CEN17LA010

NTSB accident investigation · Piper PA 28-180 · Clarendon, TX · October 2, 2016

Accident · Minor injuriesLimited investigationFinal report
Date
October 2, 2016, 15:20 local (20:20 UTC)
Place
Clarendon, TX
Injuries
1 minor
Damage
Substantial damage
Phase of flight
Enroute
Aircraft
N5196LPiper PA 28-180
Defining event
Enroute: Loss of engine power (total)
Weather
Visual (VMC) · Day
Status
Completed · report October 17, 2017
Report
Approved by Office Director
NTSB office
Central Region
Parties
Federal Aviation Administration
FAA report
20161002016159A
Case key
94149

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 failure of a cylinder piston pin, which resulted in an obstructed oil inlet screen, reduced the amount of oil available to the engine, and led to the subsequent loss of engine power. Contributing to the accident was the failure of the nonmechanic, who had recently changed the oil and oil filter, to recognize that metal in the filter was indicative of a problem.

Findings · 3

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: oilAircraft › Fluids/misc hardware · Fluid levelPiper PA-28-180: 4 casesAll aircraft: 174 casesProbable cause
Maintenance: scheduled/routine maintenancePersonnel issues › Task performance · OtherPiper PA-28-180: 6 casesAll aircraft: 320 casesProbable cause

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 student pilot was conducting a cross-country personal flight. The student pilot reported that, while in cruise flight, the single-engine airplane lost power. He then performed a forced landing to a field, during which the wings and firewall were damaged. Examination of the engine revealed damage consistent with lubrication distress. Further, a cylinder piston pin was found broken, and metal was found in the oil pickup screen and in the oil filter, which had recently been changed. It is likely that the degraded piston pin was the source of the metal in the oil, which clogged the oil inlet screen and reduced the amount of oil available to the engine and resulted in the loss of engine power. A nonmechanic had performed preventative maintenance and changed the oil and oil filter shortly before the accident. He reported that he noticed the metal in the filter but did not consider it to be an indication of a problem.

Factual narrative

On October 2, 2016, about 1520 central daylight time, a Piper PA-28-180 airplane, N5196L, was damaged during a forced landing near Clarendon, Texas. The student rated pilot sustained minor injuries and the airplane was substantially damaged. The airplane was to Tohijoco LLC and operated by Coyote Flight under the provisions of 14 Code of Federal Regulations Part 91 as a personal flight. Visual meteorological conditions prevailed for the flight which operated under visual flight rules flight following. The cross-country flight departed the Rick Husband Amarillo International Airport (AMA), Amarillo, Texas, at 1405 and was en route to the Childress Municipal Airport (CDS), Childress, Texas.The pilot reported to the responding FAA inspector that while in cruise flight the engine lost power and he performed a forced landing to a field. During the landing, the airplane's wings and firewall were damaged. The airplane was transported to the operator's facility for an examination. The engine was examined under the auspices of an Federal Aviation Administration inspector. The examination noted damage to the engine was consistent with lubrication distress. Further examination of the engine found the metal oil screen pickup fouled with metal. The source of the metal was from a broken piston pin. During the examination, it was discovered that the engine's oil and oil filter had recently been changed. The oil filter, which had been removed, was examined and metal was found in the filter. A non-mechanic rated person performed preventative maintenance, changed the oil and oil filter prior to the accident. During the oil change, he noticed the metal, but did not consider this to be an indication of a problem.

Aircraft

Registration
N5196L
Reported as
Piper PA 28-180 (180)
Category
Airplane
Serial number
28-4486
Built
1967
Engine
Lycoming O-360 SER, 180 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Operator
Coyote Flight
Registered owner
Tohijoco LLC
Airworthiness certificate
Standard, Normal
Departed
AMA · Amarillo, TX
Destination
CDS · Childress, TX
Flight plan
VFR

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
34
Injuries
Minor
Certificate
Student
Medical
Class 3, Without waivers/limitations
Seat
Left

Weather

Conditions
Visual (VMC) · Day
Wind
160° at 18 knots, gusting 26
Visibility
10 statute miles
Lowest ceiling
None
Temperature
86 °F, dew point 55 °F
Altimeter
30.00 inHg
Observed at
KAMA, 44 nm away

Docket · 1

The files NTSB released with the investigation on August 30, 2017, on NTSB’s docket system: statements, records, photos and specialists’ reports. 95 KB 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.

Other investigations on N5196L · 1

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