An assembled twin-seat jet airframe for static display, supplied alongside the complete collection of separate printing parts and alternatives. The displayed edition uses 45 actual source components: the segmented fuselage and nose, both main wings, ailerons, wing tips, both horizontal tails and elevators, the complete fin and rudder, an updated three-piece canopy and the motor hatch. Components were positioned with rigid transforms; their original surface geometry was not stretched or redesigned.

DISPLAY CONFIGURATION
This is a supported airframe display with the landing gear not installed. It is not a representation of a tested flying aircraft or a complete working retract system. The illustrated finish proposes satin silver paint, a deep blue fin and nose tip, red tip accents and opaque glossy paint that simulates canopy glazing. These are proposed modelling colours, not a verified historical scheme. The wooden plinth and clear supports are illustration scenery and are not included in the aircraft geometry.

The selected wings use the supplied solid inner sections and the supplied outer sections without tanks. The alternative wings for separate flaps, tank components, landing gear, tires, wheel hubs, doors, canopy variants, mounts, fittings and other supplied parts remain in the archive. Only one coherent display configuration is assembled in the full-airframe files; the archive retains the other configurations as separate source parts.

FILES AND FORMATS
The standalone OBJ provides the complete assembled airframe without external material or texture dependencies. The ZIP adds a coloured, 45-component 3MF assembly, the full assembled STL, the OBJ, an English guide and a file inventory. Colours in the 3MF are proposed flat paint colours; the OBJ and STL are geometry formats and may appear in a neutral viewer material.

The archive also preserves all 120 distinct supplied resources: 113 STL variants, one native FFF slicer profile and six reference images. Original STL facet coordinates, stored normals and attributes are preserved in the separate source-part copies; only nonfunctional file-header text was replaced. Native profile printing values, technical identifiers and custom G-code were retained. The FFF XML was checked for preserved semantics; this does not certify compatibility with a particular printer or slicer installation. All public filenames use new opaque identifiers. The inventory explains functional roles without relying on old filenames.

SIZE AND SCALE
The assembled coordinate span is approximately 1,399.1 wide by 1,853.2 long by 560.6 high. Export files declare millimetres for interoperability and retain the native size with a common translation to place the assembly above Z=0. Original physical units and the exact ratio to a full-size aircraft have not been independently measured. No certified historical scale is claimed.

At that assumed unit convention, 50% gives a length of about 926.6 mm and 25% about 463.3 mm. These are coordinate calculations, not print recommendations. Thin aircraft walls, hinges, clearances and hardware seats do not remain suitable simply by scaling the whole model. Check them in the intended slicer before making a smaller display edition.

PRINTING AND ASSEMBLY
Print settings have not been physically tested. Use the separate source parts for printing and the assembled files for inspection and planning. Do not treat the complete airframe 3MF as a ready-to-print machine project. Review each part's orientation, wall paths, nozzle width, layer height, support access and bed contact. Preserve mating surfaces and control clearances; test representative joints and hardware seats before a long print. Inspect duplicate or degenerate facets on a working copy if your software reports them, and retain the supplied originals.

The native FFF is a reference profile, not an instruction to run its custom machine commands. Validate its printer assumptions and operating values against your own equipment. Follow your filament maker's guidance for temperatures and cooling. Assess adhesion and warping on coupons, remove support marks carefully and dry-fit before bonding. Suggested finishing steps are light surface preparation, compatible primer, thin colour coats and a protective finish after checking material compatibility. No print time, filament quantity, flight performance, load capacity or mechanical fit is guaranteed.

PROVENANCE AND LICENCE
Published by Tomás Piernas. Original design credit: Lynxman. CC0 redistribution is provided under the account holder's stated authorisation. Necessary technical identifiers remain where they affect the supplied resources. The cover uses a locally generated AI workshop background with the actual assembled model render protected from AI redrawing. The 3D design itself is not declared AI-generated.

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