Nicollier Menestrel

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Menestrel
Nicollier HN-700 Menestrel.jpg
Nicollier HN-700 Menestrel at St. Cyr Aerodrome
Role Homebuilt aircraft
National origin France
DesignerHenri Nicollier
First flight25 November 1962
Number builtMore than 95

The Nicollier Menestrel family of French homebuilt low-wing single-engine light aircraft includes both single- and two-seat variants and a wide choice of engines. First flown in 1962, nearly 100 have been built and others remain under construction.

Contents

Design and development

The Menestrel (en: Minstral), a single-engine low-wing cantilever monoplane, was designed for homebuilders. Three variants have appeared over the course of about 27 years: the original single seat HN 433 Menestrel flew in 1962, the more powerful HN 434 Super Menestrel in 1985 and the larger two-seat HN 700/1 Menestrel II in 1989. [1]

All Menestrel variants are wooden framed and fabric covered. The wing is built around a single spar and has constant chord to mid span, with semi-elliptical outer panels. There are no flaps fitted on the single seat variants, though they are an option on the Menestrel II. [2] The fin and rudder are curved, the rudder having a horn balance. The tailplane is mounted on the top of the fuselage. [3]

The fuselage is structurally of simple square section, with a curved decking aft of the cockpit. The latter was originally open but the prototype later flew with a smooth plexiglass canopy that merged into the decking. [3] The Menestrel II has side by side seating. Most Menestrels have a tailskid or, later, tailwheel undercarriage [2] with cantilever main legs bearing Vespa scooter wheels. Many Menestrels have faired legs and spatted wheels. At least one Menestrel II, with the type number HN 701TM, [4] uses a tricycle undercarriage. [1]

Menestrels have been powered by a variety of engines, mostly variants of the Volkswagen flat-4 engine. Early versions of these were entirely air-cooled, but more recently the cylinder heads have been water-cooled. Some early Menestrels with air-cooled engines have exposed cylinder heads for cooling but more have semi-cylindrical, bulged fairings to enclose them. The water-cooled engines used in the Menestrel II have cowlings which enclose the whole engine without additional fairings, with an air intake behind the propeller. The first HN 433 Menestrel had a 22 kW (30 hp) 1.3 L engine; later HN 433s have had engines in the 22-37 kW (30-50 hp) power range. [2] [3] Super Menestrels have used 1.6 L engines, producing powers of 26-49 kW (35-65 hp). The HN 700 Menestrel II uses one of two Limbach engines of 2.0 L or 2.4 L capacity. [1]

Operational history

British registered two-seat HN700 Menestrel II Nicollier HN700 Menestrel G-CCCJ Sywell 4.9.10R edited-2.jpg
British registered two-seat HN700 Menestrel II

The first prototype HN 433 flew on 25 November 1962 and Menestrel aircraft have continued to be home built from plans since then. 4 more HD 433s have appeared on the French register. [5] The more powerful HN 434 proved more popular, with 23 on the French register [5] and 1 on the Finnish. [6]

The two-seat HN 700 has been the most successful of the three variants in numerical terms. 56 have been registered in France [5] and at least one in Spain. [7] In the UK 8 examples have had Permits to Fly. [8] Others remain under construction. The only HN 701 to appear on the French register, F-PLMT, has a tricycle undercarriage. [9]

A Centre d'essais en vol evaluation of the HN 434 declared it to be the best handling sportplane in Europe. [10]

Variants

HN 433 Menestrel
Single seat. Volkswagen engines, particularly Rectimo-VWs, in the range 22-37 kW (30-50 hp) range. Span 7.00 m (23 ft 0 in).
HN 434 Super Menestrel
Single seat with enlarged cockpit and increased tankage. Powered, typically, by a Volkswagen 1.6 L in the 26-49 kW (35-65 hp) range. [11] [10]
HN 435RL Ménestrel
One-off HN434 modified by builder Roland Lamglais [4]
HN 700 Menestrel II
Side-by-side configuration two-seat version with span increased to 7.80 m (25 ft 7 in). Powered by a 60 kW (80 hp) Limbach L2000 (2.0 L) flat four engine with water-cooled piston heads. [11] [10]
HN 701 Menestrel II
As HD 700 but with 65 kW (87 hp) Limbach 2400 (2.4 L) flat four engine with water-cooled piston heads.

Specifications (Menestrel II)

Data from Jane's All the World's Aircraft 1992-93 [2]

General characteristics

Performance

References

  1. 1 2 3 Simpson, Rod (2001). Airlife's World Aircraft. Shrewsbury: Airlife Publishing Ltd. p. 397. ISBN   1-84037-115-3.
  2. 1 2 3 4 Lambert, Mark (1992). Jane's All the World's Aircraft 1992-93. Coulsden, Surrey: Jane's Information Group Ltd. p. 480. ISBN   0-7106-0987-6.
  3. 1 2 3 Taylor, John W R (1966). Jane's All the World's Aircraft 1966-67. London: Sampson Low, Marston & Co. Ltd. p. 48.
  4. 1 2 Chillon, Jacques. Fox Pappa - Registre des avions Français amateur (2009 ed.). Brive: Ver Luisant. p. 217. ISBN   978-2-35551-066-3.
  5. 1 2 3 "French civil aircraft registrations". Archived from the original on 5 December 2010. Retrieved 22 September 2010.
  6. "Finnish civil aircraft registrations" . Retrieved 22 September 2010.
  7. "EC-ZHN image" . Retrieved 22 September 2010.
  8. "Current Menestrel II registrations on UK list" . Retrieved 22 September 2010.
  9. "F-PMLT image" . Retrieved 22 September 2010.
  10. 1 2 3 Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, page 100. Flying Pages Europe SARL, 2015. ISSN   1368-485X
  11. 1 2 Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, page 94-95. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X