ATL90FA150

NTSB accident investigation · Piper PA-18A · Conway, SC · July 28, 1990

Accident · FatalField investigationFinal report
Date
July 28, 1990, 10:40 local (14:40 UTC)
Place
Conway, SC
Injuries
1 fatal
Damage
Destroyed
Phase of flight
Maneuvering
Aircraft
N2789PPiper PA-18A
Weather
Visual (VMC) · Day
Status
Completed · report March 5, 1993
Report
Approved by Office Director
FAA report
19900728028859A
Case key
8144

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

Towline interference with the rudder, and failure of the pilot to maintain adequate airspeed, which resulted in a stall/spinn. A factor that contributed to the accident was: failure of the company/operator management to adequately guard against such interference.

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.

Miscellaneous/otherManeuvering
Sign towing equipment - entangledCause
Control interference - encountered
Acft/equip,inadequate compliance determinationCompany/operator managementFactor
Loss of control - in flightManeuvering
Airspeed - not maintainedPilot in commandCause
Stall/spin - inadvertentPilot in commandCause
In flight collision with terrain/waterDescent - uncontrolled

Analysis

Banner tow opns were being conducted. The plt took off to make the 1st banner tow of the day. When the tow hook (grappling hook on a rope) was deployed, the tow line bcm entangled in the rudder ctl & interfered with its movement. According to operator psnl, the plt should have visually checked the grappling hook line after it was deployed to assure that it was not fouled on the rudder bell crank; and if it was, he should have lndd to free the line, rather than pick up the banner. The acft was equipped with a hook release mechanism (iaw STC sa 1-349). However, there was evidence that when the banner was captured, its wt placed tension on the tow hook line & precluded its rls as well as causing a deflected rudder. Subsequently, the acft stalled & spun to the gnd. Operator psnl rprtd that the acft would have been controllable with the line fouled on the rudder bell crank. FAA circular (ac 43.13-2A) stated that the sys should have been tested to insure there was no interference with the tailwheel or adjacent structure.

Aircraft

Registration
N2789P
Reported as
Piper PA-18A
Category
Airplane
Serial number
18-4424
Airframe hours
5,000
Engine
Lycoming O-320-A2B, 150 horsepower, reciprocating
Damage
Destroyed
Fire
On-Ground
Flight
Part 91
Operator
Sky Signs Inc.
Last inspection
100 hour · July 3, 1990 · 75 hours before
Airport
NONE · Sky-Signs, runway 34, 1,500 × 50 ft, grass/turf

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
63
Certificate
Commercial
Airplane ratings
Single-engine land, Multi-engine land
Instrument ratings
Airplane
Medical
Class 2, Valid Medical--w/ waivers/lim
Toxicology
Performed
Flight hours
3,040 total · 344 in this make and model · 2,885 as pilot in command · 355 in the last 90 days · 177 in the last 30 days · 5 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
45° at 10 knots
Visibility
10 statute miles
Lowest ceiling
None
Temperature
84 °F, dew point -0 °F
Altimeter
29.00 inHg

FAA reports on this event · 1

The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.