N98D

Substantial
None

MARK DIVITA RV-8S/N: 82963

Accident Details

Date
Sunday, September 18, 2011
NTSB Number
CEN11LA658
Location
Lancaster, TX
Event ID
20110920X75214
Coordinates
32.577499, -96.717498
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

The failure of the tailwheel to remain locked during a crosswind landing, which resulted in a loss of directional control.

Aircraft Information

Registration
N98D
Make
MARK DIVITA
Serial Number
82963
Engine Type
Reciprocating
Year Built
2011
Model / ICAO
RV-8RV8
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
DIVITA MARK
Address
112 OAK HOLLOW LN
Status
Deregistered
City
RED OAK
State / Zip Code
TX 75154-4610
Country
United States

Analysis

On September 18, 2011, approximately 1540 central daylight time, a Mark Divita RV-8, N98D, experienced a loss of directional control on landing, and subsequently ground looped at the Lancaster Regional Airport (LNC), Lancaster, Texas. The commercial pilot was not injured. The airplane sustained substantial damage to the fuselage. The airplane was registered to and operated by the pilot, under the provisions of 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. The flight had originated from LNC at 1535.

According to the pilot, during the landing rollout on runway 13, the airplane began to swerve to the right. The pilot attempted to arrest the swerve by applying left rudder pedal and left brake to no avail. The airplane exited the right side of the runway and subsequently ground looped. The pilot reported that the winds were from 190 degrees at 8 knots.

The pilot further reported having 420 hours of tailwheel fight time, with approximately 400 of those hours in a Pitts Special from 2006 to 2011.

A postaccident examination of the airplane, by the National Transportation Safety Board (NTSB), investigator-in-charge (IIC), revealed that the tailwheel assembly, tailwheel steering arm, and rudder stops were all in working condition. However, when combined together, the resulting configuration allowed the tailwheel to unlock and fully swivel, 15 degrees prior to the rudder reaching full travel in either direction.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN11LA658