BRISTELL S-LSA, Руководство по техническому обслуживанию и инспекции

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4. CHAPTER - WING
Document: SLSA-MIP-5-4-0-US Date of Issue: 05/2016 Revision: -
4-3
4.2.2 Wing flaps
Flaps (Fig. 4-2) are of all-metal structure consisting of the skin (1) aluminum sheet metal,
spar (2) and ribs (3) which are connected by means of riveting. Flaps are suspended on the
rear spar by means of three hinges (4). There is a control plate (5) on flap root rib where is
the flap control pin connected.
Fig. 4-2
Wing flap (left)
1 - Flap skin 2 - Flap spar
3 - Flap ribs 4 - Flap hinges
5 - Control pin
4.2.3 Ailerons
Ailerons (Fig. 4-3) are of aluminum structure consisting of the aluminum skin (1) and ribs (2)
which are connected by means of riveting. Ailerons are suspended on the rear spar by means
of piano hinges (3). Moreover the trim tab (4) is installed on the left aileron serving the lateral
balance of airplane. Control lever (5) is installed on the root aileron rib.
Fig. 4-3
Aileron (left)
1 - Aileron skin 2 - Aileron ribs
3 - Aileron piano hinge 4 - Aileron trim
tab
5 - Aileron control lever