FTW90FA046

NTSB accident investigation · Bell 206L-1 · S Marsh Is 7 · December 27, 1989

Accident · Serious injuriesField investigationFinal report
Date
December 27, 1989, 11:30 local (17:30 UTC)
Place
S Marsh Is 7
Injuries
3 serious, 3 minor
Damage
Destroyed
Phase of flight
Approach
Aircraft
N3913SBell 206L-1
Weather
Visual (VMC) · Day
Status
Completed · report September 5, 1991
Report
Approved by Office Director
FAA report
19891227053329A
Case key
23005

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 failure to recognize and correct a situation involving loss of tail rotor effectiveness, resulting in loss of aircraft control.

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 control - in flightGo-around (vfr)
Go-around - initiatedPilot in command
Aircraft control - not maintainedPilot in commandCause
In flight collision with terrain/waterDescent - uncontrolled
Terrain condition - water
Roll overLanding
Landing gear,float assembly - separation

Analysis

The helicopter had been loaded near its max gross wt limit of 4150 lbs. The plt rprtd that during an apch to an offshore platform in the gulf of Mexico, there was virtually no wind. As the apch speed dropped below effective translational lift, the plt noted a shudder that did not seem normal, so he initiated a go-around. As he applied power & pedal to go around, the acft spun to the rgt & the nose tucked. The plt tried to correct the situation, but was unable. He rprtd that just before water impact he leveled the helicopter, deployed the emerg floats & applied full collective pitch. Also, he stated the rate of spin decreased as he applied collective pitch. One of the left floats separated on water entry & the helicopter rolled over. No feedback or restriction of the controls was noted before impact. A post-acdnt exam of the helicopter did not reveal any preimpact part failure or malfunction.

Aircraft

Registration
N3913S
Reported as
Bell 206L-1
Category
Helicopter
Serial number
45666
Airframe hours
8,764
Engine
Allison 250-C28B, 500 horsepower, turbo shaft
Damage
Destroyed
Flight
Part 135
Operator
Air Logistics
Airworthiness certificate
Standard, Normal
Last inspection
AAIP · December 25, 1989 · 2 hours before
Departed
NONE · Grand Chenier, LA
Flight plan
Company VFR

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
42
Certificate
Commercial
Instrument ratings
Helicopter
Medical
Class 2, Valid Medical--no waivers/lim.
Seat
Right
Flight hours
6,796 total · 4,867 in this make and model · 6,796 as pilot in command · 174 in the last 90 days · 57 in the last 30 days · 3 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
Calm
Visibility
7 statute miles
Lowest ceiling
None
Temperature
61 °F, dew point 54 °F
Altimeter
30.00 inHg
Observed at
7R4, 35 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.