What was found
FUSELAGE ATTACH FITTINGS: AFTER GEAR/FLAP RETRACTION FROM ORL, WE FELT A VIBRATION THROUGH THE FUSELAGE BETWEEN 500-700 FEET MSL. DIVERTED TO MCO AND LANDED WITHOUT INCIDENT. (UPDATE/CORRECTION TO SDR-ATC DECLARED AN EMERGENCY ON THE CREWS BEHALF). JACKED UP AIRCRAFT. HOOKED UP HYDRAULICS AND RETRACTED GEAR. FOUND R/H MLG DOOR LOOSE, ADJUSTED AS NECESSARY. ALL LANDING GEAR DOORS FIT CHECK GOOD WITH GEAR RETRACTED. WORK PERFORMED IAW CE680A MM 52-80-25. PERFORMED ANTI-SPIN FUNCTIONAL CHECK, NO DEFECTS NOTED. WORK PERFORMED IAW CE680A MM 32-42-00.