Aviation Crash Map

Spearman RAPTOR N750TP

12 April 2005 · Bogalusa, Louisiana, United States · Fatal

Summary

On 12 April 2005 at about 22:46 local time, a Spearman RAPTOR registered N750TP was involved in an accident near Bogalusa, Louisiana, United States. 2 people were on board and 2 died. The aircraft was destroyed. The NTSB has published a probable cause for this accident; it is quoted in full below.

The record

Date
at 22:46
Classification
Accident
Location
Bogalusa, Louisiana, United States
Nearest airport
George R Carr Memorial Air Fld (BXA)
Coordinates
30.8019, -89.8689
Aircraft
Spearman RAPTOR
Registration
N750TP
Category
Airplane
Engines
1
Operator
Not recorded
Operating rule
Part 91: General Aviation
Purpose of flight
Personal
Phase of flight
Not recorded
Route
Daytona Beach → Bogalusa
Aircraft damage
Destroyed
Weather
VMC
Light
Day
NTSB number
DFW05LA102

People

2 people died.

On board Died Serious Minor Uninjured
2 2 0 0 0

Probable cause

The pilot's failure to maintain control of the airplane. A contributing factor was the pilot's lack of experience in the make/model airplane.

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

Read the full NTSB narrative

The private pilot lost control of the high performance experimental turbo-prop powered airplane on final approach to the airport. About 1.85 miles from the airport, while at an altitude of 852 feet mean sea level (msl), the pilot began a descending right turn for a straight in approach to runway 36 (a 5,000-foot by 100-foot wide runway). Approximately 1,984 feet from the runway threshold, the airplane impacted terrain in a heavily wooded area, came to rest in an inverted position, and was destroyed by post-impact fire. All major components were accounted for at the scene, but due to fire damage a control continuity check could not be performed. An examination of the engine revealed no mechanical defects or anomalies. The 2,000-hour pilot had accumulated a total time of 3-5 hours in the accident airplane. The airplane was a retractable tricycle geared pressurized low-wing prototype of composite construction and had accrued approximately 60 total flight hours since it was manufactured in 2002. The cockpit contained two seats in a tandem arrangement and was equipped with a dual screen Electronic Flight Instrument System (EFIS). During the initial flight test program the airplane revealed several hazardous flight characteristics. The airplane's airframe and engine logbooks were not available for review during the course of the investigation so it could not be determined if any modifications were made to the airplane since the initial test flights were concluded in July 2004.

Quoted verbatim from the NTSB record.

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