SEA08CA059

NTSB accident investigation · Bell 206 B2 · La Verna, CA · January 13, 2008

Accident · No injuriesData collectionFinal report
Date
January 12, 2008, 16:15 local (Jan 13, 2008, 00:15 UTC)
Place
La Verna, CA
Injuries
2 uninjured
Damage
Substantial damage
Phase of flight
Maneuvering
Aircraft
N49588Bell 206 B2
Defining event
Maneuvering: Loss of control in flight
Weather
Visual (VMC) · Day
Status
Completed · report February 28, 2008
Report
Approved by Office Director
Case key
67366

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

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Probable cause

The pilot's improper preflight planning which resulted in a jammed cyclic control while maneuvering.

Findings · 2

NTSB’s coded findings. Those marked are part of the probable cause; the rest are factors or other findings. Under each, the cases with the same finding.

Rotorcraft flight controlAircraft › Aircraft propeller/rotor · InoperativeAll aircraft: 9 casesProbable cause
Planning/preparation: flight planning/navigationPersonnel issues › Task performance · PilotAll aircraft: 179 casesProbable cause

Sequence of events

The events NTSB coded, in order, by phase of flight. The defining event is the one that best describes the accident. Under each, the cases with the same event anywhere in their sequence.

Analysis

The pilot reported that the helicopter was in a three-foot hover, moving forward, when control was lost and the helicopter collided with terrain. The pilot reported the left cyclic control was removed prior to the flight; however, the protective cover was not installed. He stated that during the accident flight, test equipment (used for track and balance) "became entangled" at the left cyclic attach point and prevented full cyclic control.

Factual narrative

The commercial pilot and mechanic were conducting a maintenance test flight to facilitate a dynamic track and balance of the main rotor system when the accident occurred. In a written statement, the pilot reported the helicopter was in a three-foot hover, moving forward, when control was lost. The helicopter subsequently collided with terrain resulting in substantial damage to the fuselage. The pilot reported the left cyclic control was removed prior to the flight; however, the protective cover was not installed. He stated that during the accident flight, the test equipment (used for track and balance) "became entangled" at the left cyclic attach point and prevented full cyclic control.

Aircraft

Registration
N49588
Reported as
Bell 206 B2
Category
Helicopter
Serial number
1726
Engine
Rolls-Royce 250 C-20B, 400 horsepower, turbo shaft
Damage
Substantial damage
Flight
Personal · Part 91
Registered owner
Robert L. Miars
Airworthiness certificate
Standard, Normal
Departed
POC · La Verna, CA
Destination
POC · La Verna, CA
Airport
POC · Brackett Field, runway UNK

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
68
Certificate
Commercial
Airplane ratings
Multi-engine land, Single-engine land
Medical
Class 3
Flight hours
6,500 total · 2,200 in this make and model · 20 in the last 90 days · 20 in the last 30 days

Weather

Conditions
Visual (VMC) · Day
Visibility
30 statute miles
Lowest ceiling
None
Temperature
72 °F