ATL89MA070

NTSB accident investigation · Swearingen SX-300 · Wilmington, OH · January 9, 1989

Accident · FatalMajor investigationFinal report
Date
January 9, 1989, 09:01 local (14:01 UTC)
Place
Wilmington, OH
Injuries
2 fatal
Damage
Destroyed
Phase of flight
Enroute
Aircraft
N6YSwearingen SX-300
Weather
Visual (VMC) · Day
Status
Completed · report June 1, 1989
Report
Approved by Office Director
FAA report
19890109000349A
Case key
8075

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

Fatigue and resulting failure of the right wing's lower attachment fitting and inadequate quality control by the swearingen SX-300 production/design personnel.

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/malfunctionCruise - normal
Wing,wing attachment fitting - fatigueCause
Inadequate quality controlProduction/design personnelCause
Wing,wing attachment fitting - fracturedCause
Wing - separation
Loss of control - in flightCruise - normal
Aircraft control - not possible
In flight collision with terrain/waterDescent - uncontrolled

Analysis

This SX-300 (SA-29) was a proof-of-concept acft being demonstrated for the USAF at wright-patterson afb. The acft was cleared to restricted area R5503 at 8000 ft for a demonstration. Radio communications with indianapolis ARTCC were routine; there were no distress transmissions. About 7 minutes after takeoff the acft was involved in an inflight breakup. The wreckage path was about 1 mile in length with the rt wing 3000 feet from the main wreckage. The rt wing lower attachment fitting exhibited a fatigue area which progressed to failure from a weld nugget near the intersection of two weld beads. Pre-existing cracks were also present in the lug weld area of the left wing upper and lower attach- ment fittings. The acft had been in svc 571 hrs. It was certified as an experimental category exhibition acft. The designer had static load tested the wings to 6 g's & suspected the acft had been subjected to flt loads apchg 6 g's. the plt told an acquaintance that he had routinely exceeded the 'red line' by 85 mph.

Aircraft

Registration
N6Y
Reported as
Swearingen SX-300
Category
Airplane
Serial number
001
Airframe hours
571
Engine
Lycoming IO-540-L1C5, 300 horsepower, reciprocating
Damage
Destroyed
Fire
On-Ground
Flight
Part 91
Registered owner
Jafftech Industries, Inc.
Airworthiness certificate
Special, Experimental (Special)
Last inspection
Annual · March 24, 1988 · 87 hours before
Departed
FFO · Dayton, OH
Flight plan
IFR

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
55
Certificate
Commercial
Airplane ratings
Multi-engine land, Single-engine land
Instrument ratings
Airplane
Medical
Class 2, Valid Medical--no waivers/lim.
Seat
Left
Toxicology
Performed
Flight hours
7,754 total · 145 in this make and model · 30 in the last 90 days · 22 in the last 30 days · 5 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
220° at 10 knots
Visibility
15 statute miles
Lowest ceiling
12,000 ft broken
Temperature
25 °F, dew point 16 °F
Altimeter
30.00 inHg
Observed at
FFO, 18 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.