SEA05LA138

NTSB accident investigation · Bell 47G-2A · Oroville, WA · July 5, 2005

Accident · No injuriesLimited investigationFinal report
Date
July 4, 2005, 17:30 local (Jul 5, 2005, 00:30 UTC)
Place
Oroville, WA
Injuries
1 uninjured
Damage
Substantial damage
Phase of flight
Maneuvering
Aircraft
N38926Bell 47G-2A
Weather
Visual (VMC) · Day
Status
Completed · report February 28, 2006
Report
Approved by Office Director
Parties
FAA FSDO
FAA report
20050704014629A
Case key
61867

From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.

On this page

Probable cause

The failure of the throttle cable housing, which permitted the engine's RPM to decay to the idle position. Contributing factors were the trees and the lack of suitable terrain for a forced landing.

Sequence of events

NTSB’s coding before 2008: each occurrence and phase of flight, and the causes and factors under it. The codes are defined in NTSB’s coding manual.

Loss of engine power(partial) - mech failure/malfManeuvering - aerial application
Throttle/power lever,cable - failureCause
Forced landingDescent - uncontrolled
Autorotation - attemptedPilot in command
In flight collision with objectDescent - uncontrolled
Object - tree(s)Factor
Terrain condition - none suitableFactor

Analysis

The pilot said that he was spraying cherries when the engine suddenly stopped. He attempted an autorotation, but the main rotor impacted cherry trees. The helicopter's main bubble was shattered, and the skids and frame were bent. Postimpact examination of the aircraft, by a Federal Aviation Administration Inspector, revealed that the throttle cable's housing had broken, which permitted the engine's RPM to decay to the idle position.

Factual narrative

On July 4, 2005, at 1730 Pacific daylight time, a Bell 47G-2A helicopter, N38926, was substantially damaged during a forced landing attempt, following a loss of engine power near Oroville, Washington. The commercial pilot, the sole occupant on board, was not injured. Waitsburg Helicopter Service was operating the flight under Title 14 CFR Part 137. Visual meteorological conditions prevailed for the aerial application flight. A flight plan had not been filed.

The pilot said that he was spraying cherries when the engine suddenly stopped. He attempted an auto rotation, but the main rotor impacted cherry trees. The helicopter's main bubble was shattered, and the skids and frame were bent.

Postimpact examination of the aircraft, by a Federal Aviation Administration Inspector, revealed that the throttle cable's housing had broken, which permitted the engine's RPM to decay to the idle position.

Aircraft

Registration
N38926
Reported as
Bell 47G-2A
Category
Helicopter
Serial number
N.A.H. 1957-1
Engine
Lycoming VO-435-A1F, 265 horsepower, reciprocating
Damage
Substantial damage
Flight
Aerial application · Part 137
Registered owner
Waitsburg Helicopter Service
Airworthiness certificate
Special, Restricted (Special)
Last inspection
Annual · April 1, 2005 · 50 hours before
Departed
0S7 · Oroville, WA
Destination
0S7

Matched to the registry by N-number and the event date; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
59
Injuries
None
Certificate
Commercial
Medical
Class 2, Without waivers/limitations
Seat
Left
Flight hours
10,000 total · 10,000 as pilot in command · 150 in the last 90 days · 50 in the last 30 days · 5 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
190° at 6 knots
Visibility
10 statute miles
Lowest ceiling
None
Temperature
90 °F, dew point 37 °F
Altimeter
29.95 inHg
Observed at
OMK, 32 nm away

FAA reports on this event · 1

The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.

Other investigations on N38926 · 5

Matched to the same aircraft by N-number and date.