FTW89FA107

NTSB accident investigation · Pitts S-1S · Henryetta, OK · June 2, 1989

Accident · Serious injuriesField investigationFinal report
Date
June 2, 1989, 15:15 local (20:15 UTC)
Place
Henryetta, OK
Injuries
3 serious, 2 minor; on the ground: 2 serious, 2 minor
Damage
Destroyed
Phase of flight
Enroute
Aircraft
N64652Pitts S-1S
Weather
Visual (VMC) · Day
Status
Completed · report September 30, 1991
Report
Approved by Office Director
FAA report
19890602014239A
Case key
22773

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

An engine power loss due to the separation and departure of an exhaust stack. The stack failed due to poor weld. Factor(s) was: the terrain conditions of the selected forced landing site.

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(partial) - mech failure/malfCruise
Exhaust system,stack - failure,totalCause
Maintenance,major repair - poorOther maintenance personnelCause
Exhaust system,stack - separationCause
Forced landingApproach - vfr pattern - final approach
In flight collision with objectApproach - vfr pattern - final approach
Object - wire,transmissionFactor
Terrain condition - hidden obstruction(s)Factor
On ground/water collision with objectLanding - roll
Object - vehicleFactor

Analysis

Power loss occurred due to separation and departure of lower 1/2 rt exhaust stack. Plt made a forced landing on the 2 northbound lanes of a divided hwy. on short final, the acft struck power lines, crashed, and slid into a truck travelling north. A passenger car, travelling south, became entangled in the wires and was subsequently rear ended by another behicle. The power line poles were masked from view by trees on both sides of the road. Examination of the exhaust stack revealed that it had undergone extensive post-manufacture repairs in the area of the separation. There was evidence of extensive weld fusion zone porosity in the area that had been welded. Weld fusion zone porosity has been attributed in the past to poor surface preparation and weld repair techniques.

Aircraft

Registration
N64652
Reported as
Pitts S-1S
Category
Airplane, amateur-built
Serial number
731-H
Airframe hours
55
Engine
Lycoming O-320-B2B, 160 horsepower, reciprocating
Damage
Destroyed
Fire
In-Flight
Flight
Personal · Part 91
Operator
Arsenault, Donald S.
Registered owner
Lorene Swahn
Airworthiness certificate
Special, Experimental (Special)
Last inspection
Annual · October 25, 1988 · 15 hours before
Departed
MLC · Mc Alester, OK
Destination
BVO · Bartlesville, OK

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
Airplane ratings
Single-engine land
Instrument ratings
Airplane
Medical
Class 2, Valid Medical--no waivers/lim.
Seat
Front
Flight hours
2,300 total · 15 in this make and model · 2,300 as pilot in command · 30 in the last 90 days · 15 in the last 30 days · 4 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
210° at 9 knots
Visibility
15 statute miles
Lowest ceiling
None
Temperature
88 °F, dew point 70 °F
Altimeter
30.00 inHg
Observed at
MLC, 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.