1995-7: 2431 Ferguson Pl, Dallas, GA 30132, USA.
UL builder
LSA/UL
Fantasy Air Allegro 2000 / LSA America Allegro
Modern two seat microlight aircraft that are unique for its very good aerodynamics, excellent flight qualities and a high economy of operation.
Carefully designed shape of the fuselage that is made of glassfibre laminate and its high quality surface provide minimum air resistance and minimum sensibility to side wind. The wings, as well as the tail plane are of metal construction covered in part with fabrics. The centre section of the wing is welded from steel tubes.
Aircraft have a uniquely spacious cabin, which guarantees comfort namely in long cross-country flights.
The position of the control stick between the seats makes getting in and out very comfortable. Large surface organic glass cover of the cabin offers a very good view.
The Allegro is equipped with a Verner engine but can also take a Rotax 582.
LSA America took over the construction of the European-introduced Allegro LSA. The composite/aluminum Allegro comes in three versions: Classic Trainer, Voyager and Executive. It’s full-fuel payload is 580 pounds. Prices 2012: $89,000 (Classic Trainer); $94,000 (Voyager); $99,000 (Executive).
Stall: 35 kt / 40 mph / 65 kmh
Cruise: 86 kt / 99 mph / 160 kmh
VNE: 119 kt / 137 mph / 220 kmh
Empty Weight: 285 kg / 628 lbs
MTOW Weight: 450 kg / 992 lbs
Climb Ratio: 1000 ft/min / 5 m/s
Glide Ratio: 1:12
Take-off distance (50ft obstacle): 820 ft / 250 m
Landing distance (50ft obstacle): 720 ft / 220 m
Allegro
Engine: Werner 1400, 80 hp
Wing span: 10.6 m
Wing area: 15.2 sq.m
MAUW: 450 kg
Empty weight: 260 kg
Fuel capacity: 50 lt
Max speed: 162 kph
Cruise speed: 130 kph
Minimum speed: 50 kph
Certification: vVz
Seats: 2
Fantasy Air
1998:
Kollarova 511
CZ-39701 Pisek
Czech Republic
LSA builder
Falconar F-11
The Falcon Avia F9, F10, F11 and F12 series are derived from famous Jodel D9 and D11 from France – Cockpits larger, simplified fittings, shoulder harness, safer stall.
The F11 plans have step by step manuals, full size layouts for ribs, bulkheads and small parts. Built of wood and plywood for ease of construction, no expensive or unique tools are required. The are a minimum of metal fittings – under 32 fittings assemblies. Equipped with maintenance free Delrin bearings and stainless steel hardware for control surfaces, the wing and tail easily removable.
The F11A “SPORTY” is an easy to build, side-by-side 2 seater for Continental engines 65 to 100 hp.
Options include flaps, vertical coil spring main landing gear, tri gear, auxiliary tanks, 3 piece folding wing, and floats. The F-11A has a building time of 2000 4000 hours.
The F-11E has a reduced gross weight for lightweight 2 and 4 stroke engines 50 to 100 hp.
In 2010 F Series plans for the F11A cost US$200.00, and the F11E plans US$225.00.
The F11A Sporty is LSA legal.
On June 30, 2019, Falconar Avia Inc closed for business and assets dissolved. The Master Sets (Original Drawings, Plans, Info Kits, Documentation) sold included the F-9, F-10, F-11A, E, and E2, F-12A, and Minihawk Series to Manna Aviation
F-11A
Engine: Continental, 85 hp
HP range: 65-100
Height: 6.3 ft
Length: 22 ft
Wing span: 27.25 ft
Wing area: 138 sq.ft
Fuel cap: 17 USG
Weight empty: 715 lb
Gross: 1300 lb
Vne: 185 mph
Speed max: 135 mph
Cruise: 120 mph
Range: 546 sm
Stall: 35 mph
ROC: 800 fpm
Take-off dist: 250 ft
Landing dist: 300 ft
Service ceiling: 14,000 ft
Seats: 2
Landing gear: tail wheel
Take off distance: 250ft
Landing distance: 300ft
F-11A Sporty
Vne: 185 mph
Cruise: 120 mph
Stall: 35 mph
Range: 546 sm
Rate of climb: 800 fpm
Takeoff dist: 250 ft
Landing dist: 300 ft
Engine: Continental C-85, 85 hp
HP range: 60-130
Fuel capacity: 17 USG
Empty weight: 715 lb
Gross weight: 1300 lb
Length: 22 ft
Wing span: 27.3 ft
Wing area: 138 sq.ft
Cockpit width: 40 in
Landing gear: nose or tail
Seats: 2
F-11E
Vne: 140 mph
Cruise: 100 mph
Stall: 42 mph
Range: 640 sm
Rate of climb: 900 fpm
Takeoff dist: 260 ft
Landing dist: 250 ft
Engine: VW, 50 hp
HP range: 50-100
Fuel capacity: 17 USG
Empty weight: 600 lb
Gross weight: 1050 lb
Length: 21 ft
Wing span: 28 ft
Wing area: 140 sq.ft
Seats: 2
Cockpit width: 40 in
Landing gear: Tailwheel
Falconar F-10
The Falcon Avia F9, F10, F11 and F12 series are derived from famous Jodel D9 and D11 from France – Cockpits larger, simplified fittings, shoulder harness, safer stall.
The F10 plans have step by step manuals, full size layouts for ribs, bulkheads and small parts. Built of wood and plywood for ease of construction, no expensive or unique tools are required. The are a minimum of metal fittings – under 32 fittings assemblies. Equipped with maintenance free Delrin bearings and stainless steel hardware for control surfaces, the wing and tail easily removable.
The F10A is like the F9A except heavier and stronger for Continental or similar engines 40 to 100 hp.
Options include flaps and vertical coil spring main landing gear. The F10A is LSA legal.
In 2010 F10A F Series plans cost Can $195.00.
On June 30, 2019, Falconar Avia Inc closed for business and assets dissolved. The Master Sets (Original Drawings, Plans, Info Kits, Documentation) sold included the F-9, F-10, F-11A, E, and E2, F-12A, and Minihawk Series to Manna Aviation
F10
Speed max: 145 mph
Cruise: 120 mph
Range: 250 sm
Stall: 35 mph
ROC: 750 fpm
Take-off dist: 350 ft
Landing dist: 230 ft
Engine: Continental, 65 hp
HP range: 40-100
Fuel cap: 12 USG
Weight empty: 550 lb
Gross: 875 lb
Length: 19 ft
Wing span: 23 ft
Wing area: 99 sq.ft
Seats: 1
Landing gear: tail wheel
F10A
Engine: Continental C-65, 65 hp
HP range: 40-100
Height: 4.8 ft
Length: 19 ft
Wing span: 23.5 ft
Wing area: 100 sq.ft
Empty weight: 550 lb
Gross weight: 875 lb
Fuel capacity: 12 USG
Top speed: 145 mph
Cruise: 90-130 mph
Stall: 35 mph
Range: 290 sm
Rate of climb: 750 fpm
Takeoff dist: 350 ft
Landing dist: 230 ft
Seats: 1
Cockpit width: 24 in
Landing gear: tailwheel
Falconar F-9
The Falcon Avia F9, F10, F11 and F12 series are derived from famous Jodel D9 and D11 from France – Cockpits larger, simplified fittings, shoulder harness, safer stall.
The F9 plans have step by step manuals, full size layouts for ribs, bulkheads and small parts. Built of wood and plywood for ease of construction, no expensive or unique tools are required. The are a minimum of metal fittings – under 32 fittings assemblies. Equipped with maintenance free Delrin bearings and stainless steel hardware for control surfaces, the wing and tail easily removable
The most important modifications are:
A changed wing design. By moving the crank inboard, Chris Falconar could make the outer parts to fold inward and make it trailerable. This folding mechanism was a (rather heavy) option. Falconar also changed the spar and wing rib design. The original Jodel spar is not the simplest to construct due to the washout in the wing profile. The Falconar spar is more straightforward and uses different ribs to create the washout. Unfortunately, this wing seems to be less efficient than the original item.
Much more power. The original D11 had anywhere from 45 to 90 hp. Mostly A-65’s and C-90’s. The F-11 uses up to the O-290, which has around 125 hp and is heavier, uses more fuel etc. Effectively, the flight characteristics of the plane will be severely altered by this engine.
There are options for different tail configurations.
The possibility to build a 3th seat.
The building time is 1500-¬3000 hours.
In 2010 the F9A F Series plans sold for Can$190.00
On June 30, 2019, Falconar Avia Inc closed for business and assets dissolved. The Master Sets (Original Drawings, Plans, Info Kits, Documentation) sold included the F-9, F-10, F-11A, E, and E2, F-12A, and Minihawk Series to Manna Aviation
F9
Engine: VW, 60 hp
HP range: 40-75
Length: 17.9 ft
Wing span: 23 ft
Wing area: 99 sq.ft
Weight empty: 400 440 lb
Gross: 660 lb
Fuel cap: 10 USG
Speed max: 140 mph
Cruise: 100 mph
Range: 420 sm
Stall: 31 mph
ROC: 600 fpm
Take-off dist: 320 ft
Landing dist: 220 ft
Seats: 1
Landing gear: tail wheel
Take off distance: 320ft
Landing distance: 220ft
F-9A
Engine: VW, 50 hp
HP range: 40-75
Height: 4.6 ft
Length: 17.9 ft
Wing span: 23.5 ft
Wing area: 100 sq.ft
Empty weight: 360 lb
Gross weight: 600 lb
Fuel capacity: 10 USG
Top speed: 140 mph
Cruise: 80-100 mph
Stall: 35 mph
Range: 300 sm
Rate of climb: 1000 fpm
Takeoff dist: 320 ft
Landing dist: 220 ft
Seats: 1
Landing gear: tailwheel
Falconar Cubmajor / Falconar Majorette
Of similar performance and size to a Piper Cub but all wood except steel tube upper cockpit section, the Cubmajor was available with open or enclosed cockpit. A 2 seat tandem aircraft with quick fold wings, options included sealed ailerons, light or heavy structure, Delrin bearings, and various engine options.
The Cubmajor is LSA legal.
The Majorette has open cabin struts.
On June 30, 2019, Falconar Avia Inc closed for business and assets dissolved. The Master Sets (Original Drawings, Plans, Info Kits, Documentation) were available for sale and full transfer of rights included the Cub Major and Cub Majorette for $2500 USD.
Cabin
Engine: Continental C-85, 85 hp
HP range: 65-100
Height: 6.8 ft
Length: 23.8 ft
Wing span: 35 ft
Wing area: 163 sq.ft
Weight empty: 900 lb
Gross: 1400 lb
Fuel cap: 14 USG
Speed max: 116 mph
Cruise: 105 mph
Range: 275 sm
Stall: 43 mph
ROC: 860 fpm
Take-off dist: 250 ft
Landing dist: 150 ft
Seats: 2
Landing gear: tail wheel.
Cubmajor
Vne: 116 mph
Cruise: 105 mph
Stall: 43 mph
Range: 275 sm
Rate of climb: 800 fpm
Takeoff dist: 400 ft
Landing dist: 250 ft
Engine: Continental C-85, 85 hp
HP range: 85-125
Fuel capacity: 14 USG
Empty weight: 800 lb
Gross weight: 1300 lb
Height: 6.8 ft
Length: 23.8 ft
Wing span: 35 ft
Wing area: 153 sq.ft
Seats: 2
Cockpit width: 24 in
Landing gear: tailwheel
Majorette
Vne (never exceed speed): 116 mph
Cruise speed: 105 mph
Range: 390 miles
Stall: 42 mph
Length: 26.0 feet
Wing span: 35 feet
Wing area: 155 sq. feet
Falconar ARV-1 Golden Hawk
The 1996 ARV-1K has seating for two in a heated cabin for cold weather flying. With short landing capability the ARV has HIPEC covering. Easy to dismantle and haul by trailer.
ARV-1
Vne: 110 mph
Cruise speed: 100 mph
Range: 200 mi.
Stall: 40 mph
Takeoff distance: 250 ft.
Landing distance: 250 ft.
Gross weight: 990 lbs
Wing span: 34 ft.
Wing area
Total lift area including canard: 168 sq ft.
ARV-1K Golden Hawk
Engine: Hirth 2703, 55 hp
HP range: 50-60
Height: 7 ft
Length: 14 ft
Wing span: 34 ft
Total lift area including canard: 168 sq ft.
Weight empty: 500 lb
Gross weight: 990 lb
Fuel cap: 9 USG
Vne: 130 mph
Cruise: 100 mph
Range: 200 sm
Stall: 40 mph
ROC: 800 fpm
Take-off dist: 250 ft
Landing dist: 250 ft
Seats: 2
Landing gear: nose wheel
ARV-1L Golden Hawk
Engine: Hirth 2703, 55 hp
HP range: 55-75
Height: 7 ft
Length: 14 ft
Wing span: 34 ft
Wing area: 155 sq.ft
Empty weight: 500 lb
Gross weight: 890 lb
Fuel capacity: 9 USG
Top speed: 130 mph
Cruise: 100 mph
Stall: 40 mph
Range: 250 sm
Rate of climb: 1000 fpm
Takeoff dist: 250 ft
Landing dist: 250 ft
Seats: 2
Landing gear: nose wheel
Falconar Avia
1993: Falconar Aviation Ltd., 19 Airport Road, Edmonton, Alberta, T5E OW7, Canada.
1995-8: 7739 81 Ave, Edmonton, Alberta T6C 0V4, Canada.
Falconar Avia offers plans and/or components to build the Mignet HM.293 single-seat open-cockpit homebuilt, Mignet HM.360 single-seat homebuilt version of the Pou-du-Ciel and HM.380 two-seater, Cubmajor tandem two-seat cabin monoplane, Jodel F.9 single-seat monoplane and more streamlined and higher-powered F.10 variant, F.12A Cruiser side-by-side two-seat cabin monoplane, Golden Hawk ARV-1L (1996) tandem two-seat composite pusher-engined type, and two/three-seat Adam RA.14 Loisirs/Maranda, designed in France by Roger Adam.
Fairhall Special
Based on the Pietenpol Aircamper, Andy Fairhall built all the woodword, metal fittings, and deigned and carved the propeller.
The Fairhall Special features a lengthened wingspan and the cabane struts were moved slightly outward and angled. Andy added a spring steel undercarriage and steerable tailwheel.
First flown in 1997, the Special is a Class 2 microlight with a MTOW of 453 kg.
The Special is powered by a Toyota 4Y Hilux engine of 80 hp and runs mainly on Avgas, giving a three hour endurance. The water cooling allows a ducted hot air system from the radiator to heat the cockpit.
All Aero 