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NTSB Report

August 15, 1998 · Piper PA-18-150 · N3981Z

Conway, SC

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
August 15, 1998
Injury Outcomes
1 injury (1 minor injury)
Location
Conway, SC
Aircraft
Piper PA-18-150
Tail Number
N3981Z
Injuries
Minor
Aircraft Damage
Substantial
NTSB Number
MIA98LA226

The pilot was attempting a banner tow pick up when the left wing collapsed. Examination of the left wing forward and aft attachment fitting by the NTSB Materials Laboratory revealed the failure of the brackets due to corrosion and fatigue.

NTSB Probable Cause

The total failure of the left wing forward and aft attachment fitting due to corrosion and fatigue during a banner tow pick-up resulting in a subsequent in-flight collision with terrain.

Full Narrative

On August 15, 1998, about 0955 eastern daylight time, a Piper PA-18-150, N3981Z, registered to Sky Signs Inc., operating as a 14 CFR Part 91 banner tow flight, crashed while attempting a banner tow pick-up at the Sky Signs private airstrip, Conway, South Carolina. Visual meteorological conditions prevailed and no flight plan was filed. The airplane sustained substantial damage. The commercial pilot reported minor injuries. The flight originated about 5 minutes before the accident. An FAA inspector who observed the accident stated the pilot was picking up a banner on runway 34. The airplane picked up the banner and was in about a 30-degree nose-up attitude when the left wing collapsed. The airplane rolled to the right about 300 degrees, the nose pitched down, and the airplane collided with the ground inverted. Examination of the left wing revealed the left forward lift strut attachment fitting was severely corroded. The separated left wing forward and aft strut attachment fitting, and the right wing forward and aft attachment fitting were sent to the NTSB Materials Laboratory for analysis. Examination revealed the front face of the forward bracket was subjected to severe corrosion damage. The bracket separated approximately 2.8 inches away from its inboard lower end, at a location corresponding to a vertical position on assembly that is in line with or just below the lower spar cap of the forward spar. Evidence of corrosion was also apparent on the upper and lower sides of the bracket. Binocular microscope examination revealed that the most corrosion damage was on the front face of the bracket. Examination of the aft bracket revealed that it separated through the lower of the five holes used to attach the bracket to the front spar. Binocular microscope examination revealed that a portion of the aft bracket fracture was on a flat plane and contained crack arrest positions typical of fatigue cracking. (For additional information see NTSB Materials Laboratory Factual Report No. 99-49.) The components retained for further analysis were released to M. Jenkins, Sky Signs Inc., on February 12, 1999.

Flight

Event TypeAccident
Event Time09:55 EDT
Nearest Airport0nm
Runway34
Runway Length1800 ft
Runway Width100 ft
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftPiper PA-18-150
Tail NumberN3981Z
Aircraft CategoryAir
DamageSubstantial
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsLycoming · O-360-A4M · Reciprocating
Seats2

People & Injuries

Injury Summary1 injury (1 minor injury)
Fatal0
Serious0
Minor1
Uninjured0
Total1
Crew 1Age 26 · Second Class

Conditions

ConditionsIMC
LightDaylight
Wind20° @ 6 kt
Visibility4 sm
CeilingBroken clouds 15000 ft
Altimeter29.00 inHg
Observation Time13:45
Weather SourceWFAC

Appendix: Source Data