FTW85FA131

NTSB accident investigation · Piper PA-34-220T · Stigler, OK · March 3, 1985

Accident · FatalField investigationFinal report
Date
March 3, 1985, 15:50 local (21:50 UTC)
Place
Stigler, OK
Injuries
4 fatal
Damage
Destroyed
Phase of flight
Enroute
Aircraft
N8160KPiper PA-34-220T
Weather
Visual (VMC) · Day
Status
Completed
Report
Approved by Office Director
FAA report
19850303004989A
Case key
21531

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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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
Fuselage,cargo compartment - disintegratedCause
Design stress limits of aircraft - exceededCause
Airframe/component/system failure/malfunctionCruise
Flight control,stabilator - failure,totalCause
Design stress limits of aircraft - exceededCause
Airframe/component/system failure/malfunctionCruise
Wing,spar - failure,partialCause
Design stress limits of aircraft - exceededCause
Loss of control - in flightDescent - uncontrolled
Emergency procedure - not possiblePilot in commandFactor
In flight collision with terrain/waterDescent - uncontrolled

Analysis

The plt filed a VFR flt plan after the wx improved from IFR to VFR with a chance of thunderstorms en route. Ocnl mod turbulence below 5000 ft was forcast due to strong/gusty low lvl wnds. While the acft was en route, a gnd witness heard the engs rev up more than normal, then he saw the acft on a northerly heading. Shortly thereafter, he heard a loud noise& saw 2 or more pieces separate from the acft. It then entered an uncontrolled dscnt & crashed. There was evidence that the acft suffered an in-flt separation of the fiberglass nose assembly, that portions of the separated nose struck the stabilator & that a damaged area on the rt stabilator acted as a trim tab & caused a pitch-up of sufficient magnitude tocause positive bending in the wings. The loading on the stabilators caused them to fail in neg bending. The acft then entered a descending counter-clockwise spin which continued until ground impact occurred. Parts of the acft & its contents separated & descended in scattered fragments.

Aircraft

Registration
N8160K
Reported as
Piper PA-34-220T (PA-34-22OT)
Category
Airplane
Serial number
34-8333030
Engine
Continental L/TSIO-360-KB, 220 horsepower, reciprocating
Damage
Destroyed
Flight
Personal · Part 91
Registered owner
Larry L. Flocks
Airworthiness certificate
Standard, Normal
Last inspection
Annual · January 22, 1985
Departed
LBB · Lubbock, TX
Destination
FSM · Ft Smith, AR
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
41
Certificate
Private
Airplane ratings
Single-engine land, Multi-engine land
Medical
Class 2, Valid Medical--no waivers/lim.
Seat
Left
Toxicology
Performed
Flight hours
238 total · 64 in this make and model · 170 as pilot in command · 13 in the last 90 days

Weather

Conditions
Visual (VMC) · Day
Wind
180° at 12 knots, gusting 22
Visibility
15 statute miles
Lowest ceiling
1,500 ft broken
Temperature
70 °F, dew point 57 °F
Observed at
MLC, 50 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.