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Agusta A109

Category & usage
Light twin-engined multi-purpose helicopter for civil, paramilitary and armed military missions. Especially used in VIP, EMS and police operations.

Versions currently in production
There are three types of turbines available with the basic versions A190C, A190K, and A190E Power:
A109C: Allison 250C20-R/I. This is the most cost-effective version with some special variants: for border and coast guard operations (e.g. the Italian Guardia di Finanza); A109MAX with bulged doors for EMS operations; A109CM military multi-purpose version
A109K: Turbomeca Arriel 1 1K1 (best performance in high-altitude operations). The A109K2 version was developed for the Swiss REGA as a rescue/EMS helicopter. Special variants for naval (A190KM), military (A109KM) and police operations.
A109E: Pratt & Whitney Canada PW206C with FADEC.
Newest version of the A109 family. Incorporates proven and advanced technologies, more space in the cabin and luggage compartment, excellent flight performance and full compatibility to all current civil aviation rules. Modern cockpit instrumentation with multi-function liquid crystal displays.

Programme aspects
In production: >600 A109s sold until today. Type certification: Single-pilot IFR; A109E also Category A.

Description

Powerplant
Two free turbines. 3 types available.

Main rotor
Left-hand rotating. A109G and A109K2 with classic articulated rotor. A109E with new, easy to maintain and lighter titanium/FRP rotor head with one elastomeric bearing for each blade. The blades are also from FRP and are identical for all versions.

Tail rotor
Two-bladed, semi-rigid with Delta-3 coupling. Pushing, lower edge in forward direction (favourable direction). Metal blades.

Fuselage
Aluminum in semi-monoque design; doors and cowling from FRP.

Cockpit/cabin
Max. eight-seated (incl. pilot). Dual controls optional; folding doors for cockpit and cabin, sliding doors for cabin optional. EMS and VIP – with a higher standard of service – cabin configuration are available apart from the standard version.

Nose wheel unit
A109C: Main wheels retractable into fuselage sides. A109E: Completely new, simple main wheel unit retractable into sponsons. This created more space in the fuselage for other purposes. Hydraulic wheel brakes and retracting mechanism. A109K2: Not retractable.

Systems and equipment
Hydromechanical flight control. Doubly redundant hydraulical, electrical, and fuel supply systems.

Optional equipment
Wide range of special equipment available.

Armament options
e.g. Saab/Emerson HeliTOW anti-tank system with up to 8 PAL of the Hughes TOW type; missile launchers; machine guns in pods.

History
First surveys starting in 1965, searching for the most promising corner in the market for a new Agusta helicopter. At least ten drafts were developed under the leadership of Dr.-Ing. Bruno Lovera and his closest assistant, the aerodynamician Paolo Bellavitat, leading eventually to the A109 project. First flight of the first prototype was on 4 August, 1971, with chief test pilot Ottorino Lancia; first flight A109E: 8 February, 1995. The A109 was the first Agusta type with high-volume production. It still enjoys great popularity, even 25 years after its first flight, especially as a fast EMS and business helicopter. Military versions are in use in 10 countries, even – little known and seldom seen – in the "cloak-and-dagger" world of the British Special Air Service (SAS).

Version   A109C A109K2 A109E
Dimensions
Overall length m 13,04 13,04 13,04
Overall height m 3,5 3,5 3,5
Fuselage length m 11,45 11,45 11,45
Main rotor diameter m 11,00 11,00 11,00
Tail rotor diameter m 2,00 2,00 2,00
Masses
Max. take-off mass kg 2720 2850 2720
Max. take-off mass with ext. load kg 2850 3000 3000
Empty mass kg 1590 1650 1555
Powerplant
Turbines   2x Allison 250 C20R 2x Turboméca Ariel 1K1 2x Pratt & Whitney PW206C
Turbine power TOP, AEO
(total)
KW 672 1100 954
Flight performance and limits
Max. limit speed km/h 311 281 311
Max. cruise speed km/h 272 265 296
Max. climb rate m/s 8,6 9,9 10,9
Max. range km 778 806 930
Max. endurance h 4,33 4,00 4,76
Hover ceiling (IGE) m 3474 5300 5578
Hover ceiling (OGE) m 2438 3900 4115
Service ceiling (approved) m 4572 4572 6096

IGE = mit Ground-Effekt   OGE = Ohne Ground-Effekt

Agusta A109E

Mit freundlicher Genehmigung von Herrn Peter Wernli
(erstmals erschienen in der Zeitschrift HELICO REVUE Ausgabe 1/97)
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