SZD-54-2
„Perkoz”
TECHNICAL SERVICE MANUAL
SECTION 17.
SAILPLANE REPAIRS
Issue II
April 2014
Revision
Allstar PZL Glider Sp. z o.o.
Doc No. 542.4.02
page 17.27
corrected
17.6.5.
Parts replacement
Design and method of sailplane construction allow the user to replace
following worn out or damaged parts:
1. Main bolt connecting spars (item 10, Fig. 2
‒1.) with dimensions:
a) nominal
d = 22 (0,866
”) f7
b) after 1st sleeves reaming
(I)
d = 22,25 (0,876
”) f7
c) after 2nd sleeves reaming
(II)
d = 22,5 (0,886
”) f7
d) after 3rd sleeves reaming
(III)
d = 22,75 (0,896
”) f7
2. Locking pin (item 18,
Fig. 2‒1.) with dimensions:
a) nominal
d = 14 (0,551
”) f7
b) after 1st reaming
(I)
d = 14,1 (0,555
”) f7
c) after 2nd reaming
(II)
d = 14,2 (0,559
”) f7
d) after 3rd reaming
(III)
d = 14,3 (0,563
”) f7
3. Main, nose and tail undercarriage parts
4. Airbrake covers
5. Airbrake plates
6. TOST tow releases
7. Removable cockpit equipment:
a) front and rear instrument panel
b) instrument panel casing
c) front pedal, part or set
d) rear left and right foot pedal
e) Rear pedals brackets
f) assembly of rear pilot seat pan
g) front and rear pilot safety harnesses
8. Canopy:
a) perspex without frame
b) perspex with frame
9. Control surfaces:
a) rudder
b) elevator
c) ailerons
