<h3>Answer</h3>
option A)
21,300 N
<h3>Explanation</h3>
Given that,
mass of plan = 5320kg
altitude at which plan is flying = 2910m
drag force = 530N
<h3>Number of forces acting on airplane </h3><h3>1)</h3>
Downward Force
weight = mg
= 5320(9.81)
= 52189.2 N
<h3>2)</h3>
Lifting Force
<h3>3) </h3>
Force that push the airplane forward, thrust
<h3>4)</h3>
Force that opposes thrust, drag
Since plane is horizontal it means weight = lifting force, this balance out.
So, in order to calculate thrust which engines exert in order for the airplane to accelerate at 4.10 m/s²
<h3>Fnet=ma or ΣF = ma,</h3>
<em>where Fnet (or ∑F) is the net external force, </em>
<em />
<h3>Fnet = Thrust - frictionalForce(drag)</h3>
ma = T - f
5320(4.10) = T - 530
21812 = T - 530
21812 - 530 = T
T = 21282 N
T ≈ 21,300 N