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Many of the early ultralights used a "weight shift" method of control, requiring the pilot to push a control bar to shift the center of gravity of the aircraft. The Weedhopper differed from most other ultralights of the period in that it has a control stick which moves the rudder and elevator, giving it two axis control in pitch and yaw.
As for the four-cylinder engines, the Dover and Dorset variations share a displacement. They can be distinguished by the Dover's higher specifications, with an aluminium rather than a pressed steel manifold, straight-cut gears, and larger ports in the head. The engine code is also different, 2711 for the Dorset and 2722E for the Dover. [2]
Current iSpec 2200 comprises a suite of data specifications and data modules for the digital representation and exchange of technical data. Objective is to: Minimize cost and effort expended by operators and OEMs; Improve information quality and timeliness; Ensure that manufacturers provide data that meets airline operational needs
Prior to Issue 2, updates to the specification were known as changes. When the standard reached Change 9, the proposed Change 10 became Issue 2.0 with previous Changes retro-referred to as Issue 1.x. Issue 1.6 was the first publicly published version of S1000D and was notable as the first issue to include operator information (Crew) as well as ...
These specifications are in varying degrees of maturity and are maintained or supported by various standards bodies and entities. These specifications are the basic web services framework established by first-generation standards represented by WSDL, SOAP, and UDDI. [1] Specifications may complement, overlap, and compete with each other.
In Thai specs, the naturally aspirated eight-valve version claimed 90 hp in 1992. 93 mm (3.7 in) 92 mm (3.6 in) 2,499 cc (152.5 cu in) 18.4:1 76 PS (56 kW) at 4200 rpm 17.5 kg⋅m (172 N⋅m) at 2000 rpm [39] 4JA1-L The current 4JA1-L engine is turbocharged but not intercooled with an 18.5:1 compression ratio. The GM South Africa-built Isuzu ...
Data from Janes' All The World's Aircraft 1982-83 General characteristics Crew: One Capacity: Five passengers Length: 28 ft 2 in (8.59 m) Wingspan: 36 ft 9 in (11.20 m) Height: 9 ft 8 in (2.95 m) Wing area: 175 sq ft (16.3 m 2) Empty weight: 2,303 lb (1,045 kg) Gross weight: 4,000 lb (1,814 kg) Fuel capacity: 87 US gal (72 imp gal; 330 L) (usable capacity) Powerplant: 1 × Continental Motors ...
IEC 60081 Double-capped fluorescent lamps – Performance specifications; IEC 60083 Plugs and socket-outlets for domestic and similar general use standardized in member countries of IEC; IEC 60085 Electrical insulation – Thermal evaluation and designation; IEC 60086 Primary batteries; IEC 60092 Electrical installations in ships