LAX86MA268

NTSB accident investigation · Aerospatiale AS-355F-1 · Galveston, TX · June 18, 1986

Accident · No injuriesMajor investigationFinal report
Date
June 18, 1986, 09:55 local (15:55 UTC)
Place
Galveston, TX
Injuries
1 uninjured
Damage
Substantial damage
Phase of flight
Approach
Aircraft
N5796TAerospatiale AS-355F-1
Weather
Visual (VMC) · Day
Status
Completed · report May 27, 1988
Report
Approved by Office Director
FAA report
19860618087109A
Case key
25283

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.

Miscellaneous/otherApproach
Fuselage - vibration
Planned approach - continued
Airframe/component/system failure/malfunctionLanding
Reason for occurrence undeterminedCause
Fuselage,attachment - fatigue
Rotor system,main rotor hub flapping hinge/stop(s) - failure,total

Analysis

The plt rprtd that while apchg an oil drilling platform for a lndg, he observed the main rotor blades go out of track about 8 to 10 inches. He also rprtd the helicopter developed a 1:1 vertical vibration. Drg the lndg, the helicopter entered into ground resonance & the plt immediately shut down both engines. An exam of the helicopter revealed the left forward transmission support bar (tsb) was buckled & cracked at midspan. A metallurgical exam of the fracture area on the tsb revealed extensive, low cycle, high amplitude, fatigue cracking. There was evidence that the propagation time ofthe fatigue occurred ovr about 5 hrs of opn. The inv did not reveal when the original buckling of the tsb occurred. No history of a prev hard lndg or gnd reasonance was fnd. Also, the red arm of the starflex had failed; an exam indcd it had ruptured either under static loads, or very rapidly under hi dynamic loads. When tested, extn & retraction times of lndg gear dampers were 8.34 to 10.38 sec; after acdnt, time lmts established at 6 to 13 sec, previously 11.1 to 13.1 sec

Aircraft

Registration
N5796T
Reported as
Aerospatiale AS-355F-1
Category
Helicopter
Serial number
5166
Airframe hours
3,500
Engine
Allison 250-C20F, 450 horsepower, turbo shaft
Damage
Substantial damage
Flight
Positioning · Part 91
Registered owner
Petroleum Helicopters, Inc.
Airworthiness certificate
Standard, Normal
Last inspection
Continuous airworthiness · June 5, 1986 · 20 hours before
Departed
High Island 571, TX
Airport
High Island 571 Platform

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
40
Certificate
Commercial
Medical
Class 2, Valid Medical--no waivers/lim.
Seat
Right
Flight hours
7,790 total · 33 in this make and model · 7,757 as pilot in command · 87 in the last 90 days · 2 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
300° at 3 knots
Visibility
15 statute miles
Lowest ceiling
None
Temperature
82 °F, dew point 70 °F
Altimeter
30.00 inHg

FAA reports on this event · 1

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