N158T

Substantial
Serious

Nanchang CJ-6A S/N: 3151213

Accident Details

Date
Saturday, May 16, 1998
NTSB Number
MIA98LA163
Location
PAGELAND, SC
Event ID
20001211X10157
Coordinates
34.769577, -80.380767
Aircraft Damage
Substantial
Highest Injury
Serious
Fatalities
0
Serious Injuries
1
Minor Injuries
0
Uninjured
0
Total Aboard
1

Probable Cause and Findings

Was the inadvertent stall of the airplane by the pilot-in-command while attempting to clear trees beneath the airplane during the descent for the forced landing. Contributing to the accident was the partial loss of engine power due to separation of the No.9 cylinder from the engine.

Aircraft Information

Registration
N158T
Make
NANCHANG
Serial Number
3151213
Engine Type
Reciprocating
Year Built
1976
Model / ICAO
CJ-6A CJ6
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
BATES MARCUS L JR
Address
14125 PECAN HOLW
Status
Deregistered
City
LEANDER
State / Zip Code
TX 78641-7608
Country
United States

Analysis

On May 16, 1998, about 1340 eastern daylight time, a Nanchang CJ-6A, N158T, registered to a private individual, experienced a loss of engine power and collided with terrain during an attempted forced landing in a field about 1.5 miles east of Pageland, South Carolina. Visual meteorological conditions prevailed at the time and no flight plan was filed for the 14 CFR Part 91 personal flight. The airplane was substantially damaged and the private-rated pilot, the sole occupant, was seriously injured. The flight originated about 10 minutes earlier from the Cheraw Municipal Airport, Cheraw, South Carolina.

The pilot stated that while flying at 800 feet agl, he felt a vibration and observed an object protruding from the engine cowling, and a resulting loss of engine power. While attempting to clear trees with the landing gear and the speed brake extended, the airplane stalled, impacted the ground nose low, then nosed over and came to rest inverted. The pilot was not wearing the installed shoulder harness.

Examination of the engine by the FAA inspector revealed that the No. 9 cylinder was separated from the engine and the auxiliary rod piston pin hole was elongated. The auxiliary rod sleeve was not in place. Nonferrous metal was noted inside the engine case. Review of the maintenance records revealed that at the time of failure, the engine had accumulated about 425 hours since new.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# MIA98LA163