N2648P

Substantial
Serious

Piper PA-22-150 S/N: 22-2986

Accident Details

Date
Friday, October 29, 1999
NTSB Number
MIA00LA018
Location
NEWBERRY, SC
Event ID
20001212X20019
Coordinates
34.270446, -81.610382
Aircraft Damage
Substantial
Highest Injury
Serious
Fatalities
0
Serious Injuries
1
Minor Injuries
0
Uninjured
0
Total Aboard
1

Probable Cause and Findings

a fire in the cockpit caused by the exhaust muffler, which resulted in a forced landing in a field, and subsequent impact with a berm.

Aircraft Information

Registration
N2648P
Make
PIPER
Serial Number
22-2986
Engine Type
Reciprocating
Year Built
1955
Model / ICAO
PA-22-150 PA22
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
SIFFORD STEVE M
Address
7025 FAITH ROAD
Status
Deregistered
City
SALISBURY
State / Zip Code
NC 28146
Country
United States

Analysis

On October 29, 1999, about 1050 eastern daylight time, a Piper PA-22-150, N2648P, registered to a private individual, impacted with the ground during a forced landing near Newberry, South Carolina. Visual meteorological conditions prevailed at the time, and no flight plan was filed for the 14 CFR Part 91 personal flight. The airplane sustained substantial damage. The private-rated pilot reported serious injuries. The flight had departed from Thomson, Georgia, en route to Salisbury, North Carolina, at 1000.

According to the pilot, "...after 30 minutes in flight smoke started entering from right side defrost duct...my GPS gave [nearest airport]...14 nautical miles at 360 degrees heading...opened my window vents because my eyes were starting to water. Approximately 3 miles from airport fire started inside near right side rudder pedals...I decreased all power at about 3,000 feet msl [and] started descending towards field that I saw. I next remember crossing power lines and that was the last thing I can remember...."

A detailed inspection of the muffler was conducted by the FAA. The FAA inspector stated that the inspection revealed, "...the muffler had two areas of burn-through damage. The aircraft fire wall had an area about 14 inches in diameter with indications of severe overheating." In addition, the inspector wrote that it was his opinion, "...that a faulty exhaust muffler caused the aircraft's firewall to overheat and smolder the aircraft firewall insulation. The maintence records do not indicate that the exhaust muffler had ever been replaced."

The total time on the airframe was 1845 hours. The last inspection on the muffler was April 8, 1999, when AD 68-05-01, was complied with. AD 68-05-01, "...Inspect...the engine exhaust muffler and shroud assembly (including the internal baffle tube and tail pipe), carburetor heat shroud and air duct, support braces, clamps and brackets, exhaust stacks and manifolds...(f) remove muffler assembly...and visually inspect exterior and interior surfaces with a probe light and mirror for signs of cracks, corrosion, burn-throughs, heat damage, collapsed stack, or weld separations...."

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# MIA00LA018