Samiksha Jaiswal (Editor)

Dalby Pouchel

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Top speed
  
121 km/h

Length
  
4.39 m

Wingspan
  
6 m

Manufacturer
  
APEV

Dalby Pouchel wwwpouchelcom The website of the APEV


Similar
  
Mignet Pou du Ciel , APEV Pouchel Light , APEV Pouchel II

The Pouchel (also known as a "Ladder Flea") is a single-seat ultralight aircraft first flown in 1999, designed for amateur construction.

Contents

Dalby Pouchel wwwpouchelcom The website of the APEV

Design and development

The Pouchel I was conceived in 1997 by French engineer Daniel Dalby. The aim was to design an easy-to-build ultralight aircraft based on the formula, principles and writings of Henri Mignet. The core of the construction employed commercial aluminium ladders in the fuselage and as spars in both wings. The wings were assembled using styrofoam ribs, and were fabric-covered. It was powered by a Fuji engine, developing less than 15 hp. Controls were similar to Mignet Pou-du-Ciel designs, with a pivoting front wing and rudder, both operated by the control column via control rods and no foot pedals. After test hops and modifications, on 26 June 1999, Daniel Dalby piloted the Pouchel on its first true flight at Salon Eyguieres.

Dalby Pouchel paratrucblogfreefrpublicpouchel1jpg

In 2002, after many plans had been sold to other amateur constructors, the ladder manufacturer refused to sell its products for this purpose, due to concerns about liability and insurance. The aircraft was then redesigned to replace the ladders with rectangular-section aluminium tubes (100 x 50 mm), becoming the Pouchel II, with a Rotax 447 engine and an empty weight of about 150 kg (331 lb). Subsequently, the Pouchel II was superseded by the APEV Pouchel Light, with an empty weight of about 100 kg (220 lb). A closely related aircraft in the same family is the APEV Demoichelle. Plans and kits are distributed by the APEV (Association pour la Promotion des Echelles Volantes, or in English, Association for the Promotion of Flying Ladders).

Variants

Dalby Pouchel Dalby Pouchel Wikipedia
Bipouchel
tandem two-seater
HydroPouchel
the Pouchel seaplane, still at the prototype stage
Pouchel II
Version of the original Pouchel, but built without ladders
Pouchel Classic
with a fuselage made of wood
Pouchelec
with 12 kW electric motor, also at the prototype stage.
Pouchel Light
In 2012 the principal production version

Specifications (Pouchel Light)

Data from APEV (2011)

General characteristics

Dalby Pouchel wwwpouchelcom The website of the APEV

  • Crew: one pilot
  • Length: 14 ft 5 in (4.4 m)
  • Wingspan: 19 ft 8 in (6 m)
  • Height: 5 ft 7 in (1.7 m)
  • Wing area: 129 ft² (12 m²)
  • Empty weight: 220 lb (100 kg)
  • Max. takeoff weight: 551 lb (250 kg)
  • Powerplant: 1 × Rotax 377 or Rotax 447, 37 hp (27.6 kW)
  • Performance

  • Maximum speed: 75 mph (120 km/h)
  • Cruise speed: 56 mph (90 km/h)
  • Stall speed: 25 mph (40 km/h)
  • References

    Dalby Pouchel Wikipedia