Aviation Accident Summaries

Aviation Accident Summary MIA93LA148

TAMPA, FL, USA

Aircraft #1

N4106M

PIPER PA-12

Analysis

WHILE TOWING A BANNER THE PILOT NOTED THE ENGINE FAILED AND A FIRE WAS OBSERVED FROM THE COWLING. HE RELEASED THE BANNER, EXECUTED A FORCED LANDING, AND EXITED THE AIRPLANE WITHOUT INJURY. THE AIRPLANE WAS DESTROYED BY FIRE. EXAMINATION OF THE MUFFLER SYSTEM REVEALED INTERGRANULAR AND FATIGUE CRACKING OF THE INLET PIPE SEAM. THIS ALLOWED HOT EXHAUST GASSES AND FLAME TO IMPINGE OF A FUEL LINE IN THE AREA STARTING A FIRE.

Factual Information

On July 2, 1993, about 0807 eastern daylight dime, N4106M, a Piper PA-12, registered to and operated by Aerial Billboard Corporation, experienced an in-flight fire over Tampa, Florida, while on a 14 CFR Part 91 banner towing flight. Visual meteorological conditions prevailed at the time and no flight plan was filed for the local flight. The pilot was not injured and the airplane was destroyed by the fire. The flight originated from St. Petersburg, Florida, about 30 minutes earlier. The pilot stated the engine began to run rough, lose power and he observed flames from the cowling. He released the banner he was towing and executed a forced landing to an open field. He exited the airplane without injury and the airplane was destroyed by fire. The engine exhaust system and muffler were removed and forwarded to the NTSB laboratory for examination. Cracking of the inlet pipe sleeve on the heat exchanger was found with evidence that the crack had previously been repaired. The cracking exhibited signatures consistent with long term, progressive, intergranular degradation. The cracking progressed to about 1/3 of the seam and shifted from intergranular cracking to fatigue cracking at the end. This crack allowed the exhaust heat and flames to escape prematurely and impinge upon the fuel line in the area, initiating combustion and fire.

Probable Cause and Findings

the improper welding/repair by maintenence personnel of the exhaust system, which eventually failed allowing hot exhaust gasses and flame to burn a fuel line and start a fire.

 

Source: NTSB Aviation Accident Database

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