N5742N

Part: SHAFT — BEARING ROUGH (T/R DRIVE)

ROUGH BEARING.

Part: GYRO — FAILED (COCKPIT DG)

UNIT WILL NOT SLAVE. TIME SINCE REPAIR 0:00 HOURS.

Part: INDICATOR — DAMAGED (TOT)

TOT INDICATOR HAD SOMETHING LOOSE INSIDE.

Part: GYRO — PRECESSING (COCKPIT DG)

DIRECTIONAL GYRO PRECESSES IN-FLIGHT.

Part: ACTUATOR — INTERMITTENT (DROOP BAY)

ACTUATOR INTERMITTENT.

Part: ACTUATOR — FAILED (DROOP BAY)

ACTUATOR WILL NOT ACTUATE.

Part: ELT — FAILED (COCKPIT)

ELT WILL NOT TURN OFF.

Part: ALTIMETER — STUCK (COCKPIT)

ALTIMETER NEEDLE STUCK AT 54,000 FEET.

Part: FUEL PUMP — WORN (ENGINE)

FUEL PUMP EXCESSIVELY WORN INTERNAL SPLINES.

Part: LINK ASSY — BUSHING FAILED (M/R XMSN)

BUSHING ON UPPER END MOVED AGAINST SPINDLE.

Part: NOZZLE — OVER SPEC (ENG NR 4)

RECEIVING INSPECTION REVEALED: MEASURED .022 OVER SPECS (8.480 - 8.470) ON #4 NOZZLE O.D. INSTALLED A DALLAS AIRMOTIVE OVERHAULED #4 NOZZLE.

Part: FUEL PUMP — WORN (ENGINE)

FUEL PUMP WORN DRIVE SHAFT DRIVE SPLINES.

Part: CASE ASSY — CORRODED (M/R GR BOX)

CORROSION ON INLET OIL PORT NEXT TO OIL PUMP.

Part: INDICATOR — FAILED (COCKPIT ATTITUDE)

ATTITUDE INDICATOR HAS BAD BEARINGS.

Part: SEAL ASSY — PITTED (M/R GR BOX)

SEALING SURFACE PITTING BEYOND LIMITS.

Part: FUEL CONTROL — DEFECTIVE (ENGINE)

FUEL CONTROL SHEARED SCREW IN BYPASS PLATE.

Part: SHELL ASSY — MIS MFG (LT FWD FUSELAGE)

INSERTS FOR L/H FORWARD FUSELAGE STEP INSTALLED TOO FAR FORWARD. "Z" ANGLE AT BASE OF AFT BOOM CLOSET ANGLES CRACKED ON UPPER R/H END IN RADIUS. INSERTS WERE NOT SENT WITH PANEL

Part: GRIP — GREASE LEAK (M/R)

GREASE LEAKING FROM BOTH GRIPS. S/N A6065&A6067

Part: INDICATOR — DEFECTIVE (ENGINE)

TEMP NEEDLE PEGS OUT INTERMITTENTLY.

Part: INDICATOR — PRECESSES (COCKPIT ATTITUDE)

ATTITUDE POINTER BAR PRECESSES 3 DEGREES DURING SETTLING TEST.

Part: PANEL — REQ REPAIR (ROOF)

EXTERNAL DOUBLER IS OF INADEQUATE WIDTH TO SUPPORT PADS OF TRANSMISSION STOPS. REMOVE DOUBLER FROM ROOF PANEL. FABRICATE NEW DOUBLER FROM 7075-T6 .050" 5.625" X 18". BONDED TO ROOF PANEL USING EA9309.3 NA AND EXISTING TYPE RIVETS. REPAIRED AS PER 8110-3 FROM NORDAM REPAIR DIVISION DATED 18 AUGUST 1995 ANDMRR# 08930.

Part: SHELL ASSY — MIS MFG (LT STEP)

INSERTS FOR L/H FORWARD FUSELAGE STEP INSTALLED TOO FAR FORWARD. "Z" ANGLE AT BASE OF AFT BROOM CLOSET ANGLES CRACKED ON UPPER R/H END IN RADIUS. SEVERAL INSERTS NOT INSTALLED FOR CREW SEAT BACK BULKHEAD BASE ANGLES L/H AND R/H SIDESAND FUEL LINE COVER. INSERTS WERE NOT SENT WITH PANEL (20 EACH 80-005-2-12 AND 8 EACH 80-004-2-12)

Part: SHELL ASSY — CRACKED (AIRFRAME)

INBOARD HALF OF TOP CAP ON L/H AND R/H SIDES OF SHELL ASSY CRACKED IN RADIUS. AFT INSERTS FOR R/H FWD AIRFRAME STEP NOT INSTALLED THROUGH INTERNAL DOUBLER.

Part: ELBOW — CORRODED (M/R CONTROL)

CORROSION BEYOND LIMITS. REPLACED WITH SERVICEABLE PART.

Part: SUPPORT ASSY — CORRODED (M/R CONTROL)

SUPPORT ASSY CORROSION BEYOND LIMITS. REPLACED WITH SERVICEABLE PART.

Part: FUEL NOZZLE — DEFECTIVE (ENGINE)

ENGINE HARD TO START. REQUIRED BATTERY CART ON 2 OR 3 STARTS. REPLACED WITH SERVICEABLE FUEL NOZZLE.

Part: BEARING — FAILED (M/R XMSN)

INNER AND OUTER RACES AND BALL SPALLING. REPLACED WITH NEW BEARING SET AND RETURNED TO SERVICE.

Part: TRANPONDER — DEFECTIVE (COCKPIT)

TOP BROKEN. REPLACED BROKEN SWITCH BOARD ASSY AND BROKEN FACEPLATE. INSTALLED MISSING IDENT PUSH BUTTON. UNIT HAD WEAK POWER OUT. REPLACED CAVITY TUBE V101. REPAIRED. REPLACED PHOTOCELL V301 DUE TO WEAK REPLY LIGHT. FOUND UNIT TO HAVE WEAK RECEIVE. ALIGNED RECEIVER. REPAIRED AND BENCH CHECK GOOD.

Part: INDICATOR — READS HIGH (COCKPIT AIR SPD)

NEEDLE INDICATES 5 MPH HIGH AT 100 MPH.

Part: INDICATOR — STICKING (COCKPIT AIR SPD)

INDICATOR STICKING. REPLACED WITH SERVICEABLE INDICATOR.

Part: EXHAUST ASSY — CRACKED (MOUNT FLANGE)

CRACKED ON AFT SIDE NEAR MOUNTING FLANGE. CRACK IS ONE INCH LONG. INSTALLED SERVICEABLE EXHAUST STACK.