N31219

Part: AUDIO CONTROL — MALFUNCTIONED (COCKPIT)

AUDIO CONTROL HAD WEAK AND BROKEN TRANSMIT AND RECEIVE.

Part: REPEATER — INOPERATIVE (ENGINE OIL)

LIGHTS INOPERATIVE.

Part: RECEIVER — MALFUNCTIONED (COCKPIT)

NO MARKER BEACON LIGHTS ON INDICATOR.

Part: RECEIVER — MALFUNCTIONED (COCKPIT)

NO MARKER BEACON LIGHTS ON INDICATOR.

Part: ACTUATOR — INOPERATIVE (AFCS)

AFCS ACTUATOR INOPERATIVE.

Part: BUTTON — INOPERATIVE (LORAN)

ENTER BUTTON INOPERATIVE. REPLACED RUBBER KEYPAD. REPAIRED. TESTED. FUNCTION CHECK GOOD.

Part: BLADE — CRACKED (MAIN ROTOR)

LEADING EDGE CRACKED AND SEPARATION AT STATIONS 145 AND 168.

Part: BLADE — CRACKED (MAIN ROTOR)

LEADING EDGE SEPARATED AND CRACKED AT STATIONS 65 AND 76 ON MAIN ROTOR BLADE.

Part: BLADE — SEPARATED (MAIN ROTOR)

LEADING EDGE SPLICE SEPARATED AND BLADE IS DUE FOR TIME EXTENSION.

Part: STARTER — FAILED (START/GENERATOR)

STARTER/GENERATOR WILL NOT MOTOR ENGINE.

Part: TRANSCEIVER — FAILED (COCKPIT)

RADIO INTERMITTENTLY WILL NOT TRANSMIT.

Part: INDICATOR — PRECESSING (ATTITUDE)

ATTITUDE INDICATOR HAS JERKY MOVEMENT AND PRECESSES.

Part: EJECTOR — CRACKED (EXHAUST)

EJECTOR HAS EXCESSIVE CRACKING.

Part: CAUTION PANEL — MALFUNCTIONED (COCKPIT)

NO MASTER CAUTION LIGHT WITH POWER ON.

Part: INDICATOR — FAILED (COCKPIT)

RT FLAG ATTITUDE INDICATOR WILL NOT PULL.

Part: RATE GYRO — FAILED (COCKPIT)

ADI RT FLAG WILL NOT PULL.

Part: CAUTION PANEL — MALFUNCTIONED (COCKPIT)

CANNOT CANCEL MASTER CAUTION LIGHT ON NR 5 PACK.

Part: ACTUATOR — CHATTERING (AFCS)

AFCS ACTUATOR CHATTERING AND RATCHETY.

Part: CONTROL UNIT — FAILED (VHF COMM)

CANNOT LOAD FREQUENCIES INTO VHF COMM MEMORY.

Part: BLADE — DAMAGED (TAIL ROTOR)

TAIL ROTOR PADDLE 'B' HAS SOME FOREIGN OBJECT DAMAGE. THERE IS A HOLE ON LEADING EDGE STRIP AND A GOUGE IN THE AIRFOIL REGION. ON PADDLE 'A' THERE ARE CUTS INTO PRIMARY RUBBER.

Part: EJECTOR — CRACKED (ENGINE EXHAUST)

ENGINE EXHAUST HAS EXCESSIVE CRACKING.

Part: FILLER VALVE — LEAKS (FUEL SYS)

FILLER VALVE LEAKS OUT OF VALVE.

Part: TRANSPONDER — FAILED (COCKPIT)

TRANSPONDER WILL NOT TRANSMIT.

Part: SEAL — DEFECTIVE (NR 8 LAB SEAL)

ENGINE REMOVED DUE TO FOD AND TURBINE OVERHAUL. UPON INSPECTION OF TURBINE PARTS NOTED: MEASURED .001 BELOW SPECS (1.2520 - 1.2515) ON SEAL O.D. INSTALLED A NEW SEAL.

Part: DAMPER — FAILED (M/R)

M/R DAMPER HAS A DEAD SPOT.

Part: BLADE — DEFECTIVE (M/R)

BLADE TRIM TAB SPLIT OPEN AND SEPARATED.

Part: BLADE — UNBONDED (M/R)

M/R BLADE TIP RIB UNBONDED.

Part: INDICATOR — FAILED (OXY SYS)

INDICATOR INOPERATIVE.

Part: TRANSMITTER — FAILED (FUEL SYS)

FUEL PRESSURE TRANSMITTER READS HIGH OUT OF TOLERANCE.

Part: BLOWER — FAILED (AIR BLOWER)

BLOWER MOTOR WILL NOT TURN. REPLACED WITH SERVICEABLE BLOWER.

Part: LORAN — INOPERATIVE (COCKPIT)

LORAN ENTER BUTTON INOPERATIVE. MODE BUTTON INTERMITTENT.

Part: SMOKE DETECTOR — FAILED (DETECTOR BULB)

SMOKE DET WILL NOT TEST BULBS.

Part: MODULE — INOPERATIVE (ROTOR BRAKE)

ROTOR BRAKE LIGHT INOPERATIVE.

Part: CAUTION PANEL — MALFUNCTIONED (COCKPIT)

MASTER CAUTION LIGHT STAYS ON VERY LOW.

Part: WEB — UNBONDED (FUSELAGE)

WEB IS UNBONDED.

Part: INPUT HOUSING — CRACKED (M/R GR BOX)

INPUT HOUSING CRACKED. REPLACED WITH NEW INPUT HOUSING.

Part: GEAR SHAFT — STEP WEAR (SPUR ADAPTER)

ENGINE REMOVED DUE TO TURBINE CYCLES. UPON INSPECTION OF COMPRESSOR NOTED: STEP WEAR BEYOND SERVICEABLE LIMITS ON GEARSHAFT FORWARD AND AFT SPLINES. INSTALLED A NEW GEARSHAFT.

Part: CAUTION PANEL — DEFECTIVE (COCKPIT)

MASTER CAUTION STAYS ON THEN WENT OFF AND WOULD NOT COME ON.

Part: EJECTOR — CRACKED (EXHAUST)

EXH EJECTOR CRACKED AT TOP.

Part: GEARSHAFT — STEP WEAR (SPUR ADAPTER)

ENGINE REMOVED DUE TO LOW POWER. UPON INSPECTION OF COMPRESSOR PARTS NOTED: STEP WEAR BEYOND SERVICEABLE LIMITS ON SPUR GEARSHAFT AFT SPLINES. INSTALLED A NEW SPUR GEARSHAFT.

Part: OIL COOLER — DEFECTIVE (ENG OIL)

ENGINE HAS HIGH OIL TEMPERATURE.

Part: BLADE — SEPARATION (T/R)

PADDLE "A" OF ASSEMBLY HAS SOME SEPARATION NEAR THE TIP WEIGHT COVER.

Part: BLOWER — INOPERATIVE (OIL COOL)

MOTOR ASSEMBLY INOPERATIVE; WILL NOT OPERATE. TIME SINCE REPAIR 10:15.

Part: WHEEL — DEFECTIVE (TURBINE)

TURBINE WHEEL DEFECTIVE

Part: SHUT OFF VALVE — STICKS (BLEED SOV)

STICKS IN OPEN POSITION. SENT TO HELICOPTER SUPPORT, INC. FOR INSPECTION AND REPAIR.

Part: EJECTOR — CRACKED (EXH)

EJECTOR NUMEROUS CRACKS.

Part: BEVEL GEAR — EXCESS WORN (M/R GR BOX)

EXCESSIVE WEAR ON CONVEX SIDE OF GEAR TEETH. REPLACED WITH SERVICEABLE PART. SEE MMIR# HEEA0008490 FOR PINION ALSO REPLACED.

Part: PINION — EXCESS WEAR (M/R GR BOX)

EXCESSIVE WEAR ON CONVEX SIDE OF GEAR TEETH. REPLACED WITH SERVICEABLE PART. SEE MMIR# HEEA0008489 FOR PINION ALSO REPLACED.

Part: COMBUSTION LINER — DEFECTIVE (TURBINE)

UPON INSTALLATION OF COMBUSTOR LINER NOTED: UNABLE TO INSTALL FUEL NOZZLE AND IGNITER PLUGS DUE TO MISALIGNMENT. REPLACED DISCREPANT PART.

Part: ALTIMETER — NEEDLE STICKS (RADAR ALT)

RADAR ALTIMETER NEEDLE STICKS AROUND 45 FEET. DH LIGHT INOPERATIVE. NEEDLE FLUCTUATES INTERMITTENTLY.

Part: TRANSCEIVER — DEFECTIVE (COCKPIT DME)

UNIT DRAWS TOO MUCH CURRENT AND NEED TO UPDATE MODS.

Part: FITTING — CRACKED (MLG DOOR)

FITTING CRACKED APPROXIMATELY 1/4". REPLACED WITH SERVICEABLE FITTING.

Part: INDICATOR — FAILED (COCKPIT)

BLANK SCREEN.

Part: TIP CAP — SKIN BROKEN (M/R)

FIBERGLASS SKIN BROKEN BETWEEN INNER AND OUTER DOUBLERS ON THE LOWER SIDE. THE LEADING EDGE ABRASION STRIP HAS A CRACK WITH A STOP DRILL.

Part: TIP CAP — TORN (M/R)

TIP CAP HAS THE SKIN TORN NEXT TO THE ABRASION STRIP ON THE LOWER SIDE.

Part: TIP CAP — BROKEN (M/R)

TIP CAP OUTER TRAILING EDGE BROKEN OFF.

Part: NOZZLE — CRACKED (1ST STAGE)

ENGINE REMOVED DUE TO CYCLED OUT 1ST AND 2ND STAGE WHEELS. UPON INSPECTION OF TURBINE PARTS NOTED THE FOLLOWING: CRACKS BEYOND OVERHAUL LIMITS ON OUTER BAND (2 EA) AND 50% OF VANES AT TRAILING EDGE. REPLACED PART. NOTE: FUEL NOZZLE SPRAY PATTERN CHECKED GOOD. SUBMITTAL FOR CREDIT ACCOMPLISHED ON AFA# 24473A.

Part: N1 COUPLING — STEP WEAR (FWD SPLINES)

ENGINE REMOVED DUE TO TURBINE CYCLES. UPON INSPECTION OF TURBINE PARTS NOTED THE FOLLOWING: STEP WEAR BEYOND OVERHAUL LIMITS IN N1 COUPLING FWD SPLINES. REPLACED WITH SERVICEABLE PART.

Part: GEARSHAFT — STEPWEAR (SPUR ADAPTER)

ENGINE REMOVED DUE TO TURBINE CYCLES. UPON INSPECTION OF COMPRESSOR PARTS NOTED THE FOLLOWING: STEP WEAR BEYOND OVERHAUL LIMITS ON AFT SPLINES. REPLACED WITH SERVICEABLE PART.

Part: INDICATOR — DEFECTIVE (COCKPIT RADAR)

INDICATOR INTERMITTENT UNSTABLE PICTURE. UNIT HAS BAD CRT, BAD REFRESH MEMORY BOARD AND BAD VIDEO BOARD.

Part: VALVE — DEFECTIVE (BLEED SOV)

BLEED AIR ADVISORY LIGHT COMES ON WITH #1 ENGINE RUNNING AND #2 SHUTDOWN. VALVE LEAKING.

Part: ELT — DEFECTIVE (COCKPIT)

ELT STAYS ACTIVATED.

Part: ACTUATOR — DEFECTIVE (AFCS)

#1 ROLL CHATTERS. INSPECTED BY ACCESSORY OVERHAUL SHOP AND FOUND TEST POINT E.4 OUT OF CALIBRATION.

Part: VALVE — INOPERATIVE (BLEED SOV)

BLEED SOV SOLENOID INOPERATIVE.

Part: SENSOR — STICKING (CABIN TEMP)

SENSOR STICKING AND DOES NOT REGULATE TEMPERATURE.

Part: TIP CAP — CRACKED (M/R)

BLADE CRACK WITH MULTIPLE BRANCHES ON THE LEADING EDGE ABRASION STRIP.

Part: GEARSHAFT — STEPWEAR (SPUR ADAPTER)

ENGINE REMOVED DUE TO CRACKED SCROLL. UPON INSPECTION OF COMPRESSOR PARTS NOTED THE FOLLOWING: STEP WEAR BEYOND LIMITS ON SPUR ADAPTER GEARSHAFT FORWARD & AFT SPLINES. NEW PART INSTALLED.

Part: DAMPER — WORN (M/R)

M/R DAMPER HAS WEAR GROOVE ON INNER CYLINDER WALL.

Part: GEARSHAFT — STEP WEAR (SPUR ADAPTER)

ENGINE REMOVED DUE TO TURBINE OVERHAUL AND COMPRESSOR N1 SHAFTING INSPECTION. UPON INSPECTION OF COMPRESSOR PARTS NOTED THE FOLLOWING: STEP WEAR BEYOND LIMITS ON SPUR ADAPTER GEARSHAFT FORWARD AND AFT SPLINES. INSTALLED NEW SPUR ADAPTER GEARSHAFT.

Part: LORAN — INTERMITTENT (COCKPIT)

INTERMITTENT OPERATION.