LAX86MA309

NTSB accident investigation · Aerospatiale AS-355F-1 · Morgan City, LA · July 18, 1986

Accident · No injuriesMajor investigationFinal report
Date
July 18, 1986, 07:55 local (12:55 UTC)
Place
Morgan City, LA
Injuries
1 uninjured
Damage
Destroyed
Phase of flight
Approach
Aircraft
N57967Aerospatiale AS-355F-1
Weather
Visual (VMC) · Day
Status
Completed · report February 12, 1988
Report
Approved by Office Director
FAA report
19860718034609A
Case key
25285

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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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.

Airframe/component/system failure/malfunctionApproach - vfr pattern - final approach
Fuselage,attachment - failure,partial
Reason for occurrence undeterminedCause
Fuselage,attachment - fatigue
Fuselage,attachment - failure,total
Loss of control - on ground/waterLanding - flare/touchdown
Miscellaneous - vibration

Analysis

The plt flew to a nearby arpt to practice takeoffs & lndgs. He rprtd that after 3 lndgs 'out of a hover,' he returned to the departure heliport & lndd again from a hover. Drg touchdown, the helicopter bgn to rock fm side to side & enteredground resonance. The plt rprtd he lowered the collective pitch to the bottom stop, but stated the sideward bouncing fm skid to skid worsened. He reached for the overhead throttles, but was being flailed about the cockpit & could not hold onto them. Subsequently, the helicopter was extensively damaged. Witnesses verified the side to side bouncing & rprtd hearing a loud metallic sound before the helicopter touched down. A post-crash exam revealed the l front, l rear & rgt rear support tubes (gearbox bars) were buckled in a 'd' shape & fractured at midspan. Metallurgical exam of the fractureareas disclosed evidence of high stress, low amplitude fatigue. No history of hard lndgs or maintainance/manufacturing discrepancies were fnd concerning the gearbox bars; l front bar had 1522 hrs of svc, rear bars had 3396 hrs of svc.

Aircraft

Registration
N57967
Reported as
Aerospatiale AS-355F-1
Category
Helicopter
Serial number
5169
Airframe hours
3,397
Engine
Allison 250-C20F, 250 horsepower, turbo shaft
Damage
Destroyed
Flight
Instructional · Part 91
Operator
Mobil Oil Corp.
Registered owner
Petrolueum Helicopters Inc
Airworthiness certificate
Standard, Normal
Last inspection
Continuous airworthiness · July 11, 1986 · 20 hours before
Airport
Mobil Oil Heliport

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
52
Certificates
Commercial, Airline transport, Flight instructor
Airplane ratings
Multi-engine land, Single-engine land
Instrument ratings
Airplane, Helicopter
Medical
Class 1, Valid Medical--no waivers/lim.
Seat
Right
Flight hours
16,500 total · 15 in this make and model · 16,400 as pilot in command · 320 in the last 90 days · 3 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
Calm
Visibility
10 statute miles
Lowest ceiling
None
Temperature
81 °F

FAA reports on this event · 1

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