N48533

Substantial
None

Grumman-Schweizer G-164AS/N: 1665

Accident Details

Date
Friday, May 17, 2002
NTSB Number
FTW02LA152
Location
Hathaway, LA
Event ID
20020520X00705
Coordinates
30.410554, -92.634445
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

the loss of engine power for undetermined reasons. A contributing factor was the lack of suitable terrain for the forced landing.

Aircraft Information

Registration
N48533
Make
GRUMMAN-SCHWEIZER
Serial Number
1665
Engine Type
Turbo-shaft
Year Built
1976
Model / ICAO
G-164AG64T
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
SALE REPORTED
Address
XXXX
Status
Deregistered
City
BEZIERS
Country
United States

Analysis

On May 17, 2002, approximately 1230 central daylight time, a Grumman-Schweizwer G-164A agricultural airplane, N48533, was substantially damaged during a forced landing following a loss of engine power near Hathaway, Louisiana. The airplane was registered to and operated by a private individual. The commercial pilot, sole occupant, was not injured. Visual meteorological conditions prevailed for the 14 Code of Federal Regulations Part 137 aerial application flight, and a flight plan was not filed. The flight originated from a private airstrip at 1220.

The pilot stated he was operating off of a short grass airstrip and this was his fourth load of the day. The airplane was hauling 1,400 pounds of fertilizer, approximately one-half of a normal load. After making several passes, with the load down to 1,000 pounds, he pulled up out of the field, and "the airplane felt like it was settling." He added full power, but "the engine didn't respond with any more power. It didn't want to fly, and it kept settling." The pilot executed a forced landing straight ahead in a rice field and touched down in a flat, wings level attitude. The airplane bounced once, nosed over, and came to rest inverted.

According to the FAA inspector, who examined the airplane at the accident site, there was substantial damage to the empennage and the firewall. Both wings, the engine, and both main landing gear were damaged. The 600-horsepower Pratt & Whitney R-1340-AN1 engine had accumulated a total of 6,876 hours (350 hours since overhaul), and underwent its most recent annual inspection on February 4, 2002, approximately 50 hours prior to the accident.

The reason for the loss of engine power was not determined.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# FTW02LA152