SDR AU981502

Service difficulty report · Frame · Grob G115C

Difficulty date
November 10, 1998
Submitted
March 26, 2000
Operation
General aviation
Make and model
Grob G115C
Engine
Lyc O360A1F6
Part
Frame
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 FRAME (BULKHEAD) ADJACENT TO THE HORIZONTAL STABILIZER FORWARD ATTACHMENT POINT CRACKED AT FRAME TO FUSELAGE SHELL JOINT. PART TC: 129.