N96SH

Substantial
Serious

BELL 47G-3B-1S/N: 2927

Accident Details

Date
Wednesday, May 25, 2011
NTSB Number
CEN11LA370
Location
Lakeville, MN
Event ID
20110606X12931
Coordinates
44.669681, -93.239410
Aircraft Damage
Substantial
Highest Injury
Serious
Fatalities
0
Serious Injuries
1
Minor Injuries
0
Uninjured
0
Total Aboard
1

Probable Cause and Findings

The loss of engine power due to a loose B-nut on the compressor discharge pressure bleed line.

Aircraft Information

Registration
Make
BELL
Serial Number
2927
Engine Type
Turbo-shaft
Year Built
1964
Model / ICAO
47G-3B-1B47G
Aircraft Type
Rotorcraft
No. of Engines
1
Seats
3
FAA Model
47G-3B-1

Registered Owner (Current)

Name
VALIAIR LIMITED COMPANY TRUSTEE
Address
OGDEN AIRPORT GATEWAY CENTER
4248 S 1650 W BLDG 1 STE 10
City
OGDEN
State / Zip Code
UT 84405
Country
United States

Analysis

On May 25, 2011, about 1140 central daylight time, a Bell 47G-3B-1, N96SH, experienced a total loss of engine power while maneuvering near Lakeville, Minnesota. The pilot subsequently made a forced landing on a swamp near Lakeville, Minnesota. The certificated commercial pilot sustained serious injuries. The helicopter sustained substantial damage to the fuselage and tailboom when it impacted terrain during the forced landing. The helicopter was registered to and operated by Scotts Helicopter Services Inc under the provisions of 14 Code of Federal Regulations Part 137 as an aerial application flight. Visual meteorological conditions prevailed and no flight plan had been filed for the flight that originated from Flying Cloud Airport (FCM), Minneapolis, Minnesota.

Examination of the engine (Rolls Royce Allison T63A700, serial number AE-400951) by a Federal Aviation Administration inspector from the Minneapolis Flight Standards District Office revealed that the Pc bleed line (from the governor to the fuel control) was leaking at the B-nut, which had come loose. The inspector stated that the operator had a spare engine at it facilities and that engine had torque lines painted onto the engine's fittings. The accident engine did not have torque lines painted onto its fittings.

The inspector stated that there is no requirement to use torque lines and that the new engine maintenance manuals now discuss the use of torque lines.

The time since the engine's last inspection was 59.4 hours.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN11LA370