Aermacchi MB-326 / Commonwealth Aircraft Corporation CA-30 / Embraer EMB-326

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.

Aermacchi MB.326 Article

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.

A7-043 (MB-326H) in Wagga RAAF Base in Australia

RAAF Aermacchi MB-326 Article

MB-326H

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.

Some 784 MB326 were manufactured.

Gallery

Operators:

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

EMB-326GC / AT26

Aermacchi M-290TP RediGO / L.90TP / Valmet L-90TP RediGO / Aermacchi M-290TP

Derived from the earlier Valmet L.70, through an intermediate design known as the L.80TP, the Valmet L.90TP completed its maiden flight in June 1986. The Redigo differed from the L.70 primarily in having an Allison 250-B17D turboprop power plant, a new, increased-span wing, and a retractable undercarriage. The wing is NACA 63-218(mod B3) at the root and NACA 63-412(mod B3) at the tip. The L.90TP is designed to take student pilots through the first 100 hours of training, for graduation directly on to a suitable advanced trainer. Six underwing hardpoints can carry a total of 800kg of stores.
In 1996 Aermacchi took over L-90TP RediGO from Valmet of Finland and redesignated it the M-290TP RediGO.

Valmet L 90 TP Redigo
Engine: 1 x Allison 250 turboprop B17F, 309 shp.
Length: 25.919 ft / 7.9 m
Height: 9.514 ft / 2.9 m
Wingspan: 33.793 ft / 10.3 m
Wing area: 159.307 sq.ft. / 14.75 sq.m
Max take off weight: 2976.8 lb / 1350.0 kg
Weight empty: 1962.5 lb / 890.0 kg
Max. weight carried: 1014.3 lb / 460.0 kg
Max. speed: 181 kt / 335 km/h
Landing speed: 50 kt / 93 km/h
Cruising speed: 165 kt / 305 km/h
Initial climb rate: 1929.13 ft/min / 9.8 m/s
Service ceiling: 25000 ft / 7620 m
Wing load: 18.66 lb/sq.ft / 91.0 kg/sq.m
Range: 810 nm / 1500 km
T/O run (to 15m): 310 m.
Fuel internal: 360 lt.
Ldg run (from 15m): 360 m.
Endurance: 5+ hr.
Crew: 2
Armament: ext. 800kg 4 pods

Aeritalia / Aermacchi / Embraer AMX

AMX

In 1977 the Italian Air Force (AMI) issued a requirement for a multi-role strike/recce aircraft to replace its Fiat G-91R/Ys and F-104G/Ss.

Mid-1978 Aeronautica Macchi concluded an agreement with Aeritalia for the joint design, development and production of what became the AMX (Aeritalia-Macchi-eXperimental). This agreement provided for assembly lines in both countries and single-sourced sub-assemblies.

Alenia and Aermacchi started development of the AMX and in 1980 Embraer joined the project, the Brazilian Air Force (FAB) also having issued a requirement for a similar aircraft to replace its AT-26 Xavantes. The consortium was based in Rome, Alenia 46.5%, Aermacchi 23.8%, and Embraer 29.7%.

Aeritalia / Aermacchi / Embraer AMX Article

The basic single-seat aircraft is designed for daytime low-level attack and tactical reconnaissance. Work was split 70:30 between Italy and Brazil, and 70:30 between Aeritalia and Aermacchi in Italy. Embraer was responsible for the wings, flaps, intakes, and tailplane, Aermacchi for the forward and rear fuselage sections, and Aeri¬talia for the centre fuselage and fin. Italy built four prototypes and Brazil two. Final-assembly lines were located in both countries.

In May 1984 the AMX made its first flight, and in February 1987 Embraer’s first prototype flew with the purpose-designed reconnaissance pallet, and by May the aircraft was undertaking static test firing of the Brazilian versions twin 30mm DEFA cannon. A second Brazilian prototype joined the test programme in December 1986.

The AMX International AMX has high-mounted monoplane wings, twin intakes and a single engine exhaust under the single tail rudder. Crew accommodations vary with model and can either be a single pilot or pilot and rear-cockpit operator in tandem. Standard armament varies between the Italian and the Brazilian models, with the Italian version receiving a single 20mm General Electric cannon and the Brazilian version being fielded with twin 30mm DEFA cannons. Four underwing hardpoints, a centerline hardpoint and wingtip hardpoints are fitted. Wingtip mounts are reserved for short-range air-to-air missiles.

Final assembly of the first Italian production AMX began on schedule in January 1987 and was delivered to the Italian Air Force in January 1989 and to the Brazilian Air Force in 1990.

The AMX were assembled in both Italy as Brazil. Planed build was for 317 aircraft of both types (238 for Italy and 65 for Brazil). The initial order was later cut to 136 due to budgetary constraints to defences in both countries. Production continued with little in the way of developmental setbacks. Production of the AMX series broke down with Alenia (Aeritalia) handling up to 46.7% whilst Embraer took 29.7% and Aermacchi 23.6%. Final production would be handled in their respective countries.

A single-seat multi-role strike fighter aircraft, designed to fly low-altitude missions at high-subsonic speeds in day or night and in poor visibility, it is capable of operating from damaged or unprepared runways. It has a limited air-to-air capability and integrated ECM for self defense.

AMX-T is the twin-seat variant of the AMX and is used as advanced trainer. The AMX-T retains the operational capabilities of the single-seat version.

The aircraft for the Brazilian Air Force (FAB) are designated A-1 (single-seat) and TA-1 (two-seat), and are equipped with two DEFA 544 30mm cannons, while the Italian variant is fitted with one M61A1 multi-barrel 20 mm canon.

The Brazilian A-1/TA-1 fleet underwent an upgrade, the aircraft designated A-1M in FAB service, The A-1M upgrade is based on the Brazilian AT-29 and the F-5M upgrade program, giving the aircraft many simularities in avionics and capabilities. The new cockpit includes three colored MFDs, HOTAS, new multimode radar (the Italian Grifo F) and the capability to use smart weapons.

The Italian AMX and AMX-Ts went through the ACOL upgrade program. Alenia Aerospace upgraded 43 single-seat and 12 two-seat AMX aircraft as the AMX-ATA extending the operational life to 2015 and giving the AMX improved combat capabilities. It includes a new inertial navigation system/GPS, GPS-guided weapons integration, new colour MFDs, updated communications and IFF, and a new computer symbol generator with digital map functions.

The AMX aircraft under the Italian banner saw extensive service in the war against Serbia in Operation Allied Force, accounting for over 250 sorties all its own. The system was fielded with advanced Israeli Elbit Opher imaging infra-red guided bombs, Mk 82, Mk 83 and Mk 84 conventional bombs and Paveway II laser-guided bombs.

Variants:
AMX
A-1
TA-1
AMX-T
AMX-ATA

AMX International AMX (Ghibli)
Engine: 1 x R-R Spey 807 non-afterburning turbofan, 49.1 kN (11,030 lb st)
Length: 44.521 ft / 13.57 m
Height: 15.026 ft / 4.58 m
Wingspan: 29.101 ft / 8.87 m
Wing area: 226.044 sqft / 21.0 sqm
Max take off weight: 28665.0 lb / 13000.0 kg
Weight empty: 14773.5 lb / 6700.0 kg
Wing load: 126.9 lb/sq.ft / 619.0 kg/sq.m
Max. speed: 493 kts / 913 km/h
Initial ROC: 10236.22 ft/min / 52.0 m/s
Service Ceiling: 13,000 m / 42,650 ft
Maximum Range int. fuel: 345miles (556km)
Max range: 1801 nm / 3336 km
T/O run: 950 m
Ldg run: 1525 m.
Crew: 1 / 2
Hard points: 5 + 2 wing tips.
Armament:
1 x 20mm General Electric GE M61A1 Vulcan cannon (Italian AMX) with 350 rounds
2 x 30mm DEFA cannons (Brazilian AMX)
Bombload: 3800 kg (8,377 lb)

Aeritalia

Formed 12 November 1969 by equal shareholding of Fiat and IRI-Finmeccanica to combine Fiat aerospace activities (except engines) and those of Aerfer and Salmoiraghi. Fully operational January 1972. In September 1976 IRIFinmeccanica bought Aeritalia stock owned by Fiat.
Took control of Partenavia in 1981-1992 under its General Aviation Group.
As Panavia partner, designed and developed variable-geometry wing and other important features of Tornado multirole aircraft. Became partner in AMX program (see AMX International), and joined Aerospatiale of France in establishing ATR. Merged with Selenia in December 1990, to form Alenia Aerospazio.

Aerial Arts Laser

The 1987 Laser was a lightweight high performance machine which incorporated some unusual features. Additional support for the outboard leading edges was provided by a continuous wire running through the control frame to the outer leading edges. This allowed more twist transfer to occur for a given sail and crossboom tension than with conventional single side-wire designs.

The keel was placed within the double surface in a horizontal keel pocket. Another feature of this glider was a bellcrank arrangement separating the twin tensioner wires running back from the crosstube which separate as the VB is pulled tighter. This was designed to alleviate the handling problems normally brought on when the kingpost is trapped between the wires and thus prevents sideways movement of the keel.

Equipped with Variable Billow and internally sprung battens instead of bungies, the price was £1375.00 inc VAT.

Wing area: 14 m² / 150 sq ft
Wing span: 10 m / 33 ft
Aspect ratio: 7.25
Hang glider weight: 28 kg / 60 lb
Nose angle: 124°
L/D: 13:1

Aerial Arts Clubman

The Clubman 1 is a lightweight intermediate of which only a few were built in 1984, priced at £675.00.

Clubman 1

The 1984 Clubman CFX was a fifth generation lightweight intermediate glider built in three sizes.140/160/180. The Clubman CFX was price from £765.00.

Clubman CFX

Clubman 1
Wing area: 14.5 m²
Wing span: 9 m
Aspect ratio: 5.6
Hang glider weight: 21 kg / 46.5 lb
Max glide ratio (L/H): 9.5
Min Sink: 180/ft min
Number of battens: 14
Nose angle: 120°

Aériane P-Swift / Brightstar P-Swift

Though the Swift is popular in Europe, it began life as an American design from U.S. producer Brightstar. The San Francisco-area company created the unpowered Swift in the early 1990s. Soon after its introduction, Brightstar offered the Motor Swift, but the company didn’t go nearly as far with it as Belgium-based producer Aeriane, which bought the manufacturing rights.

The European company finished the cockpit area and has fully enclosed it and the aft engine. These streamlining efforts have boosted glide performance by several points.

Equipped with a fixed motor and effectively a motorglider/microlight with a glide ratio of 27:1 and a sink rate of 140 fpm, the Motor Swift is quite competitive, and it is unique for its tailless design. This 253-pound plane has been flying for a decade without problems.

The Motor Swift comes with easily removed wings for simple transport and storage and is sold ready to fly with starter, folding prop, and instruments for about $25,000 (circa 2010).

The Motor Swift can qualify as a Part 103 ultralight. There is also a tandem cage adaptable on the same wings.

Flying the Aériane P-Swift

Engine: Zanzotera F34, 25 hp
Hp range: 10-30.
Top speed: 93 mph.
Cruise: 80 mph.
Stall: 25 mph.
ROC: 700 fpm.
TO dist: 120 ft.
Ldg dist: 160 ft.
Service ceiling: 15,000 ft.
Empty wt: 200 lbs.
MTOW: 450 lbs.
Height: 5 ft.
Length: 14 ft.
Wing span: 39 ft.
Wing area: 135 sq.ft.
Seats: 1.
Undercarriage: 2 wheel tandem.
Glide ratio: 25-1.

Engine: Zanzoterra MZ 34, 25 hp
Empty weight: 110 kg
Wing span: 12 m
Wing area: 12.5 sq.m
Fuel capacity: 18 lt
MAUW: 230 kg
Seats: 1
Max speed: 140 kph
Cruise speed: 120 kph
Minimum speed: 40 kph
Climb rate: 3.5 m/s
Fuel consumption: 4 lt/hr
Price (1998): 800 000 FB ht

Engine: Konig SC430, 24 hp.
Speed max: 63 mph.
Cruise: 53 mph.
Range: 230 sm.
Stall: 27 mph.
ROC: 500 fpm.
Fuel cap: 3 USG.
Weight empty: 230 lbs.
Gross: 470 lbs.
Height: 7 ft.
Length: 10 ft.
Wing span: 39 ft.
Wing area: 135 sq.ft.
Seats: 1.
Landing gear: nose wheel.

Aériane Swift / Brightstar Swift

The original Swift (Swept Wing with Inboard Flap Trim) was made by Bright Star Gliders in California. When they were looking for a manufacturer for the European market, they found Aériane in Belgium.

The pilot lies flat in this 24-1 glide ratio motor glider. For Advanced pilots, it can switch from powered to unpowered in 30 minutes. The Swift PAS is equipped with an auxiliary motor.

The Swift was marketed by Bright Star Gliders Inc in California. From 1997 Aériane was the only manufacturer building and marketing all versions of the carbon fibre / kevlar construction Swift light sailplane.

When Bright Star closed Aériane continued building the Swift.

Gallery

Wing Span: 11.898 m
Empty weight: 63 kg
Wing area: 12.54 sq.m
Vne: 120 km/h
Stall: 35 km/h
Vzmin: 0.65 km/h
Glide Ratio: 25 @ 60 km/h
Price (1998): £ 11,750

Aériane Swift Light
Wing area: 12.54 m²
Wing span: 12.7 m
Aspect ratio: 12.86
Hang glider weight: 46 kg
Minimum pilot weight: 55 kg
Maximum pilot weight: 105 kg
Minimum speed: 35 km/h
Maximum speed: 120 km/h
Max glide ratio (L/H): 27
Max glide ratio speed: 75 km/h
Minimum sink rate: 0.6 m/s
Nose angle: 140 deg

Aériane Swift Standard
Wing area: 12.54 m²
Wing span: 11.89 m
Aspect ratio: 11.27
Hang glider weight: 60 kg
Minimum pilot weight: 55 kg
Maximum pilot weight: 105 kg
Minimum speed: 35 km/h
Maximum speed: 120 km/h
Max glide ratio (L/H): 25
Max glide ratio speed: 75 km/h
Minimum sink rate: 0.6 m/s
Nose angle: 140 deg