Service difficulty report · Exhaust Stack · Cessna T206H

Difficulty date
August 9, 2007
Submitted
October 2, 2007
Operation
General aviation
Aircraft
N168JS
Make and model
Cessna T206H
Aircraft serial
T20608735
Engine
Lyc TIO540AJ1A
Propeller
Mcauly B3D36C432
Part
Exhaust Stack
Part number
40B22318
Condition
Loose
Location
Engine
Part time
98 hours
Stage of operation
NR
How discovered
9
Nature of condition
O
Precautionary procedure
O

As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.

What was found

DURING AN INSPECTION, FOUND THE EXHAUST STACK AT NR 2 CYLINDER, PULLED DOWN .0625 INCH APPROX. FURTHER INVESTIGATION FOUND THE NR1, NR3, NR5 AND NR 6 ENGINE CYLINDERS EXHAUST STACKS PULLED DOWN, BUT NOT AS MUCH. AFTER RECOMMENDATIONS FROM ENGINE MFG ALSO, THE SUPPLIER EXHAUST SYSTEM (WHICH IS ONE IN THE SAME). DURING THE ENGINE CYLINDER REMOVAL PROCESS FOUND LOWER FWD, .7500 INCH STUD NUT UNDER TORQUED. FURTHER INVESTIGATION REVEALED THE FORWARD 2 STUDS BOTH BELOW, MFG RECOMMENDED DRIVING TORQUE OF CYLINDER HOLDDOWN STUDS IN CASE. INSTALLED NEW OVERSIZE (.003) STUDS IAW ENG MFG RECOMMENDATIONS. INSTALLED NEW NR 2 ENGINE CYLINDER AND NEW EXHAUST CROSSOVER PIPE AS REQUIRED. TIGHTENING THE EXHAUST FLANGE NUTS DOES NOT STOP THE LEAK ON ALL OF THE STUDS, SOME OF THE STUDS THE NUT BOTTOMS OUT ON THE THREAD. THE PREVIOUSLY EFFECTED EXHAUST FLANGE AREAS AFTER TIGHTENED UP HAVE COME LOOSE AGAIN IN 50 HRS TIME IN SERVICE. (K)

More about the Cessna T206H