APEV Scoutchel
| Scoutchel | |
|---|---|
| Role | Amateur-built aircraft |
| National origin | France |
| Manufacturer | APEV |
| Designer | Daniel Dalby |
| Status | In production (2012) |
| Unit cost |
€5000 (Kit, 2011) |
| Developed from | APEV Demoichelle |
The APEV Scoutchel (English: Scout ladder) is a French amateur-built aircraft, designed by Daniel Dalby and produced by APEV of Peynier. The aircraft is supplied as plans or as a kit for amateur construction.[1][2]
Design and development
The Scoutchel is derived from the earlier APEV Demoichelle, itself an updated version of the pre-First World War Santos-Dumont Demoiselle.[1]
The Scoutchel features a strut-braced high-wing, a single-seat open cockpit without a cockpit fairing, fixed tricycle landing gear and a single engine mounted above the cockpit on the keel tube, in tractor configuration.[1][2]
The aircraft is made from bolted-together aluminum tubing. The wings are the same as those used on the Pouchel Light and are built around a single aluminium spar, with ribs made from extruded polystyrene with plywood bracing, all bonded to fibreglass leading and trailing edges, covered in Dacron sailcloth. The 8.30 m (27.2 ft) span wing employs a NACA 23112 airfoil and has an area of 9.96 m2 (107.2 sq ft), with an aspect ratio of 8:1. A unique roll control system is used as the aircraft has no ailerons. Instead the wings are pivoted to +4° and -2° to produce and control roll. The wings can be folded for ground transportation or storage.[1][2]
Recommended engines are the 35 hp (26 kW) Rotax 377 or the 40 hp (30 kW) Rotax 447 two-stroke powerplants, although it can also fit electric motors as well.[1][2]
The manufacturer estimates building times at 150 hours from the kit and 300 hours from plans.[2]
Specifications (Scoutchel)
Data from Bayerl[1]
General characteristics
- Crew: one
- Length: 5.2 m (17 ft 1 in)
- Wingspan: 8.30 m (27 ft 3 in)
- Height: 2.6 m (8 ft 6 in)
- Wing area: 9.96 m2 (107.2 sq ft)
- Aspect ratio: 8:1
- Airfoil: NACA 23112
- Empty weight: 130 kg (287 lb)
- Gross weight: 250 kg (551 lb)
- Powerplant: 1 × Rotax 912ULS four cylinder, liquid and air-cooled, four stroke aircraft engine, 75 kW (101 hp)
Performance
- Cruising speed: 100 km/h (62 mph; 54 kn)
- Stall speed: 40 km/h (25 mph; 22 kn)
- Never exceed speed: 120 km/h (75 mph; 65 kn)
- g limits: +4/-2
- Wing loading: 25.1 kg/m2 (5.1 lb/sq ft)
References
External links
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Wikimedia Commons has media related to APEV aircraft. |