N80JB

Substantial
None

PIPER PA 46-350PS/N: 4622156

Accident Details

Date
Sunday, May 8, 2011
NTSB Number
CEN11LA327
Location
Chico, TX
Event ID
20110509X45652
Coordinates
33.290977, -97.789726
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

The mechanic's improper installation of the turbocharger's exhaust balance system, which resulted in an in-flight fire.

Aircraft Information

Registration
N80JB
Make
PIPER
Serial Number
4622156
Engine Type
Turbo-shaft
Year Built
1994
Model / ICAO
PA 46-350PM600
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
SALE REPORTED
Address
4312 ENCHANTED OAKS DR
Status
Deregistered
City
ARLINGTON
State / Zip Code
TX 76016-5054
Country
United States

Analysis

On May 7, 2011, at 2008 central daylight time, a Piper PA 46-350P airplane, N80JB, experienced an inflight fire near Chico, Texas. The airline transport pilot, the sole occupant, was not injured. The airplane sustained substantial thermal damage. The airplane was registered to and operated by Christian Air Brotherhood, Wichita Fall, Texas, under the provisions of 14 Code of Federal Regulations Part 91 as a personal flight. Visual meteorological conditions prevailed for the flight, which operated on a visual flight rules flight plan. The flight originated from Fort Worth about 1950.

According to a statement provided by the pilot, the airplane was in cruise flight at 4,500 feet mean sea level, when he detected a change in engine noise along with fluctuations in the engine speed. The pilot started to divert to the nearest airport, when the engine began to run rough. Shortly thereafter, the pilot smelled, and saw smoke enter the airplane cabin. The smoke increased and the pilot elected to perform a forced landing on a highway. The airplane's nose landing gear did not extend and the airplane slid to a stop on the main landing gear and fuselage nose section.

A postaccident examination of the airframe and engine was conducted by the members of the National Transportation Safety Board (NTSB), as well as technical representatives from the Piper Aircraft Company and Lycoming Engines. The examination revealed substantial damage was sustained to the airplane's forward fuselage and firewall. Distortion from heat was noted to the airplane's nose gear door, which impeded normal operation of the nose landing gear. Clamps on the turbocharger's intermediate exhaust crossover tube were found unsecured. The NTSB's fire investigator found signatures of thermal distress to the fuel flow transducer and fuel flow transducer line. No additional preimpact mechanical malfunctions or failures were found that would have precluded normal operation.

A review of maintenance logbooks noted that a propeller strike had occurred in early February 2011. Repairs on the airplane were completed May 3, 2011, when the engine was removed, cleaned, and inspected. The pilot reported that the airplane had only flown four to five hours since the airplane had been returned to service.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN11LA327