SECTION 17.
SAILPLANE REPAIRS
TECHNICAL SERVICE MANUAL
SZD-54-2
„Perkoz”
page 17.30
Allstar PZL Glider Sp. z o.o.
Doc No. 542.4.02
Issue II
April 2014
Revision No. 2
May 2017
corrected
17.7.2.
Secondary structure
These are other elements in composite structure which damage will not affect
durability and strength of sailplane structure.
Such structure includes elements like: casings, windows, inspection openings
etc.
1. Inspection openings at wing lower surface,
2. inspection openings at vertical stabilizer,
3. Canopy sliding windows.
17.8. Assemblies interchangeability
Manufacturer provides production interchangeability of following assemblies:
wings,
fuselage,
ailerons,
horizontal stabilizer,
elevator,
rudder,
canopy,
main undercarriage and nose and tail wheel,
control systems assemblies and parts,
instrument panels,
flat wingtips or winglets and long wingtips.
NOTE:
Production interchangeability means possibility to correct mounting
mating assemblies made at separate workplaces.
In specific cases this might require mutual reaming of connecting
fittings and matching contours.
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