TB 1-1520-237-25-2
.STA 648
FRAME
Figure 9. TAIL CONE STRUCTURE (Sheet 2 of 2)
Bulkhead F.S. 605 (Army/Air Force): Examine the tail cone bulkhead, F.S.605, for cracks,
(d)
dents, scratches, and corrosion.
Deleted.
(e)
Area Around the Flight Control Pulleys: Remove the tail cone flight controls access panel
(f)
and examine the airframe around the area of the flight control pulleys for cracks, corrosion,
and loose or missing fasteners.
Canted Hinge: Examine the tail cone canted hinge bulkhead, F.S. 647, for cracks, dents,
(g)
scratches, excess wear, and corrosion.
Change 1 A-15
