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NTSB Report

March 19, 1997 · Piper PA-28-140B · N98150

Fort Collins, CO

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
March 19, 1997
Injury Outcomes
No injuries (1 uninjured)
Location
Fort Collins, CO
Aircraft
Piper PA-28-140B
Tail Number
N98150
Operator
Bob Gates Aviation
Injuries
None
Aircraft Damage
Substantial
NTSB Number
FTW97LA129

The engine lost power shortly after takeoff and the pilot made a forced landing. The engine was later functionally tested and it operated normally. After disassembling the carburetor, the accelerator pump was found to function 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 was thoroughly familiar with the operation of the fuel selector.

NTSB Probable Cause

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

Full Narrative

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.

Flight

Event TypeAccident
Event Time07:09 MST
Nearest Airport0nm
Runway0
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftPiper PA-28-140B
Tail NumberN98150
Aircraft CategoryAir
DamageSubstantial
OperatorBob Gates Aviation
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsLycoming · O-320-E2A · Reciprocating · 150
Seats2

People & Injuries

Injury SummaryNo injuries (1 uninjured)
Fatal0
Serious0
Minor0
Uninjured1
Total1
Crew 1Age 60 · Third Class

Conditions

ConditionsVMC
LightDaylight
WindCalm
Visibility10 sm
CeilingNone
Temperature / Dew Point37 C / 0 C
Altimeter30.00 inHg
Observation Time14:15
Weather SourceWFAC

Appendix: Source Data