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<!-- Written on 27-Apr-2009 15:16:13 using the XML Toolbox for Matlab -->
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    <Fore_fairing_tank_length idx="1" type="double" size="1 1">0</Fore_fairing_tank_length>
    <Aft_fairing_tank_length idx="1" type="double" size="1 1">0</Aft_fairing_tank_length>
    <Aft_fuse_bladder_length idx="1" type="double" size="1 1">0</Aft_fuse_bladder_length>
    <Increment_for_aux_tanks idx="1" type="double" size="1 1">0</Increment_for_aux_tanks>
  </fuel>
  <Baggage idx="1" type="struct" size="1 1">
    <installation_type idx="1" type="double" size="1 1">0</installation_type>
    <gross_volume idx="1" type="double" size="1 1">0</gross_volume>
    <Baggage_combined_length idx="1" type="double" size="1 1">0</Baggage_combined_length>
    <Baggage_apex_per_fuselgt idx="1" type="double" size="1 1">0</Baggage_apex_per_fuselgt>
  </Baggage>
  <cabin idx="1" type="struct" size="1 1">
    <Cabin_length_to_aft_cab idx="1" type="double" size="1 1">13.1</Cabin_length_to_aft_cab>
    <Cabin_max_internal_height idx="1" type="double" size="1 1">2.2</Cabin_max_internal_height>
    <Cabin_max_internal_width idx="1" type="double" size="1 1">3</Cabin_max_internal_width>
    <Cabin_floor_width idx="1" type="double" size="1 1">2.6</Cabin_floor_width>
    <Cabin_volume idx="1" type="double" size="1 1">92</Cabin_volume>
    <Cabin_attendant_number idx="1" type="double" size="1 1">1</Cabin_attendant_number>
    <Flight_crew_number idx="1" type="double" size="1 1">3</Flight_crew_number>
    <Passenger_accomodation idx="1" type="double" size="1 1">40</Passenger_accomodation>
    <Seats_abreast_in_fuselage idx="1" type="double" size="1 1">3</Seats_abreast_in_fuselage>
    <Seat_pitch idx="1" type="double" size="1 1">0</Seat_pitch>
    <Maximum_cabin_altitude idx="1" type="double" size="1 1">8000</Maximum_cabin_altitude>
    <Max_pressure_differential idx="1" type="double" size="1 1">7.4586284760521</Max_pressure_differential>
  </cabin>
  <miscellaneous idx="1" type="struct" size="1 1">
    <Design_classification idx="1" type="double" size="1 1">2.1</Design_classification>
    <Spoiler_effectivity idx="1" type="double" size="1 1">100</Spoiler_effectivity>
    <Undercarriage_layout idx="1" type="double" size="1 1">0</Undercarriage_layout>
    <Target_operating_ceiling idx="1" type="double" size="1 1">0</Target_operating_ceiling>
  </miscellaneous>
  <weight_balance idx="1" type="struct" size="1 1">
    <Ramp_increment idx="1" type="double" size="1 1">46</Ramp_increment>
    <Weight_cont_allow_perc_of_MEW idx="1" type="double" size="1 1">0</Weight_cont_allow_perc_of_MEW>
    <Manufacturer_weights_tolerance idx="1" type="double" size="1 1">872</Manufacturer_weights_tolerance>
  </weight_balance>
  <flight_envelope_prediction idx="1" type="struct" size="1 1">
    <VD_Flight_envelope_dive idx="1" type="double" size="1 1">365</VD_Flight_envelope_dive>
    <VMO_Flight_envelope idx="1" type="double" size="1 1">285</VMO_Flight_envelope>
  </flight_envelope_prediction>
  <Wetted_areas idx="1" type="struct" size="1 1">
    <increment_fuselage_fairing idx="1" type="double" size="1 1">0</increment_fuselage_fairing>
    <increment_wings idx="1" type="double" size="1 1">0</increment_wings>
    <increment_winglet idx="1" type="double" size="1 1">0</increment_winglet>
    <increment_Vertical_tail idx="1" type="double" size="1 1">0</increment_Vertical_tail>
    <increment_pylons idx="1" type="double" size="1 1">0</increment_pylons>
    <increment_powerplant idx="1" type="double" size="1 1">0</increment_powerplant>
    <increment_Horizontal_tail idx="1" type="double" size="1 1">0</increment_Horizontal_tail>
    <anciliary_final idx="1" type="double" size="1 1">0</anciliary_final>
  </Wetted_areas>
</root>

