Aircraft T-56 Engine Parts

(Page 6) End item NSN parts page 6 of 8
Part Number
NSN
NIIN
28-12-20 Conduit Chase Nipple
005489557
28-1250 Conduit Chase Nipple
005489557
2N3393 Transistor
009132894
2N730 Transistor
007259091
309-000 Dial Indicating Pressure Gage
009514539
309-010 Dial Indicating Pressure Gage
009514539
309-014 Dial Indicating Pressure Gage
009514539
32660 Conduit Chase Nipple
005489557
332635 Cam Adjustment Plug Assembly
006750123
334784-412 Connector Adapter
005491157
336934 Machine Bolt
006774027
338301 Annular Ball Bearing
008047991
33FX Electrical Frequency Meter
006690733
33FX380-420CPS Electrical Frequency Meter
006690733
33FX9 Electrical Frequency Meter
006690733
3407361 Metallic Particle Detector
007169026
343AS160 Rail Coupling
006106495
368891-0900-H High Pass Filter
011644001
3936 Solenoid Valve
014625439
4-106-0001 Motional Pickup Transducer
005204133
Page: 6

Engine, Aircraft T-56

Picture of Aircraft T-56 Engine

An aircraft engine is the component of the propulsion system for an aircraft that generates mechanical power. Aircraft engines are almost always either lightweight piston engines or gas turbines, except for small multicopter UAVs which are almost always electric aircraft.

In commercial aviation, the major players in the manufacturing of turbofan engines are Pratt & Whitney, General Electric, Rolls-Royce, and CFM International (a joint venture of Safran Aircraft Engines and General Electric).

In general aviation, the dominant manufacturer of turboprop engines has been Pratt & Whitney.

In this entry, for clarity, the term "inline engine" refers only to engines with a single row of cylinders, as used in automotive language, but in aviation terms, the phrase "inline engine" also covers V-type and opposed engines (as described below), and is not limited to engines with a single row of cylinders. This is typically to differentiate them from radial engines. A straight engine typically has an even number of cylinders, but there are instances of three- and five-cylinder engines. The greatest advantage of an inline engine is that it allows the aircraft to be designed with a low frontal area to minimise drag. If the engine crankshaft is located above the cylinders, it is called an inverted inline engine: this allows the propeller to be mounted high up to increase ground clearance, enabling shorter landing gear. The disadvantages of an inline engine include a poor power-to-weight ratio, because the crankcase and crankshaft are long and thus heavy. An in-line engine may be either air-cooled or liquid-cooled, but liquid-cooling is more common because it is difficult to get enough air-flow to cool the rear cylinders directly. Inline engines were common in early aircraft; one was used in the Wright Flyer, the aircraft that made the first controlled powered flight. However, the inherent disadvantages of the design soon became apparent, and the inline design was abandoned, becoming a rarity in modern aviation.

Compare Now »
Clear | Hide