N5DZ

Substantial
None

Zeidler SONERAI II S/N: 223

Accident Details

Date
Thursday, October 15, 1998
NTSB Number
NYC99LA011
Location
KENTON, OH
Event ID
20001211X11332
Coordinates
40.639514, -83.609313
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

The pilot's premature rotation and failure to obtain/maintain airspeed during the takeoff, which resulted in a stall and impact with the ground. Factors in this accident were the pilot's lack of total experience in tail-wheeled aircraft, and the nose high elevator trim setting.

Aircraft Information

Registration
N5DZ
Make
ZEIDLER
Serial Number
223
Engine Type
Reciprocating
Year Built
1983
Model / ICAO
SONERAI II BPAT
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
SALE REPORTED
Address
NONE
Status
Deregistered
City
XXX
State / Zip Code
OK 73125
Country
United States

Analysis

On October 15, 1998, about 1845 eastern daylight time, a homebuilt Sonerai II, N5DZ, was substantially damaged when it impacted terrain during takeoff from the Hardin County Airport (I95), Kenton, Ohio. The certificated private pilot was not injured. Visual meteorological conditions prevailed and no flight plan had been filed for the local personal flight conducted under 14 CFR Part 91.

In a written statement the pilot said the accident flight was his first flight in the tail-wheeled airplane. After several taxi trips on the runway to establish the airplane's ground handling characteristics, and to familiarize himself with the "visual perspective," a takeoff was initiated. The pilot stated the elevator trim was at a "too nose high attitude." The pilot further stated:

"...the aircraft became light on the wheels quite early...once the aircraft was 5-10 feet above the ground, all visual relationship with runway was lost due to the aircraft's limited visibility. Airspeed was 45-50 mph as the airplane ascended to about 20 feet and broke free of ground effect. (Aircraft stall speed is 55-60 mph) At which time the plane stalled straight level and impacted the ground....

Examination of the wreckage by an FAA Inspector did not reveal any pre-impact abnormalities of the airframe or engine.

A review of the pilot's logbook revealed 90 hours of total flight experience, all in tricycle gear aircraft.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# NYC99LA011