N513EH

Part: TRANSDUCER — MALFUNCTIONED (FUEL PRESSURE)

WHILE IN CRUISE FLIGHT THE FUEL PRESSURE INDICATOR SHOWED A DECREASE IN FUEL PRESSURE. REPLACED PRESSURE TRANSMITTER.

Part: NOZZLE — CRACKED (TURBINE)

ENGINE REMOVED DUE TO MAKING METAL AND LOW POWER. UPON INSPECTION OF TURBINE PARTS NOTED: CRACKED 1ST STAGE NOZZLE VANES BEYOND SERVICEABLE LIMITS.

Part: ALTIMETER — LEAKING (COCKPIT)

ALTIMETER HAS EXCESSIVE CASE LEAKAGE.

Part: INDICATOR — MALFUNCTIONED (TOT)

RISE IN TOT INDICATION WHEN VHF MIC. KEYED-LIGHT PIN BROKEN.

Part: INDICATOR — MALFUNCTIONED (TOT)

TOT INDICATOR HAS NO MOVEMENT ON LIGHT-OFF.

Part: INDICATOR — FOGGED (COCKPIT)

FOGGED GLASS ON INDICATOR, NEEDLE ERRATIC AND INTERMITTENT.

Part: INDICATOR — MALFUCNTIONED (TOT)

INDICATOR MOVES WHEN VHF RADIO IS USED.

Part: GPS RECEIVER — FAILED (COCKPIT)

GPS RECEIVES NO SIGNAL. FOUND UNIT DISPLAYING RECEIVER FAIL MESSAGE.

Part: TRANSCEIVER — MALFUNCTIONED (COCKPIT)

LOSES DISPLAY AFTER WARM UP AND POWER IS BELOW SPECS.

Part: TRANSPONDER — FAILED (COCKPIT)

TRANSPONDER INOPERATIVE, WILL NOT TURN ON.

Part: INDICATOR — MALFUNCTIONED (COCKPIT)

REDLINE AND RED DOT FADED. CHECK FOR PROPER OPERATION AND PROPER CALIBRATION.

Part: TRANSCEIVER — MALFUNCTIONED (E/E BAY)

MODULATION DISTORTED AT 85 PERCENT ON TRANSCEIVER.

Part: SKIN — CORRODED (FUSELAGE)

SKIN CORRODED AND SEPARATED.

Part: VALVE — DAMAGED (FUEL SYSTEM)

FUEL SYSTEM VALVE E FITTING BENT.

Part: STAB ASSY — CORRODED (TAIL BOOM)

STABILIZER ASSEMBLY CORRODED BEYOND LIMITS.

Part: ANGLE — MISMANUFACTURED (FUSELAGE)

ANGLE MISMANUFACTURED. THERE IS NO EDGE DISTANCE AT THE TOP PART OF THE ANGLE AT THE LOWER INBOARD RIVET.

Part: PANEL — MISMANUFACTURED (FUSELAGE)

NOT ENOUGH METAL PROTRUDING BEYOND FUSELAGE TRANSITION ON PANEL.

Part: TUBE ASSY — DAMAGED (MAIN ROTOR)

MAIN ROTOR TUBE ASSY HAS MECHANICAL DAMAGE (NICKS, SCRATCHES) AROUND THE UPPER SLOT. DAMAGE BEYOND LIMITS. SCRAPPED PART, REPLACED WITH SERVICEABLE PART.

Part: BELLCRANK — CORRODED (MAIN ROTOR)

MAIN ROTOR BELLCRANK HAS CORROSION DAMAGE BEYOND LIMITS. SCRAPPED PART, REPLACED WITH SERVICEABLE PART.

Part: SUPPORT — CORRODED (M/R CYCLIC)

MAIN ROTOR CYCLIC HAS CORROSION DAMAGE BEYOND LIMITS. SCRAPPED PART, REPLACED WITH SERVICEABLE PART.

Part: SUPPORT — CORRODED (MAIN ROTOR)

MAIN ROTOR SUPPORT HAS EXCESSIVELY CORRODED ON BOTTOM. CORROSION BEYOND LIMITS. SCRAPPED PART, REPLACED WITH SERVICEABLE PART.

Part: ELT — FAILED (COCKPIT)

ELT UNIT FOUND IN ON POSITION FOR UNKNOWN TIME.

Part: NOZZLE — CRACKED (NR 1)

ENGINE REMOVED DUE TO OIL BLOWING OUT OF COMP. DISCHARGE. TURBINE DISASSEMBLED DUE TO LOW POWER ON TEST CELL. UPON INSPECTION OF TURBINE PARTS NOTED: CRACKED BEYOND SERVICEABLE LIMITS ON NR1 NOZZLE VANES, OUTERBAND AND KEYWELDS.

Part: ANTENNA — FAILED (LORAN)

LORAN HAS NO SIGNAL WITH THIS ANTENNA. BAD FROM STOCK.

Part: ELT — DEFECTIVE (COCKPIT)

NARCO ELT BATTERY WEAK.

Part: ACTUATOR — FAILED (DROOP COMP)

ACTUATOR INOPERATIVE AND WILL NOT MOTOR.

Part: ACTUATOR — FAILED (M/R)

ACTUATOR STICKS, INOPERATIVE.

Part: INDICATOR — FAULTY (COCKPIT)

ENGINE TEMPERATURE INDICATOR READS 10 DEGREES HIGH.

Part: ACTUATOR — INOPRATIVE (MAIN ROTOR)

M/R ACTUATOR WILL NOT ACTUATE.

Part: INDICATOR — INOPERATIVE (COCKPIT T&B)

T & B INDICATOR INOPERATIVE. TIME SINCE REPAIR 46:35.

Part: TRANSCEIVER — FAILED (COCKPIT)

ATC TRANSPONDER DOES NOT TRANSMIT. RECEIVED NEW 6-97.

Part: TRANSCEIVER — INOPERATIVE (COCKPIT)

INOPERATIVE. PERFORMED PRELIMINARY INSPECTION AND FOUND BAD ON/OFF SWITCH R106. REPLACED SWITCH R106. REPAIRED. ADJUSTED SQUELCH AND SIDETONE. BENCH CHECK GOOD.

Part: TACH GEN — FAILED (ROTOR)

TACH GEN NO OUTPUT.

Part: INDICATOR — DEFECTIVE (COCKPIT)

BEZEL LOOSE ON UNIT.

Part: TRANSCEIVER — FAILED (COCKPIT)

DISPLAY BLANKS OUT IN FLIGHT INTERMITTENTLY. CAN STILL TRANSMIT AND RECEIVE WHEN DISPLAY GOES OUT.

Part: CONTROL UNIT — DEFECTIVE (COCKPIT VHF)

THUMBWHEELS DON'T AGREE WITH DISPLAY. TRIED CLEANING THUMBWHEEL. NO HELP. REPLACED THUMBWHEEL S1. REPAIRED. BENCH CHECK GOOD.

Part: TRANSCEIVER — FAILED (COCKPIT ATC)

NOT RECEIVED BY ATC AFTER 2 HOURS OF FLIGHT. REPLACED BROKEN FACEPLATE. REPLACED PHOTOCELL V301 DUE TO WEAK REPLY LIGHT. REPAIRED. REPLACED BROKEN HOLD DOWN AND INSTALLED GROOVE PIN. ADJUSTED PULSE WIDTH. BENCH CHECK GOOD.

Part: SWITCH — FAILED (XMSN THERMO)

IN-FLIGHT, TRANSMISSION OIL TEMP LIGHT ILLUMINATED SEVERAL TIMES. TEMP INDICATOR READING NORMAL. AIRCRAFT DIVERTED TO FOURCHON. 206L-1 IPC, CHAPER 63-99-00, PAGE 8, FIGURE 63-2, ITEM 23.