N9022N

Substantial
Minor

North American T-28CS/N: 140666

Accident Details

Date
Friday, April 11, 2008
NTSB Number
LAX08LA098
Location
Kingman, AZ
Event ID
20080417X00509
Coordinates
35.210556, -113.875556
Aircraft Damage
Substantial
Highest Injury
Minor
Fatalities
0
Serious Injuries
0
Minor Injuries
1
Uninjured
1
Total Aboard
2

Probable Cause and Findings

A total loss of engine power during cruise flight due to an undetermined catastrophic internal engine failure.

Aircraft Information

Registration
Make
NORTH AMERICAN
Serial Number
140666
Engine Type
Reciprocating
Year Built
1956
Model / ICAO
T-28CT28
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
2
FAA Model
T-28C

Registered Owner (Current)

Name
GOLDBACH CHARLES H
Address
PO BOX 467
City
VALLEYFORD
State / Zip Code
WA 99036-0467
Country
United States

Analysis

On April 11, 2008, about 0730 mountain standard time, an experimental North American T-28C, N9022N, experienced a total loss of engine power while cruising about 5 miles east-southeast of the Kingman Airport, Kingman, Arizona. The pilot made a forced landing on open, rocky, desert terrain, and the airplane was substantially damaged. The private pilot was not injured, and the passenger sustained minor injuries. The airplane was owned and operated by the pilot. Visual meteorological conditions prevailed at the time of the personal flight, and no flight plan was filed. The flight was performed under the provisions of 14 Code of Federal Regulations Part 91, and it originated from Kingman about 0715.

The pilot reported to the National Transportation Safety Board investigator that the engine started running rough while cruising about 5,000 feet mean sea level (about 2,000 feet above ground level). The pilot checked the engine gauges and observed that the oil pressure was decreasing and the oil temperature was "maxing out." According to the pilot, the engine then lost all power and he made an intentional gear up landing because the tricycle gear airplane likely would have nosed over during rollout on the soft terrain. The propeller continued to rotate throughout the mishap. The pilot stated that his airplane's Curtis Wright model 1820-86B engine had been operated about 175 hours since receiving an overhaul.

At the direction of the Safety Board investigator, a Federal Aviation Administration (FAA) airworthiness inspector oversaw an examination of the accident engine. In pertinent part, the FAA inspector reported finding "an excessive amount of ferrous and non-ferrous" material in the oil screens. The number 3 cylinder was removed from the crank case and exhibited a bent connecting rod, along with "major damage to its piston and cylinder skirt." Also, numerous pieces of metal were observed in the crankcase that was associated with the number 4 and number 5 cylinders. The internal engine component that initially broke was not identified.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# LAX08LA098