SG Aviation Sea Storm

First seen in 1997 at the Bassano show, the Seastorm is aimed at the American kit plane market. Entirely composite, a 900kg MAUW four seater was under development.

Engine: Midwest 110, 115 hp
Wing span: 9.27 m
Wing area: 12.24 sq.m
MAUW: 500 kg
Empty weight: 300 kg
Fuel capacity: 120 lt
Max speed: 270 kph
Cruise speed: 210-240 kph
Minimum speed: 62-73 kph
Climb rate: 4.5 m/s
Seats: 2
Fuel consumption: 18-32 lt/hr
Price (1998): $89,000
Kit price (1998): $45,000

Engine: Midwest 105, 105 hp
HP range: 105-115
Top speed: 171 mph
Cruise: 148 mph
Stall: 44 mph
Range: 1040 sm
ROC: 1200 fpm
TO dist land/water: 400 ft / 820 ft
Ldg dist land/water: 425 ft / 620 ft
Service ceiling: 13,700 ft
Fuel cap: 26.5 USG
Empty wt: 682 lb
Gross wt: 1340 lb
Height: 6 ft
Length: 24.6 ft
Wing span: 30 ft
Wing area: 131 sq.ft
Seats: 2
Undercarriage: tail

SG Aviation Storm

Storm 280

The Storm is derived from the P 220 Pottier, using pop-riveted sheet dural.

The Storm 400Ti is a three seat version of the Storm 280, designed specifically for the US kitplane market.

Storm 400Ti

Storm 280
Engine: Rotax 912, 80 hp
Wing span: 8.6 m
Wing area: 11.6 sq.m
MAUW: 450 kg
Empty weight: 262 kg
Fuel capacity: 90 lt
Max speed: 225 kph
Cruise speed: 200 kph
Minimum speed: 65 kph
Climb rate: 5 m/s
Certification: vVZ
Seats: 2
Fuel consumption: 13 lt/hr
Price (1998): 88,328 DM
Kit price (1998): 33,335 DM

Storm 300
Engine: Jabiru, 120hp
Fuel cap: 55 lt main + 2 x 28 lt wing.

Storm 300
Engine: Rotax 912
Fuel cap: 90 lt.

Storm 300
Engine: Midwest 105, 105 hp
HP range: 80-120
Top speed: 200 mph
Cruise: 171 mph
Stall: 35 mph
Range: 650 sm
ROC: 1500 fpm
TO dist: 450 ft
Ldg dist: 360 ft
Service ceiling: 12,000 ft
Fuel cap: 23 USG
Empty wt: 617 lb
Gross wt: 992 lb
Height: 6.4 ft
Length: 20.9 ft
Wing span: 26 ft
Wing area: 119 sq.ft
Seats: 2
Undercarriage: nose or tail.

Storm 300 Special
Engine: Midwest 105, 105 hp
HP range: 80-120
Top speed: 200 mph
Cruise: 171 mph
Stall: 42 mph
Range: 650 sm
ROC: 1500 fpm
TO dist: 450 ft
Ldg dist: 360 ft
Service ceiling: 12,000 ft
Fuel cap: 38 USG
Empty wt: 710 lb
Gross wt: 1155 lb
Height: 6.4 ft
Length: 20.9 ft
Wing span: 26 ft
Wing area: 119 sq.ft
Seats: 2
Undercarriage: nose or tail

Storm 400Ti
Engine: Lycoming O-235, 116 hp
Wing span: 7.20 m
Wing area: 11.06 sq.m
MAUW: 720 kg
Empty weight: 400 kg
Fuel capacity: 90 lt
Max speed: 242 kph
Cruise speed: 220 kph
Minimum speed: 81 kph
Climb rate: 5.5 m/s
Seats: 3
Fuel consumption: 20 lt/hr
Kit price (1998): 65 000 000 L

Servoplant Aerocraft

The Aerocraft is a tandem two seat biplane built around a welded steel spaceframe fuselage and wooden wings.

Engine: Rotax 582, 64 hp
Wing span: 7 m
Wing area: 17.50 sq.m
MAUW: 450 kg
Empty weight: 200 kg
Fuel capacity: 60 lt
Max speed: 160 kph
Cruise speed: 120 kph
Minimum speed: 60 kph
Climb rate: 4 m/s
Seats: 2
Fuel consumption: 15 lt/hr
Price (1998): US$25,000

Sequoia F.8 Falco / Laverda F.8 Falco / Aeromere F.8 Falco / Aviamilano F.8 Falco

Sequoia Falco F8L

A two-place aircraft with an optional third seat for a child, the Falco of­fers an unbeatable combination of high-speed cross-country travel with complete aerobatic capability. Designed by an Italian, Stelio Frati in 1954, a Falco equipped with an optional Christen inverted fuel and oil system is capable of unlimited inverted flight and the full range of aerobatic maneuvers. Landing gear are fully retractable, activated by a simple mechanical system. Designer Frati has been responsible for such airplanes as the Waco Meteor/SF 260 and the F20 Pegaso.

Designed in 1955 and be­tween 1956 and 1968, 101 Falcos were built as production aircraft.

The initial F.8L Series 1 was produced by Aviamilano (20 built), along with 20 F.8.L series II development.

The F.8,L America was basically similar to the Series II but modified to CAR.Pt.3 requirements.

The F.8L Super Falco Series IV was generally similar to the The F.8,L America but with the 160 hp engine. 20 were built by Laverda.

Now earmarked for homebuilt construction in the United States through Sequoia Aircraft Corp., the Falco is made of wood, except for the firewall forward, the landing gear and the sliding canopy. Fuselage and wing skins are dacron. Power is supplied by either a 150- or 160-hp Lycoming behind a fixed-pitch or constant-speed prop. Gear and flaps are operated electrically.

Two examples of the Aviamilano F.8 Falco appeared in Britain during 1960.

Aviamilano F.8 Falco

On 25 April 1965, the first, I-TRIP, of ten F.8 Super Falco under construction by Vietri first flew.

Vietri F.8 Super Falco I-TRIP

The Falco has been produced in kit form since 1974.

September 1982

Price 1982: $24,000 (Excludes engine and propeller). Units delivered to June 1981: 80.
Kit price 2008: US$108,440

F,8.L Super Falco

Gallery

F.8L Series 1
Engine: Lycoming O-290-D2B, 135 hp

F.8L Series II
Engine: Lycoming O-320-A, 150 hp

F.8,L America

F.8L Super Falco Series IV
Engine: Lycoming O-320-B3B, 160-hp
Wingspan: 26’3” / 8.00 m
Length: 21 ‘4” / 6.50 m
Wing area: 107.5 sq.ft
Empty Wt: 1212 lb / 550 kg
Gross Wt: 1808 lb / 820 kg
Fuel capacity 40 USG
Full fuel payload: 434 lb
Top speed: 212 mph
Cruise 75%: 190 mph / 165 kt
Max cruise 5000ft / 1525m: 156 kt / 180 mph / 290 kph
Stall clean: 75 mph / 65 kt
Stall landing config: 62 mph / 54 kt
ROC SL fixed pitch prop: 984 fpm / 300 m/min
Service ceiling: 19,700 ft / 6000 m
Takeoff dist: 570 ft
Takeoff run: (50’) 1150 ft
Landing dist: 750 ft
Landing roll: (50’) 1150 ft
Range: 870 sm / 755 nm / 1400 km
Cabin length: 4 ft 7 in / 1.40 m
Cabin width: 3 ft 5 in / 1.05 m
Cabin height: 3 ft 4 in / 1.02 m
Baggage capacity: 90 lb / 40 kg
Seats: 2

Engine: Lycoming IO-360
Wing span: 8 m
Wing area: 9.89 sq.m
MAUW: 853 kg
Empty weight: 550 kg
Fuel capacity: 151 lt
Max speed: 344 kph
Cruise speed: 319 kph
Minimum speed: 100 kph
Climb rate: 7.5 m/s
Seats: 2
Fuel consumption: 36 lt/hr
Plan price (1998): $400
Kit price (1998): $70,000