American Legend Aircraft Legend Cub

Legend Cub AL3C-100

American Legend had 11 new registrations in the US during 2012. The Super Legend and new Legend Smart Cub (with a Garmin G3X system) were the most popular. Texas Star kit versions were also offered.

The Super Legend sports flaps, many carbon-fiber components and a 115 hp Lycoming IO-233-LSA multi-fuel engine. Continental O-200 (100 hp) and Jabiru 3300A (120 hp) versions were also offered. Price 2012: US$124,900 (open-cowl Legend Cub); US$128,900 (closed-cowl Cub); US$146,900 (Super Legend).

Gallery

Versions:
AL3C-100
Super Legend
Legend Smart Cub
Texas Star

Specifications:

Legend Cub AL3C-100
Piper J-3 replica
Engine: Continental O-200-D, 100 hp
Wingspan: 35’6″
Length: 22’5″
Empty Weight: 386 kg / 850 lbs
MTOW Weight: 600 kg / 1323 lbs
Stall: 30 kt / 34 mph / 55 kmh
Cruise: 83 kt / 95 mph / 153 kmh
VNE: 96 kt / 110 mph / 177 kmh
ROC: 500 ft/min / 3 m/s
Range: 315 mi
Ceiling: 15,000′
Take-off distance (50ft obstacle): 350 ft / 107 m
Landing distance (50ft obstacle): 350 ft / 107 m
Base price 2016: $136,900

Legend Cub AL3C
Piper J-3 replica
Engine: Jibaru 120hp

AL11C-100
2004 Piper PA-11 replica
Engine: 100hp Continental O-200

AL11J-120
2004 Piper PA-11 replica
Engine: 120hp Jabiru 3300A

American Jet Super Pinto / T-610

AJI T-610 N7754A

In June 1968 American Jet Industries Inc first flew the Super Pinto, a jet primary trainer or light strike aircraft developed from TT-1 Pinto built by Temco. Towards the end of the 1960s Aeronca undertook, in conjunction with American Jet Industries Inc., development of a light strike version of the Super Pinto, built originally as a jet primary trainer.
Work was also done on five-seat executive version.

Engine: 2950 lb GE CJ610-6 turbojet

American Jet Hustler

Unveiled at American Jet Industries plant in Van Nuys, California, in October, 1975, the seven place Hustler 400 turboprop/ turbojet has been modified since announcement was made. A major change was the redesign of the tail to a “T” tail configuration, and other changes include an increase of 52 inches in the wing span and installation of double slotted Fowler flaps on the supercritical wing. Sixteen inches have also been added to the fuselage.
An 850 shp United Aircraft of Canada turboprop PT6A 41 in the nose provides power for the Hustler while the Teledyne turbojet engine will be used for standby’ power in the event of an engine failure. According to American Jet’s data the standby engine will enable the aircraft to maintain an airspeed of 170 mph at 13,500 feet with the nose turboprop engine feathered. A top speed of 380 mph for the Hustler is predicted with a maximum range of 2970 miles.
Three prototypes were under construction at the American Jet California facility; two were to be used for flight testing and the third for ground structural testing. The Hustler faces some serious hurdles; for instance, no certificated jet engine of the size required by the design existed. Only various engines used for APUs, missiles or drones. If, on the other hand, a “single engine” classification were sought, the jet engine being viewed merely as a JATO unit, then the Hustler would face the challenge of making the FAA’s 70 mph landing speed requirement with a wing loading of at least 36 pounds per square foot.
The Hustler was powered by a Pratt & Whitney PT6A-41 turboprop in the nose and a standby turbojet in the tail and made its first flight on January 12, 1978.
Gulfstream American decided to replace the 850 shaft horsepower Pratt & Whitney PT6 turboprop engine in the nose of the Hustler with a 900 shp Garrett TPE331. The Pratt & Whitney JT15D remains Gulfstream’s choice for the Hustler’s rear mounted turbofan. Maximum takeoff weight was been increased to 10,000 from 9,500.
Flight testing of the Gulfstream American Hustler 500 began late in January 1981 at Van Nuys, California, and continued at Mojave. This second Hustler prototype was powered by a 900 shp Garrett AiResearch TPE 331 10 501 turboprop in the nose and a 2,200 lb st (1000 kgp) Pratt & Whitney JT15D 1 turbofan in the tail.

Hustler 400 A
Engine: Pratt&Whitney PT6A-41, 838 shp & Teledyne turbojet
Length: 37.795 ft / 11.52 m
Height: 10.761 ft / 3.28 m
Wing span: 32.644 ft / 9.95 m
Wing area: 185.141 sq.ft / 17.2 sq.m
Max take off weight: 7497.0 lb / 3400.0 kg
Weight empty: 3999.9 lb / 1814.0 kg
Cruising speed: 343 kts / 636 kph
Wing load: 40.59 lb/sq.ft / 198.0 kg/sq.m
Range: 1303 nm / 2414 km
Crew: 1
Payload: 6 Pax

Hustler 500
Engine: 1 x Garrett AiResearch TPE 331 10 501, 900 shp turboprop & 1 x Pratt & Whitney JT15D 1 turbofan 2,200 lb st (1000 kgp)

American Jet Industries

American Jet Industries Inc. was founded 1951, and became specialists in modification and repair of executive and transport aircraft, including large cargo types, and a successful program of Cessna turboprop conversions. In June 1968 first flew Super Pinto, a jet primary trainer or light strike aircraft developed from TT-1 Pinto built by Temco. Work was also done on five-seat executive version.
Under a 1974 expansion program, production was concentrated in a facilities at Van Nuys Airport, California, building Hustler, a seven-seat business/utility monoplane with supercritical wing, conventional turboprop, and ‘standby’ turbofan in rear fuselage. First flight January 11,1978.
Purchased Grumman American Aviation Corporation September 1978, being renamed Gulfstream American in 1979. Meantime, AJI renamed Gulfstream American Corporation of California, developing the Peregrine as a jet trainer and business aircraft. All programs stopped 1985.

American Homebuilts John Doe

A STOL utility aircraft (LSA) with interchangeable flaps and ailerons, as well as elevators and rudder, and an 18 cu.ft cargo area. First fown in 1994.

The man who designed this airplane was named Steve Nussbaum, he flew out of the airport I worked at, Galt airport 10C. I remember on a good day he could get one of these off the ground in 88 ft. He also designed the ribs to be replaceable in the field if they ever broke during a forced landing.
Ted Domski

Engine: Continental IO-240, 125 hp
Wing span: 30.6 ft
Wing area: 130.6 sq.ft
Fuel capacity: 26 USG
Empty weight: 850 lb
Gross weight: 1400 lb
Height: 6.5 ft
Length: 20.8 ft
Top speed: 140 mph
Cruise: 117 mph
Stall: 30 mph
Range: 500 sm
Takeoff dist: 100 ft
Landing dist: 125 ft
Service ceiling: 12,500 ft
Seats: 2 tandem
Landing gear: tailwheel

Cruise: 100 mph
Stall: 30 mph
Range: 490 sm
Rate of climb: 1000 fpm
Takeoff dist: 120 ft
Landing dist: 120 ft
Engine: Continental O-200, 100 hp
HP range: 100-125
Fuel capacity: 26 USG
Empty weight: 771 lb
Gross weight: 1320 lb
Length: 21.9 ft
Wing span: 30.6 ft
Wing area: 130.5 sq.ft
Seats: 2 tandem
Cockpit width: 28 in
Landing gear: tailwheel