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  • SAI
    research and manage static and flight certification test programmes Works at Vitulazio CE are being augmented by a new plant at San Salvatore Telesino BN Factory floor area 1 520 m 2 16 350 sq ft workforce six Contact Details Address Via Fillipo Bottazzi 38 I 80126 Napoli Italy Tel 39 08 18 49 63 74 Fax 39 08 18 82 97 82 A B C D E F G

    Original URL path: http://www.aviamarket.org/directory/s/1401-sai.html (2016-02-13)
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  • SHANGHAI AVIATION INDUSTRY CORPORATION
    Institute SARI Shanghai Aero Engine Manufacturing Factory and Shanghai International Aero Technology SAIC and SARI are taking part in studies for the ARJ21 regional jet being developed by ACAC Subcontract work includes components for the ATR 72 and Boeing 737 757 Contact Details Address 2668 Zhongshan North Road Shanghai 200063 Tel 86 21 62 57 33 51 Fax 86 21 62 57 33 50 E mail This e mail address

    Original URL path: http://www.aviamarket.org/directory/s/81-saic.html (2016-02-13)
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  • SHIJIAZHUANG AIRCRAFT INDUSTRY CORPORATION
    the only company now regularly building new examples of this long serving biplane Became part of Xian Aircraft Industrial Group July 1992 but relocated within AVIC II in 1999 reorganisation Latest venture is a TB20 Trinidad lookalike known as the LE 500 Little Eagle Occupies 46 ha 113 7 acre site including over 100 000 m 2 1 076 400 sq ft of covered space Workforce of 2 803 in

    Original URL path: http://www.aviamarket.org/directory/s/82-saic.html (2016-02-13)
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  • GLASS STOLGLASS SG70
    and manual Junkers ailerons and flaps No aerodynamic balances on tail surfaces STRUCTURE Generally of glass fibre LANDING GEAR Tricycle type fixed Cantilever main legs with hydraulic brakes Speed fairings on all wheels POWER PLANT One flat four piston engine option of 73 5 kW 98 6 hp Rotax 912 S or 84 5 kW 123 3 hp Rotax 914 each driving a three blade propeller Fuel capacity 76 litres

    Original URL path: http://www.aviamarket.org/reviews/civil-aircraft/1119-sg70.html (2016-02-13)
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  • Cirrus SR20 and SRV
    July 2003 when demonstrator N936CD c n 1337 shown Specification and performance generally as for SR20 except cruising speed at 75 per cent power 150 kt 278 km h 173 mph range with reserves 634 n miles 1 174 km 729 miles max range 865 n miles 1 602 km 995 miles CUSTOMERS Orders for 552 received by July 2001 Total of 53 delivered in 2001 105 in 2002 and 86 in the first nine months of 2003 By December 2002 267 had been registered COSTS SR20 US 229 700 SRV US 189 900 both 2003 DESIGN FEATURES Low wing composites construction monoplane with upturned wingtips mid set tailplane with horn balanced elevators horn balanced rudder fixed tab on starboard aileron First certified aircraft with ballistic parachute as standard equipment Cirrus Airplane Parachute System or CAPS fitted just aft of baggage compartment Wing dihedral 4 0 30 STRUCTURE Composites monocoque one piece main spar attached to fuselage on two locations under front seats spar carry through attached to fuselage side walls Wing upper and lower surfaces bonded to spars and ribs forming torsion box All flying control surfaces are flush riveted aluminium Fin integral with fuselage one piece tailplane Cabin incorporates composites roll cage acrylic windscreen and windows FLYING CONTROLS Conventional and manual Actuation by pushrods cables and bellcranks Electric trim tabs for roll and pitch activated through springed centring devices ground adjustable rudder tab Three position flaps LANDING GEAR Fixed tricycle composites cantilever main legs single wheels and speed fairings throughout Main tyres 15x6 00 6 nosewheel tyre 5 00 5 Hydraulic caliper disk brakes on mainwheels Castoring nosewheel POWER PLANT One 149 kW 200 hp Teledyne Continental IO 360 ES flat six engine driving a two blade Hartzell BHC J2YF 1BF F7694 propeller three blade 1 88 m 6 ft 2 in PHC J3YF 1MF F77392 1 propeller optional Single fuel tank in each wing each of 113 5 litres 30 0 US gallons 25 0 Imp gallons capacity of which 212 litres 56 0 US gallons 46 7 Imp gallons usable Oil capacity 7 6 litres 2 0 US gallons 1 7 Imp gallons ACCOMODATION Four 26 g energy attenuating seats in pairs two forward hinged passenger doors Dual controls Baggage compartment door aft of cabin on port side of fuselage Interior reflects modern motorcar design SYSTEMS Single axis S Tec System 20 autopilot with GPS dual axis S Tec System 30 and Fifty FiveX optional 24 V DC power system with 28 V 75 A alternator and 24 V 10 Ah battery 12 V power port AVIONICS Garmin integrated package Comms GNS 430 colour GPS com nav IFR approach certified GPS plus back up GNS 250XL GPS com GMA 340 audio panel and GTX 327 transponder Options include GNS 420 colour GPS com and or additional GNS 430 back up IFR GPS Flight Garmin GI 106 GPS VOR LOC GSI S Tec System FortyX autopilot Options include Goodrich Stormscope WX 500 S Tec System FiftyX or

    Original URL path: http://www.aviamarket.org/reviews/civil-aircraft/91-cirrus-sr20-and-srv.html (2016-02-13)
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  • SHANGHAI SIKORSKY AIRCRAFT COMPANY
    and 333 with certification and marketing assistance from Sikorsky shareholding SLEC 51 per cent Sikorsky 49 per cent Contact Details Address 3115 Chang Zhong Road Shanghai 200436 Tel 86 21 66 50 74 76 and 56 68 08 99 Fax 86 21 66 50 74 67 E mail 1 This e mail address is being protected from spambots You need JavaScript enabled to view it E mail 2 This e

    Original URL path: http://www.aviamarket.org/directory/s/221-ssac.html (2016-02-13)
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  • Sukhoi Su-24M
    sight navigation system produced during 1971 1983 The Su 24 swing wing prototype made its maiden flight on 17 January 1970 the Su 24M prototype on 29 June 1977 The Su 24Ms had been series produced at the Novosibirsk based NAPO plant during 1979 1983 A total of about 1 400 aircraft of all versions was produced The Su 24 was used as the base for deriving the following versions the Su 24MR air reconnaissance frontline aircraft 1980 Su 24MP ECM aircraft 1980 Su 24MK frontline bomber export version 1987 which was exported to Algeria Iraq Libya and Syria Presently the Su 24M is the mainstay of the Russian Air Force tactical bomber fleet The aircraft also is operated by naval strike air regiments of the Russian Navy s air branch 2001 witnessed the commencement of a Su 24 upgrade programme for the Russian Air Force under which the bombers are going to be retrofitted with advanced avionics to enhance navigation accuracy and reducing sighting errors Basic specifications Length m 24 59 Wing span m 10 37 17 64 Wing area sq m 51 02 55 17 Empty weight kg 22 300 Normal take off weight kg 35 900 Max

    Original URL path: http://www.aviamarket.org/reviews/military-aircraft/570-sukhoi-su-24m.html (2016-02-13)
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  • Sukhoi Su-26
    has been in production since 1988 with the Sukhoi Advanced Technologies company Since 1989 it has been exported to the United States and other nations as the Su 26MX version A total of eight prototypes and 65 production planes have been built Upgraded version of the Su 26 the Su 26M3 with new 420hp M 9F engine was prepared to take part in the World aerobatics championship in 2003 Basic

    Original URL path: http://www.aviamarket.org/reviews/civil-aircraft/269-sukhoi-su-26.html (2016-02-13)
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