The An-225 Mriya (dream) stemmed from the need to transport large items for the Soviet space programme. In mid-1985 Antonov began the design and the An-124 provided the basis for the new aircraft, Antonov using many of the same components to keep cost and development effort down. Standard An-124, wings are grafted on to a new centre section, thereby increasing the span while keeping the engine installations the same. An additional pair of D-36T turbofans is fitted to the new centre section.
The cabin retains the same cross-sectional dimensions but with increased length, and to save weight the rear loading ramp is removed, but the An-225 retains the nose visor.
To support the increased weight, seven pairs of wheels are fitted to each side as opposed to five in the An-124. Outsize loads are carried ‘piggy-back’, the load supported on two main attachments above the centre section. These supports and other smaller ones along the fuselage top are faired over when not in use. To avoid buffeting from the ‘piggyback’ load, the An-225 has twin vertical fins mounted on the end of a large tailplane.
The prototype made its first flight on 21 December 1988 from Hostomel Airport outside Kiev, Ukraine, and the first flew with Buran on 13 May 1989 from Baikonur cosmodrome. This combination appeared at the Paris air show in 1989, car¬rying the 62.1 tonne (136,684 lb) Buran on its back.
On 22 March 1989, in the course of a single 3 hr 30 minute flight from Kiev, the An-225 set 105 world and class records. With a payload of 344,576 lb / 156,300 kg, the machine took off at a weight of 1,120,370 lb / 508,200 kg. It proceeded to fly a 1243 mile / 2000 km closed circuit at an average speed of 505.24 mph / 813.09 kph and to reach a maximum altitude of 40,485 ft / 12,340 m.
Typically, the An-225 carries two pilots, two flight engineers and two navigators, the flight system incorporating fly-by-wire controls. NATO name Cossack.
The Antonov An-225 has been extensively modified since 1988 with its six engines being updated and a strengthened fuselage being among the many changes.
The first commercial flight was performed by the An-225 in May, 1990. A T-800 tractor weighing more than 100 tons was delivered from Chelyabinsk to Yakutia.
After the collapse of the USSR the only plane stopped flying in 1994 and some parts were disassembled to be used on other planes. However by the 2000s it was restored by efforts of some Ukrainian companies. The airliner was amended a bit to meet the standards of civil aviation first flying aain on the 7th of May, 2001.
Antonov planned to finish building a second An-225 if they have financial support. 70% was ready; the centre wing-section, fuselage and a wing remained since the Soviet times. If they had a customer they would finish it, requiring $150 million.
An-225 Mriya (Cossack) Engines: 6 x ZMKB Progress (Lotarev) D-18T turbofan, 225140 N / 22950 kp / 51,587lbs thrust Length: 84.0 m / 275 ft 7 in Height: 18.2 m / 59 ft 9 in Wingspan: 290 ft / 88.4 m Wing area: 905.0 sq.m / 9741.33 sq ft Empty Weight: 385,809lbs (175,000kg) Maximum Take-Off Weight: 1,322,774lbs (600,000kg) Max. weight carried: 661500.0 lb / 300000.0 kg Wing load: 128.74 lb/sq.ft / 628.0 kg/sq.m Maximum Speed: 528mph (850kmh; 459kts) Landing speed: 135 kts / 250 km/h Cruising speed: 432 kts / 800 km/h Range w/max.fuel: 15400 km / 9569 miles Range w/max.payload: 4500 km / 2796 miles Service Ceiling: 36,089ft (11,000m) Internal cargo hold: 43m x 6.4m x 4.4m. Crew: 4-6 +23
The Antonov An-178 (Ukrainian: Антонов Ан-178) is a short-range medium-airlift military transport aircraft designed by the Ukrainian Antonov company and based on the Antonov An-158 (An-148-200).
An-178 is a high-wing transport aircraft with moderately swept wing, winglets and a T-tail. The wing outer panels (including winglets), front fuselage with cockpit and nosewheel leg come from the An-158. The cargo hold is slightly enlarged, and there is an extra pair of main-wheels on each side. The airframe is made of aluminium alloys and composite materials. The fuselage is semi-monocoque with a circular cross-section. The retractable landing gear consists of two main wheel bogies and a dual nose wheel. The flight control system is dual duplex fly-by-wire system, consisting of two parts: FCS-A and FCS-B, each of which is responsible for two control channels. The flight control surfaces include ailerons near the wing tips, four control spoilers, six lift-dump/speed-brake spoilers, rudder and elevators, with an emergency mechanical cable back-up system. The powerplant consists of two Progress D-436-148FM turbofan engines, mounted on pylons under the wings and an auxiliary power unit. It can shift 18 tonnes over 1,000 km, or 10 tonnes over 4,000 km.
The aircraft was derived from the 99-seat An-158 regional airliner and was fitted with the commonized F1 fuselage nose section with the identical flight deck, wing panels, empennage and most of the onboard systems. The fuselage however was newly created with an enlarged diameter that had grown from 3.35 m to 3.9 m, which has resulted in an enlarged cargo hold – the cargo cabin cross section increased to 2.75 m by 2.75 m. Aside from the wing structure, outer panels (including winglets), front fuselage nose, cockpit and nose landing gear which come from the An-158, there is an extra pair of tandem main-wheels on each side.
The An-178 was previously known as the An-148T. The aircraft made its Western debut at the 2015 Paris Air Show.
It was announced on 5 February 2010, rolled out on 16 April 2015 and the maiden flight was on 7 May 2015.
There are reports that future production-standard aircraft will have a longer wingspan while retaining the organic wing panels of the An-158. Its maximal take-off weight would increase to an estimated 56 tons. Later production variants would need turbofan engines with a thrust of about 9,500 kgf to have the characteristics required. The planned engine may be the new-generation in-development Ivchenko-Progress AI-28 turbofan. The decision was made to fit the An-178 prototype with less powerful D-436-148FM engines in the interim. The D-436-148FM is a derivative of the production-standard D-436-148 with an upgraded fan, which boosted the takeoff thrust to 7,800 kgf and at emergency power rating to 8,580 kgf.
Powerplant: 2 × Progress D-436-148FM Turbofan, 73.55 kN (16,534 lbf) Wingspan: 30.57 m (100 ft 4 in) Length: 32.23 m (105 ft 9 in) Height: 9.57 m (31 ft 5 in) Max takeoff weight: 51,000 kg (112,436 lb) Fuel capacity: 14,650 kg (32,298 lb) Max landing weight: 47,000 kg (103,617 lb) Maximum speed: 990 km/h (620 mph, 530 kn) Cruise speed: 825 km/h (513 mph, 445 kn) Range: 4,700 km (2,900 mi, 2,500 nmi) Ferry range: 5,300 km (3,300 mi, 2,900 nmi) Service ceiling: 12,000 m (39,000 ft) Landing distance: 2,500 m (8,200 ft) Crew: 2 Capacity: 90 soldiers, 70 paratroopers, 48 on stretchers +15 seated, 8 medical modules and 12, or 16 tons of cargo, overload variant 18 tons.
The Antonov An-148 (Ukrainian: Антонов Ан-148) is a regional jet designed and built by Antonov of Ukraine.
The beginning of the An-148 project dates to the early 1990s, when work on the Antonov An-74 passenger modification started, headed by Petro Balabuev. In 2001, the project was renamed An-148. The An-74 fuselage was extended and the new aircraft’s wing design was created from scratch. The developers initially used Motor Sich D-436-148 engines.
The An-148 aircraft is a high-wing monoplane with two turbofan jet engines mounted in pods under the wing. This arrangement protects the engines and wing structure against foreign object damage. A built-in autodiagnosis system, auxiliary power unit, and the wing configuration allow the An-148 to be used at poorly equipped airfields. Flight and navigation equipment features five 15 by 20 cm (5.9 by 7.9 in) liquid crystal display panels built by Russia’s Aviapribor and a fly-by-wire system.
The main landing gear rotates into the belly of the aircraft when in flight, with partial doors covering the legs, and the sides of the tires remaining exposed. Built-in entrance stairs enable boarding and disembarking the aircraft without extra ground equipment.
The An-148-100 regional aircraft is the main model of the An-148. It seats 70 passengers at 864 mm (34.0 in) or up to 80 passengers at 762 mm (30.0 in) pitch in a one-class 2+3 seating layout. The aircraft is also configurable in a multiple-class layout which can carry fewer passengers, typically with four abreast business class.
In 2002, production of the first three prototypes was begun at AVIANT. On 17 December 2004, the first prototype completed its maiden flight. The second prototype joined the testing programme in April 2005. During the certification programme, the two prototypes performed about 600 flights in total. On 26 February 2007, the aircraft, its D-436-148 engine and the AI-450-МS auxiliary power unit were certified by the Interstate Aviation Committee of Russia and the State Aviation Administration of Ukraine.
The first prototype. It made its maiden flight on 17 December 2004.
The aircraft completed its certification programme on 26 February 2007. The An-148 has a maximum range of 2,100–4,400 km (1,100–2,400 nmi; 1,300–2,700 mi) and is able to carry 68–85 passengers, depending on the configuration.
The An-148 was manufactured by the Ukrainian Kyiv AVIANT plant (now Antonov Serial Production Plant) and Russia’s Voronezh Aircraft Production Association (VASO). On 28 June 2009, the first serially produced An-148, manufactured at VASO in Voronezh, took to the skies. Although numerous companies are involved in the project, at least 70% of the aircraft’s hardware is made by Russian manufacturers. The An-148’s list price is about $24–30 million. The main problem with the project has been increasing the aircraft’s sluggish production rate. The then-independent AVIANT plant initially failed to satisfy to growing orders, leading to VASO’s growing involvement in the aircraft’s assembly. VASO announced in June 2017 that the two final Russian-assembled An-148s would be delivered, and the project would not see further development.
In April 2005, the Ilyushin Finance Leasing Company ordered the first series of An-148 for the Krasair airline. Lease agreement calls for ten aircraft with an option for five units valued at $270 million.
The Antonov An-158 is a stretched fuselage version of the aircraft, accommodating up to 100 passengers.
An-158
The An-158 is a 1.7m stretched fuselage version for 99 passengers in a one-class standard configuration. Other changes include the installation of wingtip fences. The airplane successfully completed its first flight on 28 April 2010, with flight certification tests were planned to be completed before the end of 2010; on 3 March 2011, it was given Russian certification.
After flight and land test in night lands airports of Ecuador (Latacunga / Cotopaxi International Airport, 2806 m AMSL) and Bolivia (La Paz / El Alto International Airport, 4061 m AMSL) in November 2013 prepare documentation for obtaining correspondent supplements to the type certificate of this airplane.
On 2 June 2009, the first An-148 entered commercial service with the Ukrainian carrier Aerosvit. The first passenger flight was from Kharkiv to Kyiv; the aircraft had the civilian registration UR-NTA. By November 2009, Aerosvit was operating the An-148 on the Kyiv–Odessa and Simferopol–Lviv routes, performing two flights a day with the average flight time of 4–5 hours.
On 21 December 2009, the An-148 was put into service in Russia with Rossiya airline. The first passenger flight was FV135 from Pulkovo Airport in Saint Petersburg to Sheremetyevo International Airport in Moscow. By 20 May 2010, Rossiya’s An-148 fleet had accumulated a total of 915 flight hours and performed 710 landings. Rossiya complained that the aircraft experienced some reliability problems. There were some technical problems with the aircraft, and pilot training could not be ramped up fast enough, leading to pilot shortages. However, by 2011 the situation had improved.
On 15 February 2010, the An-148 started international flights to the European Union (Poland) with the Aerosvit airline.
The first An-158 in April 2010
On 18 April 2013, the first serial An-158 version was delivered to the Cuban flagship airline Cubana de Aviación. According to Antonov, Cubana additionally ordered two more aircraft, while other sources report this order to be for ten aircraft. On 28 April 2013, Ukraine’s Antonov aircraft maker handed over a third An-158 passenger airliner to Cuba and signed a contract for the delivery of three more.
Following a crash in February 2018, all An-148 and An-158 in Russia were grounded by the Russian Ministry of Transport. In addition, Cubana grounded its An-158 fleet as of May 2018 due to several technical issues with the aircraft. Until late 2018, the Antonov An-148 aircraft was also being produced in Russia by Voronezh Aircraft Production Association; however, due to the souring political relationship between Ukraine and Russia, production in Russia was discontinued. The last Russian-built An-148 was completed in October 2018.
In April 2016, Indian company Reliance defense limited and Antonov entered into an agreement to construct an aircraft based on An 148/ An 158 for defense and commercial purposes.
In April 2017, Cubana de Aviación suspended its flights between Havana and Guantánamo due to “technical problems” with its An-158 fleet. The route from Havana to Holguín also had problems: of 116 planned flights in the first months of 2017, 38 were cancelled and 36 suffered significant delays. Yoanka Acosta, head of Cubana’s commercial division, explained that the planes were leased from Ukraine but spare parts were sourced from Russia, so the state of conflict between the two countries had affected the supply of parts, making maintenance difficult. In late April, however, representatives from Antonov and Cubana met and signed a service agreement that extended the aircraft’s navigation directives to 3,600 flights and guaranteed the supply of spare parts, although it did not specify a date for normalization.
In March 2018 Rostransnadzor suspended all flights of An-148 in Russia after crash on 11 February 2018.
In May 2018, Cubana de Aviación grounded its An-158 fleet after it received an order from the Cuban National Aviation Authority. The official reason given by the Cuban National Aviation Authority was “multiple and repeating failures have been found in complex systems, built by mechanical, hydraulic and electrical components, as well as computer performance algorithms”, in addition to “evidence of design and manufacturing flaws, serious issues in flight control system, cracks in the structure and engine temperature increase above normal parameters”.
On 5 March 2011, an Antonov An-148 (assembled by VASO) carrying test registration 61708 crashed during a test flight in Russia’s Belgorod Oblast after an inflight breakup, killing all six crew members on board. An investigation commission found that the crew permitted the aircraft to accelerate more than 60 knots above its “Never Exceed” speed in an emergency descent, which led to the inflight breakup. Witnesses on the ground reported a wing had separated from the aircraft in flight. The aircraft was due to be delivered to Myanmar.
On 11 February 2018, an Antonov An-148 operating as Saratov Airlines Flight 703, crashed shortly after takeoff near Ramenskoye, outside of Moscow. The aircraft was carrying 65 passengers and six crew members. There were no survivors. This is the first fatal commercial accident for this aircraft type.
At least 47 were built.
An-148-100B
An-158
Versions
An-148-100A main version of the An-148. It has a passenger capacity of 85 in a one-class dense configuration or 68 in a two-class configuration, and a range of 2,100 km (1,100 nmi; 1,300 mi)
An-148-100B extended-range version, up to 3,500 km (1,900 nmi; 2,200 mi)
An-148-100E extended-range version, up to 4,400 km (2,400 nmi; 2,700 mi) and a maximum takeoff weight (MTOW) of 43.7 t (43,700 kg; 96,000 lb)
An-148-200 unified with An-158 by the rear part of the fuselage. Hence maximum seating capacity is increased to 89 passengers in dense configuration, comparing to 85 for An-148-100. Planned for production in Kyiv with An-158.
An-148-300 previously called An-168, business variant, seating 8-40 passengers, with a range up to 7,000 km (3,800 nmi; 4,300 mi)
Specifications:
148-100E Engines: 2 x Progress D-436-148, 14,000 lbf; 63 kN Wingspan: 28.91 m (94 ft 10 in) Wing area: 87.32 m2 (939.9 sq ft) Length: 29.13 m (95 ft 7 in) Height: 8.19 m (26 ft 10 in) MTOW: 43,700 kg (96,300 lb) Max. payload: 9,000 kg (20,000 lb) OEW: 22,000 kg (49,000 lb) Max. fuel: 12,050 kg (26,570 lb) Ceiling: 12,200 m (40,000 ft) Cruise: 800 to 870 km/h (430 to 470 kn) Range (75 pax/max): 4,400 km (2,400 nmi) Fuel burn: 1,650 kg/h (3,600 lb/h) Take off run (MTOW): 1,885 m (6,184 ft) Seats: 68–85 Seat pitch: 30–35 in Cargo: 14.60 m3 (516 cu ft) Cabin: 3.15 m (10 ft 4 in) width × 2.00 m (6 ft 7 in) height Cockpit crew: 2
An-158 Engines: 2 x Progress D-436, 15,100 lbf; 67.0 kN Wingspan: 28.91 m (94 ft 10 in) Wing area: 87.32 m2 (939.9 sq ft) Length: 30.83 m (101 ft 2 in) Height: 8.19 m (26 ft 10 in) MTOW: 43,700 kg (96,300 lb) Max. payload: 5,000 kg (11,000 lb) OEW: 22,000 kg (49,000 lb) Max. fuel: 12,050 kg (26,570 lb) Ceiling: 12,200 m (40,000 ft) Cruise: 800 to 870 km/h (430 to 470 kn) Range (75 pax/max): 2,500 km (1,300 nmi) Fuel burn: 1,800 kg/h (4,000 lb/h) Take off run (MTOW): 1,900 m (6,200 ft) Cockpit crew: 2 Seats: 86–99 Seat pitch: 30–34 in Cabin: 3.15 m (10 ft 4 in) width × 2.00 m (6 ft 7 in) height
The An-140 (first flown September 1997) short-haul regional airliner was planned to supersede the An-24. An agreement for licence production by Iranian Aviation called ‘Iran-140’ was signed in 1993. The first aircraft, supplied as a kit, flew on 7 February 2001.
The An-124 strategic airlifter, Nato code name Condor, first flew on December 26, 1982 with Vladimir Terski at the controls, and at least nine had been built by June 1987. At the time of its first flight, the An-124 was the largest aircraft in the world. The An-124 is powered by four 230kN-thrust Lotarev D-18T high-bypass turbofans, and is claimed to carry its 150-tonne maximum payload over 4,500km. Designed for simultaneous nose and tail loading, with a visor-type lifting nose and integral forward-folding ramp, the pressurised cargo hold is 36m long, 6.4m wide, and 4.4m high. A pressurised upper deck can accommodate 88 passengers. The An-124 has a six-man crew (two pilots, two engineers, a navigator and a radio operator), dual weather and ground mapping raders, quadruplex inertial navigation, and anologue fly-by-wire controls with mechanical backup operating hydraulic control servos. Two overhead travelling cranes, which have a lifting capacity of 30 tonnes, and two winches allow heavy cargo to be self-loaded without the use of special airport loading equipment. To enable the carriage of extremely heavy cargo, HeavyLift-Volga-Dnepr have developed special loading systems allowing individual items of up to 100 tonnes to be loaded. In addition, two double-deck car-racking systems have been built allowing up to 50 cars to be carried in one flight. Approximately 5,500kg of composite materials are used in doors, fairings, and panels, including 3,000kg of carbonfibre, giving a 1,800kg overall weight saving.
The second aircraft, named Ruslan, appeared at the 1985 Paris Air Salon. The aircraft entered service with Aeroflot in early 1986, and now serves principally on the Siberian run, carrying outsize items to the oil and mineral exploitation industries. In 1987 the An-124 began service with the air force. Production is reportedly eight to ten aircraft per year, and by 1989 over 25 had been completed. The An-124 was assigned the NATO reporting name ‘Condor’. The An-124-100 is a civil varient, certified in Russia. They are built one at a time and take about three and a half years to construct. Its 24-wheel undercarriage allow it to go into semi-prepared strips and the two nose-wheel units can be retracted on the ground allowing the aircraft to ‘kneel’ to assist loading. The large undercarriage system, the full-span, leading-edge slats and flaps give the An-124 very good short field performance. Full-span leading-edge slats and large flaps give the An-124 short field capability, while its 20 main wheels allow the type to use rough fields.. Civil examples were with Antonov Air Foyle, HeavyLift Volga Dnepr and the Russian-Australian joint venture, Antonov Airlines.
An-124 Engine: 4 x Lotarev D-18T Turbofan, 229.9 kN. / 51,590 lb Installed thrust: 920 kW. Wingspan: 73.0 m / 239 ft 6 in Length: 69.1 m / 226 ft 5 in Height: 68.18ft / 20.78m Wing area: 6759.792 sq.ft. / 628.0 sq.m Wing load : 132.23 lb/sq.ft / 645.00 kg/sq.m Height: 22.0 m / 72 ft 2 in Max take off weight : 893025.0 lb / 405000.0 kg Weight empty : 429975.0 lb / 195000.0 kg Max. weight carried : 463050.0 lb / 210000.0 kg Max. speed : 466 kt / 863 km/h / 537mph Landing speed : 132 kt / 245 km/h Cruising speed : 445 kt / 825 km/h Service ceiling : 39370 ft / 12000 m Range w/max.fuel: 16500 km / 10253 miles Range w/max.payload: 4500 km / 2796 miles T/O run: 1200 m. Ldg run: 800 m. Crew: 6 Capacity: 88 pax. Air refuel: No.
Flight testing of an An-74 develop¬ment of the An-72 Coaler twin-turbofan Stol transport was announced early in February 1984. The An-74 has been developed specifically for use in the Arctic and Antarctic, and may be equipped with an interchangeable landing gear, with skis available for operations from ice and snow. Principal differences apparent in the An-74 are a longer fuselage with a nose-mounted radar, and a redesigned wing. First flown in 1977, the An-72, and the related An-74, only received its airworthiness certificate when the An-74TK was certified by Aeronautical Register on 2 August 1991. The An-74 was also produced at Kharkov from December 1989.
Antonov An-74TK-100C RA-74006
Production of An-74 also started by Polyot Industrial Association at Omsk, Russia, in 1993 (assisted by Progress at Arsenyev); first Polyot aircraft (RA-74050) was flown 25 December 1993.
An An-72P maritime patrol version was demonstrated 1992 and development of the An-74-200 and An-74TK-200 by Antonov started 1995. The An-74TK-300 is basically an An-74TK-200 with underslung engines. The An-88 is a tactical battlefield surveillance aircraft based on An-72 (also known as An-72R).
An-74 Coaler Engine: 2 x Lotarev D-36 turbofan. Installed thrust: 127.4 kN. Span: 31.9 m. Length: 28.7 m. MTOW: 34,500 kg. Payload: 10,000 kg. Cruise speed: 550 kph. Ceiling: 10,500 m. T/O run: 470 m. Range/payload: 3300 km with 5000 kg.
Originating as private venture military transport based on stillborn An-60 64-73 seat civil airliner designed to meet 1967 specification, the revised design, following issue of military requirement in 1968, included relocation of engines above wings.
Two static test airframes, and two prototype An-72 were built at Kiev. The first (SSSR-197744) flew on 31 August 1977. Intended to replace the turboprop powered An 26 in Aeroflot service, its high lift devices and multi wheel landing gear make it suitable for operation from unprepared airfields with snow or ice covering and accommodate about 52 passengers. Overwing engines exhaust over the wing and trailing edge devices, to increase lift at low airspeeds. The NATO named Coaler is designed for rough-field operations and has a rear cargo door/ramp. A production order was placed in December 1980 for an improved An-72A version, when manufacture was transferred to Kharkov, Ukraine, where first production An-72 flew 22 December 1985. The An-72, and the related An-74, only received its airworthiness certificate in 1991. By mid-1992, about 50 were in industrial service, although none with Aeroflot. The An-72 platform went on to spawn other variants that included maritime surveillance An-72P model, the An-71 “Madcap” AEW model and the An-74 “improved Coaler” upgraded engines and a conventional engine mounting. The An-72P armed surveillance and maritime patrol aircraft was developed in conjunction with Israeli Aircraft Industries and featured revised cockpit glass design, specialized Elta radar, electronic warfare systems and long range day/night observation equipment and systems.
The An-74 is a civil development of the An-72.
Engine: 2 x turbo-jet Lotarev D-30, 62.8kN Length: 26.6 m / 87 ft 3 in Height: 8.2 m / 26 ft 11 in Take-off weight: 26500-30500 kg / 58423 – 67241 lb MTOW increased: 72,751 lb (33 000 kg) Max useful load: 22,046 lb (10 000 kg) Wingspan: 25.8 m / 84 ft 8 in Cruise speed: 720 km/h / 447 mph Ceiling: 11000 m / 36100 ft Range w/max.fuel: 3200 km / 1988 miles Range w/max.payload: 1000 km / 621 miles Range 16,534 lb (7500 kg) useful load: 1,243 mls (2000 km) Crew: 2-3 Passengers: 32
An-72 (Coaler-C) Engines: 2 x Lotarev D-36 turbofan, 14,330lbs thrust Length: 94.16ft (28.7m) Wingspan: 104.66ft (31.90m) Height: 28.38ft (8.65m) Empty Weight:41,998lbs (19,050kg) Maximum Take-Off Weight:76,059lbs (34,500kg) Maximum Speed: 438mph (705kmh; 381kts) Maximum Range: 497miles (800km) Service Ceiling: 125,246ft (38,175m)
An-72P Armament: 1 x 23mm gun pod, 2 x UB-23M rocket launcher system 4 x 220lb internally-held bombs Accommodation: 3
An AEW plane based on An-72 transport plane, the first prototype flew on July 12, 1985. A small tactical airborne early warning and control aircraft with rotating radome above tailfin, the program was canceled with no production orders. NATO reporting name ‘Madcap’.
An-71 Engine: 2 x D-436K turbofans, 7500kg + 1 x RD-38A, 2900kg Wingspan: 31.89 m / 104 ft 8 in Length: 23.50 m / 77 ft 1 in Height: 9.20 m / 30 ft 2 in Max. Speed: 650 km/h / 404 mph Cruise Speed: 530 km/h / 329 mph Ceiling: 10800 m / 35450 ft Crew: 6
The development of the An-70 program began in 1975 but the collapse of the Soviet Union effectively stopped the funding of most major new programs. The An-70 has the high wing and tail loading ramp for a tactical freight aircraft and uses contra-rotating propfans. Each propfan has contra-rotating propellers; the front has eight composite blades, the rear just six.
A new propfan medium-size wide-body short take-off and landing transport aircraft intended to replace An-12, the first flight was achieved on December 16, 1994 but the first prototype crashed on 10 February 1995 after colliding with its An-72 chase plane. Construction of a second prototype was completed, which began flight testing at Gostomel airport in Ukraine on April 24, 1997.
Engine: 4 x D-27 propfans, 10300kW Take-off weight: 130000 kg / 286602 lb Wingspan: 44.06 m / 144 ft 7 in Length: 40.25 m / 132 ft 1 in Height: 16.1 m / 52 ft 10 in Cruise speed: 750-800 km/h / 466 – 497 mph Ceiling: 12000 m / 39350 ft Range: 7250 km / 4505 miles Range w/max.payload: 1350 km / 839 miles Maximum payload: 47 tons. Crew: 3-5
The Antonov An-38 is a stretched and upgraded version of Antonov’s earlier An-28. It is a twin-engined turboprop transport aircraft, designed by the Antonov Design Bureau in Kyiv, Ukraine. Production is in Novosibirsk, Russia, but some crucial parts are also made in Ukraine and Belarus. It first flew in 1994, and received international flight certification in April 2000. A total of 11 were built and 2 remain in airline service as of August 2019.
Impetus for a stretch of the Antonov An-28 design began with a 1989 sales tour in India, where it became clear that a significant market existed for an aircraft similar to the An-28, but with seating in the 25–30 seat range. The design was approved a year later, and was displayed at the 1991 Paris Air Show as a model.
The An-38 is of a similar design to the older An-28, featuring the same wings and tail; but it has a longer fuselage and includes several enhancements, such as higher fuel efficiency, increased comfort (cabin and cockpit), and decreased internal noise, coupled with better sound insulation. Other improvements include an increase in passengers to 27, thanks to an increase in maximum payload to 2,500 kg (5,500 lbs), as well as a maximum speed of 405 km/h (250 mph). Its design also enables it to operate in adverse conditions—it is equipped with weather radar, sophisticated navigational systems, and low pressure tires that allow it to operate from primitive, unpaved and icy airfields. Furthermore, the aircraft is more resistant to stalling at high angles of attack and is stable and maneuverable with ice on the wing and tail assembly.
As of August 2019, 2 Antonov An-38 aircraft remain in airline service with ALROSA. Recent reviews suggest only one remains in service in 2021.
An-38-100 Powerplant: 2 × Honeywell TPE331-14GR-801E turboprop, 1,118 kW (1,499 hp) each Propellers: 5-bladed Hartzell Propeller HC-B5MA, 2.85 m (9 ft 4 in) diameter constant-speed fully-feathering reversible-pitch propellers (or 2x 1,029 kW (1,380 shp) Omsk MKB Mars TVD-20 turboprop engines driving AV-36 propellers) Wingspan: 22.06 m (72 ft 5 in) Length: 15.67 m (51 ft 5 in) Height: 4.6 m (15 ft 1 in) Airfoil: TsAGI R-II-14 (14%) Empty weight: 5,300 kg (11,684 lb) Max takeoff weight: 8,800 kg (19,401 lb) Fuel capacity: 2,210 kg (4,872 lb) Maximum speed: 405 km/h (252 mph, 219 kn) Cruise speed: 380 km/h (240 mph, 210 kn) at 4,200 m (13,800 ft) Range: 1,650 km (1,030 mi, 890 nmi) with 9 passengers + 45 minutes reserve 1,450 km (900 mi; 780 nmi) with 17 passengers + 45 minutes reserve 600 km (370 mi; 320 nmi) with 27 passengers + 45 minutes reserve Take-off run: 350 m (1,150 ft) Landing run: 270 m (890 ft) Balanced field length: 900 m (3,000 ft) Crew: 2 Capacity: 26-27 passengers / 2,500 kg (5,512 lb) max payload
