Document ID: chunk:federal_register_of_legislation:F2024C00332:reg:8:p7
Version: federal_register_of_legislation:F2024C00332
Segment Type: reg
Provision Reference: reg 8 (pt 7/12)
Character Range: 149765–152338

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 at least the total of:
 (a) the margin; and
 (b) 15 ft.

10.39  Performance class 2 — en route
  For item 3 of the table in section 10.05, the requirements for the en route stage of a flight of a rotorcraft are, if an engine becomes inoperative during that stage of the flight, the same requirements as those stated in subsection 10.35(1).
Note: Subsection 10.35 (1) states the performance class 1 requirements for the en route stage of a flight of a rotorcraft if an engine becomes inoperative during that stage of the flight.

10.40  Performance class 2 — approach and landing, or baulked landing
 (1) For item 4 of the table in section 10.05, the requirements for the approach and landing, or baulked landing stage of a flight of a rotorcraft are the requirements stated in this section.
 (2) The landing weight of the rotorcraft must not exceed the maximum weight, mentioned in the rotorcraft's flight manual, required:
 (a) for the type of approach 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 landing aerodrome; and
 (c) for the rotorcraft to safely land within the landing distance available for a landing of the rotorcraft at the aerodrome.
 (3) If an engine becomes inoperative before the defined point before landing for the rotorcraft, the rotorcraft must be able to:
 (a) conduct a baulked landing; and
 (b) clear a relevant obstacle, if any, under the baulked landing climb 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.
 (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) During the part of the flight after the defined point before landing for the rotorcraft until the point of landing, a suitable forced landing area for the flight must be available to the rotorcraft.

Division 9—Rotorcraft performance — performance class 3

10.41  Performance class 3 — take‑off
 (1) For item 1 of the table in section 10.07, the requirements for the take‑off stage of a flight of a rotorcraft