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21) Apply a bead of sealant (TB 09-002A) to the periphery of the stiffener and inside the wing along the spar (on both sides, and only over the repaired length).
22) On the repaired area, smear the spar flanges (extend beyond the edge, on the skin) and the rivet shanks 0 with sealant (TB 09-013A).
23) On the non-opened area included between Ni and N4 ribs, protect the spar flanges / skins junction with waterproof compound (TB 05-027).
24) Perform paint touch-ups on the rivet heads and on the sealant seal.
ABAA
Validity : S / N 1 - 9999 57 00 00Page 809
(CA) SEP 04
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