N3257B

Substantial
None

Piper PA-18-135S/N: 18-3275

Accident Details

Date
Saturday, June 28, 2008
NTSB Number
MIA08LA130
Location
Hollywood, FL
Event ID
20080702X00966
Coordinates
26.001111, -80.245552
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

The pilot's failure to achieve the proper touchdown point on landing and improper use of brakes. Contributing to the accident was the failure of the throttle cable attachment tab due to preexisting cracks.

Aircraft Information

Registration
Make
PIPER
Serial Number
18-3275
Engine Type
Reciprocating
Year Built
1954
Model / ICAO
PA-18-135PA18
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
2
FAA Model
PA-18-135

Registered Owner (Current)

Name
VAN WAGNER AERIAL MEDIA LLC
Address
1600 E AIRPORT RD
City
HOLLYWOOD
State / Zip Code
FL 33023
Country
United States

Analysis

On June 28, 2008, at 1403 eastern daylight time, a Piper PA-18-135, N3257B, registered to Seashore Advertising Corporation, and operated by Van Wagner Aerial Media, under the provisions of Title 14 Code of Federal Regulations (CFR) Part 91, as a banner tow flight, nosed over on landing roll out at North Perry Airport (HOW), Hollywood, Florida. Visual meteorological conditions prevailed and no flight plan was filed. The airplane received substantial damage to the vertical fin, and the pilot reported no injuries. The flight originated from HOW on June 28, 2008 at 1000.

The pilot stated he dropped the banner, applied power to go around, and the throttle stuck at 2,500 rpm. He informed the control tower he was unable to reduce power and entered a right downwind for runway 9 right. The pilot reached under the instrument panel and pulled on the throttle cable. The throttle returned to the idle position while the airplane was abeam the landing threshold. The pilot turned the airplane on base leg, and realized the airplane was high and fast. He started slipping the airplane to lose altitude and the airplane touched down on the last one-third of the runway. The pilot observed the end of the runway, applied brakes, and the airplane nosed over inverted.

Examination of the airplane by maintenance personnel revealed the throttle cable attachment tab was separated from the airframe. There was no evidence of corrosion or a preexisting crack. The throttle cable tab was sent to the National Transportation Safety Board Materials Laboratory, Washington, D.C., for further analysis. Examination of the throttle cable attachment tab revealed the tab fractured due to two preexisting cracks that extended across at least 75 percent of the tab cross-sectional area.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# MIA08LA130