Document ID: chunk:federal_register_of_legislation:F2005B00781:body:0:p5
Version: federal_register_of_legislation:F2005B00781
Segment Type: other
Provision Reference: 
Character Range: 10598–11568

corrected effective operational length line corresponding to the corrected effective operational length available for landing.
2.3 Move vertically downwards and obtain the landing weight. Record the weight thus obtained.
2.4 Ascertain the elevation of the destination aerodrome.
2.5 Apply this elevation to the aerodrome elevation co-ordinate. Move vertically to intersect the landing climb limitation line.
2.6 From this point move horizontally and read the landing weight. Record the weight thus obtained.
2.7 The maximum permissible landing weight shall be the lesser of the 2 weights as determined in paragraphs 2.3 and 2.6 above.
2.8 The landing weight as obtained by the foregoing method shall apply only where the aeroplane is to be flown in the configuration specified in the relevant Landing Chart. The use of any other configuration is prohibited except where an application to use some other condition has been made to CASA and it has approved such condition.