N98150

Substantial
None

Piper PA-28-140B S/N: 28-26075

Accident Details

Date
Wednesday, March 19, 1997
NTSB Number
FTW97LA129
Location
FORT COLLINS, CO
Event ID
20001208X07537
Coordinates
40.650695, -105.029983
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

a total loss of power for reasons undetermined. A factor was unsuitable terrain for a forced landing.

Aircraft Information

Registration
Make
PIPER
Serial Number
28-26075
Engine Type
Reciprocating
Year Built
1969
Model / ICAO
PA-28-140B P28A
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
4
FAA Model
PA-28-140

Registered Owner (Current)

Name
SCHAULIN FREDERICK S
Address
215 BLOCK DR
City
FORT COLLINS
State / Zip Code
CO 80524-2717
Country
United States

Analysis

On March 19, 1997, at 0709 mountain standard time, a Piper PA-28-140B, N98150, operated by Bob Gates Aviation and doing business as The Pilot Center, was substantially damaged when it struck a post during an emergency landing at Fort Collins, Colorado. The private pilot, the sole occupant, was not injured. Visual meteorological conditions prevailed, and no flight plan was filed for the personal flight conducted under Title 14 CFR Part 91. The flight originated at Fort Collins-Fort Collins Downtown Airpark minutes before the accident.

The pilot said that shortly after taking off from runway 11, the engine lost power. He "pumped the throttle" and the "engine sputtered twice and quit again." The pilot then made a emergency landing 1 mile south of the airport in the Prospect Ponds Natural Wildlife Area. During the landing roll, the pilot was able to avoid a concrete picnic table but the left wing struck a trail marker post, shearing off and driving the landing gear through the wing.

According to the operator, the engine was functionally tested later that day and it operated normally. They carburetor was disassembled and inspected the following morning. The accelerator pump operated normally, and the metal float moved freely. There was no evidence that the float may have shifted and was binding against the housing. There were no obstructions in the one-piece venturi.

The pilot said he had experience in the Piper PA-28-180, but had very few hours in the PA-28-140. Fuel selector operation on both types of airplanes is identical. The pilot said he was thoroughly familiar with properly selecting a fuel tank with the fuel selector. The pilot said he leaned the mixture at 1,800 rpm (revolutions per minute) prior to takeoff. According to Textron Lycoming, the mixture should be leaned at full (takeoff) power. If the mixture is leaned at a lower power setting, the mixture will enrich as power is applied.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# FTW97LA129