\section{General Data}

\begin{tabularx}{\textwidth}{ | L | c | c | }
  \hline
  \textbf{Parameter}                    & \textbf{Value}   & \textbf{Reference} \\ \hline
  \endfirsthead
  \hline
  \textbf{Parameter}                    & \textbf{Value}   & \textbf{Reference} \\ \hline
  \endhead
  Length                                & 8.28 m           & \cite{Cessna172_InformationManual,Janes20042005} \\ \hline
  Wingspan                              & 11.00 m          & \cite{Cessna172_InformationManual,Janes20042005} \\ \hline
  Height                                & 2.72 m           & \cite{Cessna172_InformationManual,Janes20042005} \\ \hline
  Wheelbase                             & 1.63 m           & \cite{Janes20042005} \\ \hline
  Wheel track                           & 2.53 m           & \cite{Janes20042005} \\ \hline
  Wing area                             & 16.17 m\textsuperscript{2} & \cite{Cessna172_InformationManual,Janes20042005} \\ \hline
  Mean aerodynamic chord                & 1.49 m           & \cite{Cessna172_InformationManual} \\ \hline
  Wing airfoil                          & NACA 2412        & \cite{Janes20042005} \\ \hline
  Horizontal tail area                  & 2.00 m\textsuperscript{2} & \cite{Janes20042005} \\ \hline
  Horizontal tail airfoil at root (Cessna 177) & NACA 0012 & \cite{Torenbeek1982} \\ \hline
  Horizontal tail airfoil at tip (Cessna 177)  & NACA 0009 & \cite{Torenbeek1982} \\ \hline
  Vertical tail area                    & 1.04 m\textsuperscript{2} & \cite{Janes20042005} \\ \hline
  Vertical tail airfoil at root         & NACA 0009        & \cite{NASA-CR-158974} \\ \hline
  Vertical tail airfoil at tip          & NACA 0006        & \cite{NASA-CR-158974} \\ \hline
  Ailerons deflection limit             & up 20\degree, down 15\degree & \cite{EASA-IM-A-051} \\ \hline
  Ailerons area (total)                 & 1.70 m\textsuperscript{2} & \cite{Janes20042005} \\ \hline
  Elevator deflection limit             & up 28\degree, down 23\degree & \cite{EASA-IM-A-051} \\ \hline
  Elevator area (including trim tab)    & 1.35 m\textsuperscript{2} & \cite{Janes20042005} \\ \hline
  Elevator trim tab deflection limit    & up 22\degree, down 19\degree & \cite{EASA-IM-A-051} \\ \hline
  Rudder deflection limit               & $\pm$17.7\degree & \cite{EASA-IM-A-051} \\ \hline
  Flaps area                            & 1.98 m\textsuperscript{2} & \cite{Janes20042005} \\ \hline
  Flaps deflection limit                & 30\degree        & \cite{EASA-IM-A-051} \\ \hline
  Standard empty weight                 & 754 kg           & \cite{Cessna172_InformationManual} \\ \hline
  Total fuel tanks capacity             & 212 l            & \cite{Cessna172_InformationManual,EASA-IM-A-051} \\ \hline
  Downwash angle derivative with respect to the aircraft angle of attack & 0.25 & \cite{NASA-CR-2605} \\ \hline
  Engine manufacturer                   & Textron Lycoming & \cite{Cessna172_InformationManual} \\ \hline
  Engine model                          & IO-360-L2A       & \cite{Cessna172_InformationManual} \\ \hline
  Engine rated power (at 2~700 RPM)     & 134.2 kW         & \cite{Cessna172_InformationManual,Cessna172_TextronLycomingOperatorsManual} \\ \hline
  Engine displacement                   & 5.9 l            & \cite{Cessna172_InformationManual} \\ \hline
  Engine height                         & 0.631 m          & \cite{Cessna172_TextronLycomingOperatorsManual} \\ \hline
  Engine width                          & 0.848 m          & \cite{Cessna172_TextronLycomingOperatorsManual} \\ \hline
  Engine length                         & 0.757 m          & \cite{Cessna172_TextronLycomingOperatorsManual} \\ \hline
  Engine standard dry weight            & 126.1 kg         & \cite{Cessna172_TextronLycomingOperatorsManual} \\ \hline
  Specific fuel consumption (at 2~200 RPM) & 253.4 g/(kW$\cdot$h) & \cite{Cessna172_TextronLycomingOperatorsManual} \\ \hline
  Propeller manufacturer                & McCauley         & \cite{Cessna172_InformationManual} \\ \hline
  Propeller model                       & 1A170E/JHA7660   & \cite{Cessna172_InformationManual} \\ \hline
  Number of blades                      & 2                & \cite{Cessna172_InformationManual} \\ \hline
  Propeller diameter                    & 1.93 m           & \cite{Cessna172_InformationManual} \\ \hline
  \caption{General Data}
\end{tabularx}
