SEA94LA065

NTSB accident investigation · Bell 47G-3B-1 · Gold Hill, OR · February 24, 1994

Accident · Serious injuriesLimited investigationFinal report
Date
February 24, 1994, 08:30 local (16:30 UTC)
Place
Gold Hill, OR
Injuries
1 serious
Damage
Destroyed
Phase of flight
Maneuvering
Aircraft
N73909Bell 47G-3B-1
Weather
Visual (VMC) · Day
Status
Completed · report December 2, 1994
Report
Approved by Office Director
FAA report
19940224002919A
Case key
41879

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

Separation of the crossover fuel line, and the inability of the pilot in command to maintain a proper rate of descent during the autorotation.

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 powerManeuvering - aerial application
Fuel system,line - separationCause
Forced landingDescent - emergency
Hard landingLanding
Autorotation - not possiblePilot in commandCause
Altitude - inadequate

Analysis

While spraying herbicide the helicopter began losing power. The pilot attempted to execute a landing in a clearing during which a total power loss occurred. The helicopter then descended vertically for approximately 75 feet before landing hard. Post crash examination revealed that the fuel line crossover 't' fitting which routes fuel from the fuel tanks to the gascolator and engine had separated at its weld.

Factual narrative

On February 24, 1994, at approximately 0830 hours Pacific standard time (PST), a Bell 47G-3B-1, N73909, registered to Kenneth & Connie Owen, being operated by Pacific Air Research, Inc., and being flown by Michael D. Owen, a certificated commercial pilot, was destroyed during an autorotation landing following a loss of power while maneuvering near Gold Hill, Oregon. The pilot sustained serious injuries. Visual meteorological conditions prevailed and no flight plan had been filed. The flight, which was to have been operated in accordance with the requirements set forth in 14CFR137, was engaged in the application of herbicide.

The pilot was interviewed by Deputy Larry Walters of the Jackson County Sheriff's Department on February 25, 1994 (refer to extract of case number 94-1935). He reported to the deputy that he had been spraying when the helicopter's engine "sputter(ed)" and began losing power. The pilot then attempted to execute a landing in a cleared area adjacent to a logging road. A total loss of power occurred during the approach to landing and the helicopter descended vertically for the remaining 75 feet before impacting the ground.

The engine and fuel system were subsequently examined at the facilities of Medford Air Service, Medford, Oregon, on April 5, 1994. There was no reported evidence of a mechanical malfunction with the powerplant (refer to Inspector's Statement).

Examination of the airframe fuel system revealed that the "fuel line crossover" which connects both fuel tanks had separated at the approximate midpoint where a "T" fitting line is welded. This line routes fuel to the engine via the gascolator and fuel shutoff (refer to Inspector's Statement and report of Thomas J. Duddy including photographs 1-3).

Aircraft

Registration
N73909
Reported as
Bell 47G-3B-1
Category
Helicopter
Serial number
2797
Airframe hours
6,176
Engine
Lycoming TVO-435-BIA, 270 horsepower, reciprocating
Damage
Destroyed
Fire
On-Ground
Flight
Aerial application · Part 137
Operator
Pacific Air Research, Inc.
Registered owner
Owen, Kenneth & Connie
Airworthiness certificate
Special, Restricted (Special)
Last inspection
Annual · February 28, 1993 · 275 hours before

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
38
Certificate
Commercial
Airplane ratings
Multi-engine land, Single-engine land
Instrument ratings
Airplane
Medical
Class 2, Valid Medical--no waivers/lim.
Seat
Left
Flight hours
5,500 total

Weather

Conditions
Visual (VMC) · Day
Wind
Calm
Visibility
25 statute miles
Lowest ceiling
9,500 ft broken
Temperature
50 °F, dew point 43 °F
Altimeter
30.00 inHg
Observed at
MFR, 10 nm away

Docket · 8

The files NTSB released with the investigation on June 6, 1995, on NTSB’s docket system: statements, records, photos and specialists’ reports. 844 KB in all.

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 N73909 · 6

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