Document ID: chunk:federal_register_of_legislation:F2014C01352:body:0:p4
Version: federal_register_of_legislation:F2014C01352
Segment Type: other
Provision Reference: 
Character Range: 8387–11375

limitations
       4.1For the purposes of paragraph 235 (2) (a) of the Regulations, the maximum weight that an aeroplane to which this section applies may not exceed at take‑off is the least of the weights determined in accordance with subparagraphs (a) to (d):
(a) a weight at which the take-off distance and accelerate-stop distance required under subsection 6 for the aerodrome elevation, ambient temperature, wind component along the runway, runway slope and runway surface conditions at the time of take-off are equal to or less than the take-off distance and accelerate-stop distance available in the direction of take-off. Approved declared conditions may be used instead of the ambient temperature and aerodrome elevation;
(b) a weight that will permit compliance with the take-off climb requirements mentioned in subsection 7 taking into account either ambient temperature and aerodrome elevation, or approved declared conditions;
(ba) for aeroplanes with maximum take-off weight in excess of 5 700 kg, a weight that will permit compliance with the obstacle clearance requirements mentioned in paragraph 7.5 and subsection 12 for take-off from a dry runway (whether it is dry or not) and taking into account either wind conditions, ambient temperature and aerodrome elevation, or wind conditions and approved declared conditions;
(c) a weight which will permit compliance with the en-route obstacle clearance requirements specified in subsection 12;
(d) a weight which, allowing for normal consumption of fuel and oil in flight to the destination and alternate aerodrome, will permit compliance with the landing weight limitations mentioned in subsection 5.

5 Landing weight limitations
       5.1For the purposes of paragraph 235 (2) (b) of the Regulations, the maximum weight which an aeroplane to which this section applies may not exceed at landing is the least of the weights determined in accordance with subparagraphs (a) to (c):
(a) a weight at which the landing distance required in accordance with subsection 11 for the aerodrome elevation, wind component along the runway, runway slope (when exceeding 1%) and runway surface conditions at the time of landing, is equal to or less than the landing distance available in the direction of landing;
(b) a weight which will permit compliance with the approach climb requirements specified in subsection 9, taking into account forecast or ambient temperature and aerodrome elevation or approved declared conditions;
(c) a weight which will permit compliance with the landing climb requirements specified in subsection 10 taking into account forecast or ambient temperature and aerodrome elevation or approved declared conditions.

6 Accelerate-stop and take-off distance required
       6.1For subparagraph 4.1 (a), and subject to paragraphs 6.3.4 and 6.4, the accelerate-stop distance required is the distance set out in the flight manual.
       6.2.1For subparagraph 4.1 (a), and subject to paragraphs 6.3.4 and 6.4, the