N969HA

Part: CONNECTOR — SHORTED (PROP CONTROL SYS) · airframe 14,718 hrs · 16,324 cycles

NR 2 ENGINE AUTO FEATHERED AT 1000 FT AGL ON TAKEOFF. MAX TQ REACHED WAS 114 PERCENT. REPLACED CONNECTOR 9811-J14.

Part: CONTROL UNIT — MALFUNCTIONED (NR 2 PROPELLER) · airframe 14,545 hrs · 16,122 cycles

AT 400 FEET NR 2 PROPELLER AUTO FEATHERED THE ENGINE TORQUE WAS AT 95 PERCENT. CREW ALSO REPORTED THE TORQUE WENT TO THE RED LINE AND REMAINED. REPLACED THE NR 2 TSCU.

Part: CONTROL UNIT — FAULTY (AUTO FEATHER SYS) · airframe 14,545 hrs · 16,122 cycles

AT 400 FEET, NR 2 PROPELLER AUTO FEATHERED THE ENGINE TORQUE WAS AT 95 PERCENT. CREW ALSO REPORTED THE TORQUE WENT TO THE RED LINE AND REMAINED. REPLACED THE NR 2 TSCU.

Part: WIRE HARNESS — INTERMITTENT (NR 2 ENGINE) · airframe 14,546 hrs · 16,125 cycles

BETWEEN 500 AND 1000 FEET AGL, CREW HEARD A LOUD NOISE FROM NR 2 ENGINE FOLLOWED BY A HIGH PITCH SOUND. CREW NOTICED THE NR 2 TORQUE AT 111 PERCENT (DIGITAL) AND RISING, THE ANALOG WAS OFF SCALE. FLIGHT ATTENDANT REPORTED SMOKE COMING FROM UNDER THE NR 2 PROP. REMOVED AND REPLACED THE NR 2 ENGINE STRUT WIRE HARNESS.

Part: WIRE — SHORTED (ENGINE INDICATOR) · airframe 14,081 hrs · 15,591 cycles

ON APPROACH INTO CLT THE NR 1 LOW OIL PRESSURE CAUTION LIGHT ILLUMINATED. NO INDICATION OF OIL QUANTITY LOW. THE CREW DECLARED AN EMERGENCY AND CONTINUED TO LAND WITHOUT INCIDENT. FOUND WIRE SEGMENT 7932-103, SHORTED BETWEEN CONDUCTOR AND SHIELD. SHORTED AT FIREWALL CONNECTOR 9811-P29, REPLACED CONNECTOR.

Part: TURBINE BLADES — CRACKED (NR 2 ENGINE)

ON TAKEOFF FROM HHH, AT 1000 FT, HEARD LOUD BANG FROM NR 2 ENGINE. ENGINE AUTO FEATHERED AND TQ WENT 0 PERCENT. COMPLETED SHUT-DOWN PER CHECKLIST AND DIVERTED TO MCAS BEAUFORT. LANDED WITHOUT FURTHER INCIDENT. INVESTIGATION REVEALED HPT BLADE FAILURE. THERE WAS NO ENGINE CASE PENETRATION.

Part: ENGINE — FROZEN (NR 2)

DURING CLIMB OUT FROM HHH CREW HEARD LOUD BANG FROM NR 2 ENGINE FOLLOWED BY TQ LOSS AND PROP AUTO FEATHERED. CREW SHUT ENG DOWN IAW CHECK LIST. REMOVE AND REPLACED ENGINE.

Part: PANEL — CORRODED (NR 1 NACELLE) · corrosion level 2 · airframe 11,620 hrs · 12,810 cycles

NR 1 NACELLE REAR DECK UNDER FINGERNAIL HAS SURFACE CORROSION, R & R REAR DECK

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,620 hrs · 12,810 cycles

SEAT TRACK CORRODED JUST INBOARD OF PAX DOOR R & R SEAT TRACK IAW RD8-53-3074, RD8-53-2295,RD8-53-1102

Part: SMOKE DETECTOR — MALFUNCTIONED (LAVATORY) · airframe 9,632 hrs · 10,697 cycles

LAV SMOKE DETECTOR SOUNDED AT 1000 FEET IN FLIGHT. NO SMOKE WAS NOTED. REPLACED LAV SMOKE DETECTOR.

Part: RUDDER — CRACKED · airframe 8,430 hrs · 9,431 cycles

R/H SKIN OF FORE RUDDER HAS LARGE CRACK AT FIRST AND SECOND RIB BELOW TOP CLOSING RIB. REPLACED RUDDER.

Part: WIRE — BROKEN (CABIN) · airframe 7,162 hrs · 8,128 cycles

NUMBER 3 AND NUMBER 4 RED FLOOR EMERGENCY LIGHTS INOP. NEW CREW FOUND BROKEN WIRES. REPAIRED BROKEN WIRE AT LIGHT ASSEMBLY.

Part: WARNING LIGHT — ILLUMINATED (COCKPIT) · airframe 1,447 hrs · 1,683 cycles

CREW REPORTED A MOMENTARY BAG BAY SMOKE WARNING LIGHT IN FLIGHT. INSPECTED BOTH DETECTORS AND CONNECTORS AND PERFORMED SYSTEM TEST. NO DISCREPANCIES FOUND.

Part: POWER SUPPLY — FAILED (CABIN) · airframe 1,339 hrs · 1,562 cycles

CABIN EMERGENCY EXIT SIGNS COME ON WITH COCKPIT SWITCH IN THE ARMED POSITION. REPLACED EMERGENCY LIGHT POWER SUPPLY 3351-PS4.

Part: CABLE — LOOSE (PAX DOOR)

PAX DOOR WOULD NOT FULLY OPEN. FOUND COUNTERBALANCE CABLE TO BE OFF THE DRUM. REPLACED COUNTERBALANCE CABLE, GAS STRUT CABLE AND BOTH GAS STRUTS.

Part: CABLE — DISPLACED (PAX DOOR)

PAX DOOR WOULD NOT FULLY OPEN. FOUND COUNTERBALANCE CABLE TO BE OFF THE CABLE DRUM. REPLACED THE COUNTERBALANCE CABLE.

Part: CABLE — DISPLACED (PAX DOOR)

CREW COULD NOT FULLY OPEN THE PAX DOOR. THE COUNTER BALANCE CABLE WAS FOUND TO BE OFF THE CABLE DRUM AND THE PULLEY GUIDE WAS LOOSE. THE CABLE WAS REPLACED AND THE PULLEY GUIDE WAS TIGHTENED.

Part: PSEU — FAILED (LT MLG)

LT MLG DOOR AMBER LIGHT ILLUMINATED UPON RETRACTION CYCLE GEAR AND UPON 2ND REACTION SAME LT ILLUMINATED ALONG WITH LANDING GEAR CAUTION LIGHT. PERFORMED MANUAL EXTENSION. FOUND PSEU DRIVER 53 FLAG. REMOVED AND REPLACED PSEU AND RETRACTED GEAR, OPS CHECK GOOD.