Document ID: chunk:federal_register_of_legislation:F2024C00333:reg:2:p1
Version: federal_register_of_legislation:F2024C00333
Segment Type: reg
Provision Reference: reg 2 (pt 1/3)
Character Range: 63188–66039

2                                  Propeller‑driven aeroplane for which there is an approved take‑off factor  The approved take‑off factor for the aeroplane

10.05  Approval of take‑off factor for a propeller‑driven aeroplane
  CASA may, under regulation 135.020 of CASR, approve a take‑off factor for a propeller‑driven aeroplane, for operations at a particular aerodrome, which is less than the standard take‑off factor for the aeroplane, only if the proposed take‑off factor has been risk-assessed by the aeroplane's operator for operations at the aerodrome.

10.06  Maximum permitted take-off weight
  The operator, and pilot in command, must each ensure that, at take‑off, the aeroplane's weight does not exceed each of the following:
 (a) a weight that would enable the aeroplane to meet the requirements stated in sections 10.07 to 10.09;
 (b) a weight that, taking account of the expected consumption of fuel and oil for the flight, will ensure a landing weight that does not exceed the maximum landing weight;
 (c) a weight that will ensure a landing weight that, taking account of the expected consumption of fuel and oil for the flight, complies with Subdivision 3.
Note: The weight at take-off for an aeroplane is also limited by the maximum take‑off weight for the aeroplane, which in the Dictionary, for a type certificated aeroplane, is defined to mean the maximum take-off weight for the aeroplane permitted by its flight manual. It is an offence under regulation 91.095, or 135.040, of CASR if an aeroplane is not operated in accordance with the aeroplane's aircraft flight manual instructions.

10.07  Take-off requirements
 (1) The operator, and pilot in command, must each ensure:
 (a) the factored take-off run, for a take-off of the aeroplane from a runway at an aerodrome, does not exceed the take-off run available for the runway; and
 (b) the take-off distance required for a take-off of the aeroplane from the runway does not exceed the take-off distance available for the runway; and
 (c) any clearway forming part of the take-off distance available for the runway does not exceed half the length of the take-off run available for the runway.
 (2) For the purposes of subsection (1), 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 type of runway surface, and runway surface condition;
 (d) the runway slope in the direction of take‑off;
 (e) unless otherwise accounted for in the performance data set out in the aeroplane's aircraft flight manual 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