N1082G

Part: RECEIVER — FAILED (GLIDESLOPE)

RECEIVER FAILED 2 YEAR INSPECTION.

Part: INDICATOR — INOPERATIVE (TRIPLE TACH)

ROTOR PORTION OF TACHOMETER INOPERATIVE.

Part: INDICATOR — READS LOW (TRIPLE TACH)

TRIPLE TACHOMETER INDICATOR READS 3 PERCENT LOW.

Part: TRANSCEIVER — FAILED (COCKPIT VHF)

VHF TRANSCEIVER WILL NOT TRANSMIT OR RECEIVE ON 119.70 THROUGH 131.57.

Part: TRANSCEIVER — FAILED (COCKPIT VHF)

VHF TRANSCEIVER INOPERATIVE WHEN INSTALLED.

Part: INDICATOR — ERRATIC (ATTITUDE)

INDICATOR SPHERE IS ERRATIC IN PITCH.

Part: ENGINE — OVERTEMP (ENGINE BAY)

ITT ABOVE 900 DEGREES FOR OVER 40 SECONDS.

Part: ENGINE — FAILED (NR 2)

ON 10-28-98 DURING RECONNAISSANCE OF OGLNY, CA, FIRE NOTICED, RPM LOW 97 PERCENT, THEN NOTICED LARGE TORQUE SPLIT. WITH N1 ON NR 2 ENGINE AT IDLE AND ITT 900 DEGREES CELSIUS, PILOT WENT TO MANUAL THROTTLE, BUT NO RESPONSE BY ENGINE.

Part: COMPRESSOR — FAILED (ENGINE)

NOISE COMING FROM COMPRESSOR.

Part: RECEIVER — FAILED (COCKPIT)

GPS RECEIVER WILL NOT HOLD SATELLITES.

Part: TRANSCEIVER — MALFUNCTIONED (COCKPIT VHF)

VHF TRANSCEIVER HAS STATIC, HARD TO RECEIVE.

Part: CAUTION PANEL — FAILED (INST PANEL)

PANEL ASSY LIGHTS FLICKER INTERMITTENTLY.

Part: WINDOW — BROKEN (COCKPIT)

DURING CRUISE FLIGHT, TOP THIRD OF WINDOW BROKE OUT AND DEPARTED AIRCRAFT. NO OTHER DAMAGE OCCURRED. CAUSE UNKNOWN. MAINTENANCE REPLACED WINDOW. REF: 212 IPC, CHAPTER 52-99-00, PAGE 46, ITEM 20, FIGURE 52-11.

Part: CONTROL UNIT — FAILED (NR 2 GENERATOR)

NR 2 GENERATOR INOPERATIVE.

Part: CONTROL UNIT — LEAKING (ENGINE)

NR 2 SIDE HAS INTERNAL AIR LEAK THAT PREVENTS NR 2 ENGINE FROM TOPPING. (BOTH SERVO VALVES LEAK).

Part: GEARBOX — MAKING METAL (COMBINING)

COMBINING GEARBOX HAS METAL CONTAMINATION ON NR 2 SIDE.

Part: DAMPER ASSY — DEFECTIVE (M/R)

DAMPER ASSY SIGHT GLASS CLOUDY AND LEAKING. SERIAL NUMBERS REMOVED ARE A1187 AND R19-11869.

Part: INDICATOR — FAILED (ENG N1)

N1 INDICATOR NEEDLE HAS STICKY OPERATION THROUGHOUT SCALE.

Part: ALTIMETER — FAILED (COCKPIT)

ALTIMETER INDICATES LOW OUT OF TOLERANCE ABOVE 3000 FEET.

Part: INDICATOR — STICKING (HYDRAULIC SYS)

TEMPERATURE NEEDLE STICKING.

Part: INVERTER — MALFUNCTION (AC SYS)

INVERTER VOLTAGE OUTPUT HIGH CAUSING INTERMITTENT INVERTER WARNING.

Part: TRIM COMPENSATOR — INTERMITTENT (ENG ITT)

INTERMITTENT ITT FUNCTION.

Part: INDICATOR — STICKS (COCKPIT RAD ALT)

RADAR ALTIMETER WHEN POINTER IS SET AT ZERO AND POWER IS SHUT OFF,UNIT POINTS INTERMITTENTLY AND STICKS BELOW ZERO.

Part: RATE GYRO — MALFUNCTION (COCKPIT)

GYRO CAUSES RATE OF TURN NEEDLE ON ADI TO PEG OFF.

Part: INDICATOR — FAILED (COCKPIT DME)

DME DOES NOT TURN ON. REPLACED HEADER DUE TO BURNT SPOT ON 192V CONTACT. APPLIED HUMISEAL. UNIT FIRES UP, BUT DOES NOT CHANNEL. FOUND BURNT R801. REPLACED R801. ALSO REPLACED 2 EACH SCREWS P/N 047-4808-01 ON COVER. UNIT HAS BAD DISPLAY SEGMENTS AND NO CHANNELING.

Part: CONTROL — DEFECTIVE (COCKPIT)

DOESN'T COME ONE. CLEANED ON/OFF SWITCH AND RESOLDERED COLD SOLDER JOINT ON SWITCH. REPAIRED. ALSO FOUND "IDENT" AND "TEST" SWITCHES INTERMITTENT. REPLACED "IDENT" (S106) P/N 031-0061-00 AND "TEST" (S108) P/N031-0061-00. REPAIRED. ALSO REPLACED MISSING BOTTOM COVER P/N 047-01366-0001. REPAIRED. BENCH CHECK GOOD.

Part: TRANSCEIVER — INOPERATIVE (COCKPIT)

TRANSCEIVER INOPERATIVE. REPLACED BURNT F1 FUSE, SHORTED Q123 TRANSISTOR, SHORTED Q105 TRANSISTOR AND BURNT R114 RESISTOR. INSTALLED TRANSMITTER SHIELD. INSPECTED AND BENCH CHECK GOOD.

Part: GRIP — DAMAGED (PITCH HORN)

THREADS ON PITCH HORN BORE ARE TO DAMAGED TO ACCEPT NEW THREAD INSERT. ALSO REPLACE BLADE BOLT BUSHING AND DRAG BRACES BUSHING AND INSTALL BUSHING IN PITCH HORN BORE.

Part: ROD END — SHEARED BARREL (TAIL ROTOR)

TAIL ROTOR PITCH LINK ASSEMBLY SEPARATED IN-FLIGHT. AIRCRAFT LANDED SAFELY. ROD END BARREL SHEARED. NO SIGNS OF CORROSION NOTED. SUSPECT EXCESSIVE ROD END BEARING WEAR PREVENTED BEARING ROTATION. (X)