N121CM

Substantial
Minor

STINSON 108-3S/N: 108-4284

Accident Details

Date
Thursday, May 23, 2013
NTSB Number
CEN13LA305
Location
Beaumont, TX
Event ID
20130529X10741
Coordinates
30.070278, -94.214996
Aircraft Damage
Substantial
Highest Injury
Minor
Fatalities
0
Serious Injuries
0
Minor Injuries
1
Uninjured
0
Total Aboard
1

Probable Cause and Findings

The lack of a forward clamp on the carburetor heat box rubber boot, which allowed the boot to be ingested into the inlet of the carburetor heat box, restricting the airflow and leading to a subsequent partial loss of engine power.

Aircraft Information

Registration
N121CM
Make
STINSON
Serial Number
108-4284
Engine Type
Reciprocating
Year Built
1948
Model / ICAO
108-3S108
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
SALE REPORTED
Address
6419 SHERMAN AVE
Status
Deregistered
City
CINCINNATI
State / Zip Code
OH 45230-2843
Country
United States

Analysis

On May 23, 2013, about 1200 central daylight time, a Stinson 108-3, N121CM, sustained substantial damage when it nosed over during a forced landing following a loss of engine power near Beaumont, Texas. The pilot received minor injuries. The airplane sustained damage to the vertical tail surfaces, wings, wing struts, and fuselage. The aircraft was registered to and operated by Aircapital Nevada, Inc., under the provisions of 14 Code of Federal Regulations Part 91 as a business flight. Visual meteorological conditions prevailed for the flight, which was not operated on a flight plan. The flight was originating from the Beaumont Municipal Airport, Beaumont, Texas, and was bound for College Station, Texas.The pilot reported that he had performed a pre-takeoff run-up and all engine indications were normal. He proceeded to take off and made two 90-degree turns prior to the loss of engine power. The pilot said that the engine was still producing some power, but he was not able to maintain altitude. He attempted to land in a field and the airplane nosed over.

Examination of the engine confirmed compression on all cylinders, valve system continuity, and magneto operation. The carburetor appeared new and the fuel strainer was clean with no debris. The fuel within the gascolator did not appear to have any water or sediment. The upper spark plugs were of three different electrode configurations. All of the plugs exhibited a wet-black appearance. The rubber boot that was located between the carburetor heat box and the cowl was very pliable and had cracks on the exterior surfaces. The rear of the boot was attached to the carburetor heat box with a clamp and sealant. The front of the boot did not have a clamp installed and one was not found in the wreckage.

Discussions with a member of the International Stinson Club (ISC) revealed that the front of the boot between the carburetor heat box and the cowl should have had a 2-piece clamp installed. The ISC member said that without the clamp installed it is possible for the boot to be sucked into the inlet of the carburetor heat box thereby restricting airflow, resulting in a rich mixture and reduction of engine power.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN13LA305