SDR AU960316

Service difficulty report · Crankcase · Cessna 404CESSNA

Difficulty date
February 29, 1996
Submitted
March 26, 2000
Operation
General aviation
Make and model
Cessna 404CESSNA
Engine
Cont GTSIO520M
Part
Crankcase
Condition
Cracked
Location
R Engine Power S
Component
Cont · GTSIO520M
Stage of operation
IN
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

(AUS) LH ENGINE CRANKCASE CRACKED - CRACK STARTED ABOVE AND FORWARD OF NO5 CYLINDER AND EXTENDED DOWNWARDS TO THE ALTERNATOR ATTACHMENT PAD - VISIBLE CRACK LENGTH 110MM (4.33IN)