N269JW

Substantial
Serious

PIPER PA-36-285S/N: 36-7560063

Accident Details

Date
Friday, June 25, 2010
NTSB Number
CEN10LA348
Location
Fremont, NE
Event ID
20100628X51650
Coordinates
41.440521, -96.490051
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 loss of control for undetermined reasons.

Aircraft Information

Registration
N269JW
Make
PIPER
Serial Number
36-7560063
Engine Type
Reciprocating
Year Built
1975
Model / ICAO
PA-36-285PA36
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
JONES JAMES A
Address
PO BOX 481
Status
Deregistered
City
SUTTON
State / Zip Code
NE 68979-0481
Country
United States

Analysis

On June 25, 2010, about 1430 central daylight time, a Piper PA-36-285 airplane, N269JW, was substantially damaged following impact with terrain and a building near Fremont, Nebraska. The commercial pilot was seriously injured. The repositioning flight originated from Tekamah (TQE), Nebraska, about 1400 and was en route to a private airstrip near Sutton, Nebraska. The flight was being conducted under the provisions of 14 Code of Federal Regulations Part 91. Visual meteorological conditions prevailed at the time of the accident.

A witness, who as driving down a road, observed the airplane flying erratically towards him as if to land. The airplane then made a sharp turn towards a small alfalfa field next to the road. The airplane hit a fence with its right wing and a fence and pole with the left wing, before it collided with a building on a farm. The witness recalled that the propeller was turning when he saw the airplane and four ground scars indicative of propeller strikes were found at the accident scene. The airplane’s empennage and left wing were separated from the fuselage. The pilot had no recollection of the accident.

A postaccident examination of the wreckage by Federal Aviation (FAA) Inspectors confirmed flight control continuity to all control surfaces. Fuel was found in the right fuel tank and the left tank was compromised and empty. No anomalies were noted with the engine that would have precluded normal operation prior to impact. Each of the three propeller blades exhibited leading edge polishing and chord-wise scratches.

According to an FAA inspector, an annual inspection had been completed on the airplane on June 24, 2010, the day prior to the accident and the airplane had accumulated less than one hour of flight time since inspection. The engine had been overhauled in 2001, and had accumulated about 65 hours since overhaul at the time of the accident.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN10LA348