Citabria Wing strut attach fitting 1000 hour inspection

I am being told that the Service Manual for the metal spar Citabria has a 4.2 section, mandating inspection of the inner landing gear leg bolt at 1000 hours.
ACA only sent the single page above - anybody with a recent Citabria Service Manual see the requirement? Did they use a separate page for 4.2? It is not in the type certificate.

Edit - just got a look at a 2001 Decathlon Service Manual. The Airworthiness Limitations section is there, but it is something like Section IX - the last one in the manual. There is an entire page devoted to the mandated lift strut bracket inspection, and not a single word about landing gear bolts.

Note that the above page from the 2011 Citabria manual is dated 2013, so presumably the Chicago ACO decided a less complicated description is appropriate. I do not own a late model ACA bird, and probably will not be more than peripherally involved in any inspections of such aircraft, so I won't be purchasing expensive Service Manuals.

But the fact remains - if these things are important, they should be in an AD, so they apply to all serial numbers.

Still opinion, of course.
 
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