During the conceptual design phase of aircraft the integration of undercarriage system is very important and it is often difficult to achieve on the first time. The nose wheel landing gear preferred configurations for light naval trainer aircraft. The main objective of this project is to improve the static strength criteria and fatigue life of Nose Landing Gear Barrel considered. The investigations includes preliminary design layout for Nose Landing Gear Barrel and initial sizing has been done. It has been designed and evaluated for strength criteria. A method of analysis for the design of Nose Landing Gear Barrel made up of Al-Cu alloy (BS L 168 T6511) with static loads of axial, bending and normal loads are applied. The geometric modeling of the Nose Landing Gear Barrel was carried out using CAD package CATIA V5 R19 and pre and post processing was done through MSC/PATRAN. The stresses and displacements are obtained with the application of MSC/NASTRAN finite element software. I. INTRODUCTION The Landing gear is the structure that supports an aircraft on the ground and allows it to taxi, take-off and land .The Landing gear system consists of the main landing gear and nose landing gear. Each landing gear includes a shock strut with two and tire assemblies. Tires and the wheel absorbs the original impact on landing and are the principal part of the aircraft involved in the ground control. It allows more forceful application of the brakes without the danger of nosing the aircraft over. Tricycle is the most widely used landing gear configuration. The wheels aft of the aircraft cg is very close to it and carries much of the aircraft weight and load, thus is referred to as the main wheel. Two main gears are in the same distance from the cg in the x-axis and the same distances in y-axis, thus both are carrying the same load. The forward gear is far from cg, hence it carries much smaller load. The share of the main gear from the total load is about 80 to 90 percent of the total load, so the nose gear is carrying about 10 to 20 percent. This arrangement is sometimes called nose-gear. Both main and nose gears have the same height, so the aircraft is level on the ground, although the main gears often tends to have larger wheels. This allows the floor to be flat for passenger and cargo loading. Unlike tail-gear, a nose gear configuration aircraft is directionally stable on the ground as well as during taxing. The reason is that if the aircraft yaws slightly while taxiing, the rolling and skidding resistance of the main gear, acting behind the cg, tends to straighten the aircraft out.