SECTION 17.
SAILPLANE REPAIRS
TECHNICAL SERVICE MANUAL
SZD-54-2
„Perkoz”
page 17.20
Allstar PZL Glider Sp. z o.o.
Doc No. 542.4.02
Issue II
April 2014
Revision No. 2
May 2017
corrected
17.3.6.
Inner structure debonding
In case of inner structure debonding (Fig. 17
‒25.) the repair should be
performed as follows:
cut out the debonded part of inner structure
– if there is an access,
precisely clean repair zone, remove old glue joint and grind expected laminating
areas,
cover repair areas with composition with colloidal silica,
laminate reinforcement bracket acc. to Fig. 17
‒26.
case I
case II
Fig. 17-25. Inner structure debonding
case I
case II
Fig. 17-26. Repair of inner structure debonding
2
