N8482V

Destroyed
Serious

Rockwell S-2R S/N: 2242R

Accident Details

Date
Wednesday, July 28, 1999
NTSB Number
MIA99LA204
Location
ISOLA, MS
Event ID
20001212X19321
Coordinates
33.259288, -90.590255
Aircraft Damage
Destroyed
Highest Injury
Serious
Fatalities
0
Serious Injuries
1
Minor Injuries
0
Uninjured
0
Total Aboard
1

Probable Cause and Findings

Failure of the No. 4 cylinder due to a leaking intake valve resulting in loss of engine power and collision with a ditch while making a forced landing on unsuitable terrain. Contributing to the accident was improper maintenance adjustment of the engine valves and spark plugs.

Aircraft Information

Registration
N8482V
Make
ROCKWELL
Serial Number
2242R
Engine Type
Reciprocating
Model / ICAO
S-2R SA02
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
SALE REPORTED
Address
NONE
Status
Deregistered
City
XXX
State / Zip Code
OK 73125
Country
United States

Analysis

On July 28, 1999, about 0650 central daylight time, a Rockwell S-2R, N8482V, registered to and operated by Gary Flying Service, Inc., crashed while attempting a forced landing following loss of engine power near Isola, Mississippi, while on a Title 14 CFR Part 137 aerial application flight. Visual meteorological conditions prevailed at the time and no flight plan was filed. The aircraft was destroyed and the commercial-rated pilot was seriously injured. The flight originated from Belzoni, Mississippi, the same day, about 0630.

The pilot stated that while performing aerial application, the engine backfired twice, lost oil pressure, backfired again, and then shut down. While making a forced landing, the aircraft collided with a ditch, which separated the landing gear. The aircraft then spun around 180 degrees and came to rest. A postcrash fire erupted in the left wing area of the aircraft and destroyed the aircraft.

Postcrash examination of the engine was conducted at an engine overhaul facility under the supervision of an FAA inspector. The No. 4 cylinder compression was 35 over 80 psi., with leakage through the intake valve. Compression limits for the engine are 60 over 80 psi or above. Seven out of 18 valves were not adjusted within normal limits. All spark plug gaps were set above normal limits. See the FAA inspector's statements and mechanic's statement attached to this report.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# MIA99LA204