ANC90FA134

NTSB accident investigation · Helio Courier H-295 · 40 Se Bettles, AK · August 4, 1990

Accident · FatalField investigationFinal report
Date
August 4, 1990, 15:05 local (23:05 UTC)
Place
40 Se Bettles, AK
Injuries
3 fatal
Damage
Destroyed
Phase of flight
Enroute
Aircraft
N6493VHelio Courier H-295
Weather
Visual (VMC) · Day
Status
Completed · report April 30, 1992
Report
Approved by Office Director
NTSB office
Alaska Regional Office
FAA report
19900804030069A
Case key
5303

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 failure and separation of the #5 connecting rod bolt and cap which resulted in the rupture of the engine housing and subsequent engine fire due to oil spillage, and an inadequately mounted vertical fin/stabilator. A contributing factor was the inadequate maintenance and inspection of the aircraft after a previous accident.

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 engine power(total) - mech failure/malfCruise - normal
Engine assembly - previous damageFactor
Maintenance,inspection - inadequateOther maintenance personnelFactor
Engine assembly,connecting rod bolt - separationCause
Engine assembly,connecting rod cap - separationCause
Engine assembly,crankcase - fracturedCause
FireCruise - normal
Engine assembly - fireFactor
Loss of control - in flightDescent - emergency
Stabilizer - looseCause
Maintenance,inspection - inadequateOther maintenance personnelFactor
Airframe/component/system failure/malfunctionDescent - emergency
Wing - overload
In flight collision with terrain/waterDescent - uncontrolled

Analysis

The pilot had indicated to bettles fss that he had lost power and that he had a fire on board. The wreckage was subsequently located 40 miles se of bettles. On-site examination showes that the right wing, both ailerons, left flap, rudder, vertical fin and stabilator had all separated from the airplane in flight. Two of the three vertical fin/stabilator-to-fuselage mounts had failed in overload; the third mount was relatively undamaged with the bolt missing and visible elongation of the bolt hole. Engine exam revealed extensive fire damage to the #5 cylinder, the head area having been completely consumed by fire. The rod cap and one bolt could not be found at the wreckage site. Four months prior to the accident major repairs were made to the airframe, the engine nose case was removed and overhauled, and the propeller was overhauled. Aircraft and pilot involved in landing accident on 6/29/88 substantially damaging the aircraft. Lycoming sb recommends engine teardown after sudden stoppage; no record of compliance.

Aircraft

Registration
N6493V
Reported as
Helio Courier H-295 (COURIER H-)
Category
Airplane
Serial number
1458
Airframe hours
3,986
Engine
Lycoming GO-480-G1D6, 295 horsepower, reciprocating
Damage
Destroyed
Fire
In-Flight
Flight
Business · Part 91
Operator
Metheny, James R
Registered owner
Vixie Rochester
Airworthiness certificate
Standard, Normal
Last inspection
Annual · April 1, 1990
Departed
Z84 · Clear, AK
Destination
Happy Valley, AK
Flight plan
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
61
Certificate
Commercial
Airplane ratings
Single-engine land, Single-engine sea, Multi-engine land
Instrument ratings
Airplane
Medical
Class 2, Valid Medical--w/ waivers/lim
Toxicology
Performed
Flight hours
7,765 total

Weather

Conditions
Visual (VMC) · Day
Wind
Calm
Visibility
30 statute miles
Lowest ceiling
None
Temperature
61 °F, dew point 41 °F

FAA reports on this event · 1

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

Other investigations on N6493V · 2

Matched to the same aircraft by N-number and date.