ORBIS AVIA SM-92T(E) Praga robust multipurpose high performance turboprop aircraft ... ORBIS AVIA SM-92T(E) Praga The SM-92T(E) Praga is a single-engine high wing all-metal turboprop aircraft with fixed landing gear complying with EASA CS- 23 and FAA FAR 23 requirements. The SM-92T(E) Praga with unpressurized cabin can accommodate up to 7 people including a minimum crew of one. The plane is powered by GE M601 F (with an alternative GE H80/PWC PT-6) turboprop engine with three blade all-metal tractor type propeller AV-803. The aircraft´s conceptual design satisfies requirements for easy operation and maintenance, including operation in difficult climatic conditions of the Arctic Circle and desert areas. The airplane is able to operate anywhere where the ground has sufficient bearing capacity and therefore does not require approved airports for its operation. The aircraft also does not require hangar services. Specially designed high-quality aerodynamic wing profile allows the aircraft to operate within huge range of speed. Adequa- tely large control surfaces allow operation within huge range of values, all that resulting in a positive assessment of the plane´s user-friendliness and safety. The advanced avionics technology provides a more reliable system with greater dispatch reliability and ensures simplicity and safety to the cockpit. The aircraft is equipped by Garmin two-display system with 10 inch flat-panel LCDs interchangeable for use as either a primary flight display (PFD) or multi-function display (MFD) as standard flight deck. With the right equipment configuration, the system is capable of presenting flight instrumentation, navigation, weather, terrain, traffic and engine data on large-format, high-resolution displays. 1 „Perfect for parachuting ...” 2 „Take off to land (time of Cycle) 3 Advantages 4 Aircraft mission configurations no need for hangar ... • Passenger transport: accommodates up to 6 passengers with luggage • Cargo transport: maximum payload 900 kg/1984 lb • Ambulance/medevac: 2 stretchers, 4 seats, 1 medical attendant seat • Photogrammetric works • Pilot Training • Towing of gliders and banners • Agricultural aerial work • Monitoring flights 5 Dimensions & Geometry 14 960 Length ......................................................... 32.72 ft / 9.974 m Height in flight .............................................13.72 ft / 4.182 m Wing span .................................................... 49.1 ft / 14.96 m 9 974 Wing area ............................................. 219.6 sq ft / 320.4 m Cabin width ................................................. 4.13 ft / 1.26 m 4 182 Cabin height .................................................. 3.9 ft / 1.2 m Cabin length ..............................................11.14 ft / 3.4 m Passenger door length ............................... 3.93 ft / 1.2 m Passenger door height .............................. 3.61 ft / 1.1 m 2 700 3 840 6 Straight lines, simplicity and the lowest price ... beautiful ... robust ... fast ... low-cost ... variable ... high-performance ... universal ... 7 ... beauty, joy, safety... 8 Performance, Benefits, Weight & Payload DistanceDistance to clear 15 m (50(50 ft)ft) is 506 m ((11 660 fft)t) Ground roll: 197 m (646 ft) Performance Maximum cruise speed KIAS ..........................................162 kt .......300 km/h Stall speed KIAS ............................................................... 54 kt .......100 km/h 1515 m Take off distance ..........................................................1 660 ft ..............506 m (50(50 ft)ft) Landing distance .........................................................1 444 ft .............440 m Climb time to H 4000 m at MTOW ................................12 min Rate of climb at sea level ...................................1 860 ft/min ............9,5 m/s Rate of climb at 10 000 ft ....................................1 530 ft/min ............7,8 m/s Endurance ..................................................................... 7 hours Distance to clear 15 m (50(50 ft) is 440 m (1 444 ft)ft) GroundGround roll: 127 m (417(417 ft) Aircraft Benefits 15 m • STOL performance (50(50 ft)ft) • Multi-purpose airplane • Low operating and maintenance costs • Rugged landing gear • Robust and solid metal structure • Structure and equipment is resilient to weather and climate conditions Weight & Payload • Big side cargo and paratroop slinding door MTOW .........................................................................6 614 lb / 3 000 kg • Easy conversion between various configurations Maximum landing weight ........................................ 6 614 lb / 3 000 kg • Highly reliable turboprop powerplant Maximum useful load .................................................. 1 984 lb / 900 kg • Long endurance Cargo pod (passenger luggage) up to ........................662 lb / 300 kg • Hot section inspection of engine – NONE (GE M601F/H80 engines only) Max. fuel load (without tip tanks) ................................... 206 gal / 786 l • Engine callendar limit – N/A Max. fuel load (with tip tanks) ....................................... 311 gal / 1180 l 9 10 Simple and low-cost maintenance ... Powerplant & Cocpit Engine The GE M601 series engine (580 kw/ 777 shp) is 840 thermodynamic SHP, light -weight, reliable, reverse-flow, two-shaft, freepower turbine turboprop engine. With more than 17 million flight hours on more than 30 applications since its intro- duction in 1975, the M601 has a proven record of durability, reliability and ease of maintenance. The H80 turboprop engine (597 kw/ 800 shp) family incorporates GE‘s 3-D aerody- namic design techniques and advanced materials to create a powerful, fuel-effi- Standard VFR DAY / NIGHT Equipment cient, durable engine with no recurrent fuel nozzle inspections and no hot section 2x Garmin GDU 1040, Transponder GTX 33, Audio panel GMA 1347, Integrated inspection. The engines feature a service life of 3,600 flight-hours or 6,600 cycles avionics unit GIA 63 W, Air data computer GDC 74A, Air temperature probe GTP between overhauls. The H80 engine family also offers a standard auto start and 59, AHRS GRS 77, Magnetometer GMU 44, ADF receiver KR 87, ELT Kannad 406 AF, limiting unit to simplify engine start-up as well as a choice of propeller governors Trilogi ESI 2000, Stall warning annunciator, cabin LED lights. to allow customers flexibility in propeller selection. Propeller Engine instruments Hydraulic, single acting. Three-blade tractor-type constant speed propeller AV-803 Engine limiters and auto start system, generator and propeller speed indicators, with reversing and feathering capability, diameter 106 in (2.7 m). ITT indicator, oil temperature and press indicators, fuel management system FS-450. 11 Cargo / Aerial Works 12 Options Auxiliary wing tanks Cargo pod Weather radar • Paratrooper kit • Autopilot • Deicing system • Auxiliary wing tanks • Oxygen system • Medevac • Floats • Custom-designed exterior • Towing hitch Medevac Towing hitch 13 Amphibious Floats Examples of color schemes Petrol blue Red & White Blue & White Note: Customized color schemes with price on request. 14 Also great on water ... 15 Fire patrolling & fighting 16 SEARCH AND RESCUE PATROL SURVEILLANCE BORDER CONTROL SPECIAL OPERATIONS Orbis Avia SM-92 T(E) Praga & adrenaline 18 19 History of the Orbis Avia SM-92 T(E) Praga In November 2008, the aircraft SM-92T received Type Certificate by MAK (Interstate Aviation Committe, Russia) according to AP-23 regulation, which is equivalent to FAA FAR-23, (Normal Category.) Since 2008, several SM-92T aircraft have been produced in the Smolensk Aircraft Plant (SMAZ) serial production plant and are still in operation. In 2015, the Orbis Avia company together with partners launched EASA validation of the MAK Type Certificate under EASA/CS-23 and then consequently under FAA/FAR-23. Currently, Orbis Avia is the holder of EASA SM-92T(E) Praga Type Certificate as well as approvals EASA DOA (Design Organisation Approval) and POA (Production Organisation Approval.) The SM-92T aircraft is being produced by Orbis Avia at it´s Production and Maintenance Center at the Hradec Králové Airport, Czech Republic. EASA certified SM-92T(E) Praga aircraft are available to customers as of early 2016. Certification Status 2008 - MAK Russia, AP-23 2016 - EASA CS-23 2017 - FAA, FAR-23 world beneath our wings ... Board: Nademlejnská str. 651/7, 190 00 Prague 9, Czech Republic Production and Maintenance Centre: Hradec Králové Airport (LKHK), HANGAR No. 74, 503 41 Hradec Králové Czech Republic e-mail: [email protected] www.orbisavia.cz Sales: PRAGA- Export s.r.o. U Císařské cesty 219, 103 00 Praha 10 - Benice, Czech Republic e-mail: [email protected] www.pragaglobal.cz SINCE 1907.