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The DR-107 is a monoplane that features a cantilever low-wing, a single-seat enclosed cockpit under a bubble canopy, fixed conventional landing gear with wheel pants and a single engine in tractor configuration. [1] The aircraft is predominantly made from wood, with some steel parts and doped aircraft fabric.
Kits are delivered in six increments, including the frame and skids, engine, transmission, main rotor subassembly, tail rotor subassembly, controls and linkages, cockpit exterior/interior, and fuel and electrical subsystems. Assembly instructions are provided in the form of video clips on video CDs or DVDs, blueprints, and checklists.
The "Project Falcon Hear" program involved the optimizing of air-ground communications on the AS-211 by upgrading and installing the AN/ARC-34 UHF radios from the F-5A/B. [9] These aircraft were fitted with a belly-mounted gun pod, which was designed, developed and manufactured by Philippine company Aerotech Industries Philippines, Inc. (AIPI).
The original aircraft was designated the DR.100 and features a cantilever low-wing, a three-seat enclosed cockpit, fixed, tailwheel conventional landing gear with a single engine in tractor configuration. [2] [3] This was developed ultimately to the DR1050M1 Sicile Record with swept fin and many other refinements such as wheel pants and ...
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Solid-state cockpit voice/data recorder See flight recorder: SSCVR Solid-state cockpit voice recorder See flight recorder: SSFDR Solid-state flight data recorder See flight recorder: SSR Secondary surveillance radar: STAR standard terminal arrival route: STARS Standard Terminal Automation Replacement System: STC supplemental type certificate: STCA
JS-3 Rapture. Type certification of the JS-MD 3 was achieved with EASA on 18 July 2019. [5]The JS3 is equipped with Tost nose and centre of gravity release hooks, retractable main undercarriage leg with elastomeric shock absorbers, and a fixed pneumatic 180 mm (7.09 in) tail wheel with an aluminium hub.
The cockpit is exposed with a plexiglass or Lexan windshield. The controls are conventional 3-axis. [citation needed] When built as a Part 103 ultralight, the aircraft is intended to be powered by a 26 hp (19 kW) Rotax 277, 35 hp (26 kW) Rotax 377, or similar engine.