N30PK

Substantial
Serious

Issoire-Aviation PIK-30 S/N: 719

Accident Details

Date
Sunday, June 18, 1995
NTSB Number
LAX95LA215
Location
DAYTON, NV
Event ID
20001207X03748
Coordinates
39.260726, -119.479324
Aircraft Damage
Substantial
Highest Injury
Serious
Fatalities
0
Serious Injuries
1
Minor Injuries
0
Uninjured
0
Total Aboard
1

Probable Cause and Findings

the pilot's delayed decision to extend and use the engine to maintain adequate terrain clearance after encountering downdrafts.

Aircraft Information

Registration
Make
ISSOIRE-AVIATION
Serial Number
719
Engine Type
Reciprocating
Year Built
1985
Model / ICAO
PIK-30 APM3
Aircraft Type
Glider
No. of Engines
0
Seats
1
FAA Model
PIK-30

Registered Owner (Current)

Name
STRAND WILLIAM C
Address
PO BOX 756
City
PICAYUNE
State / Zip Code
MS 39466-0756
Country
United States

Analysis

On June 18, 1995, about 1600 hours Pacific daylight time, an Issoire Siren PIK-30 motorized glider, N30PK, collided with mountainous terrain near Dayton, Nevada, while engaged in a soaring competition. The glider was owned and operated by the pilot. Visual meteorological conditions prevailed at the time and no flight plan was filed. The aircraft sustained substantial damage and the certificated commercial pilot, the sole occupant, sustained serious injuries. The flight originated from Minden, Nevada, at 1230 on the day of the accident.

Federal Aviation Administration (FAA) inspectors from the Reno, Nevada Flight Standards District Office, responded to the accident site, examined the glider, and interviewed persons with knowledge about the accident. According to the inspectors, the glider was taking part in a soaring competition. Strong up and downdrafts, with winds as high as 34 knots, were reported in the area of the accident. The pilot was experiencing difficulty maintaining adequate terrain clearance due to the downdrafts, and was in the process of manually extending the engine from its fuselage storage location when the glider collided with the terrain.

The inspectors reported that the engine is stored in a fuselage bay behind the pilot's seat and must be extended by use of a handcrank located on the right side of the cockpit. The engine was found about halfway extended from its storage bay. From the initial ground contact point to the glider, the inspectors measured a 20-foot-long ground scar. Vertical crush damage was noted to the bottom of the glider. No control system malfunctions were observed during the examination.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# LAX95LA215