D IAMOND AIRCRAFT
4 . 1
HK 3 6 TS
FLIGHT MANU
AL
Normal Procedures
Sect ion 4 provides checkl ists and ampl i fied procedures for the conduct
of normal operation . Normal procedures associated with optional
systems can be found in Section 9 .
4.2 RIGGING AND
4 . 2 . 1 General
The wings are connected to the fuselage with three bolts each . The
two main bol ts are placed in the middle of the spar tunnel . They are
acces s ible between the backrest s and can be inserted f rom the front
side . A spring loaded hook is placed over the bol t handles to'secure
the bol t s .
The A- and B -bolt s are f ixed to the fuselage at the wing root . The
A-bolt i s placed in f ront of the spar tunnel , the B-bolt l ies near
the trail ing edge . Self locking units are screwed onto the B-bol t s ,
which are accessible through handholes on the wings ' upper surface .
Locking rings are integrated in the B -bolt locking unit s which
therefore do not require any further safety device .
The horizontal stabil i zer i s attached to the vertical stabili zer by
means of three bol t s . The two bol t s in the rear are f ixed to the mount
in the vertical stabil i zer . The threaded bolt placed in f ront is
provided with a hexagonal socket . When screwed i n , i t i s automatically
secured by means of a locking ring integrated into the horizontal
stabilizer .
Revision No .
Date
Source
Doc . No .
I s sue
Page No .
3 . 0 1 . 0 6
Jan 1996
4 - 2
