N4887S

Substantial
None

Piper PA-32-260 S/N: 32-7100011

Accident Details

Date
Friday, August 28, 1998
NTSB Number
CHI98LA330
Location
SAULT STE MARIE, MI
Event ID
20001211X10817
Coordinates
46.480735, -84.360748
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

the pilot's failure to maintain clearance between the airplane and the runway marker. A factor contributing to this accident was the runway marker.

Aircraft Information

Registration
Make
PIPER
Serial Number
32-7100011
Engine Type
Reciprocating
Year Built
1971
Model / ICAO
PA-32-260 PA32
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
6
FAA Model
PA-32-260

Registered Owner (Current)

Name
SLATER MICHAEL C
Address
PO BOX 295
City
STILLMORE
State / Zip Code
GA 30464-0295
Country
United States

Analysis

On August 28, 1998, at 1730 eastern daylight time (edt), a Piper PA-32-260, N4887S, sustained substantial damage when during back-taxi on runway 16 at the Chippewa County Airport, Sault Ste. Marie, Michigan, the airplane struck a runway distance remaining marker. Visual meteorological conditions prevailed at the time of the accident. The personal flight was being conducted under 14 CFR Part 91. There was no flight plan on file. The pilot and passenger on board reported no injuries. The local flight was originating at Sault Ste. Marie, Michigan.

In his written statement, the pilot said that he was back taxiing on runway 16 to position himself for takeoff on runway 34. While taxiing, the pilot noticed a deer on the east side of the runway. The pilot taxied along the west side of the runway, just outside of the runway lights. The pilot looked back over his shoulder to look for the deer. When he turned around, the pilot said he noticed that the airplane was too close to the runway lights. The pilot swerved the airplane to the right, where it subsequently struck the runway marker.

A Federal Aviation Administration (FAA) inspector examined the airplane at the airport. The leading edge of the airplane's right wing was crushed inward. The forward spar was bent aft. The right horizontal stabilizer was bent back at the leading edge and punctured inward underneath. Flight control continuity was confirmed. No anomalies were revealed in the airplane's engine or other airplane systems.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CHI98LA330