N2238U

Substantial
None

Brantly Helicopter B-2B S/N: 479

Accident Details

Date
Sunday, August 15, 1999
NTSB Number
CHI99LA292
Location
HUDSON, MI
Event ID
20001212X19444
Coordinates
41.850849, -84.339836
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

was an inadequate preflight and misjudged flare to landing during the autorotation by the pilot. A factor in this accident was a totally blocked fuel tank vent system.

Aircraft Information

Registration
Make
BRANTLY HELICOPTER
Serial Number
479
Engine Type
Reciprocating
Year Built
1968
Model / ICAO
B-2B BRB2
Aircraft Type
Rotorcraft
No. of Engines
1
Seats
2
FAA Model
B-2B

Registered Owner (Current)

Name
HEWITT ROBERT E
Address
1814 GOODWATER RD
City
BYBEE
State / Zip Code
TN 37713-2405
Country
United States

Analysis

On August 15, 1999, at 1500 eastern daylight time (edt), a Brantly B-2B, N2238U, piloted by a private pilot, was destroyed during a collision with the ground during a forced landing after a total loss of engine power. Visual meteorological conditions prevailed at the time of the accident. The personal flight was operating under the provisions of 14 CFR Part 91, and was not operating on a flight plan. The pilot reported no injuries. The flight departed a restricted landing area near Jackson, Michigan, at 1400 edt.

The pilot said he was flying the helicopter about 1,000 feet above the ground when the "...engine started to sputter. It sputtered until I reached about 500 feet, then the engine quit." During the auto-rotation for the forced landing the pilot said he "...flared too late and hit the tail [on the ground]." The pilot said the helicopter rolled onto its side during the ground collision sequence.

The on-scene investigation revealed no mechanical anomalies that would prevent flight. Inspection of the fuel system's overboard vent line revealed it was plugged with what appeared to be mud from the Mud Dauber Wasp. The fuel system does not have a vented fuel cap. The overboard vent line is the only vent line for the fuel tank. The vent line's opening is located on the helicopter's fuselage bottom and is visible to the pilot. The helicopter's fuel vent system part's manual illustration is appended to this report.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CHI99LA292