Document ID: chunk:federal_register_of_legislation:F2024C00332:reg:3:p17
Version: federal_register_of_legislation:F2024C00332
Segment Type: reg
Provision Reference: reg 3 (pt 17/20)
Character Range: 86878–89629

in a way that subjects the crew member to additional flight loads, unless the crew member has been briefed on the manoeuvre by the pilot in command beforehand.
 (9) The crew member must:
 (a) advise the pilot in command, of the rotorcraft, of the crew member's proposed movements in the cabin in-flight; and
 (b) not adversely affect the rotorcraft's centre of gravity or controllability during any movements by the crew member in the cabin in-flight.
 (10) The requirements stated in subsections (2) to (9) are directions to the affected person for the purposes of regulation 11.245 of CASR.
 (11) The directions cease to be in force at the end of 1 December 2024.
 (12) In this section:
relevant approved data means:
 (a) the manufacturer's fitment and use instructions for the equipment; and
 (b) any instructions in the rotorcraft's flight manual about hard points, and securing mechanisms, of the rotorcraft.

Chapter 10 — Performance

Division 1—Preliminary

10.01  Definitions for Chapter 10
  In this Chapter:
adequate vertical margin: see section 10.02.
Category A, in relation to a rotorcraft, means a multi‑engine rotorcraft that is:
 (a) designed with engine and system isolation features stated for Category A requirements in any of the following:
  (i) Part 27 of the FARs;
 (ii) Part 29 of the FARs;
 (iii) EASA CS — 27;
 (iv) EASA CS — 29;
 (v) an equivalent airworthiness certification code of a Contracting State; and
 (b) capable of operation using take‑off and landing data scheduled under a critical engine failure concept, which assures adequate designated ground or water area and adequate performance capability for continued safe flight or safe rejected take‑off in the event of engine failure, as mentioned in the rotorcraft's flight manual.
Note: This definition is based on the ICAO, FAA and EASA definitions of the term Category A in relation to rotorcraft.
Category A rotorcraft means a rotorcraft that:
 (a) meets the requirements stated in the definition of Category A; and
 (b) is type-certificated in accordance with any of the following:
 (i) Part 27 of the FARs;
 (ii) Part 29 of the FARs;
 (iii) EASA CS — 27;
 (iv) EASA CS — 29;
 (v) an equivalent airworthiness certification code of a Contracting State.
D, for a rotorcraft, means the maximum dimension of the rotorcraft.
defined point before landing, for a rotorcraft flying in performance class 2 or performance class 2 with exposure, means the point in the approach and landing stage of the flight after which:
 (a) the rotorcraft may not be able to continue the flight safely with 1 engine inoperative; and
 (b) a forced landing may be required.
exposure time, for a rotorcraft that is flying in still air, means the period during which the rotorcraft, with