What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
(-23) Aircraft N5234A,a Grumman S-2B operated by the commemorative airforce had departed franklin, VA (fkn) enroute to cherry point mcas (nkt). On final approach the aircraft was cleared to runway 5 approximately 2 to 3 miles out at 1100 to 1200' altitude. The aircraft started an uncommanded turn to the right accompanied by a decrease in airspeed. The right engine lost power for an undetermined reason. The co-pilot flying the airplane applied right rudder instead of left rudder and the aircraft entered a right turn. Crew coordination and communication was poor as the pilot had to ask the co-pilot what was going on. When the co-pilot stated he was holding right rudder, the pilot feathered the left engine without coordination. The pilot unfeathered the engine when he did not perceive a decrease in drag on the left side. The period during this feather/unfeathering cycle reduced the thrust from the left engine at a critical stage as the airspeed dropped to 75 knots. The co-pilot flew the aircraft to the ground through the electrical powerlines and trees coming to rest in an adjacent field. The fire started from the severed powerlines which eventually engulfed the aircraft causing both wings to explode.
As the FAA filed it
(-23) AIRCRAFT N5234A,A GRUMMAN S-2B OPERATED BY THE COMMEMORATIVE AIRFORCE HAD DEPARTED FRANKLIN, VA (FKN) ENROUTE TO CHERRY POINT MCAS (NKT). ON FINAL APPROACH THE AIRCRAFT WAS CLEARED TO RUNWAY 5 APPROXIMATELY 2 TO 3 MILES OUT AT 1100 TO 1200' ALTITUDE. THE AIRCRAFT STARTED AN UNCOMMANDED TURN TO THE RIGHT ACCOMPANIED BY A DECREASE IN AIRSPEED. THE RIGHT ENGINE LOST POWER FOR AN UNDETERMINED REASON. THE CO-PILOT FLYING THE AIRPLANE APPLIED RIGHT RUDDER INSTEAD OF LEFT RUDDER AND THE AIRCRAFT ENTERED A RIGHT TURN. CREW COORDINATION AND COMMUNICATION WAS POOR AS THE PILOT HAD TO ASK THE CO-PILOT WHAT WAS GOING ON. WHEN THE CO-PILOT STATED HE WAS HOLDING RIGHT RUDDER, THE PILOT FEATHERED THE LEFT ENGINE WITHOUT COORDINATION. THE PILOT UNFEATHERED THE ENGINE WHEN HE DID NOT PERCEIVE A DECREASE IN DRAG ON THE LEFT SIDE. THE PERIOD DURING THIS FEATHER/UNFEATHERING CYCLE REDUCED THE THRUST FROM THE LEFT ENGINE AT A CRITICAL STAGE AS THE AIRSPEED DROPPED TO 75 KNOTS. THE CO-PILOT FLEW THE AIRCRAFT TO THE GROUND THROUGH THE ELECTRICAL POWERLINES AND TREES COMING TO REST IN AN ADJACENT FIELD. THE FIRE STARTED FROM THE SEVERED POWERLINES WHICH EVENTUALLY ENGULFED THE AIRCRAFT CAUSING BOTH WINGS TO EXPLODE.
NTSB investigation
The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.
Other reports on N5234A · 1
Matched to the same aircraft by N-number and date.