Fig. 5From: Evolving base for the fuel consumption optimization in Indian air transport: application of structural equation modelingProposed model of FCO; Notes: AOA fuel tankring, AOB fuel weight, AOC stage length, AOD payload weight, AOE aircraft altitude, AOF aircraft speed, AOG aircraft extra weight, ATDA engine types, ATDB lift/drag, ATDC engine by pass ratio, ATDD design range, ATDE engine thrust, ATDF new aircraft, ATDG structural weight, SEPA fuel price, SEPB ticket price, SEPC aircraft scheduling, SEPD government regulations, SEPE charges & taxes, AIA runway, AIB weather conditions, AIC flight profile, AID terminal area, AIE block hours, AIF taxiway, AIG fuel procurement, AFPA boiling point, AFPB alternate fuel type, FCO fuel consumption optimization, AFPC energy content, AFPD density, e1- e31 are the associated error terms of AOA-FCOA, e32 residual error term of fuel consumption optimizationBack to article page