Document ID: chunk:federal_register_of_legislation:F2024C00332:reg:8:p3
Version: federal_register_of_legislation:F2024C00332
Segment Type: reg
Provision Reference: reg 8 (pt 3/12)
Character Range: 140388–142991

the take‑off decision point, for the take-off, with 1 engine inoperative, by at least 35 ft; and
                   (B) if the take‑off is from an elevated aerodrome, the rotorcraft must be able to clear the edge of the aerodrome by at least 4.5 m.
 (4) If an engine becomes inoperative before the take‑off decision point for the take‑off, the rotorcraft must be able to safely land and stop within the rejected take‑off distance available – rotorcraft for the take-off.
 (5) If an engine becomes inoperative while the rotorcraft is conducting a back‑up take‑off procedure or a lateral transition take‑off procedure, the rotorcraft must be able to clear a relevant obstacle under the flight path for the procedure or transition by at least the adequate vertical margin, for the rotorcraft, for the take‑off stage of the flight.
 (6) 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.
 (7) In this section:
elevated aerodrome means an aerodrome situated on a raised structure.

10.34  Performance class 1 — take‑off and initial climb
 (1) For item 2 of the table in section 10.04, the requirements for the take‑off and initial climb stage of a flight of a rotorcraft are the requirements stated in this section.
 (2) If an engine becomes inoperative after the take‑off decision point, for the take-off, the rotorcraft must be able to achieve the rates of climb stated in paragraph 10.33(2)(b).
 (3) If an engine becomes inoperative after the take‑off decision point, for the take-off, the rotorcraft must be able, from the end of the take‑off distance required – rotorcraft for the take‑off until the rotorcraft reaches the minimum flight altitude for each point in the take‑off and initial climb stage of the flight, to clear a relevant obstacle under the flight path by a margin of at least:
 (a) for a VFR flight — 35 ft; and
 (b) for an IFR flight — the total of:
 (i) 35 ft; and
 (ii) 0.01 x S, for the point.
 (4) For subsection (3), 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.
 (5) For subsection (4), the rotorcraft may change direction by more than 15 degrees only if the rotorcraft is permitted to do so under its flight manual.

10.35  Performance class 1 — en route
 (1) For item 3 of the