SDR AU981445

Service difficulty report · Bulkhead · Grob G115C

Difficulty date
November 6, 1998
Submitted
March 26, 2000
Operation
General aviation
Make and model
Grob G115C
Engine
Lyc O360A1F6
Propeller
Hartzl HCF2YR1
Part
Bulkhead
Condition
Cracked
Location
Fuselage
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) FUSELAGE STRUCTURE CRACKED ON LT AND RT SIDES IN AREA ADJACENT TO THE FORWARD UPPER TAILPLANE ATTACHMENT AREA WHERE THE FUSELAGE SHELL JOINS THE BULKHEAD.