N925DP

Substantial
None

PFLUGRADT KitfoxS/N: KA13063258

Accident Details

Date
Tuesday, March 20, 2018
NTSB Number
WPR18LA111
Location
Clatskanie, OR
Event ID
20180323X80752
Coordinates
46.059791, -123.270965
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

A partial loss of engine power due to an improperly secured throttle cable set screw.

Aircraft Information

Registration
Make
PFLUGRADT
Serial Number
KA13063258
Engine Type
Reciprocating
Year Built
2014
Model / ICAO
KitfoxBPAT
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
2
FAA Model
KITFOX SUPERSPORT

Registered Owner (Current)

Name
PFLUGRADT DAUGLAS PAUL TRUSTEE
Address
303 AIRPORT WAY SW
City
MATTAWA
State / Zip Code
WA 99349-1908
Country
United States

Analysis

On March 20, 2018, about 1315 Pacific daylight time, an experimental Pflugradt Kitfox Super Sport airplane, N925DP, experienced a partial loss of engine power and collided with terrain near Clatskanie, Oregon. The airline transport pilot was not injured and the airplane sustained substantial damage to the right wing. The airplane was registered to and operated by the pilot as a Title 14 Code of Federal Regulations Part 91 personal flight. Visual meteorological conditions prevailed, and no flight plan was filed. The flight originated from Pacific City State Airport (PFC), Pacific City, Oregon at 1200 and was destined for Pearson Field Airport (VUO), Vancouver, Washington

The pilot reported that he departed from PFC and he followed the coast and Columbia river en route to VUO. About 800 ft above the Columbia river, he advanced the throttle to climb when the engine started to lose power. The pilot elected to land on a nearby treeless island in the river. The airplane landed uneventfully, and during the landing roll, the main wheels sunk into the ground and the airplane nosed over and came to rest on its back.

Postaccident examination of the airplane by a Federal Aviation Administration Inspector revealed that the throttle cable was loose at the throttle body attachment arm. When manipulated, the cable moved freely with no corresponding motion on the throttle body arm. The cable set screw on the aft side of the throttle body arm backed slightly out of its original position and was no longer securing the throttle cable.

Review of the maintenance logbooks revealed the the throttle body arm was built by the owner and was installed on the airplane on July 30, 2017, at 1,092.5 hours, which is about 204 hours prior to the accident. In addition, a vernier style throttle cable was installed on August 30, 2017 at 1,137 hours, about 159 hours prior to 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# WPR18LA111