My take on this -- basically the same method as statickid's. Takes 7 days instead of 3, but doesn't require advanced navigation:
1. Left MFD - Orbit, reference: Moon.
2. Right MFD - Map, reference: Moon.
3. When crossing 180 deg. longitude burn prograde raising your apoapsis above 100Mm or so. (It helps if your initial lunar orbit is retrograde and equatorial). You have entered a highly elliptic lunar orbit, with apoapsis in the direction of Earth, past the Lagrange point.
4. Right MFD - Orbit, reference: Earth.
5. Sit down and relax. When you near apoapsis, observe the G-indicator in the left MFD going down, while the G-indicator in the right MFD will be going up.
6. If you did everything right (i.e. went past the Lagrange point), Earth's gravity will capture you and you will enter an Earth orbit.
7. Burn retrograde to lower periapsis. If you want to do a direct entry, lower periapsis to be inside atmosphere (typically 60-70km) and aerobrake. Be careful though, you will enter the atmosphere pretty fast...
8. If you don't want to do a direct entry, lower periapsis to ~1000 km and then burn retrograde at periapsis to circularize.
9. Do a normal orbital reentry.
A video illustrating the concept:
Another method -- TransX + direct entry with XR2:
[ame="http://www.youtube.com/watch?v=S-hedEal3ko"]Orbiter: Moon to Earth with Direct Entry - YouTube[/ame]