N3249K

Substantial
Minor

GLOBE GC-1BS/N: 1242

Accident Details

Date
Saturday, October 30, 2010
NTSB Number
CEN11LA044
Location
Grants, NM
Event ID
20101101X15358
Coordinates
35.167221, -107.901947
Aircraft Damage
Substantial
Highest Injury
Minor
Fatalities
0
Serious Injuries
0
Minor Injuries
1
Uninjured
0
Total Aboard
1

Probable Cause and Findings

The loss of partial engine power for undetermined reasons.

Aircraft Information

Registration
N3249K
Make
GLOBE
Serial Number
1242
Engine Type
None
Year Built
1946
Model / ICAO
GC-1BFK12
No. of Engines
0

Registered Owner (Historical)

Name
SAMPSON DOUGLAS K
Address
251 MORNINGWOOD LN
Status
Deregistered
City
WIRTZ
State / Zip Code
VA 24184-3660
Country
United States

Analysis

On October 30, 2010, approximately 1300 daylight time, a Globe GC-1B, N3249K, registered to and operated by the pilot, was substantially damaged when it impacted terrain following a loss of engine power during takeoff from Grants-Milan Municipal Airport (GNT), Grants, New Mexico. Visual meteorological conditions (VMC) prevailed at the time of the accident. The personal flight was being conducted under the provisions of 14 Code of Federal Regulations (CFR) Part 91 without a flight plan. The pilot, the sole occupant on board, sustained minor injuries. The cross-country flight was originating at the time of the accident and was en route to Ozark (OZA), Arkansas.

The pilot said that there was a strong headwind component and shortly after taking off, the engine sputtered and "coughed." He enriched the mixture and was able to regain some power. He described the climb rate as "lethargic," so he pulled the throttle back prior to impact. The airplane crashed about 1/2 mile from runway.

The 200-pound pilot said he had just refueled (26 gallons), and was carrying a small bag and 10 pounds of logbooks and miscellaneous items.

He told FAA inspectors that he had purchased the airplane two days before in Flagstaff, Arizona, and was disappointed in its performance departing Flagstaff, which he described as a "long takeoff." He had owned a similar airplane before for 10 years.

On December 16, 2011, the airplane and engine were examined at Air Transport in Phoenix, Arizona. Due to impact damage to the engine mounts, propeller, and carburetor, the decision was made not to attempt to run the engine (Continental O-300-A, s.n. 15004-D-6-A-R). A compression check was performed with the following results:

Cylinder #1: 79/80

Cylinder #2: 73/80

Cylinder #3: 68/80

Cylinder #4: 77/80

Cylinder #5: 80/80

Cylinder #6: 78/80

The carburetor bowl was clean with no visible contaminants. The fuel screen in the engine-driven fuel pump was clean with no visible contaminants. Hand-turning of the crankshaft revealed power and valve train 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# CEN11LA044