N20GH

Substantial
Serious

HAWKINS AUGUST E AVENTURA IIS/N: AA2A0123

Accident Details

Date
Saturday, May 2, 2009
NTSB Number
CEN09LA276
Location
Griffith, IN
Event ID
20090505X14050
Coordinates
41.519721, -87.399444
Aircraft Damage
Substantial
Highest Injury
Serious
Fatalities
0
Serious Injuries
1
Minor Injuries
0
Uninjured
0
Total Aboard
1

Probable Cause and Findings

The pilot's failure to maintain control of the airplane due to an inadvertent stall. Contributing to the accident was the failure of the airspeed indicator due to separation of the pitot-static line at the left wing root.

Aircraft Information

Registration
N20GH
Make
HAWKINS AUGUST E
Serial Number
AA2A0123
Engine Type
Reciprocating
Year Built
2006
Model / ICAO
AVENTURA IISA02
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
HAWKINS AUGUST E
Address
10226 IDLEWILD LN
Status
Deregistered
City
HIGHLAND BRA
State / Zip Code
IN 46322-3540
Country
United States

Analysis

On May 2, 2009, about 0740 central daylight time, an amateur-built Hawkins Aventura II airplane,N20GH, was substantially damaged during an in-flight collision with terrain after takeoff from runway 26 (4,900 feet by 75 feet, asphalt) at Griffith-Merrillville Airport (05C), Griffith, Indiana. The flight was being conducted under 14 Code of Federal Regulations Part 91 without a flight plan. Visual meteorological conditions prevailed. The pilot sustained serious injuries. The local flight departed immediately prior to the accident.

The pilot stated that the airspeed indicator failed during takeoff. He elected to continue the takeoff because there was insufficient distance to stop on the remaining runway. The pilot intended to remain in the traffic pattern and return for landing. However, as he turned to left crosswind the airplane became difficult to control, pitched down and impacted the ground. The pilot noted that he was briefly knocked unconscious. When he regained consciousness, the engine was still running and he shut it off. The airplane came to rest in a swampy area about 600 feet south of the runway.

The amateur-built aircraft sustained damage to the left wing and left side of the nose. A post accident examination revealed a discontinuity in the pitot-static system. Specifically, tubing from the pitot tube was disconnected from a mating length of tubing located at the left wing root. The left wing remained attached to the fuselage at the wing root and the wing root structure was intact. Flight control continuity was confirmed. No other anomalies associated with a pre-impact failure were observed.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN09LA276