FTW00LA263

NTSB accident investigation · Piper PA-32-260 · Clinton, OK · June 3, 2000

Accident · No injuriesLimited investigationFinal report
Date
June 3, 2000, 15:00 local (20:00 UTC)
Place
Clinton, OK
Injuries
2 uninjured
Damage
Substantial damage
Phase of flight
Approach
Aircraft
N3869WPiper PA-32-260
Weather
Visual (VMC) · Day
Status
Completed · report April 25, 2001
Report
Approved by Office Director
FAA report
20000603014579A
Case key
50298

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

On this page

Probable cause

The pilot's improper setting of the cockpit fuel selector, which resulted in a total loss of engine power and 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(total) - nonmechanicalApproach - vfr pattern - final approach
Fuel tank selector position - improperPilot in commandCause
Forced landingEmergency descent/landing
On ground/water encounter with terrain/waterLanding - roll
Terrain condition - berm

Analysis

The airplane was executing a VFR approach, turning from the base leg to short final, when the engine lost total power. During the ensuing forced landing, the airplane touched down in a field short of the runway, the nose landing gear collapsed, and the airplane came to a stop upright. The pilot reported to the FAA that 'he was not sure if the fuel selector was in the detent for the selected tank and he did not have time to check prior to landing.'

Factual narrative

On June 3, 2000, at 1500 central daylight time, a Piper PA-32-260 airplane, N3869W, was substantially damaged during a forced landing following a loss of engine power at the Clinton Municipal Airport, near Clinton, Oklahoma. The private pilot, who was the registered owner and operator of the airplane, and his passenger were not injured. Visual meteorological conditions prevailed and a flight plan was not filed for the 14 Code of Federal Regulations Part 91 personal flight. The local flight originated from the Clinton Municipal Airport.

According to the FAA inspector, the airplane was turning from the "base leg to short final" for runway 17 when the engine lost total power. During the ensuing forced landing, the airplane touched down in a field short of the runway and impacted a dirt terrace. The nose gear collapsed, and the airplane came to a stop upright. Following the accident, the pilot reported that, "he was not sure if the fuel selector was in the detent for the selected tank and he did not have time to check prior to landing."

The FAA inspector reported that the engine firewall was structurally damaged, and both wings were compromised at their respective attaching points to the fuselage. There was also damage to the "structure at the main landing gear attach points."

This damage was initially reported to the NTSB as minor. Subsequently, on October 3, 2000, the damage was reported as substantial. Additionally, multiple attempts to obtain a completed NTSB Form 6120.1/2, Pilot/Operator Aircraft Accident Report, from the pilot/owner were unsuccessful.

Aircraft

Registration
N3869W
Reported as
Piper PA-32-260
Category
Airplane
Serial number
32-814
Airframe hours
5,800
Engine
Lycoming O-540-E4B5, 250 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Registered owner
Clifford D. Jones
Airworthiness certificate
Standard, Normal
Departed
CLK · Clinton, OK
Airport
CLK · Clinton Municipal, runway 17, 4,300 × 75 ft, asphalt

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
61
Certificate
Private
Airplane ratings
Multi-engine land, Single-engine land
Instrument ratings
Airplane
Medical
Class 3, Valid Medical--w/ waivers/lim
Seat
Left
Flight hours
3,000 total · 200 in this make and model · 75 in the last 90 days

Weather

Conditions
Visual (VMC) · Day
Wind
100° at 4 knots
Visibility
10 statute miles
Lowest ceiling
3,200 ft broken
Temperature
75 °F, dew point 70 °F
Altimeter
30.00 inHg
Observed at
LAW, 60 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 N3869W · 1

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