// Weights
for(i=0; i<_weights.size(); i++) {
WeightRec* wr = (WeightRec*)_weights.get(i);
- _airplane.setWeight(wr->handle, fgGetFloat(wr->prop));
+ _airplane.setWeight(wr->handle, LBS2KG * fgGetFloat(wr->prop));
}
}
Thruster* t = er->eng;
sprintf(buf, "%s/fuel-flow-gph", er->prefix);
- fgSetFloat(buf, (t->getFuelFlow()/fuelDensity) * 3600 * CM2GALS);
+ fgSetFloat(buf, (t->getFuelFlow()/fuelDensity) * 3600 * CM2GALS);
if(t->getPropEngine()) {
PropEngine* p = t->getPropEngine();