11136 Federal Register / Vol. 81, No. 42 / Thursday, March 3, 2016 / Proposed Rules under Executive Order 13132. This (e) Reason FAA, has the authority to approve AMOCs proposed AD would not have a This AD was prompted by mandatory for this AD, if requested using the procedures substantial direct effect on the States, on continuing airworthiness information (MCAI) found in 14 CFR 39.19. Send information to the relationship between the national originated by an aviation authority of another ATTN: Jim Rutherford, Aerospace Engineer, country to identify and correct an unsafe FAA, Small Airplane Directorate, 901 Locust, Government and the States, or on the Room 301, Kansas City, Missouri 64106; distribution of power and condition on an aviation product. The MCAI describes the unsafe condition as insufficient telephone: (816) 329–4165; fax: (816) 329– responsibilities among the various material strength of the tail-fuselage 4090; email:
[email protected]. Before levels of government. attachment fitting. We are issuing this AD to using any approved AMOC on any airplane For the reasons discussed above, I detect and correct tail-fuselage fittings with to which the AMOC applies, notify your appropriate principal inspector (PI) in the certify this proposed regulation: insufficient material strength, which if left uncorrected could result in detachment of FAA Flight Standards District Office (FSDO), (1) Is not a ‘‘significant regulatory the tail from the fuselage with consequent or lacking a PI, your local FSDO. action’’ under Executive Order 12866, loss of control. (2) Airworthy Product: For any requirement (2) Is not a ‘‘significant rule’’ under in this AD to obtain corrective actions from (f) Actions and Compliance a manufacturer or other source, use these the DOT Regulatory Policies and actions if they are FAA-approved.