LAX96LA346

NTSB accident investigation · Bell 206B · Fillmore, CA · September 30, 1996

Accident · No injuriesLimited investigationFinal report
Date
September 30, 1996, 13:00 local (20:00 UTC)
Place
Fillmore, CA
Injuries
2 uninjured
Damage
Substantial damage
Phase of flight
Landing
Aircraft
N59576Bell 206B
Weather
Visual (VMC) · Day
Status
Completed · report September 30, 1997
Report
Approved by Office Director
FAA report
19960930030659A
Case key
29570

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 flight instructor's inadequate supervision and delay in taking remedial action to stop the aircraft's lateral movement, which resulted in a dynamic rollover after touchdown.

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.

Roll overLanding - flare/touchdown
Supervision - inadequatePilot in command(cfi)Cause
Autorotation - initiatedDual student
Weather condition - crosswindFactor
Remedial action - delayedPilot in command(cfi)Cause
Terrain condition - sand barFactor
Dynamic rollover - inadvertentPilot in command(cfi)Cause

Analysis

According to the flight instructor (CFI), he and the student pilot were on an instructional flight, and the student was performing hovering autorotations to a clear, moist, sandy area of a river bed. The CFI reported that the student began an autorotation from a 3-foot hover when, about 1 foot above the ground, the helicopter began to drift to the left. The CFI took the controls and applied right cyclic as the rotor rpm continued to decay. His control input did not stop the helicopter's accelerating leftward movement. As the left skid touched down on sandy terrain, the helicopter experienced a dynamic rollover and rolled onto its left side. The wind at the accident site was estimated to be westerly at about 10 knots.

Factual narrative

On September 30, 1996, about 1300 hours Pacific daylight time, a Bell 206B, N59576 rolled over while practicing hovering autorotations near Fillmore, California. The aircraft sustained substantial damage; however, neither the instructor nor his student was injured. The aircraft was operated as an instructional flight by the owner/student when the accident occurred. The flight originated from Whiteman airport, Los Angeles, California, on the morning of the accident. Visual meteorological conditions prevailed at the time and no flight plan had been filed.

The flight instructor stated he directed his student to perform a hovering autorotation with an entry from a 3-foot hover. As the aircraft descended to about 1 foot above the ground, it began to drift to the left. He took the controls and applied right cyclic as the rotor rpm continued to decay. His control input did not stop the helicopter's accelerating leftward movement. As the left skid touched down, the helicopter abruptly pivoted about the skid and rolled onto its left side. During the rollover, the main rotor blade(s) severed the tailboom. He reported to an FAA inspector that he estimated surface winds at the accident site to have been westerly at approximately 10 knots.

Aircraft

Registration
N59576
Reported as
Bell 206B
Category
Helicopter
Serial number
1473
Airframe hours
28,844
Engine
Allison 250C20J, 420 horsepower, turbo shaft
Damage
Substantial damage
Flight
Instructional · Part 91
Registered owner
Richard Delaney
Airworthiness certificate
Standard, Normal
Last inspection
100 hour · April 20, 1996 · 44 hours before
Departed
WHP · Los Angeles, CA

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
39
Certificates
Commercial, Flight instructor
Airplane ratings
Single-engine land, Multi-engine land
Instrument ratings
Airplane
Medical
Class 2, Valid Medical--no waivers/lim.
Seat
Left
Flight hours
2,810 total · 1,015 in this make and model · 2,600 as pilot in command · 44 in the last 90 days · 20 in the last 30 days

Weather

Conditions
Visual (VMC) · Day
Wind
270° at 10 knots
Visibility
3 statute miles
Lowest ceiling
None
Temperature
79 °F, dew point 57 °F
Altimeter
29.00 inHg
Observed at
VNY, 15 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.