N3204S

Substantial
Serious

SHORT LANCAIR 320 S/N: 330

Accident Details

Date
Saturday, August 26, 1995
NTSB Number
LAX95LA306
Location
RIO VISTA, CA
Event ID
20001207X04300
Coordinates
38.179161, -121.730163
Aircraft Damage
Substantial
Highest Injury
Serious
Fatalities
0
Serious Injuries
1
Minor Injuries
1
Uninjured
0
Total Aboard
2

Probable Cause and Findings

the failure of the wing flap actuator pushrod creating an asymmetrical flap condition during the landing flare maneuver. A contributing factor was the failure of the owner/builder to incorporate a manufacturer's design change for a stronger actuator pushrod.

Aircraft Information

Registration
N3204S
Make
SHORT
Serial Number
330
Engine Type
Turbo-shaft
Model / ICAO
LANCAIR 320 BELF
Aircraft Type
Fixed Wing Multi Engine
No. of Engines
4

Registered Owner (Historical)

Name
SHORT RONALD H
Address
PO BOX 2842
Status
Deregistered
City
BAKERSFIELD
State / Zip Code
CA 93303
Country
United States

Analysis

On August 26, 1995 at 1203 hours Pacific daylight time, a Short Lancair 320, N3204S, was substantially damaged when the pilot lost control of the aircraft during the landing flare, impacted the runway and ground looped on runway 25 at Rio Vista, California. The amateur built aircraft was owned and operated by the pilot. Visual meteorological conditions prevailed at the time of the accident. The personal 14 CFR Part 91 flight was not operating on a flight plan. The private pilot reported minor injuries and the sole passenger received serious injuries. The flight departed from Delano, California, at 1040.

The pilot reported that during flare for landing the right wing dropped and contacted the runway despite his efforts to hold the wing up using full left aileron control. The aircraft bounced, the right wing dropped again, and the aircraft veered off the runway to the left and ground looped. The aircraft came to rest headed east, about 1500 feet beyond the runway threshold and 50 feet left (south) of the runway centerline. After exiting the aircraft, the pilot and his passenger noticed that the left wing flap was fully extended and the right wing flap was fully retracted. There were no impact marks on the right wing flap. Inspection of the aircraft revealed that the right wing flap actuating pushrod had broken. The pushrod had a long, smooth "S" bend over its length. In the threaded end of the rod near the rod-end fitting attachment there was a sharp, 85-degree bend where the rod had broken apart.

The designer of the aircraft, who sells the aircraft to builders in kit form, stated that the failed pushrod had been superseded by a stronger rod design 4 years prior to the accident in response to operator reports of bent pushrods. At that time, a bulletin regarding the change was sent to kit owners.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# LAX95LA306