SDR AU000988

Service difficulty report · Torque Box · Grob G115

Difficulty date
October 2, 2000
Submitted
November 2, 2000
Operation
General aviation
Make and model
Grob G115
Engine
Lyc O235C1B
Propeller
Mcauly 1C90LM
Part
Torque Box
Condition
Cracked
Location
Control Column
Part time
3,448 cycles
Component
Control Column
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

(AUS) CONTROL COLUMN TORQUE BOX CONTAINED TWO CRACKS ON THE LOWER SURFACE EMANATING FROM THE EDGES OF THE CONTROL COLUMN CUT-OUT. ONE OF THE CRACKS HAD BEEN STOP DRILLED AND REINFORCED WITH A SMALL DOUBLER PATCH. LOG BOOK ENTRY SHOWED THAT THE CRACK HAD BEEN REPAIRED ON 29 APRIL 1989 AT 2,523 HOURS. THIS REPAIR IS AN ILLEGAL REPAIR. AD/VAT/42 WAS LAST CARRIED OUT AT 3,399 HOURS. UNAPPROVED REPAIR. (X)