ON 2-1-95. (PREVIOUS AIRCRAFT NUMBER WAS VH-LHQ)

Part: CONTROL BOX — DEFECTIVE (COCKPIT)

INTERNAL LIGHTING INOPERATIVE. PART RECEIVED INSTALLED ON AIRCRAFT ON 2-1-95. (PREVIOUS AIRCRAFT NUMBER WAS VH-LHQ)

Part: ADC — WRONG PART (COCKPIT)

AIR DATA COMPUTER IS NOT FAA APPROVED. PART RECEIVED INSTALLED ON AIRCRAFT ON 2-1-95. (PREVIOUS AIRCRAFT NUMBER WAS VH-LHQ)

Part: BEACON — DEFECTIVE (LOCATOR BEACON)

DUKANE BEACON OUT OF BATTERY DATE 01/28/95. PART RECEIVED INSTALLED ON AIRCRAFT ON 2-1-95. (PREVIOUS AIRCRAFT NUMBER WAS VH-LHQ)

Part: BOLT — STRIPPED (ENG MOUNT)

BOLT FOR LOWER AFT ENGINE MOUNT HAS STRIPPED THREADS. PART RECEIVED INSTALLED ON AIRCRAFT ON 2-1-95. (PREVIOUS AIRCRAFT NUMBER WAS VH-LHQ)

Part: LINK ASSY — WRONG PART (M/R)

NOT AN FAA APPROVED COMPONENT. PART RECEIVED INSTALLED ON AIRCRAFT ON 2-1-95. (PREVIOUS AIRCRAFT NUMBER WAS VH-LHQ)

Part: CONTROL — WORN (COCKPIT VHF)

FACEPLATE WORN NEAR VOLUME CONTROL. FREQUENCY TRANSFER SWITCH MUST BE PRESSED TOO HARD IN ORDER TO TRANSFER FREQUENCIES. PART RECEIVED INSTALLED ON AIRCRAFT ON 2-1-95. (PREVIOUS AIRCRAFT NUMBER WAS VH-LHQ)