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Alenia Aermacchi M-311

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Via Campania, 45<br />

00187 Rome - Italy<br />

Press Office<br />

Tel. +39 06 42088985<br />

pressoffice@alenia.it<br />

A Finmeccanica Company<br />

June 2011<br />

<strong>Alenia</strong> <strong>Aermacchi</strong> M-<strong>311</strong><br />

The M-<strong>311</strong> is the new <strong>Alenia</strong> <strong>Aermacchi</strong> solution for the basic-advanced fast jet phase of the pilot training<br />

syllabus. Within the <strong>Alenia</strong> <strong>Aermacchi</strong> trainer range, the M-<strong>311</strong> provides the most cost effective overall<br />

training solution for future military pilots.<br />

The new light weight <strong>Alenia</strong> <strong>Aermacchi</strong> M-<strong>311</strong> jet trainer offers a significant reduction in acquisition and lifecycle<br />

costs, bringing them to a level similar to that of the heavy weight high power turboprops. These<br />

turboprops are in the same weight class and are equipped with similar systems, entailing similar<br />

maintenance and operating costs, but which much more limited performance and teaching effectiveness.<br />

The M-<strong>311</strong> was designed for a two-level maintenance concept: Organisation and Intermediate.<br />

Enhancement to aircraft maintainability comes from excellent accessibility to the systems and the built-in<br />

Health and Usage Monitoring System (HUMS) providing the airframe, engine and systems monitoring<br />

required easing maintenance and assessing residual airframe life. The introduction of pressure refuelling<br />

and of an On-Board Oxygen Generating System (OBOGS) brings significant reductions in manpower<br />

required for maintenance. This allows very short turn-around-time, which offers the potential to generate<br />

more sorties per day, making the aircraft even more affordable.<br />

Airframe has been designed for a fatigue life of 15,000 flight hours with fatigue spectrum allowing a<br />

significant use to perform also the more demanding basic-advanced missions. The maximum manoeuvre<br />

load factors are of +7 / -3.5 g at 3,200kg clean. The mid by-pass ratio turbofan engine (Pratt & Whitney<br />

Canada JT15D-5C) provides 1.447 kg (3,190 lb) of takeoff and maximum continuous thrust.<br />

The aircraft state of the art avionics includes a full digital glass-cockpit with three LCD MFDs 5'' x 7'' for both<br />

front and rear cockpit, HOTAS control, two mission computers for redundancy, embedded GPS/ Inertial<br />

Platform, a HUD in the front cockpit and a rear cockpit repeater. All six MFDs are identical. The new basicadvanced<br />

trainer will sport the embedded simulation introduced in the <strong>Alenia</strong> <strong>Aermacchi</strong> advanced trainers,<br />

the MB-339CD and the M-346, as well as a Stores Management System and a Digital Moving Map.<br />

Finmeccanica’s aeronautical sector is led by <strong>Alenia</strong> Aeronautica and includes the wholly owned companies <strong>Alenia</strong> <strong>Aermacchi</strong> and<br />

<strong>Alenia</strong> North America, together with its participation in jvs and consortia like ATR, SuperJet International, Eurofighter and GMAS.<br />

Finmeccanica’s aeronautical sector has a role of primary importance in the world’s civil and defence aeronautical industry, counts a<br />

total workforce of ca. 12,600 people and operates in the design, development, production and integrated support of commercial and<br />

military aircraft, trainers, unmanned aerial vehicles and aerostructures. In 2010 it reported revenues of € 2.8 billions, orders of € 2.5<br />

billions and a backlog of € 8.6 billions.


M-<strong>311</strong> TECHNICAL DATA<br />

Dimensions<br />

Span 8,47 m 27.78 ft<br />

Length 9,85 m 32.32 ft<br />

Height 3,74 m 12.27 ft<br />

Wing area 12,60 sqm 135.6 sqft<br />

Weights<br />

Takeoff (clean) 3.200 kg 7,055 lb<br />

Weapon Load, maximum 1.000 kg 2,205 lb<br />

Takeoff (maximum) 4.100 kg 9,040 lb<br />

Power Plant<br />

Pratt & Whitney Canada<br />

JT15D-5C<br />

Max Thrust, SLS (Takeoff and MCP) 1.447 kg 3,190 lb<br />

Internal fuel capacity (usable) 696 kg 1,535 lb<br />

Performance (clean, ISA)<br />

Max level speed (SL/20,000 ft)<br />

Limit speed<br />

Rate of climb (S.L.)<br />

Stall speed (landing, 20% fuel)<br />

Service ceiling<br />

Ferry range clean/2 external tanks (10% reserve)<br />

Max sustained load factor (S.L., 50% fuel)<br />

Sustained load factor, 360 kts (S.L., 50% fuel)<br />

80 / 400 KTAS<br />

430 KCAS / 0.80 Mach<br />

4,720 ft/min<br />

84 KCAS<br />

40,000 ft<br />

750 / 970 nm<br />

3.9 g<br />

2.3 g<br />

Takeoff ground run (S.L.) 470 m 1,540 ft<br />

Landing ground roll (S.L., 20% fuel) 460 m 1,510 ft<br />

Limit load factor<br />

+7 / - 3.5 g

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