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The Piper PA-34 Seneca is a twin-engined light aircraft, produced in the United States by Piper Aircraft.It has been in non-continuous production since 1971. [4] [5] [6] The Seneca is primarily used for personal and business flying [1] as well as multi-engine class rating flight training.
Data from Jane's all the World's Aircraft 1988–89 General characteristics Crew: 1 or 2 Capacity: 4 or 5 pax + optional seventh seat Length: 8.72 m (28 ft 7 in) Wingspan: 11.86 m (38 ft 11 in) Height: 3.02 m (9 ft 11 in) Wing area: 19.18 m 2 (206.5 sq ft) Airfoil: NACA 65 2 -415 Empty weight: 1,290 kg (2,844 lb) Gross weight: 1,810 kg (3,990 lb) (Max zero fuel weight) Max takeoff weight ...
A 37° flare type end fitting for flexible hose The AN thread (also A-N ) is a particular type of fitting used to connect flexible hoses and rigid metal tubing that carry fluid. It is a US military-derived specification that dates back to World War II and stems from a joint standard agreed upon by the Army Air Corps and Navy, hence AN.
Industrial exhaust ducts are pipe systems that connect hoods to industrial chimneys through other components of exhaust systems like fans, collectors, etc. Ducts are low-pressure pneumatic conveyors to convey dust, particles, shavings, fumes, or chemical hazardous components from air in the vicinity to a shop floor or any other specific locations like tanks, sanding machines, or laboratory hoods.
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HVAC turning vanes are sheet metal devices inside of mechanical ductwork used to smoothly direct air inside a duct where there is a change in direction, by reducing resistance and turbulence. See also
Gooseneck vent with check valve being repainted. A gooseneck (or goose neck) is a 180° pipe fitting at the top of a vertical pipe that prevents entry of water. Common implementations of goosenecks are ventilator piping or ducting for bathroom and kitchen exhaust fans, ship holds, landfill methane vent pipes, or any other piping implementation exposed to the weather where water ingress would ...
A swan neck duct is a jet engine component, usually situated within the compression or turbine expansion system. [1] Many jet engines have a short annular passageway, linking two components, where there is a large change in mean radius, from front to rear. The shape of the resulting passageway is often similar to that of a swan or goose neck.