N8478D

Substantial
None

Bell 47S/N: 1697

Accident Details

Date
Tuesday, July 10, 2001
NTSB Number
ATL01LA075
Location
Indianola, MS
Event ID
20010712X01391
Coordinates
33.450660, -90.749534
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

The pilot's improper use of flight controls during an autorotation that resulted inn the collapse of the skids and cross tube assembly. A factor was the loss of engine power due to the failure of # 1 connecting rod and the overload failure of the skids and cross tub assembly.

Aircraft Information

Registration
Make
BELL
Serial Number
1697
Engine Type
Reciprocating
Year Built
1957
Model / ICAO
Aircraft Type
Rotorcraft
No. of Engines
1
Seats
3
FAA Model
47G-2

Registered Owner (Current)

Name
WOOD DENTON A
Address
2206 BUTLER DR
City
FRIENDSWOOD
State / Zip Code
TX 77546-5516
Country
United States

Analysis

On July 10, 2001, at 1030 central daylight time, a Bell 47 helicopter, N8478D, registered to Talon Air, Inc., collided with the ground and rolled over during an autorotation following a loss of engine power near Indianola, Mississippi. The aerial application flight was operated under the provision of Title 14 CFR Part 137 with no flight plan filed. Visual weather conditions prevailed at the time of the accident. The helicopter sustained substantial damage, and the commercial pilot was not injured. The flight departed Indianola, Mississippi, at 1025.

The pilot reported that while enroute to the next field to be sprayed, at 500 feet, the engine lost power. After attempts to restore full power were not successful, the pilot selected a nearby field for an autorotation. The pilot stated the autorotative maneuver was normal, but when the helicopter touched down, it rolled over on the right side.

During the engine examination, metal particles were recovered from the engine oil pump screen and the engine oil filter element. Examination of the engine assembly approximately four to six ounces of water were recovered from the airframe fuel system. During the subsequent engine teardown examination, a large hole was discovered in the engine case adjacent to the No. 1 cylinder. Further examination showed the No. 1 cylinder connecting rod cap was wedged between the second crankshaft lobe and the engine case. The examination of the helicopter also revealed that the landing skid and cross-tubs were fractured into several pieces. The fracture examination showed all fractures were in overload.

A review of the airframe and engine maintenance logs showed that the airframe had accumulated 10,378 flight hours. The engine had accumulated a total of 935.1 hours since the last major overhaul.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ATL01LA075