N6832K

Substantial
None

Grumman G-164BS/N: 502B

Accident Details

Date
Saturday, June 4, 2005
NTSB Number
DFW05LA147
Location
Lake Charles, LA
Event ID
20050615X00772
Coordinates
30.131944, -93.232498
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 propeller governor which resulted in a forced landing. A contributing factor was the transmission wire.

Aircraft Information

Registration
Make
GRUMMAN
Serial Number
502B
Engine Type
Reciprocating
Year Built
1978
Model / ICAO
G-164BG64T
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
1
FAA Model
G-164B

Registered Owner (Current)

Name
HERSHEY FLYING SERVICE INC
Address
PO BOX 148
City
DAVID CITY
State / Zip Code
NE 68632-0148
Country
United States

Analysis

On June 4, 2005, at 1440 central daylight time, a single-engine Grumman G-164B agricultural aircraft, N6832K, was substantially damaged during a forced landing following a loss of propeller drive during cruise flight near Lake Charles, Louisiana. The commercial pilot, sole occupant of the airplane, was not injured. The airplane was owned and operated by O'Brien Flying Service, Inc., of Iowa, Louisiana. Visual meteorological conditions prevailed for the 14 Code of Federal Regulations Part 137 aerial application flight. The flight originated from one of the operator's remote field strips near Iowa, Louisiana, at about 1400.

The pilot reported to the operator that following takeoff, after initiating a left turn to return to the field being sprayed, the pilot reduced propeller RPM to a climb power setting when the pitch on the two bladed Hamilton Standard model 12D40-6101-12 propeller "went to the full coarse setting and lost drive."

The 19,000-hour pilot initiated a forced landing to a clearing. During the forced landing the airplane struck a power line, before impacting a rice field.

The operator reported that the 600-horsepower Pratt & Whitney R-1340-AN-1 radial engine had accumulated a total of 483 hours since its last overhaul, and the propeller had accumulated a total of 541 hours since its last overhaul. The last annual inspection was completed on January 5, 2005, approxiamately 366 hours prior to the accident.

Oil was present in the crankcase, and no evidence of metal was found in suspension or in the oil filter. The propeller governor, a Hamilton Standard model 1M12G, serial number 121470, had accumulated a total of 753.91 hours since its last overhaul. The propeller governor was removed for further examination by Aircraft Accessories of Oklahoma Inc., of Tulsa, Oklahoma.

In a telephone interview with a representative of the investigator-in-charge, a representative of Aircraft Accessories of Oklahoma stated, that the "propeller governor pilot valve had failed, causing an internal oil leak, which resulted in the failure of the propeller governor. "

The left lower wing, left main landing gear assembly, and the vertical stabilizer sustained structural damage. There was no fire.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# DFW05LA147