The Toucan is Aero Adventure’s two seat Ultralight trainer. With tandem seating for two, the Toucan is a legal Ultralight trainer that is also a simple light two place aircraft. The Toucan kit starts at $15,995 (2009).
Aero Adventure Toucan Engine: Rotax 582, 65 hp Cruise: 62 mph Range: 170 sm Stall: 28 mph ROC: 800 fpm Take-off dist: 150 ft Landing dist: 150 ft Fuel cap: 10 USG Weight empty: 460 lb Gross: 1050 lb Length: 22.6 ft Wing span: 29.8 ft Wing area: 158 sq.ft Cockpit width: 30 in Seats: 2 tandem Landing gear: tail wheel
The G700 is an Americanised version of Aero designer Tomasz Antoniewski’s certified AT-3. To qualify the all-metal Gobosh G700S as an LSA, the wingspan was increased and among other things for the US market, the addition of winglets. Even the least expensive model, the Sport Edition, includes the standard six instruments, Garmin GPS and transponder, wheelpants and leather seats. They all feature dual controls and mechanically operated split flaps.
The former Gobosh G700 lives on as the Aero AT-4, distributed by Aero AT USA of New Hampshire, in 2012. The AT-4 is made in Poland by Aero Ltd., the all-metal LSA derives from the AT-3, which was certified at a higher gross weight. AT-4 base price 2012: $105,550.
Aero AT-4
Gobosh G700S Engine: Rotax 912S, 100 hp TBO: 1500 hr Prop: Elprop 3 blade composite Cabin width: 41 in Fuel cap: 18.5 USG Full fuel payload: 390 lb LSA MTOW: 1320 lb Empty wt: 820 lb Useful load, std: 500 lb Max cruise speed: 116 kt Vso: 39 kt Best rate of climb, SL: 850 fpm Takeoff ground roll: 380 ft Landing ground roll: 686 ft Base price 2009: US$106,950 to $123,900
Aero developed the Czech P.220 low wing kit aircraft into the AT-3, first flying in January 1998. The G700 is an Americanised version of Aero designer Tomasz Antoniewski’s certified AT-3.
Italian aerospace company Leonardo’s military trainer aircraft, the M-345 was intended for the international market as both a trainer and an operational aircraft, and is designed for low price, and also low maintenance and operational costs. This is due in part to the airplane’s advanced avionics that includes the Health and Usage Monitoring System (HUMS), which monitors the state of the aircraft and reduces the need of general overhauls.
The M-345 also has an avionics suite that the company says is up to combat jet standards and includes Hands On Throttle And Stick (HOTAS) controls, Head up Display (HUD), and real-time Multi-Function Displays (MFD). The aircraft has pressure refuelling systems and an On-Board Oxygen Generation System (OBOGS) for greater efficiency and less need for ground crews.
On 29 December 2016, the prototype M-345HET (High Efficiency Trainer) tandem-seat basic jet trainer took to the skies over the Venegono Superiore airfield in Varese, Italy, under the command of test pilots Quirino Bucci and Giacomo Iannelli. According to the company, the 30-minute flight went off without incident.
Engine: 1 x Williams FJ44-4M-34 turbofan, 1,540 kg / 3,450 lb thrust Wingspan: 8.47 m / 27.78 ft Weight: 3,300 kg / 7,275 lb Cruising speed: 400 kt / 460 mph / 740 km/h Service ceiling: 40,000 ft / 12,000 m Ferry range: 760 nm / 824 mi / 1,410 km
The 1972 designed Viper 632 powered Aermacchi MB339 produced in Varese, Italy, became the successor to the MB-326 and the Fiat G91. Sharing much of the MB-326K airframe structure, the MB-339 has a redesigned forward fuselage to allow the tandem seating to be staggered vertically, for the instructor to see over the pupil, the vertical tail enlarged, raised fin, a revised nose gear, stronger wings, Martin-Baker Mk.10 zero-zero seats, nose wheel steering and modern avionics. Six hardpoints (up to 1815 kg/4,000 lb) al¬low a combined trainer/light strike role. The wing is NACA 64A212 at the root and NACA 64A114 at the tip.
The first prototype MB-339X (I NOVE) made the type’s maiden flight on 12 August 1976, the second prototype was registered I NINE. Beginning production in 1976 was the MB.339A, of which the first of 100 for the Aeronautica Militare were handed over for pre service trials on 8 August 1979. Customers have included Argentina, Dubai, Ghana, Malaysia, Nigeria, and Peru.
MB.339As were the only operational jet aircraft deployed to the Falklands by the Argentineans during the hostilities, the Port Stanley runway being unable to accommodate Mirages or A 4s. An Argentine Navy MB.339 attacked a Royal Navy frigate, causing damage with 30 mm DEFA cannon fire and four Zuni 5 inch rockets. The trainer also has provision to carry the AGM65 Maverick ASM, the AIM 9 Sidewinder and the Sistel Marte II fire and forget sea skimming anti ship missile.
The MB.339B is basically a standard MB.339A advanced trainer with an uprated Viper 680 engine, enlarged tip tanks, and increased weapons carrying capability, enhanced for the ground attack role.
The MB.339C is designed to train pilots to use modern front-line mission management systems and powered by an uprated Viper 680-43 turbojet. Envisaged as a close support/maritime attack aircraft, the MB.339C first flew on December 17, 1985, equipped with a digital navigation/attack system including a GEC navigation computer, two Kaiser Sabre headup displays, a Litton inertial platform, CRT multifunction displays, a Fiat P-0702 laser rangefinder, an ELT-156 radar warning receiver, and a GEC AD-660 Doppler radar. Armament options included AIM-9L Sidewinder, AGM-65 Maverick ASMs, and Marte Mk.II anti-shipping missiles.
The MB-339CB with the Rolls-Royce Viper 680-43 jet engine experienced a number of engine problems. Flameouts on wet runways, compressor stalls during rapid acceleration/deceleration, defective fuel supply components, and turbine blade cracks. The subsequent repairs reduced the maximum thrust of the Viper to 4,280 lbs.
In 1991 the RNZAF purchased 18 of the model MB-339CB for use an advanced pilot trainer and weapons trainer with 14 Squadron based at Ohakea.
MB-339CB
The “CD” model was offered with HOTAS (Hands on Throttle and Stick), HUDs display and three LCD screens.
Development of the MB-339 has included the MB-339RM calibration model and 15 MB-339PAN delivered in 1982 for the Italian “Frecce Tricolori” aerobatic team.
The Viper 680 engined MB-339K, also known as the Veltro II, was a single-seat attack version. This aircraft first flew on 30 May 1980. In production form, the single-seat MB.339K Veltro 2, which flew in May 1980, was avail¬able with the digital navigation/attack system from the MB.339C.
Prototype Wing span: 35 ft 7.5 in (10.86 m). Max speed: 558 mph (898 km/h).
MB-339A Engine: 1x R-R Viper 632-43. Installed thrust: 17.8 kN. Span: 10.9 m. Length: 11 m. Wing area: 19.3 sq.m. Empty wt: 3125 kg. MTOW: 5900 kg. Warload: 1815 kg. Max speed: 925 kph. Initial ROC: 2010 m / min. Ceiling: 14,600+ m. T/O run: 465 m. Ldg run: 415 m. Fuel internal: 1410 lt. Endurance: 2hr 50min. Combat radius hi-lo-hi: 590 km. Hardpoints: 6.
MB-339C Engine: Viper 680, 1995-kg (4,400 lb) thrust. Max speed SL: 480 knots Max speed 25,000 ft: 460 knots ROC SL: 6500 fpm. Time to 30,000 ft: 7 min 6 sec. TO wt clean: 10,000 lbs. Endurance: 2 hr 50 min. Fuel Burn: 2500 lb/hr. Max extenal load: 4000 lb on six pylons.
MB-339CB Engine: Rolls-Royce Viper Mk.680-43, 4000 lb thrust. Span: 11.22m. Wing area: 19.3 sq.m. Length: 11.24m. MTOW: 6350 kg. Internal fuel: 1430 kg. (+2 x 400 kg tip tanks). Empty wt: 3414 kg. Height: 3.9 m. Max speed: M0.8, 575 mph. T/o run: 550m. ROC: 8500 fpm. Service ceiling: 46,000ft. Limits: +7.33 & -4g. Ferry range: 1190 miles (2200 km)
MB-339K Veltro 2 Engine: 1 x Piaggio RR Viper 680-43 turbojet, 4,450lbs / 19.8 kN thrust. Length: 36.88ft (11.24m) Wingspan: 36.81ft (11.22m) Height: 13.09ft (3.99m) Wing area: 19.3 sq.m Empty Weight: 6,889lbs (3,125kg) Maximum Take-Off Weight: 13,999lbs (6,350kg) Fuel internal: 2030 lt Maximum Speed: 506mph (815kmh; 440kts) Maximum Range: 231miles (371km) Rate-of-Climb: 6,595ft/min (2,010m/min) Service Ceiling: 46,719ft (14,240m) T/O run: 580 m Ldg run: 450 m Armament: 2 x 30mm DEFA cannons / 1935 kg external Seats: 2 Hardpoints: 6 Air refuel: No.
Single-seat version of the MB.326, the Aermacchi MB.336 made its first flight on Saturday, August 22, 1970. The pilot was Cdte Guido Careftiato, Aermacchi chief test pilot.
The new type, developed in response to an increasing world demand for a simple, high-performance and low-cost operational trainer and close-support aircraft, differs chiefly from the two-seat version in its more powerful engine (Rolls-Royce Viper 632-Y3 of 4,0001b thrust), internal gun installation and additional fuselage tank.
The two prototypes I-AMKK and I-KMAK, were converted from MB-326G to this new model.
The MB.326 developed into the MB 326K as the latest generation model, equipped with Mk 600 Viper engine, able to push 1,814 kg to give an even better performance.
The design (by Ermanno Bazzocchi) of the MB-326 began in 1954. There were some modifications to the project: horizontal tail surfaces had reduced dihedral, and the airbrakes (two in wings) became one under the fuselage. In 1956 AMI approved the project and asked for two prototypes (MM.571 and 572) and one airframe for static tests. No weapons or pressuriisation needed, but Bazzocchi introduced them.
The first prototype, I-MAKI, first flew on 10 December 1957, powered by a Bristol-Siddeley Viper 8 turbojet, flown by test pilot Guido Carestiato. The wing is NACA 64A114 at the root and NACA 64A212 at the tip. Each wing has 22 ribs and two spars. The fuel system has a tank in the center of the plane and two at the wingtips. The aircraft was 400 kg (880 lb) more than initial estimates. The original Viper 8 engine producing 7.8 kN (1,750 lbf) of thrust, was replaced by the Viper 9 which was 0.7 kN (147 lbf) extra thrust. The first prototype was lost in Egypt on 22 April 1959.
The second prototype first flew on 22 September 1958 and a new Viper engine, the model 11, was updated to produce a thrust of 11.1 kN (1,134 kg, 2,500 lb).
On December 15, 1958, AMI placed an order for 15 pre-series examples. In 1960, orders for 100 aircraft were placed.
The first production model flew on 5 October 1960.
Guido Carestiano set C1D 1 group records for an altitude of 15 489 m during of August 1961 in an MB-326.
The machines eventually arriving at 214 ° Lecce-Galatina school Group; while deployed in Brindisi. The type entered service with 43 ° N Flyer on March 22, 1962. This engine replaces the T-6 Texan, and there is a “fully-jet” training course for AMI pilots.
Eight MB-326Bs were ordered by Tunisia in 1965. They were developed from the basic MB-326s with weapons capability, with the 37th AMI series aircraft converted (I-MAKC). The key innovation is the ability of the ground offensive, with six underwing pylons, holding a maximum of 907 kg. In the same year, Ghana ordered nine of the same MB-326Fs.
“C” and “A” models never materialized. “A” is intended as a light attack aircraft, with two 7.62 mm machine-guns in the nose, but never built. Then, a few MB-326s called “A”, but this only means that they are equipped with Marconi ADF-370 AD. “C” version is to have NASARR radar in the nose, to train F-104 pilot, but only appeared as a mock-up.
Alitalia ordered four aircraft as a coach in the D “version”; demilitarization and equipped with special instruments to train pilots in preparation for the new jet liners.
Pilot also provided publicity for the MB 326: Riccardo Peracchi, working for AMI, displayed the MB-326 in many airshows, while Massimo Ralli set many records: February 8, 1966, climb records: 2 min 2 sec to 3000 m, 3 minutes 56 seconds for 6,000 m, 6 minutes 39 seconds for 9,000 m and 12,000 m 10 minutes 53 seconds. March 18, 1966, a record of 15 690 m altitude in horizontal flight, and 17 315 m absolute. July 18, 1966, endurance record, with 970 km August 2, 1966, a record speed of more than 3 km straight: 871 km / h December 1966: the speed of 880.586 km / h over 15-25 km, 831.007 km / h over 100 km, 777.667 km / h over 500 km, and the endurance record at 777.557 km
Other MB-326G s using a Viper Mk 20 engine that provides 1,524 kg of thrust, and consequently much faster and has a payload increase of 1814 kg max. Argentina ordered eight, initially as-MB 326K, then called-MB 326GB.
Other MB-326G s using a Viper Mk 20 engine that provides 1,524 kg of thrust, and consequently much faster and has a payload increase of 1814 kg max. Argentina ordered eight, initially as-MB 326K, then called-MB 326GB.
Argentine Navy MB-326 preserved in Río Grande, Tierra del Fuego
Since that time MB 326 B/F/ GC/K and M versions with attack/COIN capability were supplied to the armed forces of the Argentine, Bolivia, Brazil (where it is known as the AT 26 Xavante), Dubai, and South Africa (known as the Impala Mk 1). Some also served with Alitalia as the MB.326D.
Dubai bought three in 1974, and a further three in 1978 (MB-326KD), Tunisia eight (MB-326KT), Ghana nine (MB-326KB) and Zaire eight (MB-326KB). The MB-326L is essentially MB-326K with two seats. Two MB-326LD supplied to Dubai and four MB-326LD to Tunisia.
The engine is typically one 3,410 lb thrust Rolls Royce Bristol Viper 20 Mk 540 turbojet, and armament of up to 4,000 lb (1,814 kg) total can be carried on six underwing stations: this can include bombs, gun packs, rockets, and missiles. The MB.326G variant was fitted with a more powerful Viper 20 engine. An improved version was in production for the Italian Air Force under the designation M.B.339A.
The type was developed for the light strike role in the 326A, which was fitted with underwing hardpoints, culminating in the MB-326K single-seat close support version, which first flew on 22 August 1970. The additional of twin 30mm DEFA cannon was also introduced with the K model to compliment the already existing 6-hardpoints.
Engine upgrades moved from the 794-kg Rolls-Royce Viper 8 to the 1814-kg RR Viper 632. Variants of the MB-326 were used by Italy, Ghana, and Tunisia.
Seventeen were built in Italy for Zaire (Forces Arienne Zairoise) and 23 for the Air Force Zambia.
The MB 326K (originally known as MB-336) is a single seat model.
The aircraft were licence-built in Australia as the MB-326H, in Brazil as the AT-26 Xavante, and in South Africa as the Impala.
Brazil is the main customer for the 326-MB, in 1970 ordered two prototypes and 166-326GC s MB, called AT-26 Xavante.
The Forca Aerea Brasileira took delivery of its last 12 MB-326E, consisting of six MB-326 updated to MB-326G, and six newly produced (MM.54384 / 389). They had provision for weaponry and powered by 11 Viper 200 engine, not the Viper Mk 20 Mk 540 in 1981, bringing the Xavante line to a close, the final half dozen aircraft being replacements for export aircraft relinquished by the FAB from earlier contracts. They had provision for weaponry and powered by 11 Viper 200 engine, not the Viper Mk 20 Mk 540.
It was produced under license by Embraer with a further six for Togo (as the AT 26 Xavante) and 10 for Paraguay. Deliveries commenced in January 1983 of 12 ex-Forca Aerea Brasileira EMB-326GB Xavantes ordered for the 4a Escuadra Aeronaval at BAN Punta del Indio, Argentina. They were to make up attrition for two MB 326GB lost in accidents and three MB 339AA lost in the Falklands.
In Italian service the MB-326 was replaced by MB 339 between 1981 and 1984, after which they acted as liaison aircraft, replacing Lockheed T-33s. Excluding the prototype, 33 Italian Air Force MB-326s were lost in accidents between 1963 and 1992.
The MB326 was selected by the RAAF in the advanced training role in 1964 and by the RAN (10 RAN, 87 RAAF) in 1969. 12 were delivered by Macchi, 18 are assembled from kits in Australia, and another 67 built by the Commonwealth Aircraft Corporation and Hawker aircraft with the designation CA-30. Manufacturered by Commonwealth Aircraft Corporation, Melbourne, Victoria, Australia, under licence to Aermacchi, the first was delivered in October 1967 and the last in September 1972.
South Africa received a license to produce MB-326M (similar to G ‘model’), as Impala Mk I in 1964 with production beginning in 1966. They received 40 Italian-built aircraft followed by about 125 built locally by Atlas Aircraft Corporation, use them both as a trainer and in the armed configuration. Seven examples of the MB-326K also purchased as a light attack aircraft, with a further 15 assembled from a kit, while about 78 were license-produced and is known as the Impala Mk II. Production licenses of the single-seat version began in 1974.
South African Impalas were used in the battle against Angola, the Cuban and some militias, usually flying at 550-650 km / h at an altitude of 15 m. One was shot down by SA-7 and another returned with an unexploded missiles (SA-7, 8 or 9) in the flue gas. Six squadrons were equipped with Impala Mk. II in the SAAF during the 1970s and 1980s. During 1987 and 1988 Impalas were withdrawn from the front line, leaving Mirage and Buccaneers. Impala Mk. IIs also shot down a total of six Mi-8 and Mi-24 helicopters.
The Silver Falcons, the SAAF aerobatic team, were equipped with Impala Mk Is and on October 2, 1993, an Impala Mark I (Aermacchi MB-326) (no. 489) from the SAAF Silver Falcons aerobatic team fell after a separation of the right wing during a performance at the Airshow Lanseria. Pilot, Captain Charlie Rudnick was injured as the ejection was started outside the design envelope ejection seat.
Flying school for Impalas were Flying Training School in Langebaanweg while operational squadron 4, 5, 6, 7 and 8 squadrons while 85 Advanced Flying School also has a small number Impalas to supplement their Mirages.
AL Argentina – The Naval Argentina Flights received eight MB-326GB plus eleven MB-326GC ex-Brazilian Air Force
Royal Australian Air Force operated 87 MB-326Hs (RAAF serial A7-001 to -072, -079 to -083) 1967-2001. No. 25 Squadron RAAF No 76 Squadron RAAF No. 77 Squadron RAAF No 79 Squadron RAAF No. 2 Flying Training School RAAF RAAF No. 2 Operational Conversion Unit No. 5 Operational Training Unit RAAF Fitness RAAF Flying School Roulettes Telstars Aircraft Research and Development Unit Fleet Air Arm (RAN operated ten MB-326Hs 1970-1983. No. 724 Squadron RAN
Brazilian Air Force received 182 MB-326GCs (known as AT-26 Xavante) and 12 Atlas Impala former South African Air Force.
Cameroon Air Force has five in service.
Air Force Democratic Republic of the Congo
Dubai Air Wing
Ghana Air Force received 15 MB.326s.
Alitalia Italian Air Force operated 106 MB-326s, including 15 pre-production version.
Paraguay Air Arm ten operated EMB-326GBs / AT-26 Xavante, all retired in 2003.
South African Air Force received a 62 MB-326s plus 125 Impala Mk.1s and 73 Mk.2s
Togo Air Force received six MB-326GCs.
Tunisian Air Force received 16 MB-326s.
United Arab Emirates Air Force purchased six aircraft.
United States of America National Test Pilot School
Zaire Air Force received 25 MB-326GBs.
Zambia Air Force receives 23 MB-326GB.
Variants: MB-326: Two prototypes and 125 production of training aircraft for the Italian Air Force. MB-326A: Proposed armed version for weapons training, not built. MB-326B: Two-seat trainer jets, light aircraft attacks to Tunisia. (Eight built). MB-326D: Two-seat jet trainer armed for Alitalia. (Four built). MB-326E: Two-seat jet trainer armed to the Italian Air Force. (Six built). MB-326F: Two-seat trainer jets, light aircraft attack for Ghana. (Nine built). MB-326G: Two-seat trainer jets, ground-attack aircraft. (Two built). MB-326GB: Two-seat trainer jets, ground-attack aircraft. Eight sold to the Argentine Navy. 17 aircraft were exported to Zaire, and another 23 aircraft to Zambia. MB-326GC: Two-seat trainer jets, ground-attack aircraft for the Brazilian Air Force. Built under license in Brazil as the Embraer EMB-326. 167 aircraft were built for the Brazilian Air Force. Eleven of the Brazilian aircraft transferred to AL Argentina after the Falklands War. Six aircraft were exported to Togo, and another ten aircraft Paraguay. Total production, 182. AT-26 Xavante: Brazilian Air Force designation MB-326GC. RT-26 Xavante: Some AT-26 Xavantes converted into reconnaissance aircraft. MB-326H: seat jet trainer-Two, 87 aircraft were built for the Royal Australian Air Force, and 10 to the Royal Australian Navy. Built twelve Italian aircraft and 85 built under license in Australia by the Commonwealth Aircraft Corporation with the designation CA-30. MB-326K: Single-seat ground-attack aircraft for the South African Air Force. Built under license in South Africa by the Atlas Aircraft Corporation. Impala II: South African Air Force designation MB 326K. MB-326KB: Single-seat ground-attack aircraft for Zaire. (Six built). MB-326KD: Single-seat ground-attack aircraft to Dubai. (Three built). MB-326KG: Single-seat ground-attack aircraft for Ghana. (Four Built). MB-326KT: Single-seat ground-attack aircraft for Tunisia. (Seven built). MB-326L: Two-seat advanced jet trainer. MB-326LD: further training Two-seat jet plane to Dubai. (Two built). MB-326LT: further training Two-seat jet aircraft for Tunisia. Four built. MB-326M: Two-seat trainer jets, ground-attack aircraft for the South African Air Force. Built under license in South Africa by the Atlas Aircraft Corporation. Impala I: South African Air Force designation MB-326M. MB-326RM: Five Italian Air Force MB-326s aircraft converted into ECM.
Specifications:
MB.326 Engine: 2 x Bristol Siddeley Viper 22 1 turbojet, 2500 lbs.t. (1134 kgp) Span: 32 ft 10.75 in (10.04 m) Length: 35 ft 1 in (10.66 m) Wing area: 204.52 sq.ft (19sq.m). Height: 3.5 m / 11 ft 6 in Never exceed speed: Mach 0.8 Max speed: 501 mph / 806 kph / 436 kt at 4,575 m (15,000 ft) Cruise: 348 mph (560 kph) Stall speed: 146 km / h (79 knots, 91 mph) Initial climb: 4,420 fpm. (22.5 m/sec) Service ceiling: 41,000ft (12,500 m) Range w/tip tank 11,500 m (38,000 ft): 1,665 km (900 nautical miles, 1,035 miles) Empty weight: 4,930 lb (2 237 kg) Loaded weight: 7,320 lb (3 320 kg). Armament: 3 machine-guns, 4 missiles Hardpoints: 6 Bombload: Up to 2000 lb (900 kg) Crew: 2
MB-326H Engine: 1 x Rolls-Royce Viper 11 Mk.22-11 turbojet, 2,500 lb Wing span: 35 ft 11 in (10.8m). Length: 34 ft 5 in Height: 11 ft 4 in Empty weight: 5,027 lb Loaded weight: 7,340 lb Crew: 2 Initial Rate of Climb: 4,420 ft/min Ceiling: 40,000 ft Speed: 506 mph Range: 940 miles Armament: 2 x 7.62 mm Miniguns and bombs
MB-326K Engine: 1 x Rolls-Royce Viper 632-42 turbojet, 4,000lbs thrust. Length: 35.01 ft (10.67m) Width: 35.60 ft (10.85m) Height: 12.20 ft (3.72m) Empty Weight: 6,535lbs (2,964kg) Maximum Take-Off Weight: 12,996lbs (5,895kg) Maximum Speed: 553mph (890kmh; 481kts) Maximum Range: 677miles (1,090km) Rate-of-Climb: 6,500ft/min (1,981m/min) Service Ceiling: 41,010ft (12,500m) Armament: 2 x 30mm DEFA cannon Max external ordnance: 4,000lbs Seats: 1 Hardpoints: 6
