Beechcraft 95-B55 N448P

Summary

On 19 February 1996 at about 01:36 local time, a Beechcraft 95-B55 registered N448P was involved in an accident near Morganton, North Carolina, United States. 6 people were on board and 2 died, one was seriously injured, 3 had minor injuries. The aircraft was destroyed. The NTSB has published a probable cause for this accident; it is quoted in full below.

Date

19 February 1996 at 01:36

Classification

Accident

Location

Morganton, North Carolina, United States

Nearest airport

Morganton-Lenoir (MRN)

Coordinates

35.7391, -81.6901

Aircraft

Beechcraft 95-B55

Registration

N448P

Category

Airplane

Engines

2

Operator

Not recorded

Operating rule

Part 91: General Aviation

Purpose of flight

Personal

Phase of flight

Not recorded

Route

St Augustine → Unknown

Aircraft damage

Destroyed

Weather

VMC

Light

Night/Dark

NTSB number

MIA96FA082

2 people died.

the pilot's delay in initiating a go-around (aborted landing), which resulted in his failure to obtain/maintain sufficient altitude or clearance from trees beyond the end of the runway. Factors relating to the accident were: the pilot's failure to ensure proper weight and balance of the airplane; and his improper flare and improper recovery from a bounced landing, which resulted in porpoising of the airplane.

Quoted verbatim from the NTSB record. This site does not paraphrase or interpret it.

Read the full NTSB narrative

The owner/pilot had recently purchased the airplane. Another pilot, who had delivered the airplane to the new owner, flew with him on 2 occasions. He said the owner/pilot was about 20 knots fast on final approach and had a tendency to flare late for landing. During the accident flight, the pilot entered the traffic pattern at night and configured the airplane for landing. During the landing, the airplane touched down (bounced) nosewheel first and began to porpoise. Following the second bounce, the airplane pitched nose up, and the pilot initiated a go-around; however, the airplane bounced a third time, and the cabin door popped open. The right front seat passenger attempted to hold the door closed as the pilot continued the go-around. After the third bounce, the airplane remained airborne about 6 to 15 feet until it collided with trees beyond the departure end of the runway; then it came to rest inverted. Examination of the engines, propellers, and flight controls revealed no evidence of preimpact failure or malfunction. Calculations showed that at the time of the accident, the gross weight was 192 pounds over the maximum limit, and the center-of-gravity (CG) was 1.56 inches behind the aft limit. Also, the POH/Flight Manual indicated that the performance would be reduced with the cabin door open. The pilot had accumulated an estimated 9 hours in the accident airplane since he purchased it.

Quoted verbatim from the NTSB record.