<?xml version="1.0" encoding="UTF-8" standalone="no"?>
<!--
************************************************************************
Sierra Super-II (550) simulation config. This files ties together
all the components used by FGFS to represent the 550. Components
include the flight data model, instrument panel, and external 3D model.

Copyright (c) 2014 Ludovic Brenta <ludovic@ludovic-brenta.org>
This program is free software: you can redistribute it and/or modify
it under the terms of the GNU General Public License as published by
the Free Software Foundation, either version 2 of the License, or
(at your option) any later version.

This program is distributed in the hope that it will be useful,
but WITHOUT ANY WARRANTY; without even the implied warranty of
MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE.  See the
GNU General Public License for more details.

You should have received a copy of the GNU General Public License
along with this program.  If not, see <http://www.gnu.org/licenses/>.

************************************************************************
-->
<PropertyList include="Citation-II-common.xml">
  <sim>
    <aero>Sierra-Super-II-yasim</aero>
    <description>Sierra Super II</description>
    <long-description>
      The Sierra Super II is an aftermarket modification of the Cessna
      550/551 which replaces the engines with Williams International
      FJ44-3 turbofans introduced in 2004.  They provide more thrust
      and less fuel consumption.  Climb performance is dramatically
      improved.  At full takeoff weight, typical cruise speed is 370
      KTAS at FL430; range is 2500 nmi.

      The new engines lack thrust reversers; they are not needed
      because their idle thrust is only 40 lbf, as opposed to 400 lbf
      on the old engines.
    </long-description>
    <fr>
      <long-description>
        Le Sierra Super II est une modification du Cessna 550/551
        pratiquée sur des avions existants.  Elle remplace les
        réacteurs par des Williams FJ44-3 introduits en 2004.  Ces
        nouveaux réacteurs fournissent davantage de poussée et
        consomment moins.  Les performances en montée sont améliorées
        de façon spectaculaire.  Après un décollage à la masse
        maximale autorisée, la vitesse de croisière habituelle est de
        370 noeuds au FL430 et le rayon d'action est de 2500
        nautiques.

        Les nouveaux réacteurs ne disposent pas d'inverseurs de
        poussée; ils sont inutiles car la poussée des réacteurs au
        ralenti n'est que de 178N au lieu de 1780N pour les anciens.
      </long-description>
    </fr>
  </sim>
  <autopilot>
    <limits>
      <!-- the number and ordering of these properties is important for the autopilot;
           see Citation-autopilot.xml, AP vertical stage 1. -->
      <max-climb-rate-fpm type="double">4500</max-climb-rate-fpm>
      <indicated-altitude-ft type="double">14000</indicated-altitude-ft>
      <max-climb-rate-fpm type="double">4000</max-climb-rate-fpm>
      <indicated-altitude-ft type="double">18000</indicated-altitude-ft>
      <max-climb-rate-fpm type="double">3250</max-climb-rate-fpm>
      <indicated-altitude-ft type="double">22000</indicated-altitude-ft>
      <max-climb-rate-fpm type="double">2500</max-climb-rate-fpm>
      <indicated-altitude-ft type="double">27000</indicated-altitude-ft>
      <max-climb-rate-fpm type="double">1250</max-climb-rate-fpm>
      <indicated-altitude-ft type="double">37000</indicated-altitude-ft>

      <max-climb-rate-fpm type="double">750</max-climb-rate-fpm>
    </limits>
  </autopilot>
</PropertyList>
