N911MJ

Part: ENGINE — OVERTEMP (NR 1) · airframe 14,127 hrs

ENGINE NR 1 OIL TEMP INDICATION ROSE AND REMAINED ABOVE RED LINE, EMERGENCY PROCEDURE PERFORMED OVER NEXT 5-10 MINUTES, AS ENGINE LEVER WAS RETARDED TO IDLE MOMENTARILY BEFORE SHUTTING DOWN, THE ENGINE NR 1 OIL PRESS LIGHT ILLUMINATED, ENGINE WAS SHUT DOWN AND AIRCRAFT DIVERTED TO MORGAN CITY PHI. REPLACED ENGINE ASSY - SUSPECT ENGINE OIL PUMP FAILURE.

Part: GENERATOR — MALFUNCTIONED (NR 1) · airframe 13,824 hrs

ON CLIMB OUT, NR 1 GEN LIGHT ILLUMINATED. FOLLOWED EMERGENCY CHECKLIST, ATTEMPTED TO RESET, WOULD NOT RESET. TURNED NR 1 GEN SWITCH OFF. LANDED, MAINTENANCE REPLACED NR 1 GENERATOR.

Part: FIRE DETECTOR — MALFUNCTIONED (NR 1 ENGINE) · airframe 13,597 hrs

NR 1 ENGINE FIRE LIGHT ON IN FLIGHT. REPLACED FLAME DETECTOR WITH PART NR 473205-01 SERIAL NR 2851.

Part: BRAKE — MALFUNCTIONED (AUTOFLIGHT) · airframe 11,862 hrs

FORE AND AFT CYCLIC STIFF AND RATCHETY.

Part: MOTOR — FAILED (COMPRESSOR) · airframe 11,862 hrs

AIR CONDITIONER DOES NOT COOL. REPLACED COMPRESSOR MOTOR WITH A SERVICEABLE MOTOR - BRUSHES BURNED.

Part: A/C PACK — ODOR · airframe 11,862 hrs

LOAD SHED BOX HAS BURNED ODOR WHEN COVER REMOVED - AIR CONDITIONER INOPERATIVE. SHOP REPAIR.

Part: INTERPHONE — MALFUNCTIONED (CABIN) · airframe 11,790 hrs

CAUSING STATIC IN CABIN ICS. SHOP REPAIR.

Part: MIXER BOX — INOPERATIVE (COCKPIT) · airframe 11,790 hrs

MIXER BOX CAUSING STATIC IN CABIN ICS. FOUND VOLUME KNOB, SELECTOR KNOB AND LIGHT PANEL BAD. REPLACED. BENCH CHECK GOOD.

Part: CONNECTOR — DAMAGED (VALVE ASSY)

ENGINE VALVE CONNECTOR DAMAGED. REPLACED CONNECTOR V5032-135 DUE TO DAMAGED. REPAIRED.

Part: INTERPHONE — WEAK (COCKPIT) · airframe 11,698 hrs

CAUSING STATIC IN PILOTS HEADSET. FOUND UNIT TO HAVE VERY WEAK AND NOISY TRANSMIT AUDIO. CLEANED S1 SWITCH. REPLACED C30 AND C31 CAPACITORS. REPLACED Q8 AND Q10 TRANSISTORS. STRAIGHTENED BENT TERMINAL ON S1 TRANSMIT SELECTOR SWITCH AND RESOLDERED WIRE TO TERMINAL. REPAIRED. BENCH CHECK GOOD.

Part: GYRO — MALFUNCTIONED (COCKPIT) · airframe 11,726 hrs

GYRO INTERMITTENTLY CAUSES ADI TO ERECT TO 45 DEGREE BANK AND ALSO INTERMITTENTLY CAUSES ADI TO TUMBLE. SENT TO B.F. GOODRICH AEROSPACE FOR WARRANTY REPAIR.

Part: ACTUATOR — CHATTERING (AFCS) · airframe 11,736 hrs

AFCS ACTUATOR CHATTERS CONTINUOUSLY WITH CHANNEL ON. INSPECTED BY ACCESSORY SHOP AND FOUND UNIT TO CHATTER WHEN TESTED AND POTENTIOMETERS OUT ON STRIP CHART. SENT TO HELICOPTER SUPPORT, INC. FOR INSPECTION AND REPAIR.

Part: GYRO — MALFUNCTIONED (VERTICAL) · airframe 11,620 hrs

NR 1 PITCH AND ROLL ACTUATORS KICKING IN FLIGHT. REPLACED VERT GYRO.

Part: INDICATOR — MALFUNCTIONED (ADI) · airframe 11,618 hrs

COPILOT ADI WILL NOT ERECT PROPERLY. SENT TO MASCO FOR INSPECTION AND REPAIR.

Part: FIRE DETECTOR — WILL NOT TEST · airframe 11,613 hrs

FIRE DETECTOR WILL NOT TEST PROPERLY.

Part: INTERPHONE — MALFUNCTIONED (COCKPIT) · airframe 11,494 hrs

CAUSING INTERMITTENT ICS COMMUNICATIONS. FOUND SWITCH S1 NOISY, THREE BULBS IN LIGHT PANEL, VOLUME AND SELECTOR KNOBS BAD. CLEANED SWITCH, REPLACED BULBS AND VOLUME AND SELECTOR KNOBS. BENCH CHECK GOOD.

Part: TRANSMITTER — READS HIGH (OIL PRESSURE) · airframe 11,578 hrs

NR 2 ENGINE OIL PRESSURE INDICATES ABOVE RED LINE ABOVE IDLE. FOUND PRESSURE TRANSMITTER INDICATING ABOVE 160 PSI WITH DEAD WEIGHT TESTER AT 130 PSI. SCRAPPED TRANSMITTER.

Part: INTERPHONE — MALFUNCTIONED (COCKPIT) · airframe 11,575 hrs

CAUSES BLEED OVER FROM AFT CABIN ICS TO PILOT AND COPILOT STATIONS. IN SHOP REPAIR.

Part: GYRO — MALFUNCTIONED (COCKPIT) · airframe 11,596 hrs

VERTICAL GYRO KICKING IN THE NR 1 PITCH AFCS CHANNEL.

Part: INDICATOR — READS HIGH (ALTIMETER) · airframe 11,534 hrs

COPILOT ALTIMETER INDICATES 110 FEET AT SEA LEVEL. TO BE SENT TO VENDOR FOR REPAIR.

Part: SEARCH LIGHT — MALFUNCTIONED (EXTERIOR) · airframe 11,536 hrs

SEARCH LIGHT WILL NOT STOW FULLY AND CONTINUES TO MOTOR WHEN SET TO SLOW. IN SHOP REPAIR.

Part: BEARING — LOOSE (M/R DAMPER) · airframe 11,534 hrs

MAIN ROTOR DAMPER BEARING LOOSE IN ROD END BORE. REPAIRED.

Part: HEATER — INOPERATIVE (FIREWALL) · airframe 11,509 hrs

FIREWALL HEATER IS INOPERATIVE DUE TO ONE TEMP SENSOR SHOWING AN OPEN LEAD CONDITION.

Part: BEARING — RATCHETING (IDLER OUTPUT)

FLIGHT CONTROL IDLER OUTPUT HAS RATCHETY BEARINGS. REPAIRED.

Part: ANTENNA — CRACKED (COMM SYS) · airframe 11,494 hrs

COMMUNICATIONS ANTENNA CRACKED. SCRAPPED.

Part: BEARING — RATCHETING (LINK ASSY)

LINK ASSY HAS RATCHETY BEARINGS. REPAIRED.

Part: INTERPHONE — DAMAGED (CABIN) · airframe 11,494 hrs

KNOB CRACKED. FOUND AMP BOARD AR2, SWITCH S1, SELECTOR KNOB AND VOLUME KNOB BAD. REPLACED SAME. REPAIRED. BENCH CHECK GOOD.

Part: SWITCH — STICKING (CENTRAL WARNING) · airframe 11,509 hrs

INTERNAL SWITCH CONTACTS STICKING CAUSING NR 2 ENGINE ANTI ICE CAUTION LIGHT TO STAY ON CONSTANTLY. PENDING VENDOR REPAIR.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 11,493 hrs

WINDSHIELD IS CRACKED.

Part: BLADE — SEPARATED (MAIN ROTOR) · airframe 11,494 hrs

MAIN ROTOR BLADE HAS THE SPLICE REPAIR NEAR STA 173 HAS SOME SEPARATION.

Part: WINDOW — MISMANUFACTURED (COCKPIT) · airframe 11,493 hrs

WINDOW HAS PRE-DRILLED MOUNTING HOLES THAT ARE 1/2 HOLE SIZE OFF.

Part: BRUSHES — WORN (STARTER GEN)

STARTER GEN HAS WORN BRUSHES. REPAIRED AND RETURNED TO SERVICE.

Part: PICKUP — INTERMITTENT (TRIPLE TACH) · airframe 11,102 hrs

TRIPLE TACH PICKUP SENSOR IS INTERMITTENTLY INOPERATIVE. SCRAPPED AND REPLACED WITH SERVICEABLE PART.

Part: ACTUATOR — LEAKING (VTA) · airframe 11,447 hrs

DURING LEAK CHECK AFTER INSTALLATION OF VTA ACTUATOR RECEIVED FROM STOCK FOUND ACTUATOR TO BE LEAKING.

Part: TURBINE WHEEL — DAMAGED (ENGINE) · airframe 11,447 hrs

ENGINE REMOVED DUE TO CRACKED NR 1 NOZZLE. UPON INSPECTION OF TURBINE PARTS NOTED SLIGHT SULFIDATION ON ALL 1ST STAGE TURBINE WHEEL BLADES AND 1ST STAGE TIP DRAG WITH 2ND STAGE NOZZLE. SCRAPPED.

Part: COVER — CRACKED (EXHAUST) · airframe 11,458 hrs

EXHAUST COVER CRACKED. REPLACED WITH SERVICEABLE PART.

Part: DISPLAY — MALFUNCTIONED (RADAR SYS) · airframe 11,445 hrs

RADAR INDICATOR DISPLAY IS DIM AT MAXIMUM INTENSITY. REPLACED WITH SERVICEABLE PART.

Part: RELAY — STUCK (DC SYSTEM) · airframe 11,094 hrs

RELAY CONTACTS SERVICING PINS 21, 22 AND 23 ARE STUCK IN THE ENERGIZED POSITION.

Part: BLADE — DAMAGED (TAIL ROTOR) · airframe 10,868 hrs

TAIL ROTOR BLADE PADDLE "B" HAS A HOLE IN THE TIP CAP.

Part: HARNESS — FAILED (MLG) · airframe 11,120 hrs

MLG WIRE HARNESS FAILED CONTINUITY CHECK. SCRAPPED.

Part: ACTUATOR — INOPERATIVE (AFCS) · airframe 11,265 hrs

NR 1 YAW ACTUATOR NOT RESPONDING ON SYSTEM CHECK.

Part: TIP CAP — MISMANUFACTURED (M/R BLADES) · airframe 11,111 hrs

TIP CAP ON MAIN ROTOR BLADES HAVE LARGE SCREW HOLES ON BOTTOM SIDE MISMATCHED ANYWHERE FROM 1/4 INCH HOLE TO 1/2 INCH HOLE. REPLACED WITH SERVICEABLE PART.

Part: ACTUATOR — INTERMITTENT (AFCS) · airframe 11,208 hrs

NR 2 PITCH CHANNEL KICKING INTERMITTENTLY IN FLIGHT.

Part: CONTROL UNIT — INOPERATIVE (DC SYSTEM) · airframe 11,094 hrs

DC CONTROL UNIT CAUSED GENERATOR SYSTEM TO BE INOPERATIVE.

Part: CONTROL UNIT — INOPERATIVE (DC SYSTEM) · airframe 11,094 hrs

DC CONTROL UNIT CAUSED GENERATOR SYSTEM TO BE INOPERATIVE.

Part: RELAY — FROZEN (ELECTRICAL) · airframe 11,094 hrs

SUSPECTED NOT LATCHING PROPERLY AND STUD AT POSITION 21 FROZEN IN PLACE. SCRAPPED.

Part: TIP CAP — DAMAGED (M/R BLADE) · airframe 11,006 hrs

MAIN ROTOR BLADE TIP CAP LEADING EDGE ABRASION STRIP SEPARATED AND BOTH INTERNAL DOUBLER.

Part: CONTROL UNIT — INOPERATIVE (DC SYSTEM) · airframe 11,094 hrs

DC CONTROL UNIT CAUSED GENERATOR SYSTEM TO BE INOPERATIVE.

Part: BLADE — CRACKED (MAIN ROTOR) · airframe 11,356 hrs

BLADE SKIN CRACKED ON LOWER SURFACE NEAR THE TIP OF TIP RIB.

Part: INDICATOR — READS HIGH (COCKPIT) · airframe 11,371 hrs

INDICATOR READS 100 - 150 DEGREES HIGH THROUGHOUT ITS OPERATIONAL RANGE.

Part: BUSHING — LOOSE (FRICTION LEVER) · airframe 11,349 hrs

ROLL FRICTION ASSEMBLY LEVERS WORN AND BUSHINGS LOOSE. SCRAPPED AND REPLACED WITH SERVICEABLE LEVER.

Part: LIGHT — INTERMITTENT (TRIPLE TACH) · airframe 11,356 hrs

PILOT TRIPLE TACH INSTRUMENT LIGHT INTERMITTENT. REPLACED WITH SERVICEABLE PART.

Part: BLADE — MISMANUFACTURED (MAIN ROTOR) · airframe 11,111 hrs

UNABLE TO INSTALL TIP CAPS - TWO DIFFERENT TIP CAPS. TIP CAP BLOCK HOLES APPEAR TO BE DRILLED 1/8 INCH TOO FAR FORWARD WHEN AFT SCREWS INSERTED.

Part: BLADE — DAMAGED (MAIN ROTOR) · airframe 11,111 hrs

TRAILING EDGE DAMAGE AT AREA OF P/N - S/N STENCIL. REPLACED WITH SERVICEABLE BLADE.

Part: BLADE — CRACKED (MAIN ROTOR) · airframe 11,111 hrs

TRAILING EDGE CRACKED JUST INBOARD OF TRIM TAB. REPLACED WITH SERVICEABLE BLADE.

Part: POWERPACK — CRACKED (SERVO SYSTEM) · airframe 11,111 hrs

POWER PACK HOUSING CRACKED AT DRAIN FITTING. PENDING VENDOR REPAIR.

Part: TRANSMISSION — MAKING METAL (MAIN ROTOR) · airframe 11,111 hrs

CHIP LIGHT ON LANDING. INSPECTED AND FOUND A 1/2" BY 3/16" PIECE OF A GEAR TOOTH ON THE LEFT CHIP PLUG. REPLACED WITH SERVICEABLE ASSEMBLY.

Part: ALTIMETER — ERRATIC (COCKPIT) · airframe 11,097 hrs

RT WAS CAUSING ERRATIC READING ON APPROACH. REPLACED WITH SERVICEABLE PART.

Part: CALIPER — LEAKING (ROTOR BRAKE) · airframe 11,090 hrs

CALIPER LEAKING. REPLACED WITH SERVICEABLE PART.

Part: CALIPER — LEAKING (ROTOR BRAKE) · airframe 11,090 hrs

CALIPER LEAKING. REPLACED WITH SERVICEABLE PART.

Part: FLOAT — WILL NOT TEST (MLG) · airframe 11,070 hrs

FAILED INFLATION TEST. PENDING VENDOR REPAIR.

Part: ANTENNA — DAMAGED (VHF) · airframe 10,798 hrs

REPORTED TO TRANSMIT GARBLED. SCRAPPED AND REPLACED WITH SERVICEABLE UNIT.

Part: TRANSCEIVER — WEAK (COCKPIT)

TRANSCEIVER HAD WEAK TRANSMIT.

Part: INDICATOR — MALFUNCTIONED (HSI)

VOR INVALID LIGHT STAYS ON AND VOR NEEDLE DOES NOT PAINT TO STATIONS. GOOD I.D. TONE.

Part: TRANSCEIVER — INTERMITTENT (COMMUNICATIONS)

ALL LED DIGITS OUT. INTERMITTENT ONE LOWER SEGMENT OF THIRD DIGIT OUT ALL THE TIME.

Part: INDICATOR — STUCK (FUEL QUANTITY)

NR 1 NEEDLE STICKS AT ZERO INTERMITTENTLY ON FUEL QUANTITY INDICATOR.

Part: INDICATOR — STUCK (FUEL QUANTITY)

NR 1 NEEDLE STUCK AT ZERO ON FUEL QUANTITY INDICATOR.

Part: RELAY — SHORTED (FLT COMPARTMENT)

RELAY HAS OPEN CONNECTION BETWEEN B3 AND B2.

Part: PUMP — MAKING METAL (SCAVENGER)

ENGINE REMOVED DUE TO SUSPECTED SCAVENGE PUMP FAILURE. OIL PUMP SCAVENGE BODY HAD EXCESSIVELY WORN GEAR WALLS. O-RINGS WERE FLAT AND HARD, OIL PUMP GEARSHAFTS HAVE EXCESSIVE GROOVES AND WEAR CONTRIBUTING TO POOR SCAVENGE. PART SCRAPPED.

Part: GYRO — MALFUNCTIONED (COCKPIT)

VERTICAL GYRO FALLS OFF TO A 30 DEGREE BANK SOMETIMES.

Part: PUMP — LEAKING (HYDRAULIC SYS)

SEAL DRAIN LEAKING AT HYDRAULIC PUMP.

Part: GENERATOR — MALFUNCTIONED (AC SYSTEM)

A/C GENERATOR HAD BEARING LIGHT ON INDICATOR PANEL.

Part: RELAY — INTERMITTENT (FLT COMPARTMENT)

RELAY INTERMITTENT.

Part: FUEL PUMP — WORN (ENGINE)

FUEL PUMP HAS WORN SPLINES ON DRIVE SHAFT.

Part: RECEIVER — FAILED (COCKPIT)

NO AUDIO, NO LIGHTS. PERFORMED PRELIMINARY INSPECTION, FOUND UNIT TO HAVE INTERMITTENT AUDIO AND NO LIGHTS.

Part: PUMP — LEAKING (HYDRAULIC SYSTEM)

NR 1 HYDRAULIC SYSTEM LOW LEVEL LIGHT ILLUMINATED IN-FLIGHT. RETURNED TO BASE AND LANDED WITHOUT INCIDENT. SYSTEM HAD LOST FLUID THROUGH NR 1 HYDRAULIC PUMP SEAL DRAIN. MAINTENANCE REPLACED HYDRAULIC PUMP. REF: S-76 IPC, CHAPTER 29-10-01, FIGURE 1, ITEM 12.

Part: SWITCH — MALFUNCTIONED (COCKPIT)

BLEED CAUTION LIGHT INTERMITTENTLY COMES ON.

Part: INDICATOR — FAILED (COCKPIT)

RATE OF CLIMB INDICATOR CANNOT CALIBRATE TO ZERO.

Part: ENGINE — FAILED (NR 2)

IN-FLIGHT, NR 2 ENGINE OIL PRESSURE DROPPED WITH OIL PRESSURE LIGHT ILLUMINATION. PILOT SECURED ENGINE AND MADE UNEVENTFUL SINGLE ENGINE LANDING. MAINTENANCE FOUND 3 QUARTS OF OIL CONSUMPTION AFTER REPLENISHING OIL. SEVEN MINUTES INTO PENALTY RUN, OIL CONSUMPTION WAS AGAIN 3 QUARTS LOW. REMOVED ENGINE ASSEMBLY.

Part: ENGINE — FAILED (NR 2)

IN-FLIGHT, NR 2 ENGINE OIL PRESSURE DROPPED WITH OIL PRESSURE LIGHT ILLUMINATION. PILOT SECURED ENGINE AND MADE UNEVENTFUL SINGLE ENGINE LANDING. MAINTENANCE FOUND 3 QUARTS OIL CONSUMPTION AFTER REPLENISHING OIL. SEVEN MINUTES INTO PENALTY RUN, OIL CONSUMPTION WAS AGAIN 3 QUARTS. REMOVED ENGINE ASSEMBLY.

Part: ENCODER — MALFUNCTIONED (COCKPIT)

NEEDLE STICKS THROUGHOUT SCALE AND ENCODER READS OUT OF TOLERANCE.

Part: COMPENSATOR — CRACKED (COCKPIT HSI)

COMPENSATOR CRACKED.

Part: CONTROL UNIT — MALFUNCTIONED (AC SYSTEM)

AC GENERATOR DROPS OFF LINE WHEN AIR CONDITIONER IS TURNED ON.

Part: RATE GYRO — MALFUNCTIONED (COCKPIT)

NR 1 TEST NO INDICATION ON GYRO.

Part: VERTICAL GYRO — INOPERATIVE (COCKPIT)

ADI INOPERATIVE.

Part: ACTUATOR — CHATTERING (AFCS)

AFCS ACTUATOR CHATTERS EXCESSIVELY.

Part: CAUTION PANEL — MALFUNCTIONED (COCKPIT)

MASTER CAUTION LIGHT WILL NOT ILLUMINATE ON CONTROL PANEL.

Part: TRANSCEIVER — MALFUNCTIONED (COCKPIT)

UPON INSTALLATION, TRANSCEIVER WOULD NOT TEST NOR RECEIVE AUDIO. PERFORMED PRELIMINARY INSPECTION. TROUBLESHOT AND FOUND S4 (SWITCH) BAD. SCRAPPED PART.

Part: MOTOR — INTERMITTENT (BOOST PUMP)

BOOST PUMP MOTOR FUNCTIONS INTERMITTENTLY.

Part: AMPLIFIER — MALFUCNTIONED (ROLL SLICE)

NR 1 ROLL ACTUATOR HARD OVER TO THE LEFT.

Part: AMPLIFIER — MALFUNCTIONED (ROLL SLICE)

AMPLIFIER DRIVES ACTUATOR HARD OFF.

Part: TRANSCEIVER — FAILED (COCKPIT)

NO TRANSMIT OR RECEIVE (400 MHZ RT INOPERATIVE ON FM RADIO) FOUND K1 RELAY CORRODED. SYNTHESIZER BOARD CAUSES NON-LINEAR POWER.

Part: VERTICAL GYRO — FAILED (COCKPIT)

STARTED TUMBLING IN FLIGHT.

Part: DAMPENER — FAILED (COLLECTIVE)

BEARING FILL OUT. COLLECTIVE DAMPER ASSY. WEAK AND RATCHETY.

Part: BATTERY — FAILLED (DC SYS)

BATTERY OFF LIGHT CAME ON IN FLIGHT ON SHORT FINAL. FOUND BATTERY CIRCUIT BREAKER ON MASTER ELECTRICAL BOX POPPED. UNABLE TO RESET BREAKER. WHEN TEMP SENSOR CONNECTOR DISCONNECTED FROM BATTERY CIRCUIT BREAKER STAYS IN. WHEN TEMP SENSOR CONNECTOR CONNECTED TO BATTERY CIRCUIT BREAKER POPS. SECOND OCCURRENCE ON THIS S/N BATTERY. (SAME PROBLEM ON 11-20-97) REPLACED BATTERY WITH A SERVICEABLE BATTERY.

Part: DAMPENER — DEFECTIVE (COLLECTIVE)

THROW OF COLLECTIVE DAMPER NOT SAME AS ONE REMOVED.

Part: EMERGENCY POWER — FAILED (DC SYS)

EMERGENCY POWER BATTERY INTERNAL FAILURE.

Part: TRANSMITTER — FAILED (ENG OIL)

ENG OIL GAUGE WENT TO ZERO.

Part: BLADE — SEPARATION (M/R)

M/R BLADE SEPARATION ON TRIM TAB WHICH IS BEYOND REPAIRS.

Part: BLADE — NICKED (T/R)

NICK ON THE TRAILING EDGE ON PADDLE "A" WHICH IS BEYOND LIMITS.

Part: INDICATOR — INTERMITTENT (OIL PRESS)

OIL PRESSURE INDICATOR OPERATES INTERMITTENTLY AT 50 PSI.

Part: ACUTATOR — FAILED (ENGINE CONTROL)

ACTUATOR SLUGGISH AND FINALLY JAMMED.

Part: COMBUSTION LINER — MIS MFG (ENGINE)

RECEIVING INSPECTION REVEALED LOWER SECTION NINETY DEGREES OFF FROM COMBUSTION LINER TOP SECTION. INSTALLED A STANDARD AERO OVERHAULED COMBUSTION LINER.

Part: ACUTATOR — INTERMITTENT (ENG CONTROL)

ACTUATOR INTERMITTENT OPERATION AND SLOW TO ERECT.

Part: CONVERTER VALVE — LEAKS (VENT VALVE)

CONVERTER VENTS LIQUID OXYGEN OVERBOARD. VENT VALVE LEAKS. TIME SINCE REPAIR 288:40.

Part: ACUTATOR — FROZEN (SERVO SYS)

ACTUATOR IS FROZEN.

Part: BELLCRANK — WRONG PART (LT NOSE DOOR)

BELLCRANK IS MISLABELED. IS ACTUALLY P/N 1944E67-01 FOR L/H NOSE DOOR. REMOVED AND REPLACED SERVICEABLE BELLCRANK.

Part: ALTIMETER — ERRATIC (COCKPIT RAD ALT)

RADAR ALTIMETER ERRATIC AND UNRELIABLE IN FLIGHT.

Part: BLEED VALVE — DEFECTIVE (ENG)

LOW POWER. BLEED VALVE DEFECTIVE.

Part: GYRO — DEFECTIVE (COCKPIT VG NR 2)

#2 ROLL KICKS.

Part: CONTROL PANEL — FAILED (COCKPIT AFCS)

ROLL CHANNEL NOT SHOWING RESPONSE OR INDICATOR PANEL.

Part: BLADE — DEFECTIVE (T/R)

T/R BLADE HAS VOID ON PADDLE "A" NEAR STATION 30. ALSO HAS A HOLE IN THE END CAP.

Part: BLADE — CRACKED (M/R)

BLADE IS CRACKED. (BLADE HAS THE TIP RIB UNBONDED, AND A CRACK AT STATION 112" WITH SEPARATION ON EACH SIDE OF THE CRACK ON THE LEADING EDGE.

Part: TIP CAP — CRACKED (M/R)

CRACK IN THE ABRASION STRIP ON THE LOWER SIDE WITH SEPARATION.

Part: TRANSMITTER — DEFECTIVE (FUEL PRESS)

CAUSING ERONEOUS PRESSURE READINGS.

Part: ACTUATOR — FAILED (AFCS)

AFCS INDICATOR PEGGED TO THE LEFT SIDE.

Part: INDICATOR — DEFECTIVE (COCKPIT ATTITUDE)

INDICATOR SHORTED AND POPS CIRCUIT BREAKER.

Part: INDICATOR — DEFECTIVE (COCKPIT ATTITUDE)

INDICATOR RATCHETS IN ROLL.

Part: CONVERTER — DEFECTIVE (OXY SYS)

VENTING LIQUID AND GAS CONTINUOUSLY FROM VENT UNTIL CONVERTOR EMPTIES.

Part: EJECTOR — CRACKED (EXHAUST)

EXH EJECTOR IS CRACKED.

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 FWD & AFT SPLINES. NEW PART INSTALLED.

Part: AMPLIFIER — KICKS (PITCH SLICE)

#1 PITCH KICK IN FLIGHT.

Part: HYD PUMP — FAILED (HYD SYS)

ON TAKE OFF THE #2 SERVO LIGHT LLUMINATED WITH DROP IN HYDRAULIC PRESSURE. REPLACED HYD PUMP AND RETURNED AIRCRAFT TO SERVICE.

Part: TIP CAP — CRACKED (M/R)

CRACK IN THE ABRASION STRIP WITH SEPARATION.

Part: RECEIVER — DEFECTIVE (COCKPIT)

LOCALIZER AND VOR FAILED INTERMITTENTLY. SLIGHT JIGGLE ON SELECTOR CAUSES VOR AND LOCALIZER TO BE FLAGGED.

Part: PUMP — FAILED (HYD SYS)

ON TAKOFF, THE NR 2 SERVO LIGHT ILLUMINATED WITH DROP IN HYDRAULIC PRESSURE. REPLACED PUMP. CHAPTER 29-20-01, FIGURE 1, PAGE 0, ITEM 11.