N52854

Substantial
Serious

CESSNA T206HS/N: T20608939

Accident Details

Date
Thursday, June 16, 2022
NTSB Number
CEN22LA253
Location
Austin, TX
Event ID
20220617105272
Coordinates
30.194527, -97.669876
Aircraft Damage
Substantial
Highest Injury
Serious
Fatalities
0
Serious Injuries
1
Minor Injuries
0
Uninjured
0
Total Aboard
1

Probable Cause and Findings

A total loss of engine power due to an engine fire that resulted from failure of the turbocharger exhaust clamp, which allowed hot exhaust gases to damage other vital engine components.

Aircraft Information

Registration
N52854
Make
CESSNA
Serial Number
T20608939
Engine Type
Reciprocating
Year Built
2009
Model / ICAO
T206HC206
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
SALE REPORTED
Address
2155 VERMONT RD
Status
Deregistered
City
RANTOUL
State / Zip Code
KS 66079-9014
Country
United States

Analysis

On June 16, 2022, about 1400 central daylight time, a Cessna T206H, N52854, was substantially damaged when it was involved in an accident near Austin, Texas. The pilot was seriously injured. The airplane was operated as a public use flight.

The pilot reported that the accident flight was the first flight following a 100-hour maintenance inspection. The pilot departed from the Austin-Bergstrom International Airport (AUS), Austin, Texas, and shortly after takeoff reported to air traffic control that there was smoke in the cockpit and he wanted to return to AUS. Shortly thereafter, the smoke increased, and the pilot was not able to see his instrument panel. He attempted to increase engine power and discovered that the engine had stopped producing power. After opening the airplane’s side windows, he could see a body of water below him and ditched the airplane into Lady Bird Lake, near Austin.

Postaccident examination revealed that the V-band exhaust coupling securing the turbocharger exhaust fractured.

The General Aviation Joint Steering Committee issued a “Best Practices Guide for Maintaining Exhaust System Turbocharger to Tailpipe v-band Couplings / Clamps”, which recommended life limits for the various styles of clamps including a 500-hour life limit on spot welded v-band couplings such as the failed coupling from the accident airplane.

Figure 1. Photo of failed V-band exhaust coupling.

The Federal Aviation Administration issued a Special Airworthiness Information Bulletin (SAIB), CE-18-07, on December 14, 2017, which described several accidents that resulted from v-band clamp failures. The SAIB recommended detailed inspections of v-band exhaust couplings be performed at 100-hour intervals. It also identified areas of concern and locations on the v-band exhaust couplings for focused inspection.

In April 2018, the General Aviation Joint Steering Committee issued a “Best Practices Guide for Maintaining Exhaust System Turbocharger to Tailpipe V-band Couplings / Clamps”, which went into further detail concerning the various designs of exhaust system couplings, and inspection of those couplings. The guide also recommended life limits for the various styles of clamps including a 500-hour life limit on spot welded v-band couplings such as the failed coupling from the accident airplane.

According to maintenance records, the airplane’s most recent annual inspection was completed on December 13, 2021, and indicated that an exhaust system inspection was included in the inspection process. A 100-hour inspection was completed on June 15, 2022, and indicated that an exhaust system inspection had been performed. Neither entry specifically noted inspection of the v-band exhaust couplings and the investigation was unable to determine if a specific inspection of the v-band clamp was accomplished. The total time in service of the clamp was not determined.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN22LA253