Force on three Bolts holding up a Jet Engine

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The discussion centers on calculating the force on three bolts supporting a 1400-kg jet engine. The initial assumption was that the force on the bolts would be 0 Newtons since they are not moving, which is incorrect. The correct interpretation involves calculating the tension on each bolt, as they support the weight of the engine. Each bolt would therefore bear a load of approximately 4,600 Newtons when the plane is stationary. Understanding the distinction between net force and tension is crucial for solving this problem accurately.
mopit_011
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Homework Statement
A 1400-kg jet engine is fastened to the fuselage of a passenger jet by just three bolts (this is the usual practice). Assume that each bolt supports one-third of the load. Calculate the force on each bolt as the plane waits in line for clearance to take off.
Relevant Equations
F=ma
y=y0+v0t+(at^2/2)
My solution was that there would be a force of 0 Newtons on the bolt as the bolt is not moving. But this answer is wrong. Where am I going wrong?
 
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mopit_011 said:
Homework Statement:: A 1400-kg jet engine is fastened to the fuselage of a passenger jet by just three bolts (this is the usual practice). Assume that each bolt supports one-third of the load. Calculate the force on each bolt as the plane waits in line for clearance to take off.
Relevant Equations:: F=ma
y=y0+v0t+(at^2/2)

My solution was that there would be a force of 0 Newtons on the bolt as the bolt is not moving. But this answer is wrong. Where am I going wrong?
I doubt they mean to ask for the net force, though I agree that is a strictly correct interpretation. Rather, they want the tension on each bolt.
 
haruspex said:
I doubt they mean to ask for the net force, though I agree that is a strictly correct interpretation. Rather, they want the tension on each bolt.
Ohhhh ok. Thank you so much!
 
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