N34926

Substantial
Serious

INTERSTATE S1AS/N: 121

Accident Details

Date
Saturday, May 1, 2010
NTSB Number
ERA10LA251
Location
Lakeland, FL
Event ID
20100503X83546
Coordinates
28.250278, -81.919998
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 clearance from terrain for undetermined reasons.

Aircraft Information

Registration
Make
INTERSTATE
Serial Number
121
Engine Type
Reciprocating
Year Built
1941
Model / ICAO
S1AS1
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
2
FAA Model
S-1A

Registered Owner (Current)

Name
PIETSCH KENT D
Address
6100 87TH ST NW
City
BURLINGTON
State / Zip Code
ND 58722-9605
Country
United States

Analysis

On May 1, 2010, about 1852 eastern daylight time, an Interstate S1A, N34926, registered to and operated by a private individual, collided with the ground shortly after takeoff from a private airstrip in the vicinity of Lakeland, Florida. The sport pilot sustained serious injuries, and the airplane was substantially damaged. Visual meteorological conditions prevailed and no flight plan was filed for the personal flight operated under the provisions of 14 Code of Federal Regulations, Part 91. The flight was originating at the time of the accident.

A witness located at the private airstrip observed the airplane climb to approximately 500 feet after takeoff. She reported that as the airplane was turning to the left, the nose of the airplane “dived”, and the airplane descended rapidly. She stated that as the airplane descended toward the ground, the pilot pulled up at the last few seconds, clipped a tree, and landed hard in a field. The airplane continued to travel forward through a fence and across a dirt road, where it nosed over and came to rest inverted.

Examination of the airplane by a Federal Aviation Administration inspector revealed that the airplane impacted a grass field. Three large propeller strikes were observed along the ground scar. Flight control continuity was established to all flight control surfaces and flight control system components revealed no evidence of preimpact mechanical malfunction. Examination of the fuel system revealed an undetermined amount of fuel remained in the fuel tanks. No water or debris was found in the fuel system. Examination of the engine revealed valve train continuity, compression, and spark from the magneto leads. The examination of the engine and system components revealed no evidence of preimpact mechanical malfunctions.

The NTSB investigator-in-charge did not receive NTSB Form 6120.1, Pilot/Operator Report from the pilot.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ERA10LA251