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Aviation safety reports, made easier to study

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July 20, 1983 · Helio H395 · N4156D

Fairbanks, AK

Overview

Report Status
Preliminary report
Event Type
Accident
Date
July 20, 1983
Injury Outcomes
1 injury (1 fatality)
Location
Fairbanks, AK
Aircraft
Helio H395
Tail Number
N4156D
Injuries
Fatal
Aircraft Damage
Substantial
NTSB Number
ANC83FA126

Takeoff was from a dirt driveway which had a usable length of 330 ft before it curved north. Before takeoff, the pilot had bent several small trees back away from the driveway and tied them down so they would not interfere with the takeoff. There are numerous trees surrounding the area, with an opening at the departure end of about 40 ft wide. The wingspan of the aircraft was 38 ft 6 inches. As the pilot tried to fly through the opening, the left wing contacted a tall tree and the leading edge slat separated. The aircraft rolled and crashed inverted onto a guard rail of an adjacent highway. The aircraft was equipped with an automobile restraint system. The shoulder harness attaching bracket was located at the top of the bench seat. The shoulder harness strap came loose from that attaching point during the crash sequence. The aircraft had been reportedly rebuilt by the pilot who is not an A&P. There were rivets missing in the vertical stabilizer, and where holes didn't match up, new ones were drilled and screwed together.

Full Narrative

TAKEOFF WAS FROM A DIRT DRIVEWAY WHICH HAD A USABLE LENGTH 0F 330 FT BEFORE IT CURVED NORTH. BEFORE TAKEOFF, THE PLT HADBENT SEVERAL SMALL TREES BACK AWAY FROM THE DRIVEWAY & TIED THEM DOWN SO THEY WOULD NOT INTERFERE WITH THE TAKEOFF. THERE ARE NUMEROUS TREES SURROUNDING THE AREA, WITH AN OPENING AT THE DEPARTURE END OF AOUT 40 FT WIDE. THE WINGSPAN OF THE ACFT WAS 38 FT 6 INCHES. AS THE PLT TRIED TO FLY THRUUGH THE OPENING, THE LEFT WING CONTACTED A TALL TREE & THE LEADING EDGE SLAT SEPARATED. THE ACFT ROLLED & CRASHED INVERTED ONTO A GUARD RAIL OF AN ADJACENT HIGHWAY. THE ACFT WAS EQUIPPED WITH AN AUTOMOBILE RESTRAINT SYSTEM. THE SHOULDER HARNESS ATTACHING BRACKET WAS LOCATED AT THE TOP OF THE BENCHSEAT. THE SHOULDER HARNESS STRAP CAME LOOSE FROM THAT ATTACHING POINT DURING THE CRASH SEQUENCE. THE ACFT HAD BEEN REPORTEDLY REBUILT BY THE PLT WHO IS NOT AN A&P. THERE WERE RIVETS MISSING IN THE VERTICAL STABILIZER, & WHERE HOLES DIDN'T MATCH UP, NEW ONES WERE DRILLED & SCREWED TOGETHER.

Flight

Event TypeAccident
Event Time17:35 AHDT
Nearest Airport6nm NNW
Runway0
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftHelio H395
Tail NumberN4156D
Aircraft CategoryAir
DamageSubstantial
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsLycoming · GO-480-G1D6 · Reciprocating · 295
Seats2

People & Injuries

Injury Summary1 injury (1 fatality)
Fatal1
Serious0
Minor0
Uninjured0
Total1
Crew 1Age 43 · Third Class

Conditions

ConditionsVMC
LightDaylight
Wind290° @ 8 kt
Visibility10 sm
CeilingOvercast 25000 ft
Temperature / Dew Point68 F / 46
Altimeter29.00 inHg
Observation Time20:53
Weather SourceWFAC

Appendix: Source Data