CHI88FA240

NTSB accident investigation · Bellanca 8KCAB · Oswego, IL · September 20, 1988

Accident · FatalField investigationFinal report
Date
September 20, 1988, 18:25 local (23:25 UTC)
Place
Oswego, IL
Injuries
1 fatal
Damage
Destroyed
Phase of flight
Maneuvering
Aircraft
N50702Bellanca 8KCAB
Weather
Visual (VMC) · Day
Status
Completed · report January 31, 1990
Report
Approved by Office Director
Safety recommendations
Yes
FAA report
19880920039529A
Case key
13973

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

Inadequate design inthe manufacture of the pilot's seat which failed during intentional aerobatic maneuvers for which the aircraft including the seat were intended.

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/malfunctionManeuvering
Aerobatics - initiatedPilot in command
Fuselage,seat - wornFactor
Fuselage,seat - failure,totalCause
Acft/equip,inadequate designManufacturerFactor
Flt control syst,elevator control - disabledCause
Design stress limits of aircraft - exceededFactor
Wing - failure,total
Wing - separation
In flight collision with terrain/waterDescent - uncontrolled

Analysis

Drg aerobatics, the acft went in a dive, gained speed, leveled off & pulled up abruptly. Drg the pull-up, the rgt wing failed upward & sepd fm the acft. The acft then went out of ctl & crashed. The plt was wearing a parachute, but did not bail-out; he was found strapped in his seat & the door rls pin was still in place. There was evidence of upward bending of the left wing; both horizontal stabilizers had evidence of being compromised in a dwnwrd drctn. An exam of the plt's seat revealed the tubular ends of the seat-back frame had failed at the pivot points (pvt pts), where the seat-back was designed to pivot fwd ovr the seat pan to allow entry to the aft seat. Attaching bolts at the pvt pts had pulled thru the ends of the frame. Evidence of overstress shear was fnd at the rgt pvt pt as if the seat-back had failed aft. Evidence of overstress shear & twisting deformation was fnd at the left pvt pt. Bellanca 7 & 8 series acft have had svrl seatback failures at the hinge point or at the welded junction of the seat's lower side tube & seatback side brace.

Aircraft

Registration
N50702
Reported as
Bellanca 8KCAB
Category
Airplane
Serial number
616-80
Airframe hours
1,343
Engine
Lycoming AEIO-360-H1A, 180 horsepower, reciprocating
Damage
Destroyed
Flight
Personal · Part 91
Operator
Lewis, Richard A.
Registered owner
Lewis, Richard A
Airworthiness certificate
Standard, Normal; Standard, Aerobatic
Last inspection
Annual · April 29, 1988 · 117 hours before
Departed
1C5 · Plainfield, IL

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
52
Certificate
Private
Airplane ratings
Single-engine land
Instrument ratings
Airplane
Medical
Class 3, Valid Medical--w/ waivers/lim
Seat
Front
Toxicology
Performed
Flight hours
1,312 total · 333 in this make and model · 55 in the last 90 days · 22 in the last 30 days · 1 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
300° at 10 knots
Visibility
15 statute miles
Lowest ceiling
None
Temperature
63 °F, dew point 52 °F
Altimeter
29.00 inHg
Observed at
DPA, 14 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.