N8498K

Substantial
None

Grumman-Schweizer G-164BS/N: 715B

Accident Details

Date
Thursday, March 28, 2002
NTSB Number
FTW02LA107
Location
Ferriday, LA
Event ID
20020401X00434
Coordinates
31.627777, -91.662780
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

the failure of the number three cylinder exhaust rocker arm, resulting in a total loss of engine power. A contributing factor was the lack of suitable terrain for the forced landing.

Aircraft Information

Registration
N8498K
Make
GRUMMAN-SCHWEIZER
Serial Number
715B
Engine Type
Turbo-shaft
Year Built
1983
Model / ICAO
G-164BG64T
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
WOODRUFF JOHNNIE
Address
PO BOX 268
Status
Deregistered
City
MONTEREY
State / Zip Code
LA 71354-0268
Country
United States

Analysis

On March 28, 2002, approximately 0935 central standard time, a Grumman-Schweizwer G-164B agricultural airplane, N8498K, sustained substantial damage when it impacted terrain while maneuvering near Ferriday, Louisiana. The commercial pilot, sole occupant of the airplane, was not injured. The airplane was being operated by W&E Air Service, Ferriday, Louisiana, under 14 Code of Federal Regulations Part 137. Visual meteorological conditions prevailed for the local aerial application flight, and a flight plan was not filed. The flight originated from the W&E Air Service private airstrip at 0920.

In a telephone interview with the NTSB investigator-in-charge, the pilot reported that this was his third load of the day. While turning back to the field after completing a spray run, the engine started "popping." After several more "pops," the engine "went dead." The pilot landed straight ahead in the open cotton field he was spraying, impacting soft terrain. After impact, the left landing gear separated, and the airplane continued for approximately 20 yards before flipping over, coming to rest inverted.

An A&P mechanic, who examined the aircraft, reported that the #3 cylinder exhaust rocker arm had failed. The front and rear spars of the right upper wing panel, and the front spar of the left lower wing panel sustained structural damage. All four wing panels sustained leading edge and skin damage. The vertical stabilizer, rudder, and right elevator were destroyed.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# FTW02LA107