GAA18CA307

NTSB accident investigation · Piper PA28 · Butler, KY · May 27, 2018

Accident · No injuriesData collectionFinal report
Date
May 27, 2018, 18:18 local (22:18 UTC)
Place
Butler, KY
Injuries
2 uninjured
Damage
Substantial damage
Phase of flight
Enroute
Aircraft
N95410Piper PA28
Defining event
Enroute: Fuel starvation
Weather
Visual (VMC) · Day
Status
Completed · report November 5, 2018
Report
Approved by Office Director
NTSB office
General Aviation Accidents
Parties
FAA
FAA report
20180527012659A
Case key
97346

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 fuel management, which resulted in fuel starvation.

Findings · 4

NTSB’s coded findings. Those marked are part of the probable cause; the rest are factors or other findings. Under each, the cases with the same finding.

Fluids: fuelAircraft › Fluids/misc hardware · Fluid managementPiper PA-28-140: 32 casesAll aircraft: 1,695 casesProbable cause
Use of equip/info: use of equip/systemPersonnel issues › Task performance · PilotPiper PA-28-140: 16 casesAll aircraft: 1,391 casesProbable cause
Object/animal/substance: ground equipmentEnvironmental issues › Physical environment · Contributed to outcomePiper PA-28-140: 2 casesAll aircraft: 52 cases

Sequence of events

The events NTSB coded, in order, by phase of flight. The defining event is the one that best describes the accident. Under each, the cases with the same event anywhere in their sequence.

Analysis

The pilot reported that, while en route, the airplane's engine began to run roughly and lose power. He immediately turned toward the nearest airport and slowed the airplane to 100 knots. He added that he pushed the mixture to full rich, which caused a short burst of power that lasted just a few seconds. He then pumped the throttle and applied carburetor heat but then realized he did not have enough altitude to make the airport and began to look for an alternate landing site. The pilot further added that, after locating a ridgetop field, he slowed the airplane to 75 knots and pulled one notch of flaps and trimmed for landing. As he lined the airplane up with the field, he pulled full flaps about 300 ft above the ground. The touchdown was smooth, and the airplane continued the landing roll in 3-ft-tall wheat. Subsequently, the right wing struck an industrial irrigation nozzle, and the right wing separated from the fuselage. The airplane sustained substantial damage to the right wing and stabilator. The pilot reported that there were no preaccident mechanical failures or malfunctions with the airplane that would have precluded normal operation. The pilot added that, during the engine failure, he did not attempt to change the fuel tank from the empty right wing fuel tank and recommended to make the fuel selector check the first part of the restart procedure. The Federal Aviation Administration inspector reported that, while on scene, he was able to run the engine. He added that the left tank was about 1/2 full of fuel. He switched the fuel selector to the left tank and started the engine normally. The oil pressure was fine; the fuel pressure was normal on both the electric pump and engine-driven pump; and the magnetos checked fine.

Factual narrative

The pilot reported that, while enroute, the airplane's engine began to run rough and lose power. He immediately turned toward the nearest airport and slowed the airplane to 100 knots. He added that he pushed the mixture to full rich, which caused a short burst of power that lasted just a few seconds. He then pumped the throttle and applied carburetor heat, but then realized he did not have enough altitude to make the airport and began to look for an alternate landing site. He further added, that after locating a ridge top field, he slowed the airplane to 75 knots and pulled one notch of flaps and trimmed for landing. As he lined the airplane up with the field he pulled full flaps at about 300 ft above the ground. The touchdown was smooth and the airplane continued the landing roll in wheat that was approximately 3 ft tall. Subsequently, the right wing struck an industrial irrigation nozzle and the right wing separated from the fuselage. The airplane sustained substantial damage to the right wing and stabilator. The pilot reported that there were no preaccident mechanical failures or malfunctions with the airplane that would have precluded normal operation. The pilot added that, during the engine failure, he did not attempt to change fuel tanks from the empty right wing fuel tank, and as a recommendation to make the fuel selector check the first part of the restart procedure. The Federal Aviation Administration inspector reported that, while on scene, he was able to run the engine. He added, the left tank was approximately ½ full of fuel. He switched the fuel selector to the left tank and started the engine normally. The oil pressure was fine; fuel pressure normal on both the electric pump and engine driven pump; and the magnetos checked fine.

Aircraft

Registration
N95410
Reported as
Piper PA28 (140)
Category
Airplane
Serial number
28-25930
Built
1969
Airframe hours
3,885
Engine
Lycoming O-320-E2A, 150 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Airworthiness certificate
Standard, Utility; Standard, Normal
Last inspection
Annual · September 25, 2017
Departed
TKX · Kennett, MO
Destination
TZR · Columbus, OH
Equipment
Electronic flight bag or handheld device, Stall warning system

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
70
Injuries
None
Certificate
Private
Airplane ratings
Single-engine land
Medical
BasicMed, Without waivers/limitations
Last flight review
May 16, 2017
Seat
Left
Flight hours
552 total · 259 in this make and model · 442 as pilot in command · 30 in the last 90 days · 22 in the last 30 days · 8 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
Calm
Visibility
10 statute miles
Temperature
82 °F, dew point 75 °F
Altimeter
29.88 inHg
Observed at
KLUK, 22 nm away

Docket · 4

The files NTSB released with the investigation on September 6, 2018, on NTSB’s docket system: statements, records, photos and specialists’ reports. 1.3 MB in all.

FAA reports on this event · 1

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