MIA03LA133

NTSB accident investigation · Piper PA-28-180 · Ocean Springs, MS · June 16, 2003

Accident · Minor injuriesLimited investigationFinal report
Date
June 16, 2003, 10:13 local (15:13 UTC)
Place
Ocean Springs, MS
Injuries
1 minor
Damage
Substantial damage
Phase of flight
Initial climb
Aircraft
N8378WPiper PA-28-180
Weather
Visual (VMC) · Day
Status
Completed · report March 30, 2004
Report
Approved by Office Director
Parties
FAA FSDO
FAA report
20030616011389A
Case key
57343

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

A loss of engine power due to starvation as a result of the pilot's continued operation of an airplane with known deficiencies.

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) - mech failure/malfTakeoff - initial climb
Fuel system,selector/valve - malfunctionCause
Maintenance - not performedPilot in commandCause
Fluid,fuel - starvation
Operation with known deficiencies in equipment - continuedPilot in commandCause
Forced landingEmergency descent/landing
On ground/water encounter with terrain/waterEmergency landing
Terrain condition - swampy
Nose overLanding - flare/touchdown

Analysis

The pilot stated that during the takeoff/initial climb, while near the end of the runway, at an altitude of 150 feet, the airplane's engine began to sputter and act as if it was going to cease operating. He stated that he glanced at the fuel selector switch and confirmed that it appeared to be at the proper position, and he then started pumping the throttle. He said the engine seemed as if it would "recover" but as he continued to pump the throttle, the engine finally ceased operating. He said he then maneuvered to avoid obstacles and executed a forced landing into the marsh. During the landing the airplane flipped over its back and was damaged. After recovery from the marsh, an FAA examiner examined the accident airplane, and the examination revealed that the fuel selector valve had been set beyond the "right tank" detent, which when tested, prevented the flow of fuel to the engine. In addition, the inspector said that the pilot told him that he had problems previously with the engine ceasing to operate when the fuel selector valve was in the "right tank" position, so he had been rotating it beyond the detent for the "right tank" position and had experienced no problems since. The inspector stated that records revealed that the accident airplane had last received an annual inspection on May 10, 1997.

Factual narrative

On June 16, 2003, about 1013 central daylight time, a Piper PA-28-180, N8378W, registered to and operated by a private individual as a Title 14 CFR Part 91 personal flight, crashed shortly after takeoff from Ocean Springs, Mississippi. Visual meteorological conditions prevailed, and no flight plan was filed. The private-rated pilot received minor injuries, and the airplane incurred substantial damage. The flight was originating at the time of the accident.

The pilot stated that during the takeoff/initial climb, while near the end of the runway, at an altitude of 150 feet, the airplane's engine began to sputter and act as if it was going to cease operating. He stated that he glanced at the fuel selector switch and confirmed that it appeared to be at the proper position, and he then started pumping the throttle. He said the engine seemed as if it would "recover" but as he continued to pump the throttle, the engine finally ceased operating. He said he then maneuvered to avoid obstacles and executed a forced landing into the marsh. During the landing the airplane flipped over its back and was damaged.

After recovery from the marsh, an FAA examiner examined the accident airplane, and the examination revealed that the fuel selector valve had been set beyond the "right tank" detent, which when tested, prevented the flow of fuel to the engine. In addition, the inspector said that the pilot told him that he had problems previously with the engine ceasing to operate when the fuel selector valve was in the "right tank" position, so he had been rotating it beyond the detent for the "right tank" position and had experienced no problems since. The inspector stated that records revealed that the accident airplane had last received an annual inspection on May 10, 1997.

Aircraft

Registration
N8378W
Reported as
Piper PA-28-180
Category
Airplane
Serial number
28-2579
Airframe hours
4,592
Engine
Lycoming O-360-A3A, 180 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Registered owner
Partick J. Hill
Airworthiness certificate
Standard, Normal
Last inspection
Annual · November 1, 1997 · 13 hours before
Departed
5R2 · Ocean Springs, MS
Destination
5R2
Airport
5R2 · Ocean Springas Airport

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
74
Injuries
Minor
Certificate
Private
Airplane ratings
Single-engine land
Instrument ratings
Airplane
Medical
Class 3, Valid Medical--w/ waivers/lim
Seat
Left
Flight hours
1,176 total · 20 in this make and model

Weather

Conditions
Visual (VMC) · Day
Wind
0° at 0 knots
Visibility
10 statute miles
Lowest ceiling
None
Temperature
86 °F, dew point 73 °F
Altimeter
30.01 inHg
Observed at
PQL

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 N8378W · 3

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