Service difficulty report · Spar · Cessna 404

Difficulty date
February 1, 2003
Submitted
March 3, 2003
Operation
Air carrier
Aircraft
N167SA
Make and model
Cessna 404
Aircraft serial
4040639
Engine
Cont GTSIO520F
Part
Spar
Condition
Damaged
Location
Lt Nacelle
Stage of operation
IN
How discovered
V
Nature of condition
O
Precautionary procedure
K

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

What was found

DURING A REPAIR FOR A EXHAUST BRACKET AND LOWER SKIN REPAIRS ON THE LEFT ENGINE NACELLE HEAT DAMAGE WAS FOUND ON THE LFET FORWARD SPAR BETWEEN WING STA CWS88-10555555. THIS DAMAGE IS MOST LIKELY DUE TO A CRACKED EXHAUST OUTLET OFF THE TURBO DIRECTING HOT EXHAUST GASES AT THE FACTORY HEAT SHIELD. THE FORWARD SPAR HAD A ELECTRICAL CONDUCTIVITY TEST DONE AND THE WEB IACS PERCENT WAS BEYOND LIMITS. A FORWARD WEB SPLICE REPAIR WAS PROVIDED. THIS DAMAGE LIKELY OCCURRED BEFORE THE EXHAUST AD WAS ISSUED, BUT WAS NEVER FOUND DUE TO THE LIMITED ACCESS TO THIS AREA.

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