N84NS

Substantial
Serious

Seguine Swift IIS/N: 01

Accident Details

Date
Monday, December 24, 2012
NTSB Number
CEN13LA116
Location
San Antonio, TX
Event ID
20121231X00053
Coordinates
29.570278, -98.468330
Aircraft Damage
Substantial
Highest Injury
Serious
Fatalities
0
Serious Injuries
1
Minor Injuries
1
Uninjured
0
Total Aboard
2

Probable Cause and Findings

The pilot's failure to attain a proper pitch attitude and airspeed during initial climb, which resulted in an aerodynamic stall.

Aircraft Information

Registration
Make
SEGUINE
Serial Number
01
Engine Type
Reciprocating
Model / ICAO
Swift IISBM3
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
2
FAA Model
SWIFT II

Registered Owner (Current)

Name
SNYDER GEORGE W
Address
5243 S BLOOMFIELD DR
City
TUCSON
State / Zip Code
AZ 85746-3941
Country
United States

Analysis

On December 24, 2012, about 1015 central standard time, an experimental amateur-built Swift II, N84NS, impacted terrain following a loss of control after takeoff from Twin-Oaks Airport (T94), San Antonio, Texas. The airplane sustained substantial damage. The pilot sustained serious injuries and the pilot rated passenger sustain minor injuries. The airplane was registered to and operated by the pilot under 14 Code of Federal Regulations Part 91 as a personal flight. Visual meteorological conditions prevailed and a flight plan had not been filed for the local flight that was originating at the time of the accident.

The pilot stated that during takeoff on runway 30 (2,225 feet by 30 feet, turf), he rotated the airplane about 75-80 knots. The airplane experienced a normal climb until reaching about 50-75 feet above ground level, when the airplane "suddenly" pitched left and was unresponsive to control inputs. The pilot tried to flare the airplane and reduce engine power "just before" the airplane impacted the ground. The airplane also impacted fences and a shed.

According to a Federal Aviation Administration inspector, a witness stated that the airplane pitched up abnormally. The pilot had modified the wings, and the wing stall progression was from the wing tip to wing root. There was about 12 gallons of fuel in the left wing fuel. The pilot stated that he was unable to counteract the left roll. Examination of the airplane flight controls confirmed flight control continuity.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN13LA116