N2258F

Part: PANEL — MISMANUFACTURED (FUSELAGE) · airframe 18,802 hrs

PANEL MISMANUFACTURED. WHEN WE STARTED TO DRILL FASTENER HOLES INTO TRIMMED PANEL AT AFT CENTER EDGE, PANEL SEPERATED AND A CLEAR HARD SUBSTANCE CAME OUT OF PANEL. PANEL REPAIRED BY ACI.

Part: ACTUATOR — MALFUNCTIONED (YAW CONTROL) · airframe 18,615 hrs

YAW NEEDLE DEFLECTS FULL LEFT AND STAYS.

Part: GPS — MALFUNCTIONED (COCKIT)

GPS WILL NOT RECOGNIZE DATA CARD. SENT TO ASM FREEFLIGHT FOR INSPECTION AND REPAIR.

Part: GPS — MALFUNCTIONED (COCKPIT) · airframe 18,709 hrs

GPS UNABLE TO ACQUIRE DATA. CLEANED DATA CARD READER CONTACTS. REPAIRED.

Part: COMPUTER — MALFUNCTIONED (AFCS) · airframe 18,763 hrs

NR 1 HELIPILOT COMPUTER PITCH HARDOVER. REPAIRED.

Part: GEARBOX — DAMAGED (TAIL ROTOR) · airframe 18,601 hrs

GEARBOX HAS EXCESSIVE BACKLASH AT FWD COUPLING. REPAIRED.

Part: INDICATOR — READS HIGH (ENG OIL PRESSURE) · airframe 18,797 hrs

ENGINE OIL PRESSURE READS HIGH. REPAIRED.

Part: ANTENNA — CORRODED (ATC TRANSPONDER) · airframe 18,621 hrs

ANTENNA HAS CORROSION AND TRANSPONDER REPORTED WEAK BY ATC. SCRAPPED.

Part: ANTENNA — FAILED (FM COMMS) · airframe 18,615 hrs

FM COMMS ANTENNA FAILED FUNCTION CHECK. SCRAPPED.

Part: COMPUTER — MALFUNCTIONED (AFCS) · airframe 18,739 hrs

AFCS COMPUTER NR 1 PITCH MOTORS ALL THE WAY UP IN SAS MODE.

Part: ACTUATOR — MALFUNCTIONED (YAW CONTROL) · airframe 18,763 hrs

YAW CONTROL NEEDLE FULL DEFLECTION TO NR 1 SIDE.

Part: INDICATOR — SPINNING (ATTITUDE) · airframe 18,615 hrs

ATTITUDE INDICATOR SPINS CONTINOUSLY, WILL NOT STABILIZE.

Part: STARTER GEN — INOPERATIVE (ENGINE) · airframe 18,763 hrs

STARTER GENERATOR WOULD NOT ROTATE.

Part: ACTUATOR — STUCK (STEP) · airframe 18,759 hrs

STEP ACTUATOR STUCK. REPAIRED.

Part: INDICATOR — ERRATIC (FUEL QTY) · airframe 18,591 hrs

FUEL QTY INDICATION ERRATIC; WILL NOT RETURN TO SAME POSITION ON TEST.

Part: INDICATOR — MALFUNCTIONED (WX RADAR SYS) · airframe 18,646 hrs

WEATHER RADAR SYSTEM WILL NOT PAINT. FOUND LOGIC NR 1 BOARD BAD, REPLACED IC U1251, U1258, U1211, U1213, U1201, REPAIRED. BENCH CHECK GOOD.

Part: AMPLIFIER — CORRODED (VOR SYSTEM) · airframe 18,759 hrs

NR 2 KDA CONNECTOR FROZE ON BOX. FOUND UNIT EXCESSIVELY CORRODED. CLEANED CORROSION AND REPLACED 18 HEADER PINS DUE TO CORROSION. BENCH CHECK GOOD.

Part: TRANSPONDER — WEAK (COCKPIT) · airframe 18,621 hrs

TRANSPONDER WEAK AND INTERMITTENT REPORTING. SENT TO HONEYWELL, IN. FOR INSPECTION AND REPAIR.

Part: ARM — CORRODED (WINDSHIELD WIPER) · airframe 18,734 hrs

WINDSHIELD WIPER ARM CORRODED. SCRAPPED.

Part: INDICATOR — MALFUNCTIONED (WX RADAR SYS) · airframe 18,759 hrs

WEATHER RADAR SYSTEM FAILS TO DISPLAY PROPERLY. FOUND LOGIC NR 1 BOARD BAD. REPLACED SEVERAL ICS. REPAIRED A BROKEN FOIL FROM PIN 19 OF J1201 HEADER TO PIN 11 OF U1260. BENCH CHECK GOOD.

Part: INDICATOR — STUCK (FUEL QTY) · airframe 18,601 hrs

FUEL QTY INDICATOR NEEDLE STICKS COMING DOWN.

Part: SWITCH — FAILED (FUEL SYSTEM) · airframe 18,630 hrs

SIDE TO SIDE TOTAL READINGS AT 240 LBS. REPLACED SWITCH.

Part: CONNECTOR — CORRODED (WX RADAR IND) · airframe 18,745 hrs

WEATHER RADAR ANTENNA WILL NOT SWEEP. FOUND UNIT DOES NOT SWEEP. FOUND CORROSION ON CONNECTOR P3001, CLEANED, REPAIRED, BENCH CHECK GOOD.

Part: INDICATOR — MALFUNCTIONED (RADAR SYS) · airframe 18,752 hrs

RADAR HAS TEST PATTERN ON ANY SCALE ABOVE 4 MILES. SHOP REPAIR.

Part: BEARING — WORN (SWASHPLATE)

SWASHPLATE GIMBAL RING BEARING WORN. REPAIRED.

Part: GYRO — MALFUNCTIONED (COCKPIT) · airframe 17,963 hrs

DIRECTIONAL GYRO WON'T SLAVE.

Part: BLEED VALVE — FAILED (ENGINE) · airframe 17,629 hrs

BLEED VALVE PRODUCING HIGH ITT (100 DEGREES HIGHER) AND ENGINE N1 FLUCTUATIONS.

Part: CYLINDER — LEAKING (MAIN ROTOR) · airframe 18,357 hrs

MAIN ROTOR SERVO CYLINDER LEAKS.

Part: LEVER — WORN (TAIL ROTOR) · airframe 13,364 hrs

T/R CONTROL LEVER IN HELL HOLE WORN BEARING. SCRAPPED AND REPLACED WITH SERVICEABLE PART.

Part: COVER — TORN (MLG) · airframe 17,629 hrs

LOOP AND HOOK TORN ON END CAP OF EMERGENCY FLOAT COVER.

Part: GEARBOX — LEAKING (TAIL ROTOR)

LEAK OUTPUT SHAFT SEAL. REPLACED SEAL AND RETURNED TO SERVICE.

Part: CROSSTUBE — CORRODED (MLG) · airframe 18,249 hrs

CROSSTUBE CORRODED BEYOND LIMITS.

Part: GEARBOX — MAKING METAL (MAIN ROTOR) · airframe 16,141 hrs

MAIN ROTOR COMBINING GEARBOX IS MAKING METAL.

Part: OIL COOLER — LEAKING (OIL SYSTEM)

OIL COOLER LEAKS.

Part: EXCITER — FAILED (ENGINE) · airframe 17,645 hrs

CAUSING THE CIRCUIT BREAKER TO POP.

Part: COVER — TORN (FLOAT BAG) · airframe 17,438 hrs

FLOAT BAG VELCRO TORN.

Part: COVER — TORN (FLOAT BAG) · airframe 17,438 hrs

FLOAT BAG COVER VELCRO TORN.

Part: GEARBOX — MAKING METAL (NR 1 ENGINE) · airframe 16,919 hrs

COMBINING GEARBOXMAKING METAL NR 1 SIDE.

Part: INDICATOR — INTERMITTENT (ITT)

STICKS INTERMITTENTLY AT ZERO.

Part: BLADE — DAMAGED (MAIN ROTOR)

BLADE DAMAGED ON THE UPPER SURFACE CENTER AT STA 120.

Part: TRANSCEIVER — MALFUNCTIONED (COCKPIT VHF)

POWER-OUT HESITATING WHEN KEYED.

Part: ENCODER — INTERMITTENT (COCKPIT)

HUNDREDS NEEDLE HAS INTERMITTENT OPERATION ON ALTIMETER.

Part: COMPUTER — MALFUNCTIONED (AFCS)

NR 2 AFCS WOULD NOT LATCH.

Part: GPS — FAILED (COCKPIT)

TIME CHANGE. PERFORMED PRELIMINARY INSPECTION. FOUND UNIT GIVING COURSE INPUT FAIL MESSAGE.

Part: TRANSCEIVER — MALFUNCTION (COCKPIT)

TRANSCEIVER POWER OUT FLUCTUATES WHEN VIBRATED.

Part: PUMP — FAILED (FUEL BOOST)

BOOST PUMP INOPERATIVE.

Part: REVERSE CURRENT — MALFUNCTION (DC DIST)

WON'T PULL OFF FLAG ON HSI.

Part: ACTUATOR — FAILED (STEP)

STEP ACTUATOR WON'T COME UP OR DOWN.

Part: ACTUATOR — FAILED (STEP)

STEP ACTUATOR MOTOR WON'T EXTEND OR RETRACT.

Part: RATE GYRO — FAILED (HSI)

RATE GYRO FAILED. WON'T PULL OFF FLAG ON HSI.

Part: TARSYN 333 — FAILED (AUTO FLIGHT)

FAILED TEST 3.1 ON SST BENCH.

Part: BLADE — DEFECTIVE (M/R)

BLADE RECEIVED FROM VENDOR WITH NO WEIGHTS IN FORWARD ROOT POCKET; BLADE IS HEAVY AND CANNOT BALANCE

Part: INDICATOR — FAILED (COCKPIT ITT)

ITT INDICATOR READS ZERO ALL OF THE TIME.

Part: TRANSCEIVER — FAILED (COCKPIT VHF)

TRANSCEIVER WEAK AND UNREADABLE, NO TRANSMIT.

Part: ACTUATOR — BROKEN (STEP)

STEP ACTUATOR ROD END BROKEN AND MOTOR WILL NOT TURN.

Part: DETECTOR — MALFUNCTION (RPM LIMIT)

RPM LIGHT FLASHES ON AND OFF AT 100%.

Part: RATE GYRO — FAILED (COCKPIT)

RATE GYRO TURN NEEDLE WILL NOT MOVE.

Part: FLOAT BAG ASSY — UNBONDED (INLET VALVE)

FLOAT BAG HAS UNBONDED INLET VALVE AND PIN HOLE LEAKAGE.

Part: TRANSCEIVER — FAULTY (COCKPIT)

TRANSCEIVER WILL NOT TRANSMIT.

Part: BLADE — SEPARATION (M/R)

BLADE HAS SKIN SEPARATION ON UPPER AND LOWER SURFACES STARTING AT STATION 172 AND ENDING AT STATION 196. SENT TO COMPOSITE TECHNICS FOR INSPECTION AND REPAIR.

Part: DOOR — DEFECTIVE (BAGGAGE)

DOOR WAS ON EVALUATION PROGRAM THROUGH BELL HELICOPTER TEXTRON.

Part: INDICATOR — READS HIGH (FUEL PRESS)

READS HIGH ON LOW END AND LOW ON HIGH END OF SCALE.

Part: RECEIVER — MALFUNCTION (COCKPIT ADF)

RECEIVER INOPERATIVE. WEAK RECEIVE IN ANTENNA MODE.

Part: INDICATOR — STICKS (COCKPIT)

INDICATOR NEEDLE STICKS THROUGHOUT SCALE.

Part: ANEROID — ERRATIC (ALTIMETER)

BAROMETRIC ANEROID UNIT HAS AN INCONSISTANT OUTPUT.

Part: TRANSCEIVER — DEFECTIVE (COCKPIT)

TX AND RX BREAKS UP DURING ENGINE RUN-UP.

Part: CONE — COATING SCORED (M/R HUB)

TEFLON COATING SCORED. SENT TO BELL HELICOPTER TEXTRON FOR INSPECTION AND REPAIR.

Part: BEARING — DEFECTIVE (T/R)

DUPLEX BEARING CAGES SQUEEZE ON INNER RACE OF BEARING CAUSING A BIND ON INNER RACE AND DOESN'T TURN FREELY.

Part: TRANSCEIVR — FAILED (COCKPIT VHF)

TRANSCEIVER WON'T RECEIVE.

Part: ELT — MALFUNCTION (COCKPIT)

ELT UNIT ACTIVATES BY ITSELF IN ARMED POSITION INTERMITTENTLY.

Part: INDICATOR — STICKING (XMSN OIL TEMP)

INDICATOR STICKING AT 50 DEGREES, METER MOVEMENT BROKEN ON TEMP SIDE.

Part: VALVE — INOPERATIVE (FUEL SYS)

VALVE INOPERATIVE.

Part: INDICATOR — DEFECTIVE (COCKPIT)

INDICATOR WILL NOT SHUT OFF IN STANDBY.

Part: INDICATOR — DEFECTIVE (COCKPIT)

DISPLAY FLICKERS IN ALL GREEN SCREEN.

Part: RECEIVER — WEAK (COCKPIT ADF)

WEAK RECEPTION. SENT TO THE RADIO SHOP FOR INSPECTION AND REPAIR.

Part: INDICATOR — STICKS (COCKPIT HSI)

INDICATOR STICKS IN ROLL AXIS.

Part: VALVE — TRIPS BREAKER (FUEL SYS)

FUEL VALVE CIRCUIT BREAKER TRIPPED.

Part: ACTUATOR — ARMATURE BURNT (STEP)

UNIT INOPERATIVE. INSPECTED AND BENCH CHECKED BY ACCESSORY OVERHAUL SHOP. UNIT SLOW TO RESPOND AND DREW EXCESSIVELY HIGH AMPS. FOUND ARMATURE BURNT.

Part: CVR — WONT TEST (COCKPIT)

CVR WILL NOT TEST.

Part: DECK ASSY — UNBONDED (LOWER SKIN)

LOWER SKIN UNBONDED APPROXIMATELY 4" X 6" ON FORWARD END. RECEIVED REPAIRED FROM NORDAM 9-17-93. INSTALLED ON AIRCRAFT 8-14-94. REPAIRED SERVICE DECK.

Part: SHAFT — RUSTED (MAIN DRIVE)

HEAT TEMP INDICATORS COMING UNBONDED AND RUSTING UNDERNEATH. REPLACED WITH SERVICEABLE MAIN DRIVE SHAFT.