2/4/2016 FIGURE AC 27.APХ B-1 ROTORCRAFT DYNAMIC STABILITY 35 30
ACCEPTABLE
REQUIREMENTS FOR IFR
UNACCEPTABLE Page Apdx B - 21 -0.2 0.05 Ø.15 AC 27-1B, Chg 7
DAMPING RATIO
AC 27 APPENDIX B (AMENDMENT 27-51) AIRWORTHINESS GUIDANCE FOR ROTORCRAFT INSTRUMENT FLIGHT.
a. Explanation.
(3) Amendment 27-51 revised section VIII (b)(5)(i), which requires isolating the pilot instrument system from any other operating systems, to only apply to pneumatic systems. This change allows other types of pilot instrument systems to be connected to other systems on the rotorcraft and allows the use of modern technology to monitor and display highly integrated information. This guidance remains unchanged except paragraphs (b)(9)(v) and (b)(9)(vi) of this AC section do not apply to nonpneumatic systems.
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