N8367F

Substantial
None

Robinson R-22 S/N: 2816

Accident Details

Date
Thursday, April 1, 1999
NTSB Number
ANC99LA040
Location
FAIRBANKS, AK
Event ID
20001205X00399
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

The failure of the pilot to maintain rotor rpm during a downwind turn. A factor in the accident was the inadequate altitude to recover from the loss of rotor rpm.

Aircraft Information

Registration
N8367F
Make
ROBINSON
Serial Number
2816
Engine Type
Reciprocating
Year Built
1998
Model / ICAO
R-22 R22
Aircraft Type
Rotorcraft
No. of Engines
1

Registered Owner (Historical)

Name
SALE REPORTED
Address
NONE
Status
Deregistered
City
XXX
State / Zip Code
OK 73125
Country
United States

Analysis

On April 1, 1999, about 1030 Alaska standard time, a Robinson R-22 helicopter, N8367F, sustained substantial damage during a forced landing about 38 miles south of Fairbanks, Alaska. The commercial pilot and sole passenger were not injured. The helicopter was operated by Chena River Aviation under 14 CFR Part 135, conducting wolf captures for the State of Alaska, Department of Fish and Game. The flight departed the Chena Marina Airport in Fairbanks at 0930. Visual meteorological conditions prevailed at the time of the accident, and a company VFR flight plan was filed.

The pilot told the NTSB investigator-in-charge (IIC) during a telephone interview on April 1, that he turned downwind in 15 knots to 30 knots of wind, at 30 feet above the ground to capture a wolf. He noticed the rotor and engine rpm decaying. He attempted to lower the collective, disengage the engine speed governor, and increase the throttle, but the rotor speed continued to decay. The pilot said the low rotor speed warning horn activated during his descent, and he made a forced landing to a clearing. The helicopter bounced, and rolled onto its side. He stated that he did not have tail rotor authority at the low rotor rpm when the helicopter bounced. The pilot estimated seven to ten gallons of fuel remained in the fuel tanks at the time of the accident.

The engine was examined and operated on a test stand at the Robinson Helicopter facility on May 3, 1999. The testing was observed by an NTSB investigator. No anomalies were noted with the governor motor, the governor controller, or the engine. The power level produced throughout the test exceeded the minimum specified by the manufacturer.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ANC99LA040