N5007N

Part: ELEMENT — MISMANUFACTURED (ENGINE OIL) · airframe 23,833 hrs

ENGINE OIL FILTER WILL NOT FIT IN THE HOUSING. THE HOLE WHERE THE O-RING GOES IS TOO SMALL ON ONE END. SCRAPPED.

Part: TRANSDUCER — FAILED (FUEL PRESSURE) · airframe 22,624 hrs

WHEN SWITCH IS TURNED ON, THE FUEL PRESSURE WILL GO UP EVEN WITH THE BOOST PUMPS OFF. REPLACED WITH SERVICEABLE PART.

Part: GPS — INOPERATIVE (COCKPIT)

GPS RECEIVER WILL NOT TRACK SATELLITE.

Part: CARTRIDGE — FAILED (BOOST PUMP) · airframe 22,220 hrs

LT BOOST PUMP FUEL PRESSURE DROPPED TO ZERO, LT BOOST PUMP LIGHT ILLUMINATED. REPLACED WITH SERVICEABLE PART.

Part: TRANSCEIVER — FAILED (COCKPIT) · airframe 21,970 hrs

FIRST START OF THE DAY UNIT WOULD NOT TRANSMIT. REPLACED WITH SERVICEABLE PART.

Part: PUMP — DAMAGED (HYDRAULIC SYSTEM)

PUMP'S RESERVOIR HOT AND BLADES HARD TO TURN.

Part: GPS — FAILED (COCKPIT)

SOME BUTTONS ON GPS INOPERATIVE AND CANNOT SCROLL WITH KNOBS.

Part: TRANSCEIVER — MALFUNCTIONED (COCKPIT)

USE SIDE OF DISPLAY UNREADABLE ON TRANSCEIVER. ONLY KHZ NUMBERS ARE DISPLAYED AND R604 SMOKES.

Part: INDICATOR — FAULTY (DUAL TACH)

ROTOR NEEDLE DROPS OFF TO ZERO PERCENT AT 35 PERCENT RPM.

Part: INDICATOR — STICKS (COCKPIT)

INDICATOR STICKING, LOW OUT OF TOLERANCE.

Part: SUPPORT — MISMANUFACTURED (ENG NOZZLE)

RECEIVING INSPECTION REVEALED: MISALIGNMENT OF G.P. SUPPORT NOZZLE SLOTS. TRIED SEVERAL NR2 NOZZLES UNABLE TO INSTALL INTO G.P. SUPPORT SLOTS.

Part: INDICATOR — STICKS (TOT)

TOT NEEDLE STICKS AT 500 WHEN HEATED.

Part: TRANSCEIVER — FAILED (COCKPIT)

RECEIVES BUT WILL NOT TRANSMIT 118 MHZ RANGE. PERFORMED PRELIMINARY INSPECTION. FOUND UNIT NOT TRANSMITTING ON CORRECT FREQUENCY FROM 118MHZ TO 129MHZ. REPLACED TRANSISTORS Q307 AND Q308 IN VCO SECTION. REPAIRED PROBLEM. FOUND UNIT TO HAVE VERY WEAK RECEIVE. ADJUSTED VCO AND ALIGNEDRECEIVER SEVERAL TIMES. NO HELP.

Part: AMPLIFIER — OVERHEAT (COCKPIT)

INTERPHONE AMPLIFIER GETS EXCESSIVELY HOT; THEN SHUTS DOWN.

Part: SKYNAV 5000 — FAILED (COCKPIT GPS)

GPS WILL NOT COME ON.

Part: DOOR — DAMAGED (LT FWD)

DOOR HAS A FLAT AREA JUST BELOW WINDOW APPROXIMATELY 8" DOWN THE FULL WIDTH OF DOOR.

Part: SHROUD HOUSING — UNDER SIZE (ENGINE)

RECEIVING INSPECTION REVEALED; UNDERSIZED THROAT CLEARANCE ON SHROUD HOUSING. INSTALLED A NEW SHROUD HOUSING.

Part: ALTIMETER — CASELEAK (COCKPIT)

ALTIMETER EXCESSIVE CASE LEAK.

Part: PANEL ASSY — MIS MFG (FS 154)

PANEL DOES NOT HAVE CORRECT CONTOUR ALONG LEFT HAND SIDE, AFT EDGE, WHERE IT ATTACHES ALONG L/H SIDE OF FORWARD BAGGAGE COMPARTMENT WALL. CUT 2 EACH DIAGONAL SLITS, 1/4" SIDE IN L/H INNER SKIN OF PANEL. SLITS RUN FROM WL30.25/F STA. 154.25 TO WL 49.25/F STA. 143.00 (WATER LINES AND FUSELAGE STATIONS APPROXIMATE) FILLED SLITS AND BONDED WITH MAGNOLIA 6398 ADHESIVE. CURED AND SANDED SMOOTH. OVERLAYED WITH 2 LAYERS FIBERGLASS CLOTH USING MAGNOLIA 6367 RESIN. CURED AND SANDED SMOOTH AND PRIMED.

Part: DOOR — WONT FIT (LT FORWARD)

DOOR DOES NOT FIT CONTOUR OF AIRCRAFT.

Part: DOOR — DAMAGED (LT FOREWARD)

FLAT AREA JUST BELOW WINDOW APPROXIMATELY 8" DOWN THE FULL WIDTH OF DOOR.

Part: FUEL CELL — UNBONDED (MOUNT INSERT)

FUEL CELL UNBONDED MOUNTING INSERT AS MARKED IN RED.

Part: FRAME — CRACKED (TAIL BOOM)

T/B FRAME CRACKED L/H MOUNT AREA, LONGERON L/H AND L/H CASTING CRACKED AT OUTBOARD RIVET ON FLANGE AND CASTING. REPLACED FRAME AND LONGERON P/N 206-031-314-037S, AND FITTING P/N 206-031-392-101S.