N247CA

Part: SIGN — INOPERATIVE (ROW 8)

EMERGENCY EXIT SIGN AT ROW 8 IS INOPERABLE. REPAIRED DAMAGED WIRES AT EXIT SIGN.

Part: CONTROLLER — MALFUNCTIONED (RT PROPELLER)

RT PROPELLER RPM WAS 99.2 TO 99.6 AFTER TAKEOFF. GROUND RUNS SHOWED PROPELLER RPM TO BE IN LIMITATIONS.

Part: RCCB — FAILED (COCKPIT)

RIGHT HAND PROPELLER DEICE FAIL WARNING. REPLACED RCCB (CB0226).

Part: LIGHT — INOP (CABIN)

FWD EMERGENCY FLOOR LIGHT WAS INOP. REPLACED LIGHT ASSY.

Part: WARNING — ACTIVATED (SERVICE DOOR)

SERVICE DOOR WARNING DURING TAKEOFF. DOOR WARNING SYSTEM PREVIOUSLY DEFERRED PER MEL.

Part: WARNING — ACTIVATED (SERVICE DOOR)

SERVICE DOOR WARNING DURING TAKEOFF. DEFERRED DOOR WARNING SYSTEM PER MEL.

Part: SENSOR — FAILED (LT MLG)

LEFT MLG DOWN INDICATOR ON WITH GEAR RETRACTED. LANDING GEAR WOULD NOT EXTEND WHEN SELECTED. FREE FALL SYSTEM USED TO EXTEND GEAR. REPLACED DOWN LOCK PROXIMITY SENSOR. (M)

Part: DEICE — INOP (RT PROP)

RIGHT HAND PROPELLER DEICE IS INOPERABLE. REPLACED THE NR 3 BLADE ON RIGHT HAND PROPELLER.

Part: FRAME — CRACKED (LT NACELLE)

LEFT NACELLE, FRAME WEB NR 10 CRACKED AT INBOARD RADIUS OF THE FLANGE. REPAIRED BY SPLICING IN A NEW FLANGE PER AERODESIGN REPORT NR 1076-2 AND EMB120 SRM 51-40-02.

Part: BATTERY PACK — DISCHARGED (CABIN)

FORWARD SECTION OF CABIN EMERGENCY LIGHTS ARE INOPERATIVE. REPLACED BATTERY PACK FOR THE FORWARD EMERGENCY LIGHTING.

Part: CONTACTOR — FAILED (EXTERNAL POWER)

EXTERNAL POWER CONTACTOR BURNT/OVERHEATED AT TERMINAL ENDS. REPLACED CONTACTOR AND POSITIVE CABLE.

Part: FASTENER — BROKEN (FUEL DOOR)

SERVICE DOOR WARNING DURING TAKEOFF. REPLACED BROKEN CAM LOCK FASTENER ON SINGLE POINT FUEL SERVICE DOOR.

Part: SENSOR — MALFUNCTIONED (RT MLG)

AFTER LANDING GEAR RETRACTED, RIGHT HAND MLG DOWN INDICATOR REMAINED ON. REPLACED DEFECTIVE DOWNLOCK PROXIMITY SENSOR.

Part: LATCH — NOT SECURED (SERVICE DOOR)

SERVICE DOOR WARNING DURING CLIMBOUT. AIRCRAFT RETURNED TO THE FIELD. CLOSED DOOR AND SECURED LATCH.

Part: PIN — NOT REMOVED (NLG)

NOSE LANDING GEAR WOULD NOT RETRACT. REMOVED NLG PIN. GEAR SWINGS GOOD.

Part: BUTTSTRAP — CORRODED (FUSELAGE)

DURING 2C INSPECTION, TASK 5310-131-01I REVEALED LEFT FORWARD BUTTSTRAP TO BE CORRODED. REMOVED BUTTSTRAP AND INSTALLED SERVICEABLE BUTTSTRAP USING EMB 120 SRM STANDARD PRACTICES.

Part: BUTTSTRAP — CORRODED (FUSELAGE)

DURING 2C INSPECTION TASK 151-01Z REVEALED LEFT NR 5 BUTTSTRAP TO BE CORRODED. REMOVED BUTTSTRAP AND INSTALLED SERVICEABLE BUTTSTRAP USING EMB 120 STANDARD PRACTICES.

Part: SILL — CORRODED (FUSELAGE)

DURING 2C INSPECTION TASK 5310-131-01I REVEALED RIGHT NR 1 SILL TO BE CORRODED. REMOVED SILL AND INSTALLED SERVICEABLE SILL USING EMB 120 SRM STANDARD PRACTICES.

Part: SILL — CORRODED (FUSELAGE)

DURING 2C INSPECTION, TASK 5310-131-01I REVEALED LEFT NR 1 STILL TO BE CORRODED. REMOVED SILL AND INSTALLED SERVICEABLE SILL USING EMB 120 SRM STANDARD PRACTICES.

Part: CROSSBEAM — CORRODED (CABIN)

DURING 2C INSPECTION, TASK 5310-131-01I REVEALED LEFT CENTER CROSSBEAM TO BE CORRODED AT FRAME 16. REMOVED AND REPLACED CROSSBEAM USING EMB 120 SRM STANDARD PRACTICES.

Part: WIRE HARNESS — OUT OF POSITION (RT BOOST PUMP)

DURING 2C INSPECTION, TASK 5720-622-01I, REVEALED THE WIRE HARNESS FOR THE RIGHT WING FORWARD FUEL BOOST PUMP TO BE CHAFFING ON THE METAL BRAIDED FUEL LINE. PUMP WIRE INSULATION WAS NOT DAMAGED ONLY WIRE HARNESS PROTECTIVE COVERING. REMOVED PUMP AND HARNESS AND INSTALLED SERVICEABLE PUMP MAKING SURE THE WIRE HARNESS WAS CLEAR OF ALL STRUCTURE AND FUEL LINES.

Part: BUTTPLATE — CORRODED (FUSELAGE)

DURING 2C INSPECTION TASK 5310-131-O1I REVEALED CENTER BUTTPLATE TO HAVE SPOTS OF CORROSION THAT WERE BEYOND LIMITS. REMOVED CENTER BUTTPLATE AND INSTALLED SERVICEABLE BUTTPLATE USING EMB120 SRM STANDARD PRACTICES AND AERODESIGN REPORT NR 1671-1.

Part: WHEEL — CRACKED (MLG)

DURING TEARDOWN VISUAL INSPECTION FOR TIRE CHANGE, THE INNER HALF OF THE MAIN WHEEL ASSY WAS FOUND TO HAVE A CRACK APPROXIMATELY 2 INCHES IN LENGTH RUNNING INWARD IN THE WEB AREA, STARTING FROM UNDER THE BEARING CUP. THE WHEEL WAS REMOVED FROM SERVICE AT THIS TIME.

Part: BATTERY — DISCHARGED (CABIN)

SOME OF THE CABIN EMERGENCY LIGHTS ARE INOPERABLE. REPLACED EMERGENCY BATTERY.

Part: WIRE — BROKEN (CABIN)

SOME OF THE CABIN FLOOR PATH EMERGENCY LIGHTS ARE INOP. REPAIRED BROKEN WIRE.

Part: FUEL DOOR — NOT LATCHED (WING)

SERVICE DOOR WARNING CAME ON AFTER TAKEOFF. SINGLE POINT FUEL SERVICE DOOR NOT LATCHED. SECURED DOOR AND AIRCRAFT RETURNED TO SERVICE.

Part: ROLLER — DIRTY (LT/RT TE FLAPS)

FLAP DISAGREEMENT AFTER FLAPS SELECTED TO 0 DEGREES. REPLACED FLAP ROLLERS ON LEFT AND RIGHT OUTBOARD FLAPS.

Part: RELAY — FAILED (CABIN)

EMERGENCY LIGHTING NOT ARMED WARNING ON MAP, CIRCUIT BREAKER TRIPPED. COULD NOT DUPLCIATE DISCREPANCY. REPLACED RELAY K201 FOR TROUBLESHOOTING.

Part: TUBING — CHAFED (LT NACELLE)

HYDRAULIC FLUID LEAKING FROM LT ENGINE NACELLE. REPLACED DAMAGED SECTION OF GREEN SYSTEM HYDRAULIC PRESSURE TUBING BETWEEN NACELLE 13 AND 14.

Part: POTENTIOMETER — MALFUNCTION (NLG)

CLUNKING SOUND AND UNCOMMANDED MOVEMENT FROM NOSE WHEEL STEERING SYSTEM. REPLACED THE NWS FEEDBACK POTENTIOMETER.

Part: SWITCH — OUT OF ADJUST (CARGO DOOR)

CARGO DOOR WARNING SOUNDED DURING TAKEOFF. ADJUSTED CARGO DOOR MICROSWITCH. AIRCRAFT CONTINUED SERVICE.

Part: CONTROLLER — FAILED (AVIONICS BAY)

TRANSPONDER NR 1 AND NR 2 REPORTED INOPERATIVE BY AIR TRAFFIC CONTROL. REPLACED CTL-92.

Part: FUEL NOZZLE — LEAKING (RT ENGINE)

FUEL LEAKING FROM RT ENGINE NACELLE. REPLACED THE RT ENGINE FUEL NOZZLES.

Part: SENSOR — DEFECTIVE (LT MLG)

WHEN LANDING GEAR SELECTED DOWN, GEAR DID NOT EXTEND. INDICATION WAS 5 RED INTRANSIT AND ONE GREEN DOWNLOCK. EMERGENCY SYSTEM USED TO EXTEND GEAR. REPLACED DEFECTIVE DOWNLOCK PROXIMITY SENSOR ON LEFT MLG.

Part: LATCH — BROKEN (RT MLG DOOR)

RIGHT MLG OUTBOARD GEAR DOOR WILL NOT CLOSE. REPLACED BROKEN DOOR LATCH ASSY.

Part: PROP CONTL UNIT — MALFUNCTION (LT PROP)

LEFT PROPELLER TAKES 30 SECONDS TO TRANSITION FROM FEATHER TO BETA RANGE. REPLACED THE PROPELLER CONTROL UNIT.

Part: FUEL DOOR — UNLATCHED (RT WING)

DOOR LIGHT ON M.A.P. ILLUMINATED ON TAKEOFF ROLL. SECURED FORWARD FASTENER ON INBOARD FUEL DOOR.

Part: GOVERNOR — DEFECTIVE (LT PROPELLER)

LT PROPELLER IS SLOW COMING OUT OF FEATHER. REPLACED THE LEFT OVER SPEED GOVERNOR.

Part: TIRE — FAILED (RT MLG)

RT MLG TIRE FAILED DURING TAKEOFF ROLL. REPLACED RT WHEEL TIRE ASSY.

Part: DOOR WARNING — ACTIVATED (CARCO COMPT)

CARGO DOOR WARNING CAME ON DURING TAKEOFF. COULD NOT DUPLICATE - INSPECTED DOOR SYSTEM AND OPERATIONAL CHECK SATISFACTORY. AIRCRAFT RETURNED TO SERVICE.

Part: PCU — DEFECTIVE (LT PROP)

LEFT PROPELLER TAKES 15 SECONDS TO UNFEATHER. REPLACED THE PITCH CONTROL UNIT.

Part: CONTROL BOX — DEFECTIVE (LANDING GEAR)

LANDING GEAR WILL NOT RETRACT. REPLACED THE LANDING GEAR CONTROL BOX.

Part: PCU — DEFECTIVE (LT PROP)

LEFT PROPELLER IS SLOW TO UNFEATHER. REPLACED THE PROP PITCH CONTROL UNIT.

Part: SUPPORTS — CRACKED (LT/RT WINGS)

THE FOLLOWING P/N WING SKIN SUPPORTS WERE FOUND CRACKED DURING INSPECTION TASK 5720-551/651-01i AND 5720-552/652-01I AT WING RIBS NR 15, 16, AND 18. P/N 120-17056-019, 2 EA; 120-17056-017, 2 EA; 120-17056-015, 4 EA; 120-17056-013, 2 EA; 120-17056-007, 2 EA; 120-17057-005, 1 EA; 120-17057-007, 2 EA; 120-17059-015, 2 EA; 120-17057-006, 1 EA. THE SKIN SUPPORTS WERE REPLACED IAW AERO DESIGN REPORT NR 1327-2.

Part: HMU — DEFECTIVE (RT ENGINE)

RT ENGINE WILL NOT START. REPLACED THE HMU.

Part: CONTROL UNIT — DEFECTIVE (TE FLAPS)

CONTROL FAULT WARNING WHEN FLAPS SELECTED FOR APPROACH. REPLACED FLAP CONTROL UNIT.