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- distortions, cracks, corrosion, binding and slack, - correct safetying of attachment nuts (44) of hinge bolts with cotter pins, - slack and loose rivets on bellcranks (45) spacers (46). 3) Inspect the brackets of bellcranks (45) for : - distortions, cracks, corrosion and loose rivets. 4) Inspect input rod (49) for : - slack, buckling, cracks, corrosion and binding, - correct safetying of the locking nuts of adjustable rod ends (48), - correct safetying of attachment nut (47) onto bellcrank (45) with a cotter pin, - correct safetying of bolt (55) to the aileron structure with lock plate (53). Ity : S / N 1 - 9999 7alAA Validity 00Page 208 (BA) SEP 04 5) Inspect arm assemblies (51) for : - distortions, cracks and corrosion, - security of arm assemblies (51) to the wings, - slack or binding of the ball joint, - correct safetying of aileron attachment bolts (54) with lock plates (53), - presence and correct tightening of stop screw (52) in the aperture of arm assy (51). F. Final steps 1) Make sure all the tools and materials are removed and the work area is clean and free from debris. 2) Install inspection doors 511, 512, 513, 611, 612 and 613. 3) Install the cowling under hull 218. 4) Install inspection doors 235L and 235R, 211L and 211R (if installed) or install the instrument panel covers, reposition and lock the instrument panel. 5) Remove the warning sign prohibiting main switch-breaker operation. 7 ty : S / N 1 - 9999 AA Validity 209 (BA) SEP 04 J ° i 18 - Torque rod |