Search results
Results From The WOW.Com Content Network
PA-28-181 Archer TX and LX Four-place, fixed landing gear landplane, Lycoming O-360-B4A engine of 180 hp (134 kW), maximum takeoff weight 2,550 lb (1,157 kg). Produced in Archer TX trainer and Archer LX personal aircraft variants, both with Garmin G1000 NXi avionics. [47] [48] PA-28-181 Archer DX of the Indonesian Navy PA-28-181 Archer DX and DLX
This page was last edited on 20 July 2013, at 20:34 (UTC).; Text is available under the Creative Commons Attribution-ShareAlike 4.0 License; additional terms may ...
The 17.9 aspect ratio wing provides a glide ratio of 28:1 with the propeller feathered, and a minimum sink speed of 3.16 feet/sec (0.96 m/s). [1] [3] The USAF Technical Orders indicate a glide ratio of between 19.3:1 and 19.7:1. [11] The SGS 2-37 was marketed by the company as being suitable for the following roles: [1] [3] Sailplane trainer
The PA-44 features a high T-tail similar to the T-tailed Arrow IV. The Seminole is visually similar to the Beechcraft Duchess. [3] Production of both versions of the Seminole was stopped in 1982, after 361 Seminoles and 87 Turbo Seminoles had been built. Production of the normally aspirated PA-44-180 restarted in 1988. [7]
The Piper PA-18 Super Cub is a two-seat, single-engine monoplane. Introduced in 1949 by Piper Aircraft , it was developed from the PA-11 Cub Special , and traces its lineage back through the J-3 Cub to the Taylor E-2 Cub of the 1930s.
The HP-11 is an all-metal design, with a wing that features a 26:1 aspect ratio, a 52 ft (15.8 m) wingspan and a NACA 65 (3)-618 airfoil, the same airfoil that had been used on the HP-8 and HP-10. [1] [2] A total of 42 HP-11s were built from kits and plans before production was ended in favour of the Schreder HP-14. [1] [2]
Data from Manufacturer General characteristics Crew: one Capacity: one passenger Length: 6.62 m (21 ft 9 in) Wingspan: 8.6 m (28 ft 3 in) Height: 2.315 m (7 ft 7 in) Wing area: 12.3 m 2 (132 sq ft) Empty weight: 388 kg (855 lb) Gross weight: 600 kg (1,323 lb) Fuel capacity: 114 litres (25 imp gal; 30 US gal) Powerplant: 1 × Rotax 912 ULS2, 73.5 kW (98.6 hp) Propellers: 3-bladed Woodcomp ...
A glider's glide ratio varies with airspeed, but there is a maximum value which is frequently quoted. Glide ratio usually varies little with vehicle loading; a heavier vehicle glides faster, but nearly maintains its glide ratio. [22] Glide ratio (or "finesse") is the cotangent of the downward angle, the glide angle (γ). Alternatively it is ...