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AIRCRAFT BASIC CONSTRUCTION

CHAPTER 4 AIRCRAFT BASIC CONSTRUCTIONINTRODUCTIONN aval AIRCRAFT are built to meet certain specifiedrequirements. These requirements must be selected sothey can be built into one AIRCRAFT . It is not possible forone AIRCRAFT to possess all characteristics; just as it isn'tpossible for an AIRCRAFT to have the comfort of apassenger transport and the maneuverability of afighter. The type and class of the AIRCRAFT determine howstrong it must be built. A Navy fighter must be fast,maneuverable, and equipped for attack and defense. Tomeet these requirements, the AIRCRAFT is highly poweredand has a very strong airframe of a fixed-wing AIRCRAFT consists of thefollowing five major units:1. Fuselage2. Wings3. Stabilizers4. Flight controls surfaces5. Landing gearA rotary-wing AIRCRAFT consists of the followingfour major units:1. Fuselage2. Landing gear3. Main rotor assembly4. Tail rotor assemblyYou need to be familiar with the terms used foraircraft CONSTRUCTION to work in an aviation STRESSLEARNING OBJECTIVE:Identify the fivebasic stresses acting on an primary factors to consider in aircraftstructures are strength, weight, and reliability.

construction are aluminum, magnesium, titanium, steel, and their alloys. Alloys An alloy is composed of two or more metals. The metal present in the alloy in the largest amount is called the base metal. All other metals added to the base metal are called alloying elements. Adding the alloying elements may result in a change in the properties of the

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