FTW96LA199

NTSB accident investigation · Piper PA-28 · Mountain Home, AR · May 1, 1996

Accident · Minor injuriesLimited investigationFinal report
Date
May 1, 1996, 13:00 local (18:00 UTC)
Place
Mountain Home, AR
Injuries
2 minor
Damage
Substantial damage
Phase of flight
Initial climb
Aircraft
N9869KPiper PA-28
Weather
Visual (VMC) · Day
Status
Completed · report November 25, 1996
Report
Approved by Office Director
FAA report
19960501009219A
Case key
19828

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 pilot's failure to visually check the fuel quantity during the preflight inspection. A factor was the unsuitable 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 powerTakeoff - initial climb
Fluid,fuel - exhaustionCause
Aircraft preflight - inadequatePilot in commandCause
Forced landingEmergency landing after takeoff
In flight collision with terrain/waterEmergency landing after takeoff
Terrain condition - none suitableFactor
Terrain condition - rock(s)/boulder(s)

Analysis

The pilot stated 'Upon takeoff, the engine died. I believe from fuel starvation.' The airplane was substantially damaged during the emergency landing to a rocky ravine. The pilot reported that he did not visually check the airplane's fuel quantity during his preflight inspection.

Factual narrative

On May 1, 1996, at 1300 central daylight time, a Piper PA-28, N9869K, registered to and operated by a private owner as a Title 14 CFR Part 91 personal flight, was substantially damaged during a forced landing following a loss of engine power during takeoff. Visual meteorological conditions prevailed and a flight plan was not filed. The private pilot and his passenger received minor injuries. The flight originated from a private airstrip near Mountain Home, Arkansas.

Shortly after takeoff, at approximately 100 feet AGL, the engine lost power. During the emergency landing to a rocky ravine, the fuselage and both wings were damaged. Both fuel tanks were compromised.

The pilot reported that during his preflight inspection, he did not visually check the fuel quantity. The airplane had been fueled 5 days earlier, and approximately 2 to 3 hours had been flown since then. The pilot also reported that the accident "possibl[y] could have been prevented by a more thorough preflight." He further reported that he did not know, at the time of departure, what the total fuel on board was. The pilot stated that "upon takeoff, the engine died. I believe from fuel starvation."

Inspection of the airplane by the pilot revealed that the fuel sump valve was missing. The pilot reported that "the interior threads inside the AN fitting were all intact." However, the attached photograph shows thread damage.

Aircraft

Registration
N9869K
Reported as
Piper PA-28
Category
Airplane
Serial number
28-7816199
Airframe hours
5,015
Engine
Lycoming O-320D3G, 160 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Registered owner
Paul H. Wedin
Airworthiness certificate
Standard, Normal
Last inspection
Annual · January 20, 1996 · 44 hours before
Departed
6AR4
Destination
BPK

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
53
Certificate
Private
Airplane ratings
Single-engine land, Multi-engine land
Medical
Class 3, Valid Medical--no waivers/lim.
Seat
Left
Flight hours
2,128 total · 40 in this make and model

Weather

Conditions
Visual (VMC) · Day
Visibility
10 statute miles
Lowest ceiling
None
Temperature
70 °F

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 N9869K · 1

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