EASA Regulations for Cessna T206H

3 airworthiness directives and regulations affecting Cessna T206H.

EASA SIB CE-13-07R1

Cessna T206H Aeroplanes — Engine Exhaust Tailpipe V-band Couplings

The FAA Special Airworthiness Information Bulletin SAIB: CE-13-07R1 addresses the risk of in-flight fire caused by failure of the engine exhaust tailpipe V-band couplings on Cessna T206H airplanes. It highlights issues with the V-band clamps securing the tailpipe to the turbocharger or wastegate components and provides guidance on inspection and replacement procedures for these parts. The bulletin specifically references Cessna part number S1921-1 and approved replacement parts for Model T206H aircraft from 1998 and later.

May 14, 2013
Safety Information BulletinMaintenanceSafety MgmtTextron Aviation 206H (Stationair)Cessna T206H

EASA SIB CE-12-15

Cessna 172R/S, (T)182T and (T)206H Aeroplanes with Garmin G1000 Avionics - Master Switch Failure

The Special Airworthiness Information Bulletin SAIB: CE-12-15 is an FAA informational bulletin addressing a potential failure of the avionics master switch on Cessna 172R, 172S, 182T, T182T, 206H, and T206H airplanes equipped with Garmin G1000 avionics. The bulletin highlights a risk of accelerated switch failure that could lead to loss of avionics equipment, though essential flight and landing systems remain powered through alternate electrical sources.

Feb 1, 2012
Safety Information BulletinMaintenanceSafety MgmtCessna 172RCessna 172SCessna 182TCessna T182TCessna 206HCessna T206H

EASA SIB CE-09-11

Turbocharged Piston Engines Experiencing Turbocharger System Malfunction or Failure

The Special Airworthiness Information Bulletin SAIB: CE-09-11 is an FAA informational bulletin addressing turbocharged piston engines, specifically highlighting turbocharger system malfunctions or failures. It references a fatal accident involving a seized turbocharger on a Cessna T206H and provides operational guidance for owners and operators of aircraft equipped with turbocharged engines. The bulletin emphasizes monitoring manifold pressure and proper engine warm-up and cool-down procedures to prevent turbocharger damage.

Feb 11, 2009
Safety Information BulletinFlight OpsSafety MgmtCessna T206H