N91642

Substantial
Minor

Bradley Rans S-7S/N: 491080

Accident Details

Date
Tuesday, August 28, 2001
NTSB Number
DEN01LA153
Location
Fruita, CO
Event ID
20010831X01849
Coordinates
39.222499, -108.731391
Aircraft Damage
Substantial
Highest Injury
Minor
Fatalities
0
Serious Injuries
0
Minor Injuries
1
Uninjured
0
Total Aboard
1

Probable Cause and Findings

loss of engine power due to both piston rings failing, and the subsequent inadvertent stall/spin during the attempted forced landing. A contributing factor was the lack of suitable terrain for a forced landing.

Aircraft Information

Registration
Make
BRADLEY
Serial Number
491080
Engine Type
Reciprocating
Model / ICAO
Rans S-7
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
2
FAA Model
RANS S-7

Registered Owner (Current)

Name
WEHLING PATRICK L JR
Address
1620 O RD
City
LOMA
State / Zip Code
CO 81524-9414
Country
United States

Analysis

On August 28, 2001, at approximately 1340 mountain daylight time, a Bradley Rans S-7 homebuilt airplane, N91642, was substantially damaged during a forced landing following a loss of engine power near Fruita, Colorado. The airline transport pilot, the sole occupant aboard the airplane, was not injured. A private individual was operating the airplane under Title 14 CFR Part 91. Visual meteorological conditions prevailed for the local test flight that was originating at the time of the accident. No flight plan had been filed.

According to the pilot, shortly after takeoff (approximately 30 feet above the ground), the engine began to lose power. He said the airplane lost the ability to climb at about 60 feet above ground level. The pilot said there was a fence and a barn directly in his flight path; he turned the aircraft left toward an alfalfa field to make an emergency landing. The engine continued to lose power and attempts to regain engine power failed. The airplane started to lose airspeed until the onset of a stall. The pilot reduced the airplane's angle of attack so that the airplane would not stall. The airplane contacted the ground with its right wing first, then rotated until its heading was 180 degrees from its flight path, subsequently coming to rest against a fence. The airplane's engine mount, both wings, and the horizontal stabilizer were bent, and the fuselage was wrinkled.

Postaccident examination of the two cylinder engine by the pilot revealed that both piston rings had failed. The owner reported that the engine had approximately 4 hours of flight operation time.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# DEN01LA153