Aviation Crash Map

Boeing A75SN1 N5805V

4 May 2002 · Georgetown, Texas, United States · Minor injuries

Summary

On 4 May 2002 at about 19:00 local time, a Boeing A75SN1 registered N5805V was involved in an accident near Georgetown, Texas, United States. 2 people were on board and 2 had minor injuries. The aircraft was substantially damaged. The NTSB has published a probable cause for this accident; it is quoted in full below.

The record

Date
at 19:00
Classification
Accident
Location
Georgetown, Texas, United States
Nearest airport
Georgetown Municipal (GTU)
Coordinates
30.6789, -97.6794
Aircraft
Boeing A75SN1
Registration
N5805V
Category
Airplane
Engines
1
Operator
Not recorded
Operating rule
Part 91: General Aviation
Purpose of flight
Air Race/Show
Phase of flight
Not recorded
Route
Georgetown → Burnett
Aircraft damage
Substantial
Weather
VMC
Light
Day
NTSB number
FTW02LA139

People

2 people had minor injuries.

On board Died Serious Minor Uninjured
2 0 0 2 0

Probable cause

The pilot's inadequate planning/decision resulting in the wake turbulence encounter during the takeoff/initial climb of the formation flight. A contributing factor was the partial loss of engine power for an undetermined reason.

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

Read the full NTSB narrative

The airplane encountered wake turbulence during the takeoff/initial climb of the formation flight of 4 airplanes at an air show. The 2 lead airplanes had engines rated at 450 horsepower. The accident airplane engine was rated at 220 horsepower. According to the pilot, following the wake turbulence, the airplane had "reduced" power and did not maintain altitude. The airplane descended, struck power lines, trees, and a residence before coming to rest nose low on the ground. Examination revealed that compression on two of the engine cylinders was below recommended specifications, and one magneto was timed approximately 2 1/2 degrees retarded. According to the FAA inspector, the propeller diameter was longer than the maximum allowable per the Type Certification Data Sheet (TCDS), and the reported take-off and climb rpm of 1700-1800 was lower than the TCDS specification of 2,075 rpm at 220 horsepower. According to the propeller manufacturer's representative, there were "no indications of any type of propeller failure prior to impact."

Quoted verbatim from the NTSB record.

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