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  • LVIV STATE AIRCRAFT REPAIR PLANT STATE ENTERPRISE OF MINISTRY OF DEFENCE OF UKRAINE
    repair and modernization of the aircraft MiG 21 MiG 23 MiG 27 MiG 29 of all versions The Enterprise holds the well developed base and capable professional staff able to carry out the high quality repair of the aircraft of MiG type in the shortest possibly time The high level of quality of repair is guaranteed operating on the enterprise since 1978 Quality Management System which meets the requirements the

    Original URL path: http://www.aviamarket.org/directory/l/802-lviv-state-aircraft-repair-plant-state-enterprise-of-ministry-of-defence-of-ukraine.html (2016-02-13)
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  • Myasishchev M-55
    aerial monitoring of construction sites The M 55 can fly six hour plus high altitude missions with a 1 500 2 000kg equipment payload used for direct measurements and analysis of the ambient environment as well as for remote chemical and microphysics research at a range of several kilometres Within one hour the aircraft can monitor at least 100 000 sq km The M 55 s unique altitude characteristics and excellent lifting capacity make it a valuable asset for high atmospheric research Its two engines provide enhanced flight safety with one engine failed the M 55 can continue flight at an altitude of 12 14 km and safely land at home base The M 55 can be operated from airfields situated at up to 4 000 m above the sea level in ambient temperatures of 40 to 60oC EQUIPMENT The M 55 is a versatile high altitude air platform with a wide mission scope The overall volume of its equipment compartment equals 11 cu m Optional external containers can house extra 1 2 cu m of equipment The aircraft s baseline design and the capabilities of its systems and power plant ensure normal operation of radar optical and radio relay

    Original URL path: http://www.aviamarket.org/reviews/civil-aircraft/146-m-55-geofizika-high-altitude-aircraft.html (2016-02-13)
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  • XAC MA60
    year period Launch operator Sichuan Airlines five ordered plus five on option introduced first leased example B 3426 into revenue service August 2000 Other reported orders by March 2003 from Changan Airlines two China Northern five Wuhan Airlines three and Lao Aviation three Of these 18 six said to be in airline operation at that time Most of first 60 expected to be of improved MA60 100 standard COSTS Approximately US 11 million 2002 DESIGN FEATURES Further upgrade of Y 7 series mainly through Western engines and avionics and improved passenger comfort incorporates best features of earlier Y7 200A and B programmes Airframe life 40 000 hours 25 000 cycles or 25 years Non swept high mounted wings with 2 12 12 anhedral on tapered outer panels basically circular section fuselage sweptback fin and rudder 9 dihedral on tailplane twin ventral strakes under tailcone Wing sweepback 6 50 at quarter chord of outer panels incidence 3 FLYING CONTROLS Conventional mechanical Mass balanced servo compensated ailerons with electrically actuated trim tabs tab in each elevator electric trim servo tab in rudder Hydraulically actuated single slotted inboard and double slotted outboard trailing edge flaps landing deflection 30 STRUCTURE Conventional light alloy two spar wing with spot welded skins bonded welded semi monocoque fuselage LANDING GEAR Retractable tricycle type with twin wheels on all units Hydraulic actuation with emergency gravity extension Multidisc carbon brakes on mainwheels hydraulically steerable 45 and castoring nosewheel unit POWER PLANT Two 2 051 kW 2 750 shp Pratt Whitney Canada PW127J PW127G in cargo version turboprops each driving a Hamilton Sundstrand 247F 3 four blade composites fully reversible scimitar propeller Fuel in integral wing tanks immediately outboard of nacelles and bag type tanks in centre section total usable capacity 5 200 litres 1 374 US gallons 1 144

    Original URL path: http://www.aviamarket.org/reviews/civil-aircraft/1118-ma60.html (2016-02-13)
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  • Aermacchi MB-326
    for two in tandem ARMAMENT MB 326G Provision for up to 1815kg 4000lb of armaments including bombs rockets and gun pods on six underwing pylons OPERATORS Argentina Australia Brazil Dubai Ghana Italy Paraguay South Africa Togo Tunisia Zaire Zambia HISTORY Macchi initiated design of this classic two seat jet trainer in 1954 against an Italian Air Force requirement The 326 was designed by Dr lng Ermano Bazzochi responsible for the B in the MB prefix and a prototype flew for the first time on December 10 1957 The prototype MB 326 was powered by a 7 8kN 1750lb thrust Bristol Siddeley later Rolls Royce Viper 8 turbojet and the aircraft was of the same basic configuration of almost every two seat jet trainer to follow it with a low straight wing a single jet engine tandem seating and pleasant handling characteristics Flight testing of the prototype revealed an aircraft that was highly suited to its intended role displaying viceless flying characteristics and relatively snappy performance The aircraft impressed the Italian Air Force which ordered the type into production with the first examples arriving on strength in 1962 The Italian Air Force took delivery of 100 basic 11 1KN 2500lb Viper 11 powered MB 326s including 15 preproduction aircraft and was offered the armed MB 326A with six underwing hardpoints but did not order Similar armed versions were built for other nations though including Ghana MB 326F and Tunisia MB 326B while the Italian airline Alitalia took delivery of four unarmed MB 326Ds Significant orders for the basic Viper 11 model meanwhile came from South Africa and Australia the former taking delivery of 191 most of which were assembled locally by Atlas as Impala Mk 1s the latter 97 MB 326HS the majority of which were built locally by CAC A

    Original URL path: http://www.aviamarket.org/reviews/military-aircraft/462-aermacchi-mb-326.html (2016-02-13)
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  • Aermacchi MB-326K
    000lb DIMENSIONS Wing span 10 85m 35ft 7in with tip tanks 10 15m 33ft 4in without tip tanks length 10 67m 35ft Oin height 3 72 12ft 2in Wing area 19 4m2 208 3sq ft ACCOMMODATION Pilot only ARMAMENT Max payload of 1815kg 4000lb on six hardpoints comprising bombs wire guided AS 12 ASMs Matra R550 Magic AAMs unguided rockets cannon and reconnaissance pods Fixed armament comprises two 30mm DEFA 553 cannon with 125 rounds per gun OPERATORS Dubai Ghana Tunisia Zaire South Africa Impala Mk 2 HISTORY The MB 326K is the most successful single seat development of a two seat jet trainer and has provided a number of third world nations with an effective light attack capability Right from the beginning of the MB 326 jet trainer program its designer Dr lng Ermano Bazzochi intended that the aircraft also be an effective light strike platform and this capability no doubt influenced a number of the two seat MB 326 s customers to order it The two seater proved to be a stable and effective weapons platform and a single seater optimised for light attack became a logical development The single seat MB 326K was developed well into the 326 s career given that the prototype two seater flew in 1957 and the single seat prototype flew on August 22 in 1970 The K was based on the MB 326G which compared to earlier Macchis featured a strengthened airframe and more powerful Viper 20 engine The first K prototype featured the 15 2kN 341 Olb Viper 20 while the second had the more powerful 18 8kN 4000lb Viper Mk 632 43 intended for production aircraft which allowed an increased armament capability compared with two seaters and the fitting of two internal 30mm DEFA cannon The second seat meanwhile gave

    Original URL path: http://www.aviamarket.org/reviews/military-aircraft/463-aermacchi-mb-326k.html (2016-02-13)
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  • Aermacchi MB-339
    46 700ft Ferry range with two drop tanks 2035km 1100nm Combat radius with four Mk 82 bombs hi lo hi 500km 270nm WEIGHTS MB 339A Empty equipped 3125kg 6889lb max takeoff 5895kg 13 000lb MB 339C Empty equipped 3310kg 7297lb max takeoff 6350kg 14 000lb DIMENSIONS MB 339A Wing span over tip tanks 10 86m 35ft 8in length 10 97m 36ft Oin height 3 99m 13ft 1in Wing area 19 3m2 207 7sq ft MB 339C Same except wing span over tip tanks 11 22m 36ft 10in length 11 24m 36ft 11 in ACCOMMODATION Seating for two in tandem ARMAMENT MB 339A Up to 2040kg 4500lb of external stores on six hardpoints including bombs rockets cannon pods Matre anti shipping missiles MB 339AM and Magic and Sidewinder AAMs MB 339C Up to 1815kg 4000lb of external ordnance as above plus Maverick ASMs and Vinten recce pod OPERATORS Argentina Ghana Italy Malaysia New Zealand Nigeria Peru UAE HISTORY As the MB 326 was Aermacchi s most successful postwar design an upgraded successor was a logical development The main change to the airframe was that the forward fuselage was reprofiled to feature stepped tandem cockpits giving the instructor who normally sits in the rear seat greatly improved forward vision Aermacchi also considered a number of new powerplant options including turbofans and twins but settled upon the familiar Viper turbojet for its performance ease of maintenance and lower acquisition cost despite higher fuel consumption The first of two prototypes flew on August 12 1976 since which time the basic aircraft has been developed into a small number of models The base MB 339A has accounted for almost all sales and 101 were delivered to the Italian Air Force some as MB 339PANS fitted with smoke generators for the Italian Air Force s Frecce

    Original URL path: http://www.aviamarket.org/reviews/military-aircraft/464-aermacchi-mb-339.html (2016-02-13)
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  • MOSCOW STATE TECHNICAL UNIVERSITY OF CIVIL AVIATION
    on a wide range of scientific technical humanities and economic directions are carried out MSTUCA is the base of the training methodological amalgamation of higher education establishments which train aviation equipment specialists MSTUCA has a training airfield and radiofield equipped with modern aircraft and radar equipment where classes are conducted under conditions close to real ones MSTUCA is a major research center Students scientific research groups are set up and

    Original URL path: http://www.aviamarket.org/directory/m/811-moscow-state-technical-university-of-civil-aviation-mgtuga.html (2016-02-13)
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  • MOSCOW INSTITUTE OF ELECTRICAL ENGINEERING AND AUTOMATION
    the institute ensures a complete cycle of work including research development tests production and after sales maintenance of a wide range of its products Where aviation is concerned the institute majors in integration of avionics navigation computing systems aut matic control systems aircraft handling systems strapdown platform and guided inertial navigation systems and initial information sensors Based on the technologies mastered and improved in the course of airborne systems development

    Original URL path: http://www.aviamarket.org/directory/m/807-moscow-institute-of-electrical-engineering-and-automation-miea.html (2016-02-13)
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