The applicant must prepare a Rotorcraft-Load Combination Flight Manual and submit it for approval by the Administrator. The manual must be prepared in accordance with the rotorcraft flight manual provisions of subpart G of part 27 or 29 of this chapter, whichever is applicable. The limiting height-speed envelope data need not be listed as operating limitations. The manual must set forth—

1. (a) Operating limitations, procedures (normal and emergency), performance, and other information established under this subpart;
2. (b) The class of rotorcraft-load combinations for which the airworthiness of the rotorcraft has been demonstrated in accordance with §§ 133.41 and 133.43; and

3. (c) In the information section of the Rotorcraft-Load Combination Flight Manual—

   1. (1) Information on any peculiarities discovered when operating particular rotorcraft-load combinations;
   2. (2) Precautionary advice regarding static electricity discharges for Class B, Class C, and Class D rotorcraft-load combinations; and
   3. (3) Any other information essential for safe operation with external loads.

[Docket 1529, 29 FR 603, Jan. 24, 1964, as amended by Amdt. 133-9, 51 FR 40709, Nov. 7, 1986]