Answer:
30.72i+ 135.89j +53.46k
Explanation:
If we measure angle φ up from the horizontal and angle θ CCW from east, the direction vector of the airplane at take-off is ...
(ρ, θ, φ) = (173 mph, 90°, 18°)
The rectangular expression of this vector will be ...
(ρ·cos(θ)·cos(φ), ρ·sin(θ)·cos(φ), ρ·sin(φ)) = (0, 164.53, 53.46) . . . mph
__
The wind vector is ...
(ρ, θ, φ) = (42, -43°, 0°) ⇒ (30.72, -28.64, 0) . . . mph
And the rectangular coordinate sum of these vectors is ...
(0, 164.53, 53.46) +(30.72, -28.64, 0) = (30.72, 135.89, 53.46)
The resultant velocity vector of the airplane is ...
30.72i+ 135.89j +53.46k