Aviation Crash Map

Hrosik Gene AVENTURA II N5842

29 March 2011 · Crescent City, Florida, United States · Minor injuries

Summary

On 29 March 2011 at about 20:30 local time, a Hrosik Gene AVENTURA II registered N5842 was involved in an accident near Crescent City, Florida, United States. One person was on board and one 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 20:30
Classification
Accident
Location
Crescent City, Florida, United States
Nearest airport
Thunderbird Air Park (2FA5)
Coordinates
29.4725, -81.5681
Aircraft
Hrosik Gene AVENTURA II
Registration
N5842
Category
Airplane
Engines
1
Operator
Not recorded
Operating rule
Part 91: General Aviation
Purpose of flight
Positioning
Phase of flight
Not recorded
Route
Crescent City → Lakeland
Aircraft damage
Substantial
Weather
IMC
Light
Day
NTSB number
ERA11LA228

People

1 person had minor injuries.

On board Died Serious Minor Uninjured
1 0 0 1 0

Probable cause

The pilot's failure to maintain adequate airspeed during climb after takeoff, resulting in an aerodynamic stall.

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

Read the full NTSB narrative

The pilot stated that he conducted the preflight, engine start, taxi, and takeoff, with no anomalies noted. The pilot described a full-power takeoff at 5,800 rpm and a rotation speed of 48 mph, and then he lowered the nose of the airplane to climb out at 60 mph. As the airplane reached treetop height, the left wing dipped due to turbulence over the trees, and the pilot perceived a loss of engine power. The pilot said he again lowered the nose to gain airspeed, but the airplane nosed over and struck trees, the ground, and a fence. A postaccident examination of the airplane revealed no pre-impact mechanical anomalies. There was no checklist for the airplane, no placarded V-speeds in the cockpit, and no color-coded airspeed range markings on the airspeed indicator. According to the airplane kit’s manufacturer, the airplane’s rotation speed was 60 mph and the standard climb speed was 65 mph. The stall speed for the airplane was approximately 44 mph with the flaps retracted, depending on the airplane’s weight and the builders' modifications.

Quoted verbatim from the NTSB record.

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