DFW06CA084

NTSB accident investigation · Piper PA-28-140 · Cherokee City, AR · March 15, 2006

Accident · No injuriesData collectionFinal report
Date
March 15, 2006, 06:30 local (12:30 UTC)
Place
Cherokee City, AR
Injuries
2 uninjured
Damage
Substantial damage
Phase of flight
Approach
Aircraft
N5537FPiper PA-28-140
Weather
Visual (VMC) · Day
Status
Completed · report August 29, 2006
Report
Approved by Office Director
Parties
Little Rock, Arkansas
FAA report
20060315003599A
Case key
63346

From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.

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Probable cause

The loss of engine power for undetermined reasons. A contributing factor was the lack of suitable terrain for the forced landing.

Sequence of events

NTSB’s coding before 2008: each occurrence and phase of flight, and the causes and factors under it. The codes are defined in NTSB’s coding manual.

Loss of engine power(partial) - nonmechanicalGo-around (vfr)
Reason for occurrence undeterminedCause
Forced landingEmergency descent/landing
In flight collision with objectEmergency landing
Object - fence
Object - tree(s)
Terrain condition - none suitableFactor

Analysis

The 75-hour private pilot/owner planned a simulated low-approach to an open area within his property where he was planning on building a grass airstrip. The pilot reported that he had no intention to land and had planned to execute a go-around and then continue his flight on to his intended destination. As the pilot approached the field to the south, he added one notch of flaps and retarded the throttle to idle. He did not apply carburetor heat. When the airplane was on final approach, at approximately 200 feet above the ground, the pilot added power to initiate the intended go-around; however, there was no response and power did not increase above idle speed. The pilot was unable to maintain altitude and the airplane landed short of the field, colliding with a fence and tree stumps. The pilot stated that when the airplane first touched down, the engine regained full power but, he immediately pulled the power back to idle to prevent further damage. The pilot and the passenger were able to egress the airplane unassisted and were not injured. Both wings were reported to have sustained structural damage. According to the pilot, he had owned the airplane for approximately seven months and had no previous problems with the engine. At the time of the accident, the temperature was reported as 37 degrees Fahrenheit and the dew point was 21 degrees Fahrenheit. The reason for the intermittent loss of engine power could not be determined.

Factual narrative

The 75-hour private pilot/owner planned a simulated low-approach to an open area within his property where he was planning on building a grass airstrip. The pilot reported he had no intention to land and had planned to execute a go-around and then continue his flight on to his intended destination. As the pilot approached the field to the south, he added one notch of flaps and retarded the throttle to idle. He did not apply carburetor heat. When the airplane was on final approach, while at approximately 200 feet above the ground, the pilot added power to initiate the intended go-around; however, there was no response and power did not increase above idle speed. The pilot was unable to maintain altitude and the airplane landed short of the field, colliding with a fence and tree stumps. The pilot stated that when the airplane first touched down, the engine regained full power but, he immediately pulled the power back to idle to prevent further damage. The pilot and the passenger were able to egress the airplane unassisted and were not injured. Both wings were reported to have sustained structural damage. According to the pilot, he had owned the airplane for approximately seven months and had no previous problems with the engine. At the time of the accident, the temperature was reported as 37 degrees Fahrenheit and the dew point was 21 degrees Fahrenheit. The reason for the intermittent loss of engine power could not be determined.

Aircraft

Registration
N5537F
Reported as
Piper PA-28-140
Category
Airplane
Serial number
28-24936
Engine
Lycoming O-320, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Registered owner
Donald Amos
Airworthiness certificate
Standard, Normal
Departed
SLG · Siloam Springs, AR
Destination
GMJ · Grove, OK
Airport
NONE · None, runway 19

Matched to the registry by N-number and the event date; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
48
Certificate
Private
Airplane ratings
Single-engine land
Medical
Class 3
Flight hours
75 total · 66 in this make and model

Weather

Conditions
Visual (VMC) · Day
Visibility
10 statute miles
Temperature
37 °F, dew point 21 °F
Altimeter
30.26 inHg
Observed at
7 nm away

FAA reports on this event · 1

The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.

Other investigations on N5537F · 1

Matched to the same aircraft by N-number and date.