In-line Aircraft

Combat

The Air Force ensures the surveillance and defense of the national airspace 365 days ayear, 24 hours a day, with an integrated defense system, since peacetime, with that ofother NATO countries.

AMX and AMX-T

AMX and AMX-T

Ghibli is the “nickname” attributed in the nineties to the AMX (aeronauticalnomenclature A-11B), a single-engine attack and reconnaissance aircraft, alsoavailable in the two-seat advanced trainer version (AMX-T), the result of industrialcollaboration between Italy, with Alenia holding 70.3% of the program, and Brazil,with Embraer taking care of the remaining 29.7%. The AMX-T (aircraftnomenclature TA-11B) is mainly training aircraft and OCU (Operational ConversionUnit), but also has operational capabilities similar to those of the single-seater. TheGhibli is able to carry out close support missions, tactical reconnaissance and aircooperation with surface forces (land and naval). The aircraft is equipped with an in-flight refueling system and, thanks to the avionics system supplied, is able to carryout all-weather missions. To increase the potential use of the fleet, specific trainingprograms have been developed for the AMX line to operate with the aid of nightvision goggles and an ACOL (Operational and Logistic Capabilities Update)modernization program has been completed, aimed, among other things, atequipping the Ghibli with more modern, precise and advanced ammunition.

Specifications:

Wingspan: 9,97 m – length: 13,23 m – height: 4,55 m – maximum take-off weight: 13,000 kg – propulsion system: a Rolls-Royce Avio RB.168-807 Spey turbofan of 5,000 kg/s – maximum speed: 940 km/h (0.86 mach) – tangency: 13,000 m – Range: 3,600 km (transfer) – crew: 1 pilot/1-2 pilots* – Armament: 1 cannon cal. 20 mm, up to 3,800 kg of external loads (auxiliary tanks, reconnaissance pods, AIM-9L Sidewinder air-to-air missiles, etc.). *AMX-T

TORNADO

TORNADO IDS-IT ECR

The Tornado (aeronautical nomenclature A-200A) is a two-seat combat aircraft withvariable geometry wing and all-weather capability, which the Italian Air Forceacquired in 1982. Once the risk of a global military confrontation has faded, the
Aeromobili2probability of using an aircraft such as the Tornado, whose effectiveness has beenincreased by the acquisition of cutting-edge weapon systems, essentially concernsthe so-called “crisis response operations”, that is, interventions in the most virulentphases of a military confrontation with the aim of activating the process ofprogressive stabilization and carrying out the deterrence action to guarantee thesafety of surface forces from the sky and to extinguish, in the bud, any possible”flame returns”. The role of these aircraft must therefore be framed solely with thepurpose to pursue the peaceful vocation of our country. In the standard IDS(Interdiction Strike) version, the Tornado can be used as a fighter-bomber andreconnaissance aircraft. The IT-ECR (Electronic Combat Reconnaissance – EA-200B aircraft nomenclature) variant is instead specialized in the suppression ofenemy air defenses through the use of AGM-88 HARM air-to-surface missiles.

Specifications:

Wingspan min./max: 13,91/8,60 m – length: 16,70 m – height: 5,95 m – maximum take-off weight: 28.000 kg – propulsion system: two Turbo Union RB.199 Mk.103 turbofans of 7.260 kg/s with afterburner – maximum speed at low altitude: about 1.480 km/h (1,2 mach) – Tangency: 15.000 m – Autonomy: 3.800 km (transfer) – crew: 1 pilot, 1 navigator – armament:  2 guns cal. 27 mm (1 on IT-ECR), up to 9,000 kg of external loads (auxiliary tanks, reconnaissance pod and target designation, AIM-9L Sidewinder air-to-air missiles, etc.).

EUROFIGHTER

EUROFIGHTER

The Eurofighter (aircraft nomenclature F-2000A) is a latest-generation fighter, themost advanced combat aircraft ever developed in Europe, able to offer wide-rangingoperational capabilities and unparalleled effectiveness in the Air Defense sector.The inclusion of these aircraft in the national alarm service, guaranteed by the AirForce departments for Air Defense 24 hours a day, 365 days a year, allows toprovide greater capacity to that complex device that, in a few minutes, ensures thetake-off of the fighters to intercept and identify any suspicious air trace detected byradar. It is the result of the industrial collaboration of Germany, Great Britain, Italyand Spain.

Specifications:

Wingspan: 10,95 m – length: 15,96 m- height: 5,28 m – wing area: 50 sqm – emptyweight: 10,995 kg – maximum take-off weight: 23,000 kg – propulsion system: 2Eurojet EJ200 turbofans of 60kN (13,490 lb) dry and 90kN (20,000 lb) withafterburner – maximum speed: 2 mach – operating tangency: 13,000 m – maximumrange: 3,600 km – range: over 1,350 km – crew: 1/2 pilots – armament: 1 Mausercannon cal. 27 mm, up to 6,500 kg of external loads (auxiliary tanks, radar-guidedand infrared air-to-air missiles, etc.).

F-35

F-35

The F-35 aircraft is a fifth-generation aeronautical weapon system with a spectrumof operational capabilities such as to allow the simultaneous and autonomous
Aeromobili3performance of all the missions of the aerotactic doctrine.The state of the art of technology applied to on-board sensors and the lowobservability of the aircraft (reduced ability to be detected by hostile RADARs), aredistinctive elements that allow to exponentially increase its operationaleffectiveness, ensuring not only greater levels of survival in hostile territories, butalso a high awareness and knowledge of the tactical scenario, the latter element,extremely valuable in modern crisis scenarios.The high capabilities of discovery, identification and precision of engagement, givethe aircraft a potential of absolute importance that, combined with innovativecommunication capabilities and real-time sharing of essential information (Net-Centric capability), provides the pilot with an unparalleled management of thetheater of operation, making the F-35 a valuable asset that fits perfectly into themodern operational context.For these peculiar characteristics, the F-35 aircraft has been chosen as the mostsuitable weapon system for the first operational lines of many allied nations.Italy’s participation in the Joint Strike Fighter Program began in 2002, and in 2009the Italian Parliament approved the acquisition of the aircraft and the construction ofa national assembly and final verification line. Since then, Italy’s growinginvolvement has led to the achievement of important milestones such as, forexample: the first flight of the first aircraft assembled in Italy (September 2015), thefirst Atlantic flight in the history of the F-35 (February 2016), the first Partnercountry to activate a JSF operational base outside the US borders at the 32nd Wingof Amendola (December 2016).The aircraft currently in use by the Italian Air Force is the one in variantA, Conventional Take-Off and Landing (CTOL): conventional take-off and landingversion. On January 25, 2018, version B, Short Take-Off and VerticalLanding (STOVL), was also delivered to the Ministry of Defense : short take-off andvertical landing version for use both on austere runways and on naval units such asLHA/LHD/CV (Amphibious Assault Ships and Aircraft Carrier).
 
 
 

Specifications:

Version A – Wingspan: 10,6 mt – length: 15,4 mt – height: 4,6 mt – wing area:42,7 mq – maximum speed: 1.6 mach – operating tangency: 15,240 mt – range:over 1100 km – propulsion system: 1 Pratt & Whitney F135 191kN turbofan (with
Aeromobili4afterburner) – internal fuel weight: over 8000 kg – crew: 1 pilot – armament: internalgun, GPS- and laser-guided fall armament, Radar-guided and infrared air-to-airmissiles.

Version B – Wingspan: 10,6 mt – length: 15,6 mt – height 4,6mt – wing area:42,7 mq – maximum speed: 1.6 mach – operating tangency: 15,240 mt – range:over 800 km – propulsion system: 1 Pratt & Whitney F135 187kN turbofan (withafterburner) – internal fuel: over 6000 kg – crew: 1 pilot – armament: external gun,GPS-guided and laser drop armament, Radar-guided and infrared air-to-airmissiles.

Supply and Transport

Transport has always been the “job” of the aircraft of the 46 ^ Air Brigade of Pisa and,mainly on long-haul routes, of the cargo / tanker of the 14 ° Wing of Pratica di Mare(Rome) that also meet the needs of in-flight refueling. The importance of these assets,vital for the Armed Forces, has grown exponentially with the projection “out of area” ofthe National Military Instrument. There is no place on the planet where our contingentsare located that is not periodically reached by the C-130J Hercules and the C-27JSpartan which, even in situations of threat, are able to guarantee their supply androtation. The Air Force’s transport aircraft make it possible to create and sustain overtime that network of air connections that acts as a “trait d’union” with the most important”out of area” operational theaters. In addition to its use in the field of humanitarian aidand civil protection, the Air Force is engaged in “biocontainment air transport” andmedical transport of the sick and traumatized, as well as patients in need of organtransplants. The latter is an activity that, given the “imminent danger to life” of thepeople transported, imposes a level of readiness comparable to that of Air Defense orSAR fighters, twenty-four hours a day, 365 days a year.

AIRBUS A-319CJ

AIRBUS A319CJ

Since March 2000, the 31st Wing has taken charge of the first of the three AirbusA319 twin-jet airliners, Corporate Jet (CJ) version, equipped with auxiliary tanks thatincrease its autonomy compared to the commercial version. The Airbus A319CJ(aircraft nomenclature VC-319A) is the first aircraft of the Italian Air Force certified
Aeromobili5to perform ILS (Instrument Landing System) CAT3 approaches, i.e., in the absenceof vertical and horizontal visibility it can land and stop on the runway automatically.The interior consists of four areas: a conference room, a high-comfort rest areareserved for the highest authorities on board, the passenger compartment, and thestaff rest compartment. The A319CJ has a fly by wire control system that receivesinput from two sidestick “side cloches”. The instrumentation is very modern, withtwo automatic pilots, two Flight Directors, an Autothrust for automatic poweradjustment in the various phases of flight, an electronic digital data presentationsystem and a Hud (Head-Up Display) to facilitate landings on runways without radioassistance and take-offs in low visibility conditions.

Specifications:

Wingspan: 33.91 m; length: 33,80 m; height: 11,80 m; wing area: 122.40 sqm;Weights: empty 40,160 kg, max take-off: 75,500 kg; fuel – 27,000 kg; propulsionsystem: two CFM56 turbofans of 27,000 kg/s; maximum speed: 0.82 mach (900km/h); Tangency: 10,060 m (41,000 ft); Range (with auxiliary tanks): 8500 km;Minimum crew: 2 pilots, 2 specialists, 2 flight attendants, 50 passengers the firstaircraft acquired, 36 the other two.

C-27J SPARTAN

C-27J SPARTAN

The C-27J Spartan, is the new and advanced version of the tactical transportaircraft supplied to the Italian Air Force. Derived from the G-222 and equipped withthe same engines and numerous equipment as the C-130J, the C-27J has provedto be a medium cargo particularly versatile and flexible in its use and able toeffectively carry out the various tactical transport missions also operating from semi-prepared or deteriorated runways. This aircraft guarantees the Air Force toeffectively carry out medical missions and airdrop of materials and paratroopers.Although not a specific task entrusted to the C27J, the aircraft can also carry outmaritime patrol missions. The version delivered to the Italian Air Force is among therichest and most complete, and provides an advanced data projection system,with digital map and a double Head Up Display (HUD), an in-flight refueling systemand a DASS (Defensive Aids Sub System) self-protection.

Specifications:

Wingspan: 28,70 m – length: 22,70 m – maximum take-off weight: 31,800 kg –maximum speed: 590 km/h – range: 5,950 km – crew: 2 pilots, 1 loading and launch
Aeromobili6operator – load capacity: 40 paratroopers – propulsion system: 2 Rolls Royce AE2100d2 4700 HP engines.

C-130J HERCULES II

C-130J HERCULES II

A four-purpose transport turbine, also suitable for airdrop missions of paratroopersand materials, the C-130J Hercules II has been in service since 2000 in thestandard and “stretched” version (C-130J-30). Used by the 46 ^ Air Brigade of Pisa,this aircraft is today the backbone of the transport component of the Air Force thathas grown exponentially due to the changed tasks of the Armed Forces of ourcountry that have seen in the use outside the national borders the natural projectionof their mission at the service of defense and security. The greatest dailycommitment of the C-130J Hercules is the network of air links that acts as a “traitd’union” with the most important “out of area” operational theaters, in the presenceof threat and at night, often carrying out landings and assault take-offs from semi-prepared and small runways. The availability of a carrier such as the C-130J hasalso made it possible to acquire special equipment such as the ATI (AircraftTransport Isolator) stretcher that allows the safe transport by air of biocontaminatedpatients in view of their subsequent admission to specialized hospitals.

Specifications:

Wingspan: 40,41 m – length: 29,79/34,37* m – height: 11,84/11,81* m – maximumtake-off weight: 79,380 kg – embarkable fuel: 20,819 kg – propulsion system: fourturboprops Rolls-Royce (Allison) AE2100D3 4,700 sHP – maximum speed: 645km/h – tangency: 9,315 m (at the weight of 66,680 kg) – range: 5,250 km (with18,144 kg of load) – crew: 2 pilots, 1 loading and launch operator, 92/128* soldiersor 76/112* paratroopers. *C-130J-30

FALCON 50

FALCON 50

The medical transport of the sick, traumatized or patients who need organtransplants, is a recurring use of the Falcon 50 tri-reactors (aeronauticalnomenclature VC-50A), in service at the 31st Wing of Ciampino (Rome) since 1985which, like the larger and more modern Falcon 900EX, have intercontinentalautonomy. Depending on the requirements of use, the aircraft can quickly adopt oneof the following configurations: VIP, with nine passengers, and Medical transport,with two stretchers and five passengers. In 2006, two of the four Falcon 50s of the31st wing were replaced by two ultra-modern Falcon 900 EASy, equipped with
Aeromobili7cutting-edge on-board instrumentation and greater mileage autonomy. Produced bythe French company Dassault Aviation since the mid-seventies, to meet thedemands of the US light civil and commercial transport market that required anaircraft capable of operating long-haul routes, the Falcon 50 has only recently beendiscontinued. Derived from the previous Falcon 20, the Falcon 50 retains almostentirely the construction characteristics with the integration of a third engineinstalled in the tail. It was the first aircraft built by Dassault Aviation to be equippedwith a three-engine jet propulsion.

Specifications:

Wingspan: 18,86 m – length: 18,52 m – height: 6,97 m – maximum take-off weight:17,600 kg – embarkable fuel: 6,000 kg – propulsion system: three AlliedSignalTFE731-3 turbofans of 1,680 kg/s – maximum speed: 940 km/h (Mach 0.86) –tangency: 14,800 m – range: 5,500 km – crew: 2 pilots, 1 specialist, 1 flightattendant, 9 passengers.

FALCON 900EX

FALCON 900EX

The Falcon 900EX trijet with intercontinental autonomy (VC-900 aircraft nomenclature) is one of the aircraft used by the 31st Wing of Ciampino (Rome) for state transport and medical flights. The latter is an activity that given the “imminent danger of life” of the people transported, imposes a level of readiness of twenty-four hours a day, 365 days a year. The Falcon 900EX has one of the most sophisticated on-board electronics in its class and accommodates more passengers than the Falcon 50. The 900EX can operate from small airports at high altitudes even on days with high temperatures. It is counted among the most versatile and safe aircraft thanks to its low approaching speed, lower than that of twin-engine competitors. The on-board instrumentation offers pilots the ability to easily follow the progression of the mission while the spacious cabin offers passengers high comfort during the flight. The EASy (Enhanced Avionics System) version is equipped with LCD screens that allow faster reading of flight parameters and allow data entry via a special slider. The standard interior equipment for the Air Force allows the transport of twelve passengers.

Specifications:

Wingspan: 19,33 m – length: 20,21 m – height: 7,55 m – maximum take-off weight: 21,909 kg – embarkable fuel: 11,700 kg – propulsion system: three AlliedSignal TFE731-60 turbofans from 2,760 kg/s – maximum speed: 940 km/h (Mach 0,86) – tangency: 15,500 m – range: 8,019 km – crew: 2 pilots, 1 specialist, 1 flight attendant, 12 passengers.

KC-767A

KC-767A

The KC-767A is derived from the Boeing 767-200 “Extended Range” commercialaircraft. The KC-767 Tanker/Transport guarantees a high range of flight and load,combined with the ability to refuel in flight, as a “receiver” or “tanker”. The refuelingsystems are compatible with Italian and allied aircraft; The KC-767A is also able tobe refueled to extend its range.In-flight refueling system capacity: rigid rod “boom” refueling system with flushingcapacity up to 4,091 liters per minute; central point with tube and basket withcapacity up to 2,727 liters per minute; wing tip points to tubes and baskets withcapacity up to 1,818 liters per minute; Universal receptacle with capacity to embarkup to 4,091 liters per minute.The aircraft can be set up in three different configurations (COMBI, CARGO andFULL PAX), with a payload of up to 25,000 kg:1. CARGO can embark 19 standard NATO military pallets;2. FULL PAX (passengers) can embark up to 200 passengers with their luggage;3. COMBI can carry up to 100 passengers and 10 standard NATO military pallets.

Specifications:

Length: 48,51 m – Wingspan: 47,57 m – Height: 15,85 m – Propulsion: 2 GeneralElectric (27,306 kg x2) – Maximum take-off weight: 180,000 kg – Maximum fuel onboard: 70 tons – Operating tangency: 13,000 m – Hourly autonomy: 14 hours –Range: 11,500 km – Cruising speed: Mach 0.8 (about 900 km/h).

P-180

P-180

The Piaggio P-180 (aircraft nomenclature VC-180) is an extremely versatile twin-turbine propeller aircraft used by the Italian Air Force to perform various institutionaltasks. In particular, it is used by the Multi Crew Training Center (C.A.E. CentroAddestramento EquipaggiMulticrew) for the training of Military Pilots intended forthe transport lines, by the 14th Wing for the Radio Measures activity and by the 31stWing for the needs of the Civil Protection Department. Gearedtowards the Executive market, the P-180 is extremely well designed as it offers theperformance of a turbofan aircraft of the same category but with the economy ofturboprop engines. The inspiring concept of the project is the search for maximumefficiency highlighted above all by the particular flowing lines of the fuselage and theprofile of the nose of continuous shape and with the large glass surfaces. Thepropulsion configuration with pushing propellers, guarantees the aircraft low noiselevels in the cabin. The aircraft offers the possibility to practice in the conduct ofasymmetric flight and allows you to move from a basic conduct to a fully operationaluse, through the use of multiple automated systems on board.

Specifications:

Wingspan: 14,03 m – length: 14,41 m – height: 3,97 m – maximum take-off weight:5.239 kg – propulsion system: two Pratt & Whitney of Canada PT6A-66 turbopropsfrom 850 HP – maximum speed: 732 km/h – tangency: 12.500 m – autonomy: 2.592km – crew: 2 pilots, 1 specialist, 5/8 passengers.

Training

Among the peculiar activities carried out by the Italian Air Force, particular importance iscovered by all the selection and training activities of its own personnel and of otherArmed Forces and / or Military Corps for what concerns air navigation. The FlightSchools of the Air Force depend on the Air Force Schools Command / 3 ^ Air Region ofBari.

GROB G-103

GROB G-103 TWIN ASTIR

The Grob G-103 Twin Astir II is a two-seat medium-wing trainer glider produced bythe German company Grob Aircraft and used, among other things, in the context ofthe training of the students of the Air Force Academy.

Specifications:

Wingspan: 17,5 m – Length: 8,18 m – Height: 1,3 m – Maximum take-off weight:650 kg – Crew: 1/2 pilots – Maximum speed: 135 kts.

LAK-17A

LAK-17A

High performance single-seater glider for “15/18 meters” class flying competitions,non-aerobatic, equipped with flaps and retractable landing gear.

Specifications:

Wingspan: 15/18 m – length: 6,53 m – height: 1,29 m – maximum weight: 500 kg –wing loading: 51kg/mq – maximum speed: 148 kts – load factor: +5.3/ -2.65 g –crew: 1 pilot.

MB-339A

MB-339A

It is a training and light attack aircraft supplied to the 61 ° Wing of Galatina (Lecce)with which the student pilots of the Italian Air Force carry out phase II (Primary PilotTraining), common to all military pilot students, aimed at identifying the lines onwhich they will fly: fighters, RPA remote piloting, helicopters, conventional(transport). Mainly used for training and connection, the MB.339A (in the photo theaircraft forward) can also be used for close air support missions and has proved tobe very valid for the demonstration activity of the “Frecce Tricolori” (NationalAcrobatic Team) that use the PAN (Pattuglia Acrobatica Nazionale, NationalAcrobatic Team) variant, equipped with a smoke system. To extend its operationallife, the MB.339A/PAN fleet has been subjected over the years to a MLU (Mid-LifeUpdate) program, mainly concerning radio and navigation equipment with theinstallation of “GPS”. Successor of the MB.326, it retains the Viper turbojet, but ischaracterized by the raised rear seat that is essential to provide the instructor withgood forward visibility especially during armed exercises. The 339 in service on theGalatina base, in the different versions, have accumulated about 330,000 flighthours, testifying to the high levels of performance of the aircraft.

Specifications:

Wingspan: 10,85 m – length: 10,97 m – height: 3,99 m – maximum take-off weight:5,895 kg – propulsion system: a Rolls-Royce Viper Mk.632 turbojet of 1,814 kg/s –maximum speed: 940 km/h (0.86 mach) – tangency: 13,000 m – range: 3,600 km(transfer) – crew: 1/2 pilots – armament: up to 2,040 kg of external loads (pod formachine guns or 30 mm cannon, auxiliary tanks, etc.).

MB-339CDII

MB-339CDII

The MB.339CD (Fully Digital) is an updated and improved version of the “three-three-nine” in avionics. The main innovation on this aircraft is represented by theadvanced instrumentation it has: the classic round dial instruments have beenreplaced by 3 color screens (Multifunction Display) and the Head Up Display typehead-up viewer in both cockpits. This characteristic represents an almost exclusivepeculiarity in the training sector. The aircraft is used by the 61st Wing for Phase III”Fighter Track” and “Remotely Piloted Aircraft”, aimed exclusively at student pilotsselected for the “Fighter” and “remotely piloted” lines. Phase III ends with theachievement of the Military Pilot License (turreted eagle). The MB.339CD can alsobe used for Air Defense tasks. Today, in fact, any form of flight can become apotential danger to the safety of citizens and the inviolability of our skies. Hence thenew operational tasks assigned to the MB.339CD that are particularly effective forcountering low-speed, low-altitude air threats such as those that could be used in apossible terrorist attack.

Specifications:

Wingspan: 11,22 m – length: 11,24 m – height: 3,99 m – maximum take-off weight:6,350 kg – propulsion system: a Rolls-Royce Viper Mk.632 turbojet of 1,814 kg/s –maximum speed: 0.77 mach (at 9,150 m) – tangency: 13,000 m – range: 2,037 km(with 2 underwing tanks) – crew: 1/2 pilots – armament: up to 2,040 kg of externalloads (pod for machine guns or 30 mm cannon, auxiliary tanks, AIM-9L Sidewinderinfrared-guided air-to-air missiles, etc.).

NIMBUS-4DM

NIMBUS-4DM

High performance two-seater glider for “free” class flying competitions, non-aerobatic, equipped with flaps, retractable landing gear and able to take offautonomously thanks to a 63HP engine.

Specifications:

Wingspan: 26,5 m – length: 8,62 m – height: 1 m – maximum weight: 820 kg – wingloading: 37,5kg/sqm – maximum speed: 285 km/h – load factor: +5, -2.65 g – crew:1/2 pilots.

S-208M

S-208M

In the mid-60s SIAI-Marchetti, developed from its four-seater light aircraft S.205, afive-seater aircraft, substantially similar but with a higher power engine. Theprototype of this new aircraft, designated S.208, flew for the first time on May 22,1967. Monoplane, single-engine low-wing all-metal construction was mass-produced from the spring of 1968 and in the first five years about eighty were built,of which more than half were destined for the Air Force in the S.208M version (U-208A aeronautical nomenclature) which used it for liaison and training. Other tasksassigned at the civil level to this light aircraft were, marginally, the medical one, thecargo transport and finally the agricultural one in the S.208AG version. The versionintended for the Armed Forces, differed from the civilian version for the modified on-board instrumentation, two doors for the pilot’s seat, the possibility of mounting thehook for towing gliders and the lack of tanks at the wing tips. It is currently used bythe liaison squadrons and by the 60 ° wing for towing gliders.

Specifications:

Wingspan: 10,86 m – length: 8,10 m – height: 2,89 m – maximum take-off weight:1,500 kg – propulsion system: an Avco Lycoming 0-540-E4A5 piston engine with260 HP – maximum speed: 285 km/h – tangency: 5,400 m – range: 1,200 km –crew: 1/2 pilots.

SF-260EA

SF-260EA

As soon as they enter the Academy, the student pilots are sent to the 70th Wing ofLatina to obtain the pilot and airplane navigator license on the SF.260 single-enginepropeller aircraft. The original SF.260AM version, in service since 1976, wasreplaced after 235,500 flight hours flown, by the more modern SF.260EA (aircraftnomenclature T-260B), wanted and requested by the Armed Forces and of whichthe Air Force has acquired a total of 30 specimens. Among the main novelties thecomplete equipment for instrument flight and a much more spacious and air-conditioned cockpit. The SF.260EA aircraft is an elegant low-wing monoplane oflight alloy construction with retractable landing gear and differs from the SIAISF.260AM mainly for the electric trim, the digital instrumentation, the updated
Aeromobili12avionics for the achievement of IFR certifications, improved roominess. On-boardradio communication systems include two VHF/AM and UHF/AM transceivers aswell as an intercom system. The instruments and control panels are equipped withintegrated lights that allow them to be easier to read. Easy access to the batterycompartment through a panel on the side of the fuselage and many other smallfeatures ensure easier maintenance.

Specifications:

Wingspan: 8,35 m – length: 7,10 m – height: 2,68 m – maximum take-off weight:1,250 kg – propulsion system: an Avco Lycoming 0-540-E4A5 piston engine with260 HP – maximum speed: 236 kts – tangency: 4,267 m – range: 1,440 km – crew:1/2 pilots.

T-346A

T-346A

The T-346A twin-jet is the most advanced pre-operational trainer in the world today.With completely digital flight controls and avionics, “care free” maneuverability athigh angles of attack, the 346 is responsible for training pilots for 4 ^ and 5 ^generation aircraft. It also allows considerable savings because it can carry out alarge part of the training program previously carried out on more demandingmachines.Supplied to the 61st Wing of Galatina, it is used for phase IV of training (Lead In toFighter Training – LIFT), preparatory to subsequent use on Fighters aircraft.The 346 is not only an aircraft, but also a complex integrated system that includes,in addition to the aircraft itself, a ground segment consisting of various simulationsystems.The LVC (Live, Virtual and Constructive) philosophy is the flagship of the system. The latter allows pilots to operate simultaneously, and in a combined way, in realflight (live) and on the various types of simulators (Virtual), interfacing with any typeof threat force generated by the computer (Constructive).
 
 
 

Specifications:

Aircraft length: 11.49 m – aircraft height: 4.76 m – wingspan: 9.72 m – wing area:23.52 m2 – take-off weight: 6.700 kg – maximum take-off weight (armed): 9.500 kg– maximum speed: 590 ktas – maximum level speed: 590 kts at 1.524 m (5.000 ft) –limiting speed: 572 kts (Mach 1.2).

 

Helicopters

The helicopter component of the Italian Air Force is called upon to carry out a widerange of operations. It has the task of effectively ensuring the air search and rescueservice, both for the institutional tasks of possible recovery of crews and militarypersonnel in difficulty and for the activities of competition to the community in case ofemergency medical flights, natural disasters and major national events. It also providesair support to Special Operations and carries out training activities.

HH-212

HH-212

The HH.212 allow the Air Force to ensure search and rescue service on the entirepeninsula and territorial waters. Thanks to their usability during day, night and incritical weather conditions, with the use of NVG (Night Vision Goggles), the HH.212and their crews represent a staple in the most complex and difficult to managemissions. Also, the HH.212 of the 21st “Tiger” Group of the 9 ° Wing of Grazzanise,in the ICO configuration (Implementation Operational Capacity) equipped withpassive crew protection, defensive armament and infrared-guided anti-missilecountermeasures, have been redeployed in the operational theater in support of theISAF contingent in Afghanistan. The HH.212 units of the 15° Wing have alsodeveloped a Combat SAR capability.

Specifications:

Rotor diameter: 14,60 m – length: 17,40 m (with rotor in motion) – height: 4,40 m –maximum take-off weight: 5.080 kg – propulsion system: a Twin Pac complex withtwo Pratt & Whitney PT6T-3D turbines of 1.193 HP – maximum speed: 240 km/h –tangency: 5.180 m – autonomy: 750 km – crew: 2 pilots, 1 multipurpose specialist, 1aerorescuer – armament (AB.212ICO): 2 tiltable machine guns cal. 7.62 mm.

HH-101A

HH-101A

The HH-101A, indicated by the name “Caesar” in the version of the Italian AirForce, is a latest-generation aircraft, capable of operating day and night in anyweather condition and performs multiple roles including Air Support for SpecialOperations, Slow Mover Interceptor as well as Personnel Recovery , i.e. therecovery of people, civilians and soldiers, in difficult situations in crisis areas. These
Aeromobili14capabilities allow the 9° Wing to meet the high standards required by theinternational organizations of which Italy is a part. The HH-101A has a highsurvivability in hostile areas thanks to an advanced integrated self-protectionsystem. It is equipped with an “emergency float” system that allows to increase thechances of survival of the crew in case of forced landing or immediate landing. Ithas a particularly wide range of action, given the ability to refuel in flight and is alsocharacterized by the high degree of maneuverability that allows it to support thetypical tactical flight at very low altitude. The aircraft also has high-tech equipment,especially in favor of human-machine interaction and communications (thanks to thepresence of tactical datalinks).

Specifications:

Length: 22,81 m.; height: 6,65 m.; main rotor diameter: 18,59 m.; propulsion: 3 GECT7-8E (2500 SHPx3); maximum take-off weight: 15.6T; Cruising speed: 150kts(guaranteed in operational configuration); Practical Tangency: 15000ft; range:>250NM (without air to air refueling); Autonomy: 5 hours (without air to airrefueling); armament: 3 machine guns M134D 7,62).

HH-139

HH-139

The AW-139, which in the Italian Air Force version is called HH, Hospital Helicopter,is a mid-range twin-turbine. The HH-139A is a solution identified on the market tocontinue to effectively ensure the air search and rescue service, both for theinstitutional tasks of possible recovery of crews and military personnel in difficulty,and for the activities of competition to the community in case of emergency medicalflights, natural disasters, and major national events. Being a helicopter alreadytested and in service with other national civil and military realities (Financial Police,Coast Guard, various local authorities), the HH-139A allows to achieve significantsynergies – training, logistical and above all operational – in the inter-force andinter-agency field in the delicate and complex sector of air rescue, fundamental tointervene successfully when required, often in prohibitive conditions, at night, withbad weather, in particularly inaccessible and isolated areas. The HH-139A is able tooperate both day and night thanks to the use of Night Vision Goggles (NVG), inparticularly demanding areas, even from unprepared surfaces, in dustyenvironments, snowy areas or in the marine environment. The helicopter is aparticularly versatile machine: in maximum 30 minutes it is possible to change theinternal configuration, passing from that for air rescue (primary SAR version: 5 passengers + 1 stretcher) to that of air rescue and emergency medical (MEDEVACversion: from 2 to 4 stretchers) or passenger transport (UTILITY version: up to 14passengers).The HH-139B version, on the other hand, has some technical features that allow toimprove the operational capacity and therefore to increase the flexibility of use torespond to emergencies and safety needs. In particular, it has been equipped with adouble winch that increases the reliability of the system and safety during recoveryoperations and a “mission console” that allows better management of the on-boardequipment for the purpose of searching for any missing persons. In addition, themaximum take-off weight has been increased, from 6800kg to 7000kg, which allowsa greater load capacity and finally the avionics and on-board sensors have beenupdated with the latest generation systems (such as the AIS – AutomaticIdentification System – which allows better interaction with naval vessels and theOPLS – Obstacle Proximity LIDAR System – which favors identification andseparation with orographic obstacles.

Specifications:

Rotor diameter: 13,8 m – length: 16,66 m – maximum width (horizontal shelf): 4,22m – maximum take-off weight: 6,800 kg (7,000 version B) – propulsion system: twoPratt & Whitney PT6C-67C Turboshafts turbines with FADEC – maximum speed:306 km/h.

TH-500B

TH-500B

The 72 ° Wing of Frosinone, dependent on the Air Force Schools Command /3rd Air Region of Bari, is the only rotary-wing school in Italy dedicated to the trainingof helicopter pilots of the Air Force, of the other Armed Forces and of the ArmedCorps of the State, as well as of foreign visitors. For this educational activity, theTH-500B helicopter is used, a light, five-blade, single-turbine training and liaisonhelicopter, characterized by high flexibility of use and versatility that the 72 ° Winghas been using since 1990. The aircraft was chosen by the Italian Air Force in theconfiguration that allows the most complete training capacity. In addition to trainingtasks, it can perform concurrence missions in SAR operations, transport ofpersonnel, goods or wounded, rescue operations, defense of military bases andinstallations, shooting training, reconnaissance, observation and liaison. It has theability to operate on bodies of water with the adoption of fixed floats and on snowysurfaces with the appropriate snow skates.

Specifications:

Rotor diameter: 8,04 m – length: 9,39 – height: 2,83 m – maximum take-off weight:1.361 kg – propulsion system: an Allison 250C-20B turbine of 420 sHP “limited” to375 sHP- maximum speed: 278 km/h – tangency: 5.280 m – autonomy: 442 km –crew: 1/2 pilots.

Reconnaissance and Surveillance

The military response to the transversality and unpredictability of future threats, theterrorist one in the first place, but also the use of weapons of mass destruction andregional instability, passes through adequate cognitive and information skills. More thanin any other sector, these resources suffer from the extraordinary opportunities offeredby modern technologies. The reconnaissance and surveillance capabilities allow toprovide “real time” support to the air and surface forces, and to contribute in “near realtime” to the creation of an overall intelligence framework.

PREDATOR B

MQ-9A PREDATOR B

The MQ-9A “Predator B” aircraft, built by General Atomics, is a Remotely PilotedAircraft (RPA) used by the Italian Air Force to carry out reconnaissance,surveillance and target acquisition missions. The aircraft, with a wingspan of over20 meters, a speed of over 400 km / h and a flight capacity at medium and highaltitude, guarantees a great flight autonomy, allowing to obtain high performanceboth in the conduct of ISTAR missions (Intelligence, Surveillance, Target Acquisitionand Reconnaissance) and both, in the maritime and terrestrial fields, as part ofPatrol, Search and Rescue operations. The Air Force Predator Bs are able toperform a wide range of tasks demonstrating high flexibility, versatility andeffectiveness. For example, it is possible to detect the presence of threats such asimprovised explosive devices that represent the most insidious and widespreaddanger in today’s theaters of operations. Missions may also be carried out in hostileoperational environments, in the presence of nuclear, biological, chemical orradiological contamination, or acquire data and information relating to small andlarge targets in areas potentially subject to operations. In addition, the Predator Baircraft allow to contribute in a unique way to the creation and maintenance of theso-called “Situational Awareness”, i.e. to the control of the evolution of the situation by the authorities responsible for the command of the activities. The characteristicsof autonomy, speed, persistence and range, combined with low operating costs,make the System one of the best tools for border control, environmental monitoring,police support and intervention in the event of natural disasters. The WeaponSystem consists of at least three elements:1. the aircraft, equipped with a high-performance “Turboprop” engine;2. the Ground Control Station (G.C.S.), a ground control station that thanks to asatellite link can control the aircraft during operations even hundreds ofkilometers away;3. the Exploitation Data Station (E.D.S.), where the images received from theaircraft are analyzed in real time and, through a telecommunications node,transmitted to operational users.The control station is a real cockpit placed on the ground, connected by antennasand receivers able to communicate with the aircraft also via satellite. The electro-optical, infrared and radar sensors placed under the fuselage, allow uniqueobservation and detection capabilities, able to operate even at night; The syntheticaperture radar sensor, in particular, allows, in all weather conditions, the ability toobtain high-definition images. The videos and images acquired thanks to thePredator B System are immediately analyzed within the E.D.S. by the “Intelligence”staff who has passed a long training course to become an “Image Data Analyst”and who now has the task of providing timely information and documents to theCommanders and the Operational Units. The cameras placed on the nose of theairplane represent, instead, “the eyes” of the pilot, and are the precious tools usedduring take-off and landing.

Specifications:

Wingspan: 20,1 m – length: 10,8 m – height: 3,8 m – maximum speed: 445 Km/h –propulsion system: Turbo Prop 900 HP.

P72-A

P72-A

The P-72A is a multirole aircraft able to perform, thanks to a very advanced suite ofsensors, different types of missions. The main features are versatility, speed ofintervention, the possibility of redeployment, the ability to share acquired data in realtime and reliability, which make it a cutting-edge weapon system able to effectivelycarry out all assigned missions. It is able to operate effectively on the sea at low and medium altitude, even near the coast, at various latitudes, with considerablydifferent climatic factors, regardless of light conditions (H24) and in marginalweather conditions in the performance of capacitive functions of maritime andelectronic surveillance, of collaboration with other State institutions and in searchand rescue for the protection of human life.The crew is made up of pilot officers and non-commissioned officers who belong tothe Air Force and the Navy. This is a typical feature of the 41st Wing that maintains,therefore, a typically inter-force look through a combination of two perfectlyintegrated components (Airforce and Navy), which in the 45-year history of theAtlantic aircraft has given excellent results.The aircraft is able to carry out research, acquisition of information (objectives,geographical situation, meteorological situation, position of contacts) both throughdirect observation, and through electronic systems for the discovery, localization,recognition, classification, tracking and identification of surface contacts. Thesefunctions are managed by the ATOS system that integrates the various on-boardsensors, managed by 4 multifunctional consoles, through:an electronically scanned radar, for the localization and tracing of surface andaircraft contacts, even small ones;an electro-optical turret, with all-weather detection and contact tracingcapabilities;capabilities of identification and analysis in real time, on board the aircraft, ofthe electromagnetic emissions present in the area of operations;ability to transmit information in real time by means of a satellite communicationsystem;high communication and data transmission capacity also through its ownintegrated systems.The aircraft is also equipped with a self-protection suite with the possibility of useeven in hostile territory. The structure provides, in addition to the flying personnel,the use of highly specialized figures able to manage both the mission system andthe suite of sensors related to self-defense and the release of SAR search andrescue devices.The P-72A aircraft arrived in Sigonella on November 25, 2016.

Specifications:

Wingspan: 27,05 m – length: 27,16 m – height: 7,65 m – maximum take-off weight:23,000 kg – maximum speed: 480 km/h – range: 3,240 km at 15,000 feet (10hhours at 5,000 feet).

G550 CAEW

GULFSTREAM G550 CAEW

The CAEW (Conformal Airborne Early Warning) aircraft is a multi-sensor systemwith air surveillance, command, control and communications functions, instrumentalto air supremacy and support to ground forces. It is based on the commercialplatform Gulfstream G550, subsequently modified in part by the manufacturer itself(Type A modification), and in part by the company Elta Systems Ltd in Ashdod,Israel, with the preparation and assembly of mission systems (Type B modification).The result is a platform with aerodynamic performance substantially comparable tothe civil carrier (hence the definition of “conformal”), with a drag index (aerodynamicdrag index) very low despite structural changes. The ability to stay on the objectiveis a function of the mission parameters, with maximum dimensions of use andtransfer speed absolutely significant. The latest generation avionics suiteHoneywell Primus Epic Avionics, integrated with the information of the AEWsystem, allows the flight crew (2 pilots) a high SA (Situational Awareness) in realtime, 360 ° and long distance. The mission system consists of:a phased array radar;a 360º Identification Friend or Foe (IFF) system;a modern and state-of-the-art electronic support system;an advanced communications system.The information obtained from the individual sensors is analyzed and “merged”automatically, allowing a rapid and accurate acquisition and identification of targets,target acquisition and target information – at the center of the actual EarlyWarning function – with the added advantage of greater radar coverage thanks tothe airborne sensor. The RASP (Recognized Air Surface Picture) obtained by thesystem and validated by the mission operators, is displayed through the 6 on-boardstations and can be disseminated safely and promptly to the ground commandcenters thanks to a powerful datalink system.

The mission system also has the ability to conduct Maritime Patrol and BattlefieldManagement missions, thanks to the compatibility with the Rover systems of thepersonnel employed on land or on the surface of the sea (through the transmissionof video images useful for the interpretation of the environment in which it isoperating).The AEW-BM&C (Airborne Early Warning, Battlefield Management &Communication) capability provided by the CAEW aircraft is an indispensable toolto ensure an adequate extension of the Homeland Defence/Security surveillancecapability, including the management of the unconventional threat represented bythe so-called “RENEGADE” and safeguard the full capacity to support theatermilitary operations.

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