Did not remove upper forward fuselage skin - currently installed as part of cowling fit. Did not need to check for loose rivets since incorporating this Service Bulletin prior to placing aircraft into service. Will need to remove upper forward fuselage skin at a later time to clean up wiring and will remove rivet reminants at that time. (steps 1 and 2)
Removed 6 rivets at specified locations for each engine mount bracket. (step 3)
Installed six CR3213-4-2 Cherry Max rivets at each engine mount bracket. (step 4)
Upper forward fuselage skin already installed - never removed for this Service Bulletin. (step 5)
Logbook entry will be made prior to completion of PAP. (step 6)
