Tooling for assembly of aircraft frame type units of welded or rivet structures

Maximum dimensions of tooling - 1500х2500 mm. Tooling can be manufactured according to the drawings, templates, mat model. Design and production cycle is 4 months.

Tooling for assembly of aircraft panel type units of welded or rivet structure

Tooling of such type make it possible to arrange assembly of the unit at several working places and thus to reduce the assembly cycle. Maximum dimensions of tooling - 2500х4500х800 mm. Tooling can be manufactured according to the drawings, templates, mat model. Design and production cycle is 3-6 months.

Unit attachment benches (complexes)

The benches are designed for provision with interchangeability the aircraft units at their attachment at breakdown points. Maximum dimensions are as per overall dimensions of the item. Design and production cycle is 12-18 months.

Non-standard tooling for assembly of aircraft units of welded or rivet structure

Maximum dimensions are as per overall dimensions of the item. Design and production cycle is 12-18 months.

Master models

Master models and gauges are used to reduce time of repair and restoration of rigging for aircraft. Maximum dimensions are as per overall dimensions of the item. They can be manufactured according to the drawings, templates, mat model. Design and production cycle is 3-10 months.

Assembly tooling for manufacture of aircraft canopy

Maximum dimensions are as per overall dimensions of the item. They can be manufactured according to the drawings, templates, mat model. Design and production cycle is 3-5 months.

Non-standard tooling for assembly of structures of any complexity

Maximum dimensions are as per overall dimensions of the item. They can be manufactured according to the drawings, templates, mat model.