N2189H

Substantial
Minor

PIPER PA-28-181 S/N: 28-7990211

Accident Details

Date
Saturday, September 4, 1993
NTSB Number
BFO93LA165
Location
COLUMBIA STN, OH
Event ID
20001211X13341
Coordinates
41.380634, -81.790687
Aircraft Damage
Substantial
Highest Injury
Minor
Fatalities
0
Serious Injuries
0
Minor Injuries
1
Uninjured
2
Total Aboard
3

Probable Cause and Findings

THE PILOT'S DELAY IN INITIATING A GO-AROUND (ABORTED LANDING), AND HIS IMPROPER RAISING OF THE FLAPS AT A LOW AIRSPEED AFTER LIFT-OFF, WHICH RESULTED IN A STALL/MUSH. A FACTOR RELATED TO THE ACCIDENT WAS: THE PILOT'S FAILURE TO ATTAIN THE PROPER TOUCHDOWN POINT FOR LANDING.

Aircraft Information

Registration
N2189H
Make
PIPER
Serial Number
28-7990211
Engine Type
Reciprocating
Model / ICAO
PA-28-181 P28A
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
ILLINOIS VALLEY FLYING CLUB INC
Address
PO BOX 293
Status
Deregistered
City
PERU
State / Zip Code
IL 61354
Country
United States

Analysis

On Monday, August 9, 1993, at about 1245 EDT, a Piper PA-28-181, N2189H, owned and operated by the Illinois Valley Flying Club, Incorporated of Peru, Illinois, continued off the departure end of runway 36 after landing and was substantially damaged. The pilot received minor injuries; the two passengers were not injured. Visual meteorological conditions prevailed, and no flight plan was filed. The flight originated at Bolling Green, Ohio, and was conducted under 14 CFR Part 91.

The pilot reported that during the approach, the airplane was high, and subsequently, it touched down long. He said he elected to go around when there appeared to be an inadequate amount of runway remaining to stop. He initiated a go-around by applying full throttle. He said the airplane did not seem to climb fast enough, so he raised the flaps, and the airplane settled. It touched down hard and the nose gear collapsed. The airplane then angled off the runway near the departure end and encountered soft terrain. Subsequently, it slid into brush and trees and was substantially damaged.

During a post-accident examination of the airplane, the throttle was found in the full forward position. The condition of the propeller indicated that the engine was running when the accident occurred. No malfunction or pre-accident failure of the aircraft or engine was found.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# BFO93LA165