N22608

Part: BATTERY — WILL NOT TEST (MASTER) · airframe 22,489 hrs

MASTER BATTERY WON'T TEST PROPERLY.

Part: STARTER GEN — FAILED (ENGINE) · airframe 22,472 hrs

STARTER GEN WILL NOT TURN OVER. SHOP REPAIR.

Part: BLADE — SEPARATED (MAIN ROTOR) · airframe 22,428 hrs

UPPER TRAILING EDGE FRETTING PAD IS SEPARATED. SENT FOR INSPECTION AND REPAIR.

Part: BLADE — CRACKED (MAIN ROTOR) · airframe 22,428 hrs

MAIN ROTOR BLADE FRETTING PAD ON THE LOWER SIDE HAS SOME SEPERATION. FIBERGLASS CRACKED NEAR THE INBOARD TRIM TAB.

Part: VALVE — INOPERATIVE (ENGINE OIL)

PLATE LOOSE. REPLACED WITH SERVICEABLE PART.

Part: TRANSCEIVER — INOPERATIVE (VHF SYSTEM) · airframe 21,798 hrs

TRANSCEIVER INOPERATIVE. REPLACED BAD I309 IC CHIP. REPAIRED. ADJUSTED C/N SQUELCH, CARRIER SQUELCH, MIC GAIN, TRANSMIT COMPRESSOR AND SIDETONE. BENCH CHECK GOOD.

Part: TRANSCEIVER — WEAK (ADF) · airframe 21,633 hrs

ADF TRANSCEIVER WEAK AND UNRELIABLE. REPAIRED.

Part: BLADE — CRACKED (MAIN ROTOR) · airframe 21,920 hrs

MAIN ROTOR BLADE OUTBOARD ABRASION STRIP HAS A CRACK NEAR THE SPLICE AREA.

Part: TRANSCEIVER — NOISY (ADF) · airframe 21,660 hrs

ADF TRANSCEIVER HAS CONTINUOUS NOISE IN BACKGROUND. REPAIRED.

Part: TRANSCEIVER — WEAK (VHF SYSTEM) · airframe 21,536 hrs

TRANSCEIVER WEAK. REMOVED CORROSION FROM CHASSIS. ADJUSTED VCO VOLTAGE AND ALIGNED RECEIVER. REPAIRED WEAK RECEIVER. ADJUSTED MIC GAIN, TRANSMIT COMPRESSOR, POWER OUTBACK AND SIDETONE. BENCH CHECK GOOD.

Part: TRANSPONDER — INOPERATIVE (COCKPIT) · airframe 21,555 hrs

TRANSPONDER WILL NOT COME ON. LOWER CHASSIS CORRODED. CLEANED CORROSION FROM UNIT. REPLACED Q104, Q501, Q502 TRANSISTORS, REPLACED 3 EACH WASHERS AND 3 EACH INSULATORS. BENCH CHECK GOOD.

Part: ARM — STIFF (WINDSHIELD WIPER) · airframe 21,644 hrs

WINDSHIELD WIPER ARM STIFF, SPRING WILL NOT HOLD WIPER ON WINDOW. REPAIRED.

Part: BATTERY PACK — DISCHARGED (MAIN) · airframe 21,660 hrs

MAIN AIRCRAFT BATTERY PACK DEAD. REPAIRED.

Part: BEARING — WORN (DRIVE LINK) · airframe 21,590 hrs

MAIN ROTOR SWASHPLATE DRIVE LINK HAS A WORN BEARING. REPAIRED.

Part: BEARING — WORN (DRIVE LINK) · airframe 21,590 hrs

MAIN ROTOR SWASHPLATE DRIVE LINK HAS A WORN BEARING. REPAIRED.

Part: BATTERY PACK — DISCHARGED (MAIN) · airframe 21,555 hrs

MAIN AIRCRAFT BATTERY PACK WEAK. REPAIRED.

Part: CONTROL BOX — FAILED (GENERATOR) · airframe 21,590 hrs

GENERATOR DROPS OFF LINE INTERMITTENTLY.

Part: TARSYN — MALFUNCTIONED (AUTO FLIGHT) · airframe 21,772 hrs

TARSYN 333 CAUSES YAW CHANNEL TO KICK. REPLACED WITH SERVICEABLE PART.

Part: INDICATOR — MALFUNCTIONED (TRIPLE TACH) · airframe 21,616 hrs

TRIPLE TACH LIGHT INOPERATIVE.

Part: INDICATOR — READS LOW (TRIPLE TACH) · airframe 21,684 hrs

TRIPLE TACH READS 3 PERCENT LOW.

Part: FLOAT — LEAKING (MLG) · airframe 21,644 hrs

EMERGENCY FLOAT BAG LEAKS.

Part: COVER — WORN (MLG) · airframe 21,644 hrs

EMERGENCY FLOAT COVER WORN.

Part: COVER — TORN (MLG) · airframe 21,585 hrs

EMERGENCY FLOAT BAG TORN.

Part: GPS — FAILED (COCKPIT)

GPS LOST MEMORY.

Part: FORCE GRADIENT — BINDING (FLIGHT CONTORLS) · airframe 21,612 hrs

CYCLIC FORCE GRADIENT IS BINDING AND HANGING UP. REPLACED WITH SERVICEABLE PART.

Part: PUMP — MALFUNCTIONED (FUEL BOOST) · airframe 21,668 hrs

LT FUEL BOOST PUMP CAUSES NOISE IN ADF AUDIO.

Part: LIGHT — MALFUNCTIONED (SEARCH LIGHT) · airframe 21,725 hrs

SEARCH LIGHT WILL NOT RETRACT. REPLACED WITH SERVICEABLE PART.

Part: INDICATOR — FAILED (ATTITUDE) · airframe 21,612 hrs

ATTITUDE INDICATOR WILL NOT TURN ON BOTH AXIS.

Part: PLATE — LOOSE (VALVE) · airframe 21,703 hrs

PLATE LOOSE. REPLACED WITH SERVICEABLE PART.

Part: INTERPHONE — MALFUNCTIONED (CABIN) · airframe 21,585 hrs

ADF SELECTOR SWITCH WILL NOT TURN IT'S AUDIO OFF (INTERMITTENTLY). FACEPLATE NEEDS REFURBISH.

Part: CROSSTUBE — CORRODED (MLG) · airframe 21,275 hrs

CROSSTUBE CORRODED BEYOND LIMITS IN SEVERAL AREAS.

Part: VENT — LEAKING (FUEL SYSTEM)

HAD STRONG FUEL ODOR IN COCKPIT. FOUND A SMALL AMOUNT OF FUEL HAD SEEPED THROUGH THE RT EXTERNAL TANK VENT DUE TO HIGH FUEL LEVEL AND THE ATTITUDE OF THE AIRCRAFT.

Part: FUEL CONTROL — FLUCTUATES (ENGINE)

AFTER DEPARTURE, NR 1 ENGINE STARTED TO HAVE N1 FLUCTUATIONS. REPLACED FUEL CONTROL.

Part: EXHAUST STACK — CRACKED (ENGINE)

EXHAUST STACK IS CRACKED AT SEAMS OF DUCT HALVES. REPLACED WITH SERVICEABLE PART.

Part: ACTUATOR — SLOW (STEP)

ACTUATOR MOVES VERY SLOW. TIME SINCE REPAIR 117:05 HOURS.

Part: TRANSCEIVER — MALFUNCTIONED (VHF COMM)

TRANSCEIVER TRANSMITS MUFFLED SIGNAL. TIME SINCE REPAIR 3:15 HOURS.

Part: GPS — FAILED (COCKPIT)

RECEIVER FAILED.

Part: CONTROL UNIT — MALFUNCTIONED (DC SYSTEM)

SHOWS ONLY GENERATOR RESIDUAL VOLTAGE. WILL NOT EXCITE THE GENERATOR FIELD. CAUSES THE AIRCRAFT VOLTMETER TO BE DRIVEN DOWN BELOW ZERO WHEN THE GENERATOR SWITCH IS PLACED IN THE ON POSITION.

Part: TRANSCEIVER — INTERMITTENT (COCKPIT)

TRANSCEIVER HAS INTERMITTENT OPERATION.

Part: TRANSCEIVER — WEAK (COCKPIT)

VERY WEAK AND FOUND WATER IN RADIO.

Part: RECEIVER — MALFUNCTIONED (ADF)

TRANSCEIVER WILL NOT RECEIVE AND POINT TO STATION.

Part: TRANSCEIVER — FAILED (COCKPIT)

TRANSCEIVER WILL NOT TRANSMIT O.D. RECEIVE.

Part: BEARING — WORN (MAIN ROTOR)

LINK ASSEMBLY HAS WORN BEARING. REPLACED WITH SERVICEABLE BEARING.

Part: BEARING — WORN (MAIN ROTOR)

WORN BEARING. REPLACED WITH SERVICEABLE BEARING.

Part: ENCODER — READS HIGH (ALTIMETER)

ENCODER READOUTS ERRATIC AND INDICATES HIGH.

Part: DETECTOR — FAILED (RPM LIMIT)

RPM LIMIT DETECTOR NOT FUNCTIONING.

Part: PROBE — READS HIGH (FUEL SYSTEM)

FUEL PROBE READS HIGH OUT OF TOLERANCE.

Part: INDICATOR — MALFUNCTIONED (FUEL QUANTITY)

INDICATION CONSTANTLY FLUCTUATES 50 POUNDS ON TEST, LEFT TO RIGHT.

Part: PROBE — READS HIGH (FUEL SYSTEM)

FUEL PROBE READS HIGH OUT OF TOLERANCE ON CAP METER.

Part: INDICATOR — READS HIGH (XMSN OIL)

OIL TRANSMITTER INDICATION INTERMITTENTLY STICKS AND READS HIGH.

Part: RECEIVER — MALFUNCTIONED (ADF)

RECEIVER WEAK SCRATCHY 1799 KHZ NOT POINTING CORRECTLY IN ADF.

Part: RECEIVER — INTERMITTENT (COCKPIT)

INTERMITTENT, DISTORTED AUDIO.

Part: RECEIVER — INOPERATIVE (ADF)

BFO INOPERATIVE AND VERY WEAK RECEIVE.

Part: ACTUATOR — INOPERATIVE (STEP)

STEP ACTUATOR INOPERATIVE.

Part: INDICATOR — FAILED (FUEL QTY)

WHEN TRYING TO CALIBRATE INDICATOR, FOUND TO BE OFF AT ZERO USING EMPTY ADJUSTMENT SCREW TO CALIBRATE AT ZERO, NEEDLE PEGGED TO THE RIGHT OF ZERO AND STAYED. CHECKED FULL SIDE, NEEDLE WOULD ONLY GO TO 1000 POUNDS.

Part: COMPUTER — FAILED (AFCS)

AFCS FAILS TEST 35.3 AND 35 ON SST IN YAW.

Part: TRANSCEIVER — MALFUNCTIONED (COCKPIT)

TRANSCEIVER CAUSES ATC TRANSPORTATION REPLY LIGHT TO FLICKER CONSTANTLY.

Part: INDICATOR — FLUCTUATES (COCKPIT)

PRESSURE FLUCTUATES IN-FLIGHT, FUNCTION CHECK BAD, PRESSURE NEEDLE INDICATES HIGH AND FLUCTUATES.

Part: COMPUTER — FAILED (AFCS)

AFCS COMPUTER INTERMITTENT, FAILS TEST 10.2 ON SST.

Part: TARSYN 333 — PRECESSING (3 AXIS)

ADI PRECESSING AND INTERMITTENT FLAG. VG BECOMES INVALID.

Part: COMPUTER — MALFUNCTIONED (AFCS)

AFCS COMPUTER KICKING IN PITCH.

Part: INDICATOR — FAILED (COCKPIT)

NR 1 INDICATOR ON DUAL AMMETER WILL NOT READ.

Part: COMPUTER — FAILED (COCKPIT)

AIR DATA COMPUTER WILL NOT SHOW FUEL BURN AND ON OCCASION POWER CHECK.

Part: INDICATOR — FAILED (COCKPIT)

INDICATOR BALL ROTATES SLOW AND RATCHETS IN CLIMB AND DRIVE.

Part: BLADE — DEFECTIVE (MAIN ROTOR)

CANNOT TRACK OR BALANCE. SUSPECT WATER IN THE BLADE CORE.

Part: INDICATOR — INOPERATIVE (COCKPIT)

ENGINE OIL PRESSURE INDICATOR INOPERATIVE. PRESSURE SIDE ONLY.

Part: LORAN — FAILED (COCKPIT)

LORAN HAS NO RELAY AND CODING PULSES BAD.

Part: CONTROL UNIT — FAULTY (NR 1 GENERATOR)

KICKS OFF LINE AND POSITIVE TACK DISTORTED.

Part: DETECTOR — FAILED (RPM LIMIT)

NR 2 ENGINE RPM LIMIT OUT LIGHT REMAINS ON WITH ENGINE ON LINE.

Part: ACTUATOR — FAILED (DROOP COMP)

DROOP COMP INTERNAL STOPS SEEMS BROKEN. MOTOR INTERMITTENT.

Part: INDICATOR — FAILED (COCKPIT)

TO-FROM FLAG WILL NOT PULL.

Part: SELECTOR — READS HIGH (FUEL QTY)

FUEL QUANTITY SELECTOR CAPACITANCE READS HIGH OUT OF TOLERANCE.

Part: TRANSMITTER — MALFUNCTIONED (FLUX VALVE)

FLUX VALVE FREQUENCY BETWEEN F AND B AND F AND C IS HIGH ON TRANSMITTER.

Part: CONTROLLER — FAILED (AUTOFLIGHT)

HP AND CPL SWITCHES WILL NOT ENGAGE ON CONTROLLER.

Part: INDICATOR — STICKING (ENGINE N1)

GAUGE STICKS AND DROPS TO ZERO, UNIT FUNCTION CHECKED BAD, UNIT HAS NO NEEDLE MOVEMENT.

Part: CONTROLER — INOPERATIVE (AUTOPILOT)

HP AND CPL SWITCHES WILL NOT ENGAGE.

Part: INDICATOR — FAULTY (COCKPIT)

FUEL QUANTITY INDICATOR ERRATIC.

Part: BLADE — FAULTY (MAIN ROTOR)

MAIN ROTOR BLADE WILL NOT TRACK.

Part: BLADE — FAULTY (MAIN ROTOR)

MAIN ROTOR BLADE WILL NOT TRACK.

Part: GYRO — MALFUNCTIONED (COCKPIT)

INCORRECT DEGREE OF TILT FOR 412 INSTRUMENT PANEL, NEEDS BENCH CHECK. BENCH CHECK GOOD.

Part: INDICATOR — FAILED (OIL PRESS)

ENG OIL TEMP/PRESS PSI NEEDLE FLUCTUATES WHEN VIBRATED.

Part: CONTROL UNIT — FAILED (DC SYS)

CONTROL UNIT WOULD NOT ALLOW NR1 GENERATOR TO COME ON LINE.

Part: CVR — FAILED (COCKPIT)

CVR CAUSES THE "TEST" LIGHT TO STAY ILLUMINATED CONSTANTLY.

Part: SMOKE DETECTOR — FAILED (FUSELAGE)

SMOKE DET FAILS FUNCTION TEST.

Part: DIGITAL CLOCK — FAILED (COCKPIT)

CLOCK GOES OFF AND ON.

Part: LINEAR ACTUATOR — BROKEN (M/R)

LINEAR ACTUATOR TERMINAL STUD IS BROKEN.

Part: TRACK — MISMANUFACTURED (RT DOOR)

REMOVE AND REPLACE MISMANUFACTURED UPPER R/H DOOR TRACK ON AIRFRAME FWD SECTION.

Part: SELECTOR — FAILED (FUEL QTY)

CAPACITANCE LOW OUT OF TOLERANCE.

Part: DUAL AMMETER — FAILED (COCKPIT)

NR2 NEEDLE WILL NOT INDICATE.

Part: INDICATOR — STICKS (AIRSPEED)

AIRSPEED NEEDLE STICKS AND HAS ERRATIC OPERATION.

Part: INDICATOR — FAILED (HYD SYS)

HYD SYS TEMP. NEEDLE STICKS. PAINT RANGE MARKING.

Part: INDICATOR — ERROR (TRIPLE TACH)

10 ERROR SPLIT EXCESSIVE FRICTION ERROR.

Part: RIB — DAMAGED (T/B FIN)

TAIL BOOM FIN RIB HAS SANDING MARKS BEYOND 10 PERCENT OF METAL.

Part: INDICATOR — DEFECTIVE (COCKPIT)

RATE OF CLIMB INDICATOR. INSPECT FOR POSSIBLE WATER DAMAGE. COMPLY WITH ASB 214ST-97-79, PART 2.

Part: DUCT ASSY — CRTACKED (LT EXH)

EJECTORS ARE CRACKED.

Part: DUCT ASSY — CRACKED (RT EXH)

EJECTORS ARE CRACKED.

Part: SKIN — MIS MFG (FUSELAGE)

SKIN WAS NOT MANUFACTURED WIDE ENOUGH FOR PROPER EDGE DISTANCE ON RIVETS. APPROXIMATELY 1/4" SHORTER THAN ORIGINAL SKIN.

Part: FLOAT — BURST (FUSELAGE)

FLOAT BAG BUSTED.

Part: TRANSMITTER — DEFECTIVE (ENG TORQ)

TORQUE READING LOW. COULD NOT ADJUST. SENT TO OTTO'S INSTRUMENT SERVICE, INC. FOR INSPECTION AND REPAIR.

Part: TRANSCEIVER — INOPERATIVE (COCKPIT)

TRANSCEIVER INOPERATIVE.

Part: CVR — MALFUNCTION (COCKPIT)

CVR VERY WEAK, ON PILOT'S SIDE NO TEST LIGHT.

Part: DUCT ASSY — CRACKED (RT EXH)

DUCT ASSY CRACKED.

Part: ACTUATOR — STICKING (M/R CONTROL)

ROTARY ACTUATOR STICKING INTERMITTENTLY.

Part: ACTUATOR — FAILED (STEP)

ACTUATOR WOULD NOT RETRACT

Part: ACTUATOR — FAILED (STEP)

ACTUATOR WOULD NOT RETRACT. SENT FOR INSPECTION AND REPAIR.

Part: CROSSTUBE — UNBONDED (WEAR PAD FWD)

CROSSTUBE HAS WEAR ON PADS AND UNBONDED.

Part: TRANSCEIVER — INTERMITTENT (COCKPIT)

TRANSCEIVER INTERMITTENT OPERATION.

Part: TRANSCEIVER — FAILED (DME)

NO DME INDICATIONS ON CONTROL HEAD.

Part: CASE ASSY — CORRODED (MT LUGS)

POSSIBLE REPAIR DUE TO CORROSION AT MOUNTING LUGS.

Part: ACTUATOR ROTARY — FAILED (M/R CONTROL)

ACTUATOR WOULD NOT MOVE ON GROUND TEST.

Part: COMBINING GRBOX — MAKING METAL (ENGINE)

CONTAMINATION ON GEARBOX CHIP PLUG AND FILTER.

Part: INDICATOR — STICKS (COCKPIT VOLTS)

NEEDLE ON AIRCRAFT SIDE INTERMITTENTLY STICKS.

Part: TARSYN — PRECESSES (AUTO FLIGHT)

TARSYN PRECESSES EXCESSIVELY.

Part: 7000 RCU — DEFECTIVE (COCKPIT LORAN)

COMES UP CODE 5. ADVISORY LIGHT STAYS ON.

Part: 7000 RCU — FAIL SELF TEST (LORAN)

7000 RCU WILL NOT GO THROUGH SELF TEST. SHOWS OSCILLATOR ERROR.

Part: ANTENNA — DEFECTIVE (LORAN ANTENNA)

TROUBLESHOOTING LORAN ADVISORY LIGHT STAYING ON.

Part: BLADE — CRACKED (M/R)

BLADE IS CRACKED. (CRACK IN THE UPPER SKIN AT STATION 83.5" RUNNING IN A 45 DEGREE DIRECTION.

Part: INVERTER — MALFUNCTION (AC SYS)

FUEL QUANTITY FLUCTUATES. TIME SINCE REPAIR 214:55.

Part: 7000 RCU — INOPERATIVE (COCKPIT LORAN)

UNIT WENT OFF LINE. LOST ALL LIGHTS ON CDU.

Part: TRANSPONDER — INTERMITTENT (COCKPIT)

TRANSPONDER INTERMITTENTLY INOPERATIVE.

Part: 7000 CDU — FAILED (COCKPIT LORAN)

UNIT WENT OFF LINE. LOST ALL LIGHTS ON CDU AND PUSHBUTTON SWITCHES UNREADABLE.

Part: INVERTER — TRIPS BREAKER (AC SYS)

POPS CIRCUIT BREAKER.

Part: RECEIVER — INOPERATIVE (COCKPIT ADF)

ADF IS INOPERATIVE.

Part: LORAN — DEFECTIVE (COCKPIT)

LOCKS UP AND DISPLAYS WARNING CODES.

Part: LORAN — DEFECTIVE (LORAN CDU)

SEVERAL LED'S ARE INOPERATIVE.

Part: ANTENNA — DEFECTIVE (LORAN)

LORAN SLOW TO ACQUIRE STATIONS AND GIVE READOUTS.

Part: LORAN — DEFECTIVE (COCKPIT)

ADVISORY LIGHT STAYS ON AT ALL TIMES.

Part: LORAN — DEFECTIVE (COCKPIT)

CDU BLANKS OUT ON BRG/DIST. SELECTION - GIVES NO DATA.

Part: VALVE — DEFECTIVE

VALVE FLUTTERING; CAUSES ENGINE ITT TO FLUCTUATE WITH HEATER TURNED OFF.

Part: EJECTOR ASSY — CRACKED (RT EXH)

EJECTOR IS CRACKED AND HAS BROKEN RIVETS.

Part: ALTIMETER — READS HIGH (COCKPIT)

ALTIMETER READS 500 FEET HIGH.

Part: INDICATOR — STICKS (TRIPLE TACH)

TRIPLE TACH NEEDLE STICKS AND EXCESSIVE NEEDLE SPLIT.

Part: INDICATOR — NEEDLE SPLIT (TRIPLE TACH)

#1 AND #2 NEEDLES HAVE A 3% SPLIT. SENT TO AIR DALLAS INSTRUMENTS FOR WARRANTY REPAIR. TIME SINCE REPAIR 17:00.

Part: SWITCH — DEFECTIVE (FUEL INDICATION)

SWITCH PIN D NOT GROUNDED TO CASE. CAUSES INDICATOR TO FLUCTUATE.

Part: EJECTOR ASSY — CRACKED (RT EXHAUST)

EJECTOR ASSY EXCESSIVE INTERFERENCE WITH EXHAUST STACK.

Part: MOTOR — DEFECTIVE (WIPER)

WHEN MOUNTED IN AIRFRAME WIPER MOTOR VIBRATES. COMING LOOSE FROM CONVERTER.

Part: RECEIVER — DEFECTIVE (COCKPIT ADF)

BANDS IN HIGHER FREQUENCY INOPERATIVE. SENT TO THE RADIO SHOP FOR INSPECTION AND REPAIR.

Part: YAW CONTROL — DEFECTIVE (T/R CONTROL)

YAW ACTUATOR DEFLECTS LEFT, WILL NOT ENTER.

Part: LORAN — LIGHTS INOP (COCKPIT)

4 LED LIGHTS INOPERATIVE.

Part: CONE LWR — WORN (M/R HUB)

BONDED FABRIC MATERIAL GALLED AND WORN.

Part: INDICATOR — DEFECTIVE (TRIPLE TACH)

NEEDLES SPLIT, #1 AND #2 NEEDLES.

Part: CVR — WONT TEST (COCKPIT)

CVR UNIT WILL NOT TEST IN PILOT OR COPILOT POSITION.

Part: MOTOR ASSY — INOPERATIVE (STEP)

INSPECTED BY ACCESSORY SHOP AND FOUND MOTOR INOPERATIVE.

Part: TRANSCEIVER — FAILED TEST (RADIO ALT)

FAILED OUTPUT TEST 5.2 ON SST.

Part: INDICATOR — STICKS (COCKPIT ITT)

NEEDLE INTERMITTENTY STICKS WHEN POWER IS APPLIED. TIME SINCE REPAIR 573:50.

Part: FITTING — CRACKED (FUSELAGE)

FITING CRACKED AT CENTER INBOARD EDGE AT RIVET HOLE OF ADEL WITH NO EDGE DISTANCE. REMOVED AND REPLACED FITTING AND SHIMS AS NEEDED. SUBMITTER SUGGESTS SHIM PROPERLY, ALLOW FOR PROPER EDGE DISTANCE, AND DEBURR ALL HOLES.

Part: TRANSDUCER — DEFECTIVE (YAW CHANNEL)

PEDALS WOULD NOT RESPOND TO NORMAL INPUT. FOUND YAW CHANNEL CONTROL MOTION TRANSDUCER STICKING. CLEANED AND LUBED. FIGURE 67-15, ITEM 45.

Part: INDICATOR — TRIPS BREAKER (NR 2 TORQUE)

#2 SIDE POPS CIRCUIT BREAKER.

Part: CONNECTOR — SHORTED (NR 2 ENG CHIP)

#2 ENGINE CHIP LIGHT IN FLIGHT. FOUND PINS IN CONNECTOR SHORTED. REPLACED CONNECTOR AND RETURNED TO SERVICE.

Part: LORAN — DEFECTIVE (COCKPIT)

PARTIAL LIGHT SEGMENT IN DISPLAY.