Document ID: chunk:federal_register_of_legislation:F2024C00332:reg:8:p6
Version: federal_register_of_legislation:F2024C00332
Segment Type: reg
Provision Reference: reg 8 (pt 6/12)
Character Range: 147427–149986

x S, for the point).
 (5) For subsection (4), if a change of direction of more than 15 degrees is required to achieve the margin, the rotorcraft must be able, during the change of direction, to clear the relevant obstacle by at least the total of:
 (a) the margin; and
 (b) 15 ft.
 (6) If an engine becomes inoperative at or after the landing decision point for the landing, the rotorcraft must be able to safely land and stop within the final approach and take‑off area for the aerodrome.
 (7) The dimensions of the final approach and take‑off area, for the aerodrome, must be at least the larger of the following:
 (a) the dimensions of the final approach and take‑off area, as mentioned in the rotorcraft's flight manual;
 (b) 1.5 x D, for the rotorcraft.

Division 8—Rotorcraft performance — performance class 2

10.37  Performance class 2 — take‑off
 (1) For item 1 of the table in section 10.05, the requirements for the take‑off stage of a flight of a rotorcraft are the requirements stated in this section.
 (2) The take‑off weight of the rotorcraft must not exceed the maximum weight, mentioned in the rotorcraft's flight manual, required:
 (a) for the type of take‑off procedure to be used; and
 (b) to achieve a rate of climb, with 1 engine inoperative, of 150 ft per minute at 1 000 ft above the departure aerodrome for the flight.
 (3) If an engine becomes inoperative before the defined point after take‑off, the rotorcraft must be able to do one of the following without creating a hazard to a person under the flight path:
 (a) safely continue the climb out;
 (b) safely land on a suitable forced landing area for the flight.

10.38  Performance class 2 — take‑off and initial climb
 (1) For item 2 of the table in section 10.05, the requirements for the take‑off and initial climb stage of a flight of a rotorcraft are that, if an engine becomes inoperative at the lower of the following:
 (a) the defined point after take‑off for the rotorcraft;
 (b) 300 ft above the departure aerodrome for the flight;
  the rotorcraft must be able to achieve the rate of climb stated in paragraph 10.37(2)(b), and clear a relevant obstacle, if any, under the flight path by a margin of at least:
 (i) for a VFR flight — 35 ft; or
 (ii) for an IFR flight — the total of:
                   (A) 35 ft; and
                   (B) 0.01 x S, for the point.
 (2) For subsection (1), if a change of direction of more than 15 degrees is required to achieve the margin, the rotorcraft must be able, during the change of direction, to clear the relevant obstacle by