If one soft rivet and one hard rivet are installed on any of the four rod ends, within 200 flight hours or 12 months of the visual inspection required by paragraph (g)(1) of this AD, whichever occurs first after the effective date of this AD, replace the soft rivet with rivet part number MS20470AD4-12 in accordance with the Accomplishment Instructions, paragraph 7., of Beechcraft Mandatory SL MTL-27-07.
Get notified when this obligation is modified in proposed, final, or codified rules.
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