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TMM Avia T-10 Avia-Tor

The TMM Avia T-10 Avia-Tor is a single engine two seat Ukrainian light aircraft, with a high wing and transparent blister cabin doors for extra visibility, designed to be robust enough for a range of applications.

T-10 Avia-Tor
Role Light aircraft
National origin Ukraine
Manufacturer TMM-Avia, Kharkiv
Designer Serhiy Ryabikov
First flight 2002
Status In production (2015)
Number built at least 6

Design Edit

The Avia-Tor is a conventionally arranged single engine high wing light aircraft, seating two side-by-side. It was designed as a sport machine, with applications as a basic trainer, agricultural sprayer, patroller and air photographer.[1][2]

It has constant chord wings built around two wooden spars with fibreglass ribs and synthetic fabric covering. They are braced from the lower fuselage with V-struts on each side, assisted by further intermediate bracing. Three position (0°, 10° and 40°) flaps are fitted. The square sided fuselage has a stainless steel truss structure and is fabric covered apart from the glass fibre engine cowling and cabin roof. The two upward hinged cabin doors are entirely transparent blisters for optimum visibility. The empennage is formed from steel tubes with fibreglass ribs, all fabric covered. The tailplane is wire braced from above to the fin with a pair of wires on each side and similarly below to the lower fuselage. The elevators are mass balanced and the port side one has a trim tab. The rudder also has a tab. Wings and tailplane can be easily folded for transport.[1][2][3][4]

The Avia-Tor normally uses a fixed tricycle undercarriage, though floats or skis are options. Each mainwheel is supported by a V-pair of struts joined to the lower fuselage longerons and with a half-axle from wheel to the central fuselage. A MVEN KS-500-2 Cobra ballistic parachute recovery system is standard.[1]

Development Edit

The first prototype flew in 2002 and was followed by four more T-10 pre-production aircraft. These were followed by a batch of production T-10M machines for purchase as complete aircraft. The production of kits may follow.[1]

The T-10M has some changes to undercarriage and fin, plus a change of engine. The main gear sprung element has been moved from the half-axle to the rearward V strut and the early castoring nosewheel replaced with a steerable system with a simpler single leg. The fin of the T-10M is more angular and narrower than that of the T-10 and incorporates a triangular fillet. The T-10s are powered by 60 kW (80 hp) Jabiru 2200s, the T-10Ms by 74 kW (100 hp) Rotax 912S flat four engines.[3]

Operational history Edit

Four of the five T-10 pre-production aircraft are currently on sale as T-10 Frigates.[3] All five T-10s and one T-10M aircraft remain on the Ukrainian private aircraft register in mid-2010. [5] Ukrainian certification was anticipated in 2009.[1]

Engenious Aerospace Ltd (EAL) has the Indian dealership for the T-10.[6]

Specifications Edit

Data from Jane's All the World's Aircraft 2010/11[1]

General characteristics

  • Capacity: 2
  • Length: 6.355 m (20 ft 10 in)
  • Wingspan: 9.13 m (29 ft 11 in)
  • Height: 2.24 m (7 ft 4 in)
  • Wing area: 13.70 m2 (147.5 sq ft)
  • Airfoil: TsAGI R-IIIa 12%
  • Empty weight: 315 kg (694 lb) including ballistic rescue parachute
  • Max takeoff weight: 550 kg (1,213 lb)
  • Powerplant: 1 × Rotax 912S flat four , 73.5 kW (98.6 hp)
  • Propellers: 2-bladed fixed pitch, wooden, 1.86 m (6 ft 1 in) diameter

Performance

  • Maximum speed: 190 km/h (120 mph, 100 kn)
  • Cruise speed: 150 km/h (93 mph, 81 kn)
  • Stall speed: 65 km/h (40 mph, 35 kn) flaps down
  • Never exceed speed: 255 km/h (158 mph, 138 kn)
  • Range: 700 km (430 mi, 380 nmi)
  • Service ceiling: 3,000 m (9,800 ft) maximum certified altitude
  • g limits: +4/-2
  • Rate of climb: 6.2 m/s (1,220 ft/min) pilot only

References Edit

  1. ^ a b c d e f Jackson, Paul (2010). Jane's All the World's Aircraft 2010-11. Coulsdon, Surrey: IHS Jane's. p. 614. ISBN 978-0-7106-2916-6.
  2. ^ a b Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, page 82. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X
  3. ^ a b c "Official site". Retrieved 2010-11-16.
  4. ^ Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, page 85. Flying Pages Europe SARL, 2015. ISSN 1368-485X
  5. ^ Partington, Dave (2010). European registers handbook 2010. Air Britain (Historians) Ltd. p. 513. ISBN 978-0-85130-425-0.
  6. ^ "Engenious Aerospace Ltd". Retrieved 2016-12-21.

avia, avia, single, engine, seat, ukrainian, light, aircraft, with, high, wing, transparent, blister, cabin, doors, extra, visibility, designed, robust, enough, range, applications, avia, torrole, light, aircraftnational, origin, ukrainemanufacturer, avia, kha. The TMM Avia T 10 Avia Tor is a single engine two seat Ukrainian light aircraft with a high wing and transparent blister cabin doors for extra visibility designed to be robust enough for a range of applications T 10 Avia TorRole Light aircraftNational origin UkraineManufacturer TMM Avia KharkivDesigner Serhiy RyabikovFirst flight 2002Status In production 2015 Number built at least 6 Contents 1 Design 2 Development 3 Operational history 4 Specifications 5 ReferencesDesign EditThe Avia Tor is a conventionally arranged single engine high wing light aircraft seating two side by side It was designed as a sport machine with applications as a basic trainer agricultural sprayer patroller and air photographer 1 2 It has constant chord wings built around two wooden spars with fibreglass ribs and synthetic fabric covering They are braced from the lower fuselage with V struts on each side assisted by further intermediate bracing Three position 0 10 and 40 flaps are fitted The square sided fuselage has a stainless steel truss structure and is fabric covered apart from the glass fibre engine cowling and cabin roof The two upward hinged cabin doors are entirely transparent blisters for optimum visibility The empennage is formed from steel tubes with fibreglass ribs all fabric covered The tailplane is wire braced from above to the fin with a pair of wires on each side and similarly below to the lower fuselage The elevators are mass balanced and the port side one has a trim tab The rudder also has a tab Wings and tailplane can be easily folded for transport 1 2 3 4 The Avia Tor normally uses a fixed tricycle undercarriage though floats or skis are options Each mainwheel is supported by a V pair of struts joined to the lower fuselage longerons and with a half axle from wheel to the central fuselage A MVEN KS 500 2 Cobra ballistic parachute recovery system is standard 1 Development EditThe first prototype flew in 2002 and was followed by four more T 10 pre production aircraft These were followed by a batch of production T 10M machines for purchase as complete aircraft The production of kits may follow 1 The T 10M has some changes to undercarriage and fin plus a change of engine The main gear sprung element has been moved from the half axle to the rearward V strut and the early castoring nosewheel replaced with a steerable system with a simpler single leg The fin of the T 10M is more angular and narrower than that of the T 10 and incorporates a triangular fillet The T 10s are powered by 60 kW 80 hp Jabiru 2200s the T 10Ms by 74 kW 100 hp Rotax 912S flat four engines 3 Operational history EditFour of the five T 10 pre production aircraft are currently on sale as T 10 Frigates 3 All five T 10s and one T 10M aircraft remain on the Ukrainian private aircraft register in mid 2010 5 Ukrainian certification was anticipated in 2009 1 Engenious Aerospace Ltd EAL has the Indian dealership for the T 10 6 Specifications EditData from Jane s All the World s Aircraft 2010 11 1 General characteristicsCapacity 2 Length 6 355 m 20 ft 10 in Wingspan 9 13 m 29 ft 11 in Height 2 24 m 7 ft 4 in Wing area 13 70 m2 147 5 sq ft Airfoil TsAGI R IIIa 12 Empty weight 315 kg 694 lb including ballistic rescue parachute Max takeoff weight 550 kg 1 213 lb Powerplant 1 Rotax 912S flat four 73 5 kW 98 6 hp Propellers 2 bladed fixed pitch wooden 1 86 m 6 ft 1 in diameterPerformance Maximum speed 190 km h 120 mph 100 kn Cruise speed 150 km h 93 mph 81 kn Stall speed 65 km h 40 mph 35 kn flaps down Never exceed speed 255 km h 158 mph 138 kn Range 700 km 430 mi 380 nmi Service ceiling 3 000 m 9 800 ft maximum certified altitude g limits 4 2 Rate of climb 6 2 m s 1 220 ft min pilot onlyReferences Edit a b c d e f Jackson Paul 2010 Jane s All the World s Aircraft 2010 11 Coulsdon Surrey IHS Jane s p 614 ISBN 978 0 7106 2916 6 a b Bayerl Robby Martin Berkemeier et al World Directory of Leisure Aviation 2011 12 page 82 WDLA UK Lancaster UK 2011 ISSN 1368 485X a b c Official site Retrieved 2010 11 16 Tacke Willi Marino Boric et al World Directory of Light Aviation 2015 16 page 85 Flying Pages Europe SARL 2015 ISSN 1368 485X Partington Dave 2010 European registers handbook 2010 Air Britain Historians Ltd p 513 ISBN 978 0 85130 425 0 Engenious Aerospace Ltd Retrieved 2016 12 21 Retrieved from https en wikipedia org w index php title TMM Avia T 10 Avia Tor amp oldid 993822864, wikipedia, wiki, book, books, library,

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