Each angle of attack system sensor must be heated or have an equivalent means of preventing malfunction in the heavy rain conditions defined in Table 1 of Sec. 25.1323, the mixed phase and ice crystal conditions as defined in part 33, Appendix D, of this chapter, the icing conditions defined in Appendix C of this part, and the following icing conditions specified in Appendix O of this part:
(a) For airplanes certificated in accordance with Sec. 25.1420(a)(1), the icing conditions that the airplane is certified to safely exit following detection.
(b) For airplanes certificated in accordance with Sec. 25.1420(a)(2), the icing conditions that the airplane is certified to safely operate in and the icing conditions that the airplane is certified to safely exit following detection.
(c) For airplanes certificated in accordance with Sec. 25.1420(a)(3) and for airplanes not subject to Sec. 25.1420, all icing conditions. [79 FR 65527, Nov. 4, 2014]
Effective Date Note: At 79 FR 65527, Nov. 4, 2014, Sec. 25.1324 was added, effective Jan. 5, 2015.