N212TC

Substantial
None

North American SNJ-5S/N: 12141732

Accident Details

Date
Monday, September 19, 2005
NTSB Number
DEN05LA143
Location
Torrington, WY
Event ID
20050926X01527
Coordinates
42.074165, -104.154724
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

failure of the #7 connecting rod, causing engine seizure. A contributing factor was the berm.

Aircraft Information

Registration
Make
NORTH AMERICAN
Serial Number
12141732
Engine Type
Reciprocating
Year Built
1944
Model / ICAO
SNJ-5B25
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
2
FAA Model
SNJ-5

Registered Owner (Current)

Name
BURNHAM KENNETH J
Address
6932 COUNTY ROAD 110
City
CARR
State / Zip Code
CO 80612-8908
Country
United States

Analysis

On September 19, 2005, approximately 1745 mountain daylight time, a North American SNJ-5, N212TC, piloted by a private pilot, was substantially damaged when it impacted terrain during an off-airport forced landing just east of the Torrington Municipal Airport (TOR), Torrington, Wyoming. Visual meteorological conditions prevailed at the time of the accident. The personal cross-country flight was being conducted under Title 14 CFR Part 91 without a flight plan. The pilot reported no injuries. The flight originated in Ogden (OGD), Utah, approximately 1500, and was en route to Scottsbluff (BFF), Nebraska.

According to the Aircraft Accident Report Form 6120.1/2 submitted by the pilot, he was eastbound and descending from a cruising altitude of 13,500 feet for landing at Scottsbluff, Nebraska. During the descent, the "cylinder number 1 failed followed immediately by the failure of cylinder number 2 and within about 4 seconds a total seizure of the engine." The pilot made a forced landing in an alfalfa field approximately 2 miles east of TOR. During the landing, the airplane impacted a berm that separated the left main landing gear and wrinkled the left wing. According to a Federal Aviation Administrationn (FAA) inspector, the left wing was wrinkled, one blade on the propeller was bent, and the right main gear and wheel were destroyed.

On December 24, 2005, the engine was disassembled and examined at Tulsa Aircraft Engines, Inc., Tulsa, Oklahoma, under the direction of the FAA. The engine had seized and could not be turned because connecting rods 1, 2, 3, 4, 7, and 9 were found broken, and numbers 5 and 6 were found severely damaged. Connecting rod 8 was not broken or damaged. Metal contamination was noted in the push rod housings, oil sump, thrust cover and bearing; cam, cam rollers, cam drive gear and inspection hole; main case, and oil screen. According to the FAA inspector's report, there were indications that the #7 connecting rod had struck the crankcase between #6 and #7 cylinders, breaking the through bolts.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# DEN05LA143