Document ID: chunk:federal_register_of_legislation:F2005B00781:body:0:p4
Version: federal_register_of_legislation:F2005B00781
Segment Type: other
Provision Reference: 
Character Range: 7974–10891

elevation of the aerodrome to the aerodrome elevation co-ordinate. Move vertically to intersect the take-off climb limitation line.
2.6 From this point move horizontally and read the all-up weight. Record the weight thus obtained.
2.7 The maximum permissible take-off weight shall be the lesser of the 2 weights as determined in paragraphs 2.4 and 2.6 above.
2.8 The take-off weight as obtained by the foregoing method shall apply only where the aeroplane is to be flown in the configuration specified in the relevant Take-off Weight Chart and with the engine power specified therein. The use of any other configuration or engine power is prohibited except where an application to use some other condition has been made to CASA and it has approved such condition.

APPENDIX 2
CASA LANDING WEIGHT CHARTS — P SERIES —
INSTRUCTIONS FOR USE
1 Under Ambient Conditions:
1.1 Obtain the forecast temperature and pressure altitude for the destination aerodrome.
1.2 Apply the pressure altitude to the pressure altitude in feet co-ordinate on the chart. Move vertically to intersect the temperature line representing the forecast temperature.
1.3 From this point move horizontally to intersect the corrected effective operational length to the corrected effective operational length available for landing.
1.4 Move vertically downwards and read take-off weight. Record the weight thus obtained.
1.5 Ascertain the elevation of the aerodrome.
1.6 Apply this elevation to the aerodrome elevation co-ordinate. Move vertically to intersect the landing climb limitation line.
1.7 From this point move horizontally and read the landing weight. Record the weight thus obtained.
1.8 The maximum permissible landing weight is the lesser of the 2 weights as determined in paragraphs 1.4 and 1.7 above.
1.9 The landing weight as obtained by the foregoing method shall apply only when 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.
1.10 When it is necessary to specify an alternate aerodrome, the above procedure shall be repeated for that aerodrome.
2 Under Declared Conditions:
2.1 Use the appropriate seasonal Declared Density Altitude Chart, and add the elevation of the destination aerodrome to the value(s) read from the chart and thus obtain the declared seasonal density altitude.
2.2 Apply the declared seasonal density altitude to the density altitude co-ordinate of the landing weight chart. Move horizontally to intersect the 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