An aerobatic tandem two seater, the wood TR 200 has been sold since 1996.

Power can be up to 260 hp.

Engine: Lycoming IO-360, 200 hp
Wing span: 7.42 m
Wing area: 9.89 sq.m
MAUW: 870 kg
Empty weight: 570 kg
Fuel capacity: 159 lt
Max speed: 325 kph
Cruise speed: 270 kph
Minimum speed: 95 kph
Climb rate: 11 m/s
Seats: 2
Fuel consumption: 40 lt/hr
Plan price (1998): 5000 Fttc
Kit price (1998): 230 000 Fttc

The Team Tango Tango 2 is an American low-wing composite homebuilt aircraft, marketed as a kit for amateur construction by Team Tango of Williston, Florida. The Tango 2 was developed from the 1983 Aero Mirage TC-2 design.

The Tango 2 and Foxtrot 4 wing uses a constant chord, constant thickness airfoil which gives it gentle, textbook stall characteristics. Wing root first, ailerons last, with no built in twist required. The stall itself is simple with distinctive aerodynamic warning and little to no tendency to drop off. Differential ailerons counteract adverse yaw.

The wing spars are factory assembled. They are a one piece composite I-beam structure that goes from wing tip to wing tip. Both airplanes were designed to 6/-4 G’s and have been successfully tested to 1.5 design limits. Each wing and horizontal stabilizer spar is tested to 6 G’s before it leaves the factory.

All of the fuel is carried in the wings. There is no fuel storage anywhere in the fuselage or engine compartment. Capacitance type fuel probes run the entire length of the wing. This allows accurate fuel quantity readings from full right down to zero, a rarity in many airplanes. Total unusable fuel is less than a pint. The fuel selector is in plain view on the forward console and is easily accessible for switching from left to right. The 57 usg capacity tanks provide a reserve even after a four or five hour flight.

Team Tango uses only FAA approved foam core in the structures. It is more expensive, but compared to other popular foam cores it is the only one that does not create cyanide gas when exposed to flame, is self extinguishing and fuel -proof. The Tango and Foxtrot both feature a dual gull wing canopy system which incorporates a reinforced roll bar. Both can cruise at 200+ mph, have a range over 1400 s.m., carry over 100 pounds of baggage, and operate off a grass strip.

The fuselage sits level in cruise flight which is three degrees lower than the ground attitude. The molded fiberglass seats put the pilot and passenger in a semi-reclining position leaning back approximately 30 degrees. The Tango and Foxtrot are 44 and 46 inches wide. Various antennas are installed into the fuselage during the lay-up process, when it is easy. The instrument panel is divided into three sections. This allows easier installation and access for maintenance and upgrades. The fuselages use quarter inch foam core that is reinforced at the horizontal stab attach points and up into the vertical stab.

A build center is available to build your airplane at the factory, guided and instructed by the staff, and that expertise is included in the price of your aircraft. The seat installation is adjustable for leg room and height as well as recline. The airframe can be customized. The wing can be longer to reduce wing loading, reduce stall speed, climb better at lower airspeeds and have greater high altitude performance. We use ½” foam core in and around the doors ensure stiffness so they won’t pull away from the fuse in flight and cause air leaks or allow rain to enter the cabin. A vinyl ester resin in the composite is a safer and less toxic alternative that won’t induce an allergic reaction and is pleasant to work with.

Tango 2 is a side by side two seat composite aircraft that can be flying in as little as 1000 hours of build time. Current aircraft have been built with engines ranging from the 150 HP O-320 Lycoming to the Geared Drives 205 hp EcoTech 2.2 liter supercharged Cobalt SS power package, with the most popular the 180 hp IO-360 Lycoming. Cruise speeds run from 170 knots with the 150 hp/fixed pitch combo to 195 knots on a 200 hp Lycoming equipped with a constant speed prop. Both the fuselage and the main wing and horizontal spars are molded as single pieces for exceptional strength and ease of building.

The Tango XR has increased structural strength and upgraded useful load. The Tango XR is a two place, 200+ MPH guaranteed, composite built aircraft, with a 90 US gallon tank.

First flown in 1996, eighteen Tango 2 had been built to December 2013, plus one Tango XR by December 201.

The design was further developed into a four-seat aircraft, the Team Tango Foxtrot.

In 2000, the factory claim was that an airframe could be built by the “average” builder in 650-700 hours using Tango’s “EZ-Buildo System” at US$18,995.

Gallery

Variants:

Tango 2
Base model

Tango XR
Extended range aircraft with 90 gallon wet wing fuel tanks.

Tango 2
Engine: Lycoming IO-360, 180 hp (130 kW)
Horsepower range: 150-200
Height: 6.75 ft (2.06 m)
Length: 20 ft 7 in (6.27 m)
Wingspan: 26 ft (7.9 m)
Wing area: 78 sq. ft (7.2 m2)
Fuel capacity: 58 gal US
Empty weight: 1,150 lb (522 kg)
Gross weight: 2,000 lb (907 kg)
Useful Load: 850 lb
Payload, full fuel: 502 lb
Baggage Capacity: 158 lb
Maximum speed: 184 kn; 341 km/h (212 mph)
Cruise (TAS): 182 kn; 338 km/h (210 mph)
Stall (IAS): 51 kn; 95 km/h (59 mph)
Vne (IAS): 200 kn; 370 km/h (230 mph)
Range: 1,440 sm
Rate of Climb: 1,600 ft/min
Takeoff: 500 ft
Landing: 800 ft
Service ceiling: 24,000 ft
Baggage Area: 12 cu. ft
Cabin Width: 44 in
Cabin Height: 37 in
Wing Loading: 25.6 lbs./sq. ft
Aspect Ratio: 8.7:1
G-load (design): +6 / -6
Seats: 2
Landing gear: Fixed Tri-gear
Building materials: Composite
Kit cost 2009: US $ 29,750

Tango-XR
Top speed (TAS): 212 mph
Cruise (TAS): 210 mph
Stall (IAS): 63 mph
Vne (IAS): 230 mph
Range: 2,100 sm
Rate of Climb (gross wt): 1,600 ft/min
Takeoff: 500 ft
Landing: 800 ft
Service ceiling: 24,000 ft
Engine: Lycoming IO-360, 180 hp
Horsepower range: 180-210
Fuel capacity: 90 gal US
Empty weight: 1,225 lb
Gross weight: 2,200 lb
Useful Load: 1,000 lb
Payload, full fuel: 435 lb
Baggage Capacity: 50 lb
Baggage Area: 12 cu. ft
Cabin Width: 44 in
Cabin Height: 37 in
Height: 6.75 ft
Length: 20.7 ft
Wingspan: 26 ft
Wing area: 78 sq. ft
Wing Loading: 28.2 lbs./sq. ft
Aspect Ratio: 8.7:1
G-load (design): +5 / -4
Seats: 2
Landing gear: Fixed Tri-gear
Building materials: Composite
Kit cost 2009 ($US): $31,750

The Tango 2 and Foxtrot 4 wing uses a constant chord, constant thickness airfoil which gives it gentle, textbook stall characteristics. Wing root first, ailerons last, with no built in twist required. The stall itself is simple with distinctive aerodynamic warning and little to no tendency to drop off. Differential ailerons counteract adverse yaw.
The wing spars are factory assembled. They are a one piece composite I-beam structure that goes from wing tip to wing tip. Both airplanes were designed to 6/-4 G’s and have been successfully tested to 1.5 design limits. Each wing and horizontal stabilizer spar is tested to 6 G’s before it leaves the factory.

All of the fuel is carried in the wings. There is no fuel storage anywhere in the fuselage or engine compartment. Capacitance type fuel probes run the entire length of the wing. This allows accurate fuel quantity readings from full right down to zero, a rarity in many airplanes. Total unusable fuel is less than a pint. The fuel selector is in plain view on the forward console and is easily accessible for switching from left to right. The large capacity tanks provide a reserve even after a four or five hour flight.

Team Tango uses only FAA approved foam core in the structures. It is more expensive, but compared to other popular foam cores it is the only one that does not create cyanide gas when exposed to flame, is self extinguishing and fuel -proof. The Tango and Foxtrot both feature a dual gull wing canopy system which incorporates a reinforced roll bar. Both can cruise at 200+ mph, have a range over 1400 s.m., carry over 100 pounds of baggage, and operate off a grass strip.

The fuselage sits level in cruise flight which is three degrees lower than the ground attitude. The molded fiberglass seats put the pilot and passenger in a semi-reclining position leaning back approximately 30 degrees. The Tango and Foxtrot are 44 and 46 inches wide. Various antennas are installed into the fuselage during the lay-up process, when it is easy. The instrument panel is divided into three sections. This allows easier installation and access for maintenance and upgrades.

The fuselages use quarter inch foam core that is reinforced at the horizontal stab attach points and up into the vertical stab. A build center is available to build your airplane at the factory, guided and instructed by the staff, and that expertise is included in the price of your aircraft. The seat installation is adjustable for leg room and height as well as recline. The airframe can be customized. The wing can be longer to reduce wing loading, reduce stall speed, climb better at lower airspeeds and have greater high altitude performance. We use ½” foam core in and around the doors ensure stiffness so they won’t pull away from the fuse in flight and cause air leaks or allow rain to enter the cabin. A vinyl ester resin in the composite is a safer and less toxic alternative that won’t induce an allergic reaction and is pleasant to work with.

Foxtrot 4
Engine: Lycoming IO-540, 300
Engine option: Lycoming IO-360
Horsepower range: 200-300
Height: 7.25 ft
Length: 24.8 ft
Wingspan: 32 ft
Wing area: 128 sq. ft
Fuel capacity: 100 gal US
Empty weight: 1,750 lb
Gross weight: 3,000 lb
Useful Load: 1,100 lb
Payload, full fuel: 650 lb
Baggage Capacity: 150 lb
Stall (IAS): 62 mph
Vne (IAS): 245 mph
Range: 1,800 sm
Rate of Climb: 1,600 ft/min
Takeoff: 350 ft
Landing: 800 ft
Baggage Area: 14 cu. ft
Cabin Width: 47 in
Cabin Height: 43 in
Wing Loading: 23.4 lbs./sq. ft
Aspect Ratio: 8:1
G-load (design): +6 / -4
Seats: 4
Landing gear: Fixed Tri-gear
Building materials: Composite
Kit cost 2009: US $ 45,995

Offered as a Quick Build Kit, these airframes are built by HPA International, a manufacturing subdivision in the Czech Republic. Their group of highly skilled engineers and aircraft assembly specialists have assisted to completely engineer the F-1 QB, paying particular attention to craftsmanship and ease of assembly. Complying with the FAA 51% rule, the Quick Build Kit is offered as a complete airframe. The F-1 QB is powered by a fuel-injected Lycoming IO-540 engine, commonly used in Piper Aztecs. Horsepower may range from 250 to 300+ and either a 2- or 3-bladed prop can be used. The engine is not included in the kit.

All wing ribs and internal wing parts are anodized for corrosion protection. All wing skins are primed with epoxy chromate. The F-1 QB wings are delivered with the spars completed, all ribs riveted in place and the top skins riveted on. The customer will need to install the wiring necessary for landing lights (if desired) and strobe and position lights. The pitot tube bracket and pitot lines must also be installed. Once this has been completed, the bottom skins can be riveted in place.

The fuselage is delivered with all bulkheads completed and all skins riveted in place. All bulkheads and internal parts are anodized for corrosion protection. All skins have been primed with epoxy chromate for corrosion resistance. The ELT and battery trays are preformed and ready for your final assembly and installation. All fuselage floor and baggage compartment panels are pre-cut and pre-drilled ready to install. The customer will install the torque tube and control sticks, rudder pedals and cables, seats and seatback support, and instrument panel.

The F-1 QB finish kit is the most complete and comprehensive finish kit that can be provided. Most parts that are considered upgrades by other manufacturers, are standard in our kit. Fiberglass wing root fairings, fiberglass gear leg and gear leg intersection fairings, Rocket-tip wingtips with strobe and position light bulkheads pre-molded into place with Lexan plexiglass covers are all included as standard. Our cowl is delivered in three pieces for ease of installation. The oil door is pre-molded for ease of construction. The F-1 QB canopy is a slider canopy. The gear legs are manufactured from titanium and are pre-drilled to the engine mount. The wheels, brakes, tires, tubes, brake lines, pitot lines, master cylinders, and fuel lines are all included in the finish kit.

The empennage kit is not included in the Quick Build Kit and is considered a starter kit. This is done for two reasons: 1) This gives first time builders an opportunity to discover mistakes on parts that are not expensive rather than on areas that are very expensive. 2) When we went through the FAA 51% certification process, it was determined that we could do considerably more of the difficult construction on the wings and fuselage by making the tail its own kit.

Prices at 1 September 2006
Evo kit (w/emp) ..Lycoming Config – $49720
Evo kit (w/o emp)..Lycoming Config – $47720
Evo kit (w/emp)..TCM.IO-550.Config – $50700
Evo kit (w/o emp)..TCM IO-550.Config – $48700
Emp Kit – $2150

Sports QB kit (w emp kit) – $44270
Sports QB kit (w/o emp kit) – $42720

F-1 Rocket
Engine: Lycoming IO-540, 250 hp
HP range: 250-300
Length: 21 ft
Wing span: 22.6 ft
Wing area: 106 sq.ft
Fuel capacity: 52 USG
Empty weight: 1200 lb
Gross weight: 2000 lb
Cruise: 230 mph
Stall: 56 mph
Range: 1150 sm
Rate of climb: 3000 fpm
Takeoff dist: 300 ft
Landing dist: 700 ft
Seats: 2 tandem
Cockpit width: 30 in
Landing gear: tailwheel

F-1 Evo
Engine Lycoming IO-540 / Continental 550
HP Range 235-350
Length 21 ft.
Wing Span 24’10”
Wing Area 102 sq. ft.
Top Speed 265 m.p.h.
Fuel Capacity 52 gal
Empty Weight 1300 lbs
Gross Weight 2100 lbs
Cruise Speed (75% power@ 8000′ MSL) 240 m.p.h
Stall Speed 50 m.p.h.
Range @55%pwr 1150 sm
Rate of climb sea level 3500 fpm
Take off Distance 300ft
Landing Distance 700ft
Seats 2
Cockpit width 30 in
Landing Gear tail wheel
Building Material Metal
G. Limit +6 -3 g

F1 Sport wing
Engine Lycoming IO-540
HP Range 250-300+
Length 21 ft.
Wing Span 21′ 10″
Wing Area 104 sq. ft.
Fuel Capacity 52 gal
Empty Weight 1200lbs
Gross Weight 2000 lbs
Top Speed 250 m.p.h.
Cruise Speed ( TAS @ 10,000MSL @ 60% power) 230 m.p.h
Stall Speed 54 m.p.h.
Range @55%pwr 1000 sm
Rate of climb sea level 3500 fpm
Take off Distance 300ft
Landing Distance 700ft
Seats 2
Landing Gear tail wheel
Building Material Metal
G. Limit +6 -3 g