Daniel B. answered 12/15/22
A retired computer professional to teach math, physics
Let
m = 3000 kg be the mass of the helicopter,
α be the degree of tilt against the vertical,
D = 1200 N be drag,
g = 9.81 m/s² be gravitational acceleration.
Your picture does not make it clear whether the 14° angle is against the vertical or horizontal.
Therefore I will show a solution for some angle α against the vertical.
You need to pug in α = 14° or α = 76° depending on the actual helicopter's orientation.
There are three forces acting on the helicopter:
the drag D, the unknown thrust T, and gravity mg.
The net force is their vector sum.
We are told that the helicopter is not gaining or loosing altitude.
That implies that the vertical component of the net force must be 0.
Let's see who contributes to that vertical component of the net force.
The drag D has no vertical component.
The thrust has vertical component Tcos(α) directed up.
Gravity has vertical component mg directed down.
Therefore
Tcos(α) = mg
So
T = mg/cos(α)
Now compute the horizontal component of the net force, which is the only one that could be non-zero.
Gravity contributes nothing to the horizontal component.
Thrust has horizontal component Tsin(α) oriented forwards.
Drag D is oriented backward.
So the net force F is
F = Tsin(α) - D = mgtan(α) - D
Whichever meaning you pick for the specification if tilt, the next force turns out positive,
which means that it is directed forward.
The helicopter's acceleration, a, by Newton's Second Law is
a = F/m = gtan(α) - D/m