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The Panther is a single seat, low wing aircraft, built of aluminum with a bubble canopy. The forward fuselage is constructed from welded 4130 steel tubing, with the aft fuselage, tail and wings made from 2024-T3 aluminum sheet. The landing gear can be assembled in either tricycle or conventional gear arrangements. The wings are designed to be ...
It is made from 7075-T6 aluminum tubing, with the control bar and kingpost made from 6061-T6 aluminum. The single-surface wing is covered in Dacron sailcloth. Its 39.0 ft (11.9 m) span wing is cable braced from a single kingpost. The nose angle is 115°, wing area is 330 sq ft (30.7 m 2) and the aspect ratio is 5:1. Pilot hook-in weight range ...
The aluminum structure wing, covered in flush riveted aluminum sheet, ... The aircraft was designed for a maximum gross weight of 1,500 lb (680 kg) in the utility ...
The aircraft is made from composites. Its 25.0 ft (7.6 m) span wing is made with an aluminum spar and S-glass vinyl-ester resin, is detachable for ground transport or storage and has a wing area of 87.5 sq ft (8.13 m 2). The standard engine used is the 50 hp (37 kW) Rotax 503 two-stroke powerplant. [1] [2]
The CAF Southern California Wing Museum (commonly shortened to CAF SoCal) is an air museum at Camarillo Airport in Camarillo, California. [1] It is a unit of the Commemorative Air Force . [ 2 ] [ 3 ] It is home to several airworthy historic aircraft, as well as static aircraft, displays, models, and artifacts primarily related to military ...
The speed wing restricts the aircraft's useful load to 170 lb (77 kg), while the standard wing allows 250 lb (113 kg). [1] [5] The standard engine is the 40 hp (30 kW) Rotax 447, although engines of 28 to 52 hp (21 to 39 kW) can be used. The manufacturer estimates that a builder will take 100–120 hours to complete this aircraft from the kit.
Its wing has an area of 195 sq ft (18.1 m 2). [3] Falcon 3 Tandem Tandem model for flight training, introduced in 2009. [3] Falcon 4 145 Small-sized model for lighter pilots, HGMA certified in 2015. Its wing has a span of 28 ft (8.5 m), wing area is 145 sq ft (13.5 m 2) and the aspect ratio is 5.4:1. The pilot hook-in weight range is 120 to 190 ...
They are commonly used in the fuselage, wing, and supporting structure of aircraft because they are resistant to corrosion and have a good strength to weight ratio. [17] Aluminum that is used in aircraft is commonly mixed with copper, lithium, magnesium, manganese, silicon, silver, and zinc to form alloys. [2]