Nord Noralpha

Noralpha
	Nord 1101 Noralpha, in French Air Force markings, taking off from Coventry Airport, England, in 2000
Role	Communications and liaison monoplane
Manufacturer	Nord Aviation
First flight	1944
Number built	200
Developed from	Messerschmitt Bf 108

The Nord 1100 Noralpha was a French-built and re-engined

Messerschmitt Bf 108 produced by Nord Aviation

.

Development

Construction of the

occupied France

in 1942. The company built two prototypes of the Messerschmitt Me 208 during 1943/44. One survived the liberation and was redesignated Nord 1100.

The company then produced a re-engined version of the

Turbomeca Astazou II

turboshaft engine as the S.F.E.R.M.A.-Nord 1100 Noralpha (S.F.E.R.M.A. - Société Française d'Entretien et de Réparation de Matériel Aéronautique) in 1959.

The Noralpha was a low-wing cantilever monoplane with a braced horizontal tail surface and single rudder. It had a retractable tricycle landing gear. The engine was nose-mounted and it had an enclosed cabin with side-by-side seating for two and room behind for a further two passengers.

Operational history

Toussus airfield near Paris

in June 1975

Nord built 200 production examples of the Noralpha and these served as communications aircraft with the French Air Force and French Navy. Later, many examples were civilianised. The final Air Force Noralphas were replaced in service with the Centre d'essais en vol (CEV) at

Bretigny-sur-Orge during 1974-75, whilst a few naval examples continued for a further brief period.^[1]

Variants

1100: 2x French-built Me 208 prototypes, powered by a single 180 kW (240 hp)
Argus As 10C-1
engine.
1101 Noralpha / Ramier I

Operators

France

Armée de l'Air
(ALA)
Aviation Légère de l’Armée de Terre
(ALAT)
Aéronavale

Specifications (1101 Noralpha)

Data from Illustrated Encyclopedia of Aircraft^[2]

General characteristics

Crew: one
Capacity: three passengers
Length: 8.53 m (28 ft 0 in)
Wingspan: 11.48 m (37 ft 8 in)
Height: 3.25 m (10 ft 8 in)
Wing area: 17.37 m² (187 sq ft)
Empty weight: 948 kg (2,090 lb)
Gross weight: 1,645 kg (3,627 lb)
Powerplant: 1 ×
Renault 6Q-10
inline piston engine , 174 kW (233 hp)

Performance

Maximum speed: 305 km/h (189 mph, 164 kn)
Range: 1,200 km (745 mi, 647 nmi)
Service ceiling: 5,900 m (19,355 ft)

References

Notes

^ Jackson, 1979, pp. 162-163
^ ^a ^b ^c ^d ^e Orbis 1985, p. 2616
^ ^a ^b ^c ^d Simpson 1991, p. 3087
^ ^a ^b "Contractions FAAO JO 7340.2". "Federal Aviation Authority". Retrieved 2010-01-12.
^ ^a ^b "Doc 8643 - ICAO - Aircraft Type Designators". International Civil Aviation Organization. 8 October 2009. Retrieved 2010-01-12.
^ Ricco 1998, p. unknown

Bibliography

Jackson, Paul A. (1979). French Military Aviation. Midland Counties Publications (Aerophile) Limited.
ISBN 0-904597-18-0
.

Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions.

The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985). Orbis Publishing. p. 2616.
Ricco, Philippe; Jean-Claude Soumille (1998). Les avions allemands aux couleurs françaises de 1914 à nos jours - Tome 2. Lela Presse.
Simpson, R.W. (1991). Airlife's General Aviation. England: Airlife Publishing.
ISBN 1-85310-194-X
.

[1] Jackson, 1979, pp. 162-163

[orbis-2] Orbis 1985, p. 2616

[simpson-3] Simpson 1991, p. 3087

[faa-4] "Contractions FAAO JO 7340.2". "Federal Aviation Authority". Retrieved 2010-01-12.

[icao-5] "Doc 8643 - ICAO - Aircraft Type Designators". International Civil Aviation Organization. 8 October 2009. Retrieved 2010-01-12.

[Ricco-6] Ricco 1998, p. unknown

[1]

[2]