SECTION 17.
SAILPLANE REPAIRS
TECHNICAL SERVICE MANUAL
SZD-54-2
„Perkoz”
page 17.4
Allstar PZL Glider Sp. z o.o.
Doc No. 542.4.02
Issue II
April 2014
Revision No. 2
May 2017
corrected
When in doubt in interpretation of type or size of defects communicate with
Type Certificate Holder, who will transmit its views on the matter after familiarize with
description and photographic documentation of defect.
Damage repairs in the following cases are only performed by Type Certificate
Holder:
a) fittings torn out or damaged composite structure (white spots) around main
fittings;
b) broken spar flange;
c) damaged wing root rib or spar root;
d) broken fuselage or wing, horizontal stabilizer, aileron, rudder, elevator;
e) in case of fuselage skin is damaged in area where inner fuselage reinforcement
exists, for example cabin cut-out frame;
f)
in case of damages requiring replacement wing or fuselage shells;
g) in any other case, where professional repair cannot be assured.
Fig. 17-1. Zoning and material specification for fuselage repairs
2
