Document ID: chunk:federal_register_of_legislation:F2024C00333:reg:2:p2
Version: federal_register_of_legislation:F2024C00333
Segment Type: reg
Provision Reference: reg 2 (pt 2/3)
Character Range: 65797–68651

instructions, not more than 50% of the headwind component, or not less than 150% of the tailwind component, for the runway.

10.08  Initial climb performance and obstacle clearance
 (1) This section applies if the flight of an aeroplane is an IFR flight, or VFR flight at night.
 (2) The operator, and pilot in command, must each ensure that until the aeroplane reaches the minimum height (the relevant height) for the flight in accordance with regulation 91.265, 91.267, 91.277, or 91.305, of CASR, as applicable:
 (a) for all flights — the aeroplane has the performance to clear all obstacles by a safe margin, as determined by the operator's exposition; and
 (b) for flights not conducted in VMC by day — the aeroplane has the performance to reach, and maintain, the relevant height.
 (3) For the purposes of subsection (2), the following matters must be taken into account:
 (a) the take-off configuration of the aeroplane;
 (b) the pressure altitude, and presumed temperature, at the aerodrome;
 (c) the obstacles, if any, in the vicinity of the take‑off path and en route;
 (d) the forecast weather en route.

10.09  En route obstacle clearance for multi‑engine aeroplane
 (1) The operator, and pilot in command, of a multi-engine aeroplane must each ensure that the aeroplane has the performance to conduct the flight in accordance with regulation 91.265, 91.267, 91.277, or 91.305, of CASR, as applicable, if:
 (a) an engine of the aeroplane becomes inoperative, during a flight, before the aeroplane reaches the planned cruising altitude, or cruising level, for the flight; and
 (b) each remaining engine of the aeroplane is operating within the maximum continuous power limitations stated in the aeroplane's flight manual.
 (2) Subsection (1) does not apply if the operator's exposition states procedures requiring the pilot in command to have a plan, in the circumstances mentioned in subsection (1), that enables the aeroplane to return to the departure aerodrome, or divert to a take‑off alternate aerodrome, clear of all ground, water and obstacles.
 (3) The procedures mentioned in subsection (2) may include drift-down procedures, provided that the procedures enable the aeroplane to descend, and land, at an aerodrome with at least 2 000 ft vertical separation from all ground, water and obstacles within 5 nautical miles on either side, or ahead, of the aeroplane's track until established within the aerodrome's circuit area.

Subdivision 3—Landing performance

10.10  Purpose of Subdivision 3
  The purpose of this Subdivision is to prescribe requirements for subregulation 135.350(1) of CASR.

10.11  Meaning of factored landing distance
  For an aeroplane mentioned in column 1 of an item in Table 10.11, conducting a landing mentioned in column 2 of the item, the factored landing distance is the landing distance required, for the