N677DT

Substantial
None

Freeman Glastar S/N: 1

Accident Details

Date
Sunday, August 19, 2001
NTSB Number
ANC01LA126
Location
Glennallen, AK
Event ID
20010913X01930
Coordinates
62.357498, -144.030273
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

The pilot's failure to abort the landing. Factors associated with the accident were the pilot's selection of an unsuitable landing area, and his failure to attain a proper touchdown point. An additional factor was a tailwind.

Aircraft Information

Registration
Make
FREEMAN
Serial Number
1
Engine Type
Reciprocating
Year Built
1999
Model / ICAO
Glastar BPAT
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
2
FAA Model
GLASTAR

Registered Owner (Current)

Name
FREEMAN MATTHEW D
Address
PO BOX 671554
City
CHUGIAK
State / Zip Code
AK 99567-1554
Country
United States

Analysis

On August 18, 2001, about 1600 Alaska daylight time, a wheel-equipped Freeman Glastar, an experimental, homebuilt airplane, N677DT, sustained substantial damage during landing at an off airport site, about 22 miles northwest of Glennallen, Alaska. The certificated commercial pilot, and the one passenger, were not injured. The airplane was being operated as a visual flight rules (VFR) personal flight under Title 14, CFR Part 91, when the accident occurred. Visual meteorological conditions prevailed, and a VFR flight plan was filed. The flight originated about 1545, from the Gulkana Airport, Gulkana, Alaska.

During a telephone conversation with the National Transportation Safety Board investigator-in-charge on August 29, the pilot reported that he was landing to the south on a 675 feet long, uphill site. He added that due to obstructions at the south end of the site, he had to land to the south, and downwind. He said that as the airplane's main wheels touched down on the rough gravel surface, the airplane bounced. He recovered from the bounce, and flew further down the runway and landed about midfield on the site. He said that during the landing roll, while applying heavy braking, the airplane went off the end of the site, and nosed over. The airplane sustained substantial damage to the vertical stabilizer and rudder.

The pilot said that there were no preaccident mechanical anomalies with the airplane.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ANC01LA126