What was found
(CAN) AFTER TAKEOFF FLIGHT INCURRED A LANDING GEAR SHOCK ABSORBER FAULT AND AN INDICATION THAT THE NOSE WHEEL DOORS WERE NOT CLOSED AND LOCKED. A PATCH WITH MAINTENANCE CONTROL WAS CARRIED OUT. THE PILOT DID NOT WANT TO RETURN OUT OF CONCERNS FOR POSSIBLE TURBULENCE AND ELECTED TO CARRY OUT A DIVERSION. RESOLUTION ACFT JACKED IAW 07-11-00-581-001 FOUND FORE, AFT GAP ON 24GA AND 25GA OUT OF TOLERANCE. FOUND TARGET SUPPORT ON NOSE GEAR LOOSE. SUPPORT TIGHTENED AND CHECKED SERV IAW 32-31-73-820-006.