Light follows null geodesics. Those geodesics are curved near any concentration of mass / energy, but spacetime curvature is usually quite small, except in extreme circumstances.
There's a difference between gravitational field strength and gravitational potential. The field strength is basically the gravitational acceleration, so it determines how heavy you feel when you're standing on a planet, or hovering above it. But the potential controls things like orbital motion and escape velocity.
In Newtonian gravity, the acceleration due to a point source or uniform sphere is given by
$$g = GM/r^2$$
The potential is given by
$$\Phi = -GM/r$$
Note that the field strength is the derivative of the potential,
$$g = \frac{d\Phi}{dr}$$
The circular orbit velocity is given by
$$v^2 = GM/r$$
and the escape velocity is given by
$$v_e^2 = 2GM/r$$
Combining the last equation with the first acceleration equation we get
$$v_e^2 = 2gr$$
So two planets with identical surface gravity $g$ but different density can have very different escape velocities. If you were on a planet with Earth gravity but four times the radius (so much lower density), the escape velocity would be twice as high, and rockets would need four times the kinetic energy to escape. And of course escape velocity also affects what gases a planet can retain in its atmosphere.
I should also mention that the tidal stress is determined by the derivative of the field strength, so it's proportional to $1/r^3$.
It may seem counter-intuitive that for two planets with identical surface gravity that the one with lower density has the higher escape velocity. Density is mass per unit volume, so a sphere of radius $r$ and mean density $\rho$ has mass
$$M = \left(\frac{4\pi}{3}\right) r^3 \rho$$
Plugging that into our previous equations, we get
$$g = \left(\frac{4\pi G}{3}\right) r \rho$$
and
$$v_e^2 = \left(\frac{8\pi G}{3}\right) r^2 \rho$$
So for a fixed $g$, $r$ and $\rho$ are inversely proportional. If we multiply $r$ by some constant $k$ and divide $\rho$ by $k$ then $g$ remains the same, but $v_e^2$ is multiplied by $k$.
Rearranging the previous equation for $g$, we get
$$r = \left(\frac3{4\pi G}\right)g/\rho$$
Plugging that into $v_e^2 = 2gr$ we get
$$v_e^2 = \left(\frac3{2\pi G}\right)g^2/\rho$$
or
$$v_e = \sqrt{\frac3{2\pi G}}\left(\frac{g}{\sqrt{\rho}}\right)$$
So escape velocity is proportional to $g$, but inversely proportional to the square root of the mean density.
The equations are slightly more complicated in GR, but the same principle applies.
The Schwarzschild radius of a body is proportional to its mass
$$r_s = 2GM/c^2$$
The photon sphere radius is just $1.5×r_s$.
Near a small black hole of a few solar masses, the field strength changes quickly with radial distance, so the tidal stress is extreme. For example, a $3 M_\odot$ (solar mass) BH, has $r_s \approx 8.860$ km. The tidal stress on a $1$ metre long A36 steel bar in vertical freefall is enough to rupture it at a distance of $112$ km. That makes it a bit tricky to observe curved light trajectories without a telescope. ;)
But around a SMBH the field strength changes slowly, so in freefall you can safely approach the vicinity of its photon sphere. You can even cross the event horizon without being spaghettified.
However, it's still not exactly easy to get close to a SMBH with safety. If you're falling towards the BH, or in an orbit, you have to be moving at relativistic speed. You can't simply hover: the field strength is extremely high, so your hovering rocket would need extreme acceleration. That requires a ridiculous amount of fuel, and the acceleration would crush you and your ship into an atom-thick paste.
I haven't actually said much about the gravitational deflection of light. I have some info about that in my recent answer to Are there actually any photons in orbit in the photon sphere of a black hole? which also links to a couple of other answers I've written on this topic.
On Astronomy.SE I wrote:
Here's a simple approximation for the deflection angle [of a light ray] which is valid when the deflection angle is small:
$$\theta = \frac{2r_s}b$$
where $\theta$ is in radians, $r_s$ is the Schwarzschild radius of the lensing body, and $b$ is the impact parameter of the light ray, which is basically the minimum distance between the ray and the centre of the lensing body if you could turn gravity off so that the ray was just a straight line.
A more accurate equation for small deflections is
$$\theta = \frac2{r/r_s - 71/73}$$
where $r$ is the minimum distance from the deflected ray to the centre of the lensing body. The exact equation relating $b$ and $r$ is
$$b^2 = \frac{r^3}{r-r_s}$$
When $b$ is large, $r \approx b - r_s/2$.
When $b$ is small, we need to use an elliptic integral to compute the deflection. Here's a diagram of a ray deflected by 60°, with $b\approx 3.62r_s$, from the Physics.SE answer I linked above.

The diagram uses units where $r_s=1$, so it applies to any Schwarzschild black hole. The circle of radius $1$ is the event horizon, $b$ is is the perpendicular distance from the dashed black lines to the BH, and $r$ is the length of the dashed purple line where the trajectory makes its closest approach to the BH. Actually, the diagram applies to any spherically symmetrical body with negligible spin, but only black holes and neutron stars are smaller than their photon sphere.
For typical stars and planets we can calculate the deflection angle using the equation I gave earlier, $\theta = \frac2{r/r_s - 71/73}$. The relative error in using this equation to compute the deflection angle near the Sun is ~$8.21×10^{-11}$.
The Schwarzschild radius of the Sun is ~$2.95325$ km. The radius of its photosphere is ~$695700$ km. So the deflection of a ray of starlight grazing the Sun during a solar eclipse is ~$1.7511976$ arc-seconds or ~$1/117785$ radians. Thus the star's apparent position is shifted by ~$1.75$ arcsecs, and the deflected light ray drops by ~$1$ mm over a distance of $117.785$ metres.
The Schwarzschild radius of the Earth is only ~$8.870056$ mm. Its equatorial radius is ~$6378.137$ km. So the deflection of a light ray near the Earth's surface is only ~$0.000573704$ arcsecs or ~$1/359531949$ radians. That's very tiny, and totally undetectable in the atmosphere. If you have a light beam travelling through an evacuated horizontal pipe $359.5$ km long, the beam only drops $1$ mm.