FTW88DPJ12

NTSB accident investigation · Snyder Stolp SA-300 · Oklahoma City, OK · September 17, 1988

Accident · FatalFinal report
Date
September 17, 1988, 11:27 local (16:27 UTC)
Place
Oklahoma City, OK
Injuries
1 fatal
Damage
Destroyed
Phase of flight
Maneuvering
Aircraft
N57DHSnyder Stolp SA-300
Weather
Visual (VMC) · Day
Status
Completed · report January 16, 1990
Report
Approved by Office Director
FAA report
19880917045399A
Case key
22462

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

Total failure of the rudder control due to failure of the metal welds on the cable attachment to the rudder pedal, due to improper welding by the manufacturer.

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 - performed
Flt control syst,rudder control attach points - improperCause
Inadequate quality controlManufacturerCause
Flt control syst,rudder control attach points - overload
Loss of control - in flightManeuvering
Stall/spin - uncontrolled
In flight collision with terrain/waterDescent - uncontrolled

Analysis

Witnesses rprtd the plt was doing aerobatics near the arpt. They observed two snap rolls, then saw the acft enter a spin to the right. The witnesses said the acft was maneuvering at an estimated 1,500 to 1,900 feet AGL, then it spun, uncorrected to ground impact. An investigation revealed that in the rear cockpit, the rudder cable attachment on the left rudder pedal had failed. A metallurgical examination revealed the fracture was typical of overstress, but the welded area had voids & there was a lack of fusion & penetration in the welded area.

Aircraft

Registration
N57DH
Reported as
Snyder Stolp SA-300 (STOLP SA-3)
Category
Airplane, amateur-built
Serial number
826
Engine
Lycoming O-360, 180 horsepower, reciprocating
Damage
Destroyed
Flight
Personal · Part 91
Operator
Howard, H. David
Registered owner
H. David Howard
Airworthiness certificate
Special, Experimental (Special)
Last inspection
Annual · August 15, 1988
Departed
HSD5
Airport
HSD · Sundance, runway 17, 5,000 × ft, concrete

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
44
Certificate
Private
Airplane ratings
Single-engine land
Medical
Class 3, Valid Medical--no waivers/lim.
Seat
Rear
Flight hours
708 total · 658 as pilot in command

Weather

Conditions
Visual (VMC) · Day
Wind
200° at 10 knots
Visibility
8 statute miles
Lowest ceiling
None
Temperature
79 °F, dew point 72 °F
Altimeter
30.00 inHg
Observed at
PWA, 3 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.