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Aviation safety reports, made easier to study

NTSB Reports is an independent research and search tool for public aviation accident and incident records. It brings NTSB aviation reports, structured fields, docket files, extracted figures, photos, videos, and update history into one searchable interface.

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NTSB Report

June 30, 1996 · Cessna 172H · N1686F

Pierce, CO

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
June 30, 1996
Injury Outcomes
No injuries (3 uninjured)
Location
Pierce, CO
Aircraft
Cessna 172H
Tail Number
N1686F
Injuries
None
Aircraft Damage
Substantial
NTSB Number
FTW96LA281

While on a student training flight, the flight instructor retarded the throttle and activated the carburetor heat to simulate an engine failure. At the termination of the exercise when the throttle was advanced and the carburetor heat terminated, the engine failed to respond. A forced landing was made in a field which was unsuitable terrain for a safe landing. No evidence was found during the investigation to account for the engine response failure.

NTSB Probable Cause

a loss of engine power for undetermined reasons. A factor was the unsuitable terrain.

Full Narrative

On June 29, 1996, at 2000 mountain daylight time, a Cessna 172H, N1686F, made a forced landing in a field approximately 9 miles east of Pierce, Colorado, while on an instructional flight. The certified flight instructor, student pilot, and passenger were not injured and the aircraft sustained substantial damage. The flight was being conducted under Title 14 CFR Part 91 and no flight plan was filed. Visual meteorological conditions prevailed for this local area instructional flight which departed Greeley-Weld County, Colorado, Airport at 1900. According to the flight instructor, he gave the student a simulated engine failure by retarding the throttle. After an idle descent of about 1 and 1/2 minutes, the exercise was terminated and power was added. The engine failed to respond and an emergency landing was made in a field. During landing roll, the nose gear collapsed and damage was sustained to one wing and the fire wall. In an interview with the flight instructor, he stated that carburetor heat had been applied when the engine was retarded at the beginning of the exercise and had been removed when the throttle was advanced. He also stated the engine was cleared several times during the descent. An examination of the engine was conducted by the IIC assisted by an FAA airworthiness inspector, and representatives of the airframe and engine manufacturer. No evidence was found to explain the loss of power. Due to damage to supporting structure, the engine was not run during the examination.

Flight

Event TypeAccident
Event Time20:00 MDT
Nearest Airport0nm
Runway0
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftCessna 172H
Tail NumberN1686F
Aircraft CategoryAir
DamageSubstantial
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsLycoming · O-360-A1A · Reciprocating · 180
Seats4

People & Injuries

Injury SummaryNo injuries (3 uninjured)
Fatal0
Serious0
Minor0
Uninjured3
Total3
Crew 1Age 44 · First Class

Conditions

ConditionsVMC
LightDaylight
Wind130° @ 6 kt
Visibility10 sm
CeilingOvercast 11000 ft
Temperature / Dew Point48
Altimeter30.00 inHg
Observation Time02:16
Weather SourceWFAC

Appendix: Source Data