M20TN PILOT’S OPERATING HANDBOOK

1--3 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1--4 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1--5 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1--6 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1--7 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1--8 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1--9 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1--10 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1--11 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1--12 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1--13 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1--14 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2--1 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2--2 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2--3 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2--4 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2--5 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2--6 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2--7 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2--8 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2--9 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2--10 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2--11 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2--12 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2--13 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2--14 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2--15 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2--16 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2--17 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2--18 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2--19 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2--20 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3--1 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3--2 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3--3 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3--4 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3--5 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3--6 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3--7 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3--8 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3--9 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3--10 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . MOONEY M20TN INTRODUCTION ii POH/AFM POH--003900 This POH/AFM effective with S/N 31--0001 THRU 31--TBA ORIGINAL ISSUE -- 12--22--2006 3--11 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3--12 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3--13 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3--14 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3--15 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3--16 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3--17 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3--18 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3--19 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3--20 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3--21 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3--22 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3--23 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3--24 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4--1 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4--2 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4--3 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4--4 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4--5 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4--6 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4--7 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4--8 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4--9 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4--10 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4--11 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4--12 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4--13 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4--14 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4--15 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4--16 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4--17 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4--18 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5--1 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5--2 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5--3 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5--4 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5--5 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5--6 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5--7 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5--8 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5--9 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5--10 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5--11 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5--12 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5--13 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5--14 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5--15 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5--16 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5--17 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5--18 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5--19 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5--20 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5--21 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5--22 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5--23 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5--24 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 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MOONEY M20TN INTRODUCTION iii POH/AFM POH--003900 This POH/AFM effective with S/N 31--0001 THRU 31--TBA ORIGINAL ISSUE -- 12--22--2006 5--25 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5--26 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5--27 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5--28 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5--29 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5--30 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5--31 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5--32 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5--33 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5--34 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5--35 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5--36 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5--37 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5--38 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5--39 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5--40 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5--41 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5--42 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5--43 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5--44 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5--45 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5--46 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5--47 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5--48 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6--1 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6--2 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6--3 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6--4 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6--5 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6--6 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6--7 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6--8 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6--9 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6--10 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6--11 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6--12 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6--13 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6--14 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6--15 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6--16 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6--17 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6--18 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6--19 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6--20 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6--21 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6--22 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6--23 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6--24 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6--25 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6--26 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6--27 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6--28 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6--29 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6--30 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6--31 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6--32 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 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MOONEY M20TN INTRODUCTION iv POH/AFM POH--003900 This POH/AFM effective with S/N 31--0001 THRU 31--TBA ORIGINAL ISSUE -- 12--22--2006 7--1 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7--2 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7--3 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7--4 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7--5 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7--6 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7--7 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7--8 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7--9 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7--10 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7--11 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7--12 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7--13 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7--14 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7--15 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7--16 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7--17 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7--18 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7--19 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7--20 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7--21 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7--22 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7--23 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7--24 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7--25 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7--26 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7--27 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7--28 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7--29 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7--30 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7--31 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7--32 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7--33 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7--34 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7--35 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7--36 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7--37 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7--38 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8--1 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8--2 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8--3 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8--4 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8--5 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8--6 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8--7 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8--8 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8--9 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8--10 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8--11 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8--12 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9--1 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9--2 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9--3 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9--4 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . (Plus applicable supplements inserted) MOONEY M20TN INTRODUCTION v POH/AFM POH--003900 This POH/AFM effective with S/N 31--0001 THRU 31--TBA ORIGINAL ISSUE -- 12--22--2006 10--1 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10--2 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10--3 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10--4 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10--5 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10--6 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10--7 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10--8 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10--9 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10--10 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10--11 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10--12 ORIGINAL ISSUE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . MOONEY M20TN INTRODUCTION iii POH/AFM POH--003900 ORIGINAL ISSUE -- 12--22--2006 LOG OF REVISIONS REVISION NUMBER REVISED PAGES DESCRIPTION OF REVISIONS FAA APPROVED DATE ORIGINAL ISSUE ALL -- 12--22--06 MOONEY M20TN INTRODUCTION v ORIGINAL ISSUE -- 12--22--2006 TABLE OF CONTENTS TITLE SECTION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . GENERAL I . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . LIMITATIONS II . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . EMERGENCY PROCEDURES III . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . NORMAL PROCEDURES IV . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PERFORMANCE V . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . WEIGHT & BALANCE VI . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AIRPLANE & SYSTEM DESCRIPTIONS VII . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . HANDLING, SERVICE & MAINTENANCE VIII . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SUPPLEMENTAL DATA IX . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SAFETY & OPERATIONAL TIPS X . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . MOONEY M20TN INTRODUCTION vi ORIGINAL ISSUE -- 12--22--2006 BLANK MOONEY M20TN SECTION I GENERAL 1 -- 1 ORIGINAL ISSUE -- 12--22--2006 TABLE OF CONTENTS TITLE SECTION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . THREE VIEW 1--3 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . INTRODUCTION 1--4 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DESCRIPTIVE DATA 1--5 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ENGINE 1--5 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PROPELLER 1--6 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FUEL 1--6 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OIL 1--6 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . LANDING GEAR 1--7 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . MAXIMUM CERTIFICATED WEIGHTS 1--7 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . STANDARD AIRPLANE WEIGHTS 1--7 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CABIN & ENTRY DIMENSIONS 1--7 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . BAGGAGE SPACE & ENTRY DIMENSIONS 1--7 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SPECIFIC LOADINGS 1--8 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . IDENTIFICATION PLATE 1--8 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . GARMIN G1000 1--8 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SYMBOLS, ABBREVIATIONS & TERMINOLOGY 1--9 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . GENERAL AIRSPEED TERMINOLOGY & SYMBOLS 1--9 . . . . . . . . . . . . . . . . . . . . . . . . . . ENGINE POWER TERMINOLOGY 1--9 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AIRPLANE PERFORMANCE & FLIGHT PLANNING TERMINOLOGY 1--10 . . . . . . . . . . . ENGINE CONTROLS & INSTRUMENTS TERMINOLOGY 1--10 . . . . . . . . . . . . . . . . . . . . . METEOROLOGICAL TERMINOLOGY 1--10 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . WEIGHT & BALANCE TERMINOLOGY 1--11 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . MEASUREMENT CONVERSION TABLES 1--12 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . USE OF THE TERMS WARNING, CAUTION AND NOTE 1--13 . . . . . . . . . . . . . . . . . . . . . . . . . MOONEY M20TN SECTION I GENERAL 1 -- 2 ORIGINAL ISSUE -- 12--22--2006 BLANK MOONEY M20TN SECTION I GENERAL 1 -- 3 ORIGINAL ISSUE -- 12--22--2006 9’--2” (279.4 cm) 11’--9” (358.1 cm) 36’--6” (1112.5 cm) 6’--7 1/2” (201.9 cm) 26’ --8” (812.8 cm) 8’--6” (259.1 cm) 76” (193.04 cm) POHTN002 FIGURE 1--1 THREE VIEW MOONEY M20TN SECTION I GENERAL 1 -- 4 ORIGINAL ISSUE -- 12--22--2006 INTRODUCTION This Operators Manual conforms to GAMA Specification No. 1 and includes both Manufacturer’s material and FAA APPROVED material required to be furnished to the pilot by the applicable Federal Aviation Regulations. Section IX contains supplemental data supplied by Mooney Air- plane Company, Inc.. Section I contains information of general interest to the pilot. It also contains definitions of the terminology used in this Operators Manual. This Pilot’s Operating Handbook is not designed as a substitute for adequate and competent flight instruction, knowledge of current airworthiness directives, applicable federal air regula- tions or advisory circulars. It is not intended to be a guide for basic flight instruction or a training manual and should not be used for operational purposes unless kept in an up--to--date status. All limitations, procedures, safety practices, servicing and maintenance requirements published in this POH/AFM are considered mandatory for the Continued Airworthiness of this airplane in a condition equal to that of its original manufacture. MOONEY M20TN SECTION I GENERAL 1 -- 5 ORIGINAL ISSUE -- 12--22--2006 DESCRIPTIVE DATA ENGINE Number of Engines 1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Engine Manufacturer Teledyne Continental Motors (TCM) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Model TSIO--550--G(1) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Recommended TBO 2000 Hours . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Type Reciprocating, air cooled, fuel injected, turbocharged . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Number of Cylinders 6, Horizontally opposed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Firing Order 1--6--3--2--5--4 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Displacement 552 Cu. In. (9.05 Liters) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Bore 5.25 In. (13.3 cm) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Stroke 4.25 In. (10.8 cm) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Compression Ratio 7.5 : 1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Fuel System Type Fuel Injection . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Make TCM . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Fuel -- Aviation Gasoline 100 octane --100LL . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Accessories Magnetos Bendix S6RSC--25P (pressurized) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Ignition Harness Shielded/Braided . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Spark Plugs AC 273 (or equivalent) (18 m/m) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Oil Cooler TCM Full Flow . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Alternator 28 Volt DC, 100 AMPS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Starter 24 volt DC . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Intercooler TCM . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Turbocharger TCM/Kelly Aerospace Model TA36 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Turbocharger Controller System TCM . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Ratings: Maximum Continuous Power 280 BHP at 2500 RPM . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Recommended Cruise Power 262 BHP at 2500 RPM . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . MOONEY M20TN SECTION I GENERAL 1 -- 6 ORIGINAL ISSUE -- 12--22--2006 PROPELLER Hartzell Number 1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Manufacturer Hartzell . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Model Number PHC--J3YF--1RF/F7693DF--2 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Number of Blades 3 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Diameter (MAX.) 76 in. (193.0 cm) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . (MIN.) 75 in. (190.5 cm) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Type Constant Speed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Governor (Hartzell) Hydraulically controlled by engine oil . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Blade Angles @ 30.0 in. Sta.: Low 16.5 degrees +/-- 0.2 degrees . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . High 38.0 degrees +/-- 1.0 degrees . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FUEL Minimum Fuel Grade (Color) 100 LL (Blue) or 100 Octane (Green) . . . . . . . . . . . . . . . . . . . . . . Total Fuel -- Useable 89 U.S. Gal. (386.1 liters) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Unusable Fuel 6 U.S. Gal. (22.7 liters) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OIL Oil Specification or Oil Grade (First 25 Engine Hours) -- Non dispersant mineral oil conforming to SAE J1966 shall be used during the first 25 hours of flight operations. However, if the engine is flown less than once a week, a straight mineral oil with corrosion preventative MIL--C--6529 for the first 25 hours is recommended. Oil Specification or Oil Grade (After 25 Engine Hours) -- Teledyne Continental Motors Specifica- tion MHS--24. An ashless dispersant oil shall be used after 25 hours. Oil Grades Recommended for Various Average Air Temperature Ranges Below 40 o F (4 o C) SAE 30, 10W30, 15W50 or 20W50 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Above 40 o F (4 o C) SAE 50, 15W50 or 20W50 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Total Oil Capacity 8 Qts. (7.57 liters) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Oil Filter Full Flow . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Oil grades, specifications and changing recommendations are contained in SECTION VIII. NOTE: The first time the airplane is filled with oil, additional oil is required for the filter, oil cooler and propeller dome. This oil is not drainable on subsequent oil changes. Add- ed oil is mixed with a few quarts of older oil in the system. MOONEY M20TN SECTION I GENERAL 1 -- 7 ORIGINAL ISSUE -- 12--22--2006 LANDING GEAR TYPE: Electrically operated, fully retractable tricycle gear with rubber shock discs. The main wheels have hydraulically operated disc brakes. The nose wheel is fully steerable 11 o left to 13 o right of center. Wheelbase 6’--7 1/2” (201.9 cm) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Wheel Track 9’--2” (279.4 cm) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Tire Size: Nose 5.00 x 5 (6 ply) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Main 6.00 x 6 (6 ply) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Tire Pressure Nose 49 PSI . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Main 42 PSI . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Minimum Turning Radius (No brakes applied) Right 40 ft. (12.0 m) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Left 48 ft. (14.4 m) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . MAXIMUM CERTIFICATED WEIGHTS Gross Weight 3368 Lbs. (1528 Kg) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Maximum Landing Weight 3200 Lbs. (1452 Kg) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Useful Load (No Options) 1049 Lbs. (475.8 Kg) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Baggage Area 120 Lbs. (54.4 Kg) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Rear Storage Area 10 Lbs. (4.5 Kg) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Cargo (Rear Seats Folded Down) 340 Lbs. (154.2 Kg) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . STANDARD AIRPLANE WEIGHTS Basic Empty Weight See Page 1--11 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Useful Load Varies with installed equipment . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . See SECTION VI for specific airplane weight. CABIN AND ENTRY DIMENSIONS Cabin Width (Maximum) 43.5 In. (110.5 cm) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Cabin Length (Maximum) 126 In. (315 cm) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Cabin Height (Maximum) 44.5 In. (113 cm) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Entry Width (Minimum) 29.0 In. (73.4 cm) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Entry Height (Minimum) 35.0 In. (88.9 cm) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . BAGGAGE SPACE AND ENTRY DIMENSIONS Compartment Width 24 In. (60.9 cm) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Compartment Length 43 In. (109.2 cm) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Compartment Height 35 In. (88.9 cm) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Compartment Volume 22.6 cu. ft. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . (0.63 cu. m) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Cargo Area (with rear seat folded down) 38.6 cu. ft. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . (1.09 cu. m) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Entry Height (Minimum) 20.5 In. (52.1 cm) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Entry Width 17.0 In. (43.2 cm) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Ground to Bottom of Sill 46.0 In. (116.8 cm) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . MOONEY M20TN SECTION I GENERAL 1 -- 8 ORIGINAL ISSUE -- 12--22--2006 SPECIFIC LOADINGS Wing Loading -- @ Maximum Gross Weight 19.26 lbs./sq. ft. . . . . . . . . . . . . . . . . . . . . . . . . . . . . (94 kg/sq. m) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Power Loading -- @ Maximum Gross Weight 12.03 lbs./HP . . . . . . . . . . . . . . . . . . . . . . . . . . . . . (5.46 kg/HP) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . IDENTIFICATION PLATE All correspondence regarding your airplane should include the Serial Number as depicted on the identification plate. The identification plate is located on the left hand side, aft end of the tailcone, below the horizontal stabilizer leading edge. The aircraft Serial Number and type certificate are shown. GARMIN G1000 GENERAL The GARMIN G1000 Integrated Avionics System is a fully integrated flight, engine, communica- tion, navigation and surveillance instrumentation system. The system consists of a Primary Flight Display (PFD), Multi--Function Display (MFD), audio panel (GMA), Air Data Computer (ADC), Attitude and Heading Reference System (AHRS), engine/airframe processing unit (GEA), and integrated avionics (GIA) containing VHF communications, VHS navigation, and GPS navigation. The primary function of the PFD is to provide attitude, heading, air data, navigation, and alerting information to the pilot. The PFD may also be used for flight planning. The primary function of the MFD is to provide engine information, mapping terrain information and for flight planning. The audio panel is used for selection of radios for transmitting and listening, intercom functions, and marker beacon functions. The primary function of the VHF Communication portion of the G1000 is to enable external radio communication. The primary function of the VOR/ILS Receiver portion of the equipment is to receive and demodulate VOR, localizer, and Glide Slope signals. The primary function of the GPS portion of the system is to acquire signals from the GPS satellites, recover orbital data, make range and Doppler measurements, and process this information in real time to obtain the user’s position, velocity, and time. Provided the GARMIN G1000 GPS receivers are receiving adequate and usable GPS and/or VHF navigation signals, it has been demonstrated capable of and meets the accuracy specifica- tions for the following types of flight operations: VFR/IFR en--route, oceanic, and terminal operations as well as nonprecision instrument approach (GPS, Loran--C, VOR, VOR--DME, TACAN, NDB, NDB--DME, RNAV) opera- tion within the U.S. National Airspace System in accordance with AC20--138A. Navigation in the North Atlantic Minimum Navigation Performance Specification (MNPS) Airspace in accordance with AC91--49 and AC 120--33. The GARMIN G1000 system meets RNP5 airspace (BRNAV) requirements of AC 90--96 and in accordance with AC 20--138A, JAA AMJ 20X2 Leaflet 2 Revision 1, and FAA Order 8110.60 for oceanic and remote airspace operations, provided it is receiving usable navigation information from the GPS receiver. (A separate software application for prediction of GPS navigation availability may be required for oceanic and remote op- erations. Refer to appropriate limitations for the airspace you are operating in to deter- mine if this GPS prediction software is required). Navigation is accomplished using the WGS--84 (NAD--83) coordinate reference datum. GPS navigation data is based upon use of only the Global Positioning System (GPS) operated by the United States of America. MOONEY M20TN SECTION I GENERAL 1 -- 9 ORIGINAL ISSUE -- 12--22--2006 SYMBOLS, ABBREVIATIONS & TERMINOLOGY GENERAL AIR SPEED TERMINOLOGY & SYMBOLS GS GROUND SPEED -- Speed of an airplane relative to the ground. KCAS KNOTS CALIBRATED AIR SPEED -- The indicated speed of an aircraft, corrected for position and instrument error. Calibrated airspeed is equal to true airspeed in standard atmosphere at sea level. KIAS KNOTS INDICATED AIRSPEED -- The speed of an aircraft as shown on its airspeed indicator. IAS values published in this handbook assume zero instrument error. KTAS KNOTS TRUE AIRSPEED -- The airspeed of an airplane relative to undis- turbed air which is the KCAS corrected for altitude and temperature. Va MANEUVERING SPEED -- The maximum speed at which application of full available aerodynamic control will not overstress the airplane. Vfe MAXIMUM FLAP EXTENDED SPEED -- The highest speed permissible with wing flaps in a prescribed extended position. Vle MAXIMUM LANDING GEAR EXTENDED SPEED --The maximum speed at which an aircraft can be safely flown with the landing gear extended. Vlo MAXIMUM LANDING GEAR OPERATING SPEED -- The maximum speed at which the landing gear can be safely extended or retracted. Vne NEVER EXCEED SPEED -- The speed limit that may not be exceeded at any time. Vno MAXIMUM STRUCTURAL CRUISING SPEED -- The speed that should not be exceeded except in smooth air and then only with caution. Vs STALLING SPEED -- The minimum steady--flight speed at which the air- plane is controllable. Vso STALLING SPEED -- The minimum steady flight speed at which the air- plane is controllable in the landing configuration. Vx BEST ANGLE--OF--CLIMB SPEED -- The airspeed which delivers the greatest gain of altitude in the shortest possible horizontal distance. Vy BEST RATE--OF--CLIMB SPEED -- The airspeed which delivers the great- est gain in altitude in the shortest possible time with gear and flaps up. ENGINE POWER TERMINOLOGY BHP BRAKE HORSEPOWER -- Power developed by the engine. CHT CYLINDER HEAD TEMPERATURE -- Operating temperature of engine cylinder(s) being monitored by sensor unit. Expressed in o F. TIT TURBINE INLET TEMPERATURE -- Temperature at turbine inlet used to identify the lean fuel flow mixtures for various power settings. Expressed in o F. EGT EXHAUST GAS TEMPERATURE -- The exhaust gas temperature mea- sured in the exhaust pipe manifold. Expressed in o F MCP MAXIMUM CONTINUOUS POWER -- The maximum power for take off, normal, abnormal or emergency operations. MP MANIFOLD PRESSURE -- Pressure measured in the engine’s induction system and expressed in inches of mercury (Hg). RPM REVOLUTIONS PER MINUTE -- Engine speed. MOONEY M20TN SECTION I GENERAL 1 -- 10 ORIGINAL ISSUE -- 12--22--2006 AIRPLANE PERFORMANCE AND FLIGHT PLANNING TERMINOLOGY Demonstrated Crosswind Velocity The velocity of the crosswind component for which adequate control of the airplane during take off and landing test was actually demonstrated during certification. The value shown is not considered to be limiting. g Acceleration due to gravity. Service Ceiling The maximum altitude at which aircraft at gross weight has the capability of climbing at the rate of 100 ft/min. ENGINE CONTROLS & INSTRUMENTS TERMINOLOGY Propeller Control The control used to select engine speed. Throttle Control The control used to select engine power by controlling MP. Mixture control Provides a mechanical linkage to the fuel injector mixture control to control the size of the fuel feed aperture, and therefore the air/fuel mixture. It is the primary method to shut the engine down. CHT Gauge Cylinder head temperature indicator used to determine that engine operat- ing temperature is within manufacturers specifications. Tachometer An instrument that indicates rotational speed of the engine. The speed is shown as propeller revolutions per minute (RPM). Propeller Governor The device that regulates RPM of the engine/propeller by increasing or decreasing the propeller pitch, through a pitch change mechanism in the propeller hub. METEOROLOGICAL TERMINOLOGY AGL Above ground level. Density Altitude Altitude as determined by pressure altitude and existing ambient tempera- ture. In standard atmosphere (ISA) density and pressure altitude are equal. For a given pressure altitude, the higher the temperature, the higher the density altitude. Indicated Altitude The altitude actually read from an altimeter when, and only when baromet- ric subscale (Kollsman window) has been set to Station Pressure. ISA INTERNATIONAL STANDARD ATMOSPHERE assumes that 1. The air is a dry perfect gas; 2. The temperature at sea level is 15 degrees Celsius (59 o F); 3. The pressure at sea level is 29.92 inches Hg (1013.2 MB); 4. The temperature gradient from sea level to the altitude at which the temperature is --56.5 o C (--69.7 o F) is --0.00198 o C (--0.003564 o F) per foot. OAT OUTSIDE AIR TEMPERATURE -- The free air static temperature, obtained either from in--flight temperature indications or ground meteorological sources. It is expressed in o C. Pressure Altitude The indicated altitude when Kollsman window is set to 29.92 In. Hg. or 1013.2 MB. In this handbook, altimeter instrument errors are assumed to be zero. Station Pressure Actual atmospheric pressure at field elevation. MOONEY M20TN SECTION I GENERAL 1 -- 11 ORIGINAL ISSUE -- 12--22--2006 WEIGHT AND BALANCE TERMINOLOGY Arm The horizontal distance from the reference datum to the center of gravity (C.G.) of an item. Basic Empty weight The actual weight of the airplane and includes all operating equipment (in- cluding optional equipment) that has a fixed location and is actually installed in the aircraft. It includes the weight of unusable fuel and full oil. Center of Gravity (C.G.) The point at which an airplane would balance if suspended. Its distance from the reference datum is found by dividing the total moment by the total weight of the airplane. C.G. Arm The arm obtained by adding the airplane’s individual moments and divid- ing the sum by the total weight. C.G. in % MAC Center of Gravity expressed in percent of mean aerodynamic chord (MAC). C.G. Limits The extreme center of gravity locations within which the airplane must be operated at a given weight. MAC Mean Aerodynamic Chord. Maximum Weight The maximum authorized weight of the aircraft and its contents as listed in the aircraft specifications. Maximum Landing Weight The maximum authorized weight of the aircraft and its contents when a normal landing is to be made. Moment The product of the weight of an item multiplied by its arm. (Moment divided by a constant is used to simplify balance calculations by reducing the number of digits). Reference Datum An imaginary vertical plane from which all horizontal distances are mea- sured for balance purposes. Station A location along the airplane fuselage usually given in terms of distance from the reference datum. Tare The weight of chocks, blocks, stands, etc. used when weighing an air- plane, and is included in the scale readings. Tare is deducted from the scale reading to obtain the actual (net) airplane weight. Unusable Fuel Fuel remaining after a run--out test has been completed in accordance with Federal regulations. Usable Fuel Usable Fuel available for aircraft engine combustion. Useful Load The basic empty weight subtracted from the maximum weight of the air- craft. This load consists of the pilot, crew (if applicable), useable fuel, pas- sengers, and baggage. MOONEY M20TN SECTION I GENERAL 1 -- 12 ORIGINAL ISSUE -- 12--22--2006 MEASUREMENT CONVERSION TABLES LENGTH U. S. Customary Unit Metric Equivalents . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 inch 2.54 centimeters . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 foot 0.3048 meter . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 yard 0.9144 meter . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 mile (statute, land) 1,609 meters . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 mile (nautical, international) 1,852 meters . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AREA U. S. Customary Unit Metric Equivalents . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 square inch 6.4516 sq. centimeters . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 square foot 929 sq. centimeters . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 square yard 0.836 sq. meter . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . VOLUME OR CAPACITY U. S. Customary Unit Metric Equivalents . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 cubic inch 16.39 cubic centimeters . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 cubic foot 0.028 cubic meter . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 cubic yard 0.765 cubic meter . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . U.S. Customary Metric Equivalents . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Liquid Measure 1 fluid ounce 29.573 milliliters . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 pint 0.473 liter . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 quart 0.946 liter . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 gallon 3.785 liters . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . U.S. Customary Metric Equivalents . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Dry Measure 1 pint 0.551 liter . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 quart 1.101 liters . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . British Imperial U. S. Metric Liquid and Dry Measure Equivalents Equivalents . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 fluid ounce 0.961 U.S. 28.412 milliliters . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . fluid ounce . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1.734 cubic inches 1 pint 1.032 U.S. 568.26 milliliters . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . dry pints 1.201 U.S. liquid pts. 34.678 cubic inches 1 quart 1.032 U.S. 1.136 liters . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . dry quarts 1.201 U.S. liquid qts. 69.354 cubic inches 1 gallon 1.201 U.S. 4.546 liters . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 277.420 cubic inches MOONEY M20TN SECTION I GENERAL 1 -- 13 ORIGINAL ISSUE -- 12--22--2006 WEIGHT U. S. Customary Unit Metric Equivalents . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . (Avoir du pois) 1 grain 64.79891 milligrams . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 dram 1.772 grams . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 ounce 28.350 grams . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 pound 453.6 grams . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PRESSURE U.S. Customary Unit Metric Equivalents . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 PSIG 6.895 KPA . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 inch Hg 3.388 KPA . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 inch Hg 25.40 mm Hg . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . COMMON CONVERSIONS 1 pound/square foot 0.488 kg/meter square . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 pound/square inch 2.036 inch Hg . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 pound/HP 0.4538 kg/HP . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . USE OF THE TERMS WARNING, CAUTION AND NOTE The following conventions will be used for the terms Warning, Caution and Note: --WARNING-- The use of a Warning symbol means that information which follows is of critical importance and concerns procedures and techniques which could cause or re- sult in personal injury or death if not carefully followed. --CAUTION-- The use of the Caution symbol means information which follows is of significant importance and concerns procedures and techniques which could cause or re- sult in damage to the airplane and/or its equipment if not carefully followed. NOTE: The use of the term Note means the information that follows is essential to em- phasize. MOONEY M20TN SECTION I GENERAL 1 -- 14 ORIGINAL ISSUE -- 12--22--2006 BLANK MOONEY M20TN SECTION II LIMITATIONS FAA APPROVED 2 -- 1 AIRPLANE FLIGHT MANUAL ORIGINAL ISSUE -- 12--22--2006 TABLE OF CONTENTS TITLE SECTION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . INTRODUCTION 2--3 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . NOISE LIMITS 2--3 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AIRSPEED LIMITATIONS 2--4 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AIRSPEED MARKINGS 2--5 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . POWER PLANT LIMITATIONS 2--6 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . POWER PLANT INSTRUMENT MARKINGS 2--7 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FUEL LIMITATIONS 2--8 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . WEIGHT LIMITS 2--8 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CENTER OF GRAVITY LIMITS (GEAR DOWN) 2--8 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . MANEUVER LIMITS 2--9 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FLIGHT LOAD FACTOR LIMITS 2--9 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FLIGHT CREW 2--9 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OPERATING LIMITATIONS 2--9 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . KINDS OF OPERATION LIMITS 2--9 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . KINDS OF OPERATION EQUIPMENT LIST 2--10 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . TYPES OF OPERATION 2--11 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . GENERAL 2--11 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . G1000 SYSTEM 2--11 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ADVISORY MESSAGES 2--13 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DECALS & PLACARDS 2--14 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CABIN INTERIOR 2--14 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FUSELAGE INTERIOR 2--18 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . EXTERIOR 2--19 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . MOONEY M20TN SECTION II LIMITATIONS 2 -- 2 AIRPLANE FLIGHT MANUAL ORIGINAL ISSUE -- 12--22--2006 BLANK MOONEY M20TN SECTION II LIMITATIONS FAA APPROVED 2 -- 3 AIRPLANE FLIGHT MANUAL ORIGINAL ISSUE -- 12--22--2006 INTRODUCTION SECTION II includes the mandatory operating limitations, instrument markings, and basic plac- ards necessary for the safe operation of the airplane, its engine, standard systems and standard equipment. The limitations included in this section have been approved by the Federal Aviation Administra- tion. When applicable, limitations associated with optional systems or equipment such as autopilots are included in SECTION IX. NOTE: The airspeeds listed in the Airspeed Limitations chart (Figure 2-1) and the Air- speed Indicator Markings chart (Figure 2-2) are based on Airspeed Calibration data shown in SECTION V with the normal static source. If the alternate static source is being used, ample margins should be observed to allow for the air- speed calibration variations between the normal and alternate static sources as shown in SECTION V. Your Mooney is certificated under FAA Type Certificate No. 2A3 as a Mooney M20TN. NOISE LIMITS The certificated noise level per 14 CFR Part 36, Appendix G, Amendment 36-22 of the Federal Aviation Regulations for the Mooney M20TN, with the Hartzell 3 blade propeller installed at 3368 lbs (1528 Kg.) maximum weight is 78.0 dB(A). No determination has been made by the Federal Aviation Administration that the noise levels of this airplane are or should be acceptable or unac- ceptable for operation at, into, or out of, any airport. MOONEY M20TN SECTION II LIMITATIONS 2 -- 4 AIRPLANE FLIGHT MANUAL FAA APPROVED ORIGINAL ISSUE -- 12--22--2006 AIRSPEED LIMITATIONS Airspeed limitations and their operational significance are shown in Figure 2-1. This calibration assumes zero instrument error. V/SPEED KCAS/KIAS REMARKS VNE Never Exceed Speed 196/194 Do not exceed this speed in any op- eration. VNO Maximum Structural Cruising Speed 175/173 Do not exceed this speed except in smooth air, and then only with caution. VA Maneuvering Speed at: lbs. /Kg. 2232/1012 104/103 . . . . . . . . . 2430/1102 109/108 . . . . . . . . . 3300/1497 127/126 . . . . . . . . . 3368/1528 128/127 . . . . . . . . . Do not make full or abrupt control move- ment above this speed. VFE Maximum Flap Ex- tended Speed 111/110 Do not exceed this speed with flaps in full down position. VLE Maximum Landing Gear Extended Speed 166/164 Maximum speed at which the aircraft can be safely flown with the landing gear extended. VLO (EXT) Max. Speed for Gear Extension 141/140 Max. speed at which the landing gear can be safely extended. VLO (RET) Max. Speed for Gear Retraction 107/106 Maximum speed at which the landing gear can be safely retracted. Maximum Pilot Win- dow Open Speed 133/132 Do not exceed this speed with pilot win- dow open. Figure 2-1 AIRSPEED LIMITATIONS MOONEY M20TN SECTION II LIMITATIONS FAA APPROVED 2 -- 5 AIRPLANE FLIGHT MANUAL ORIGINAL ISSUE -- 12--22--2006 AIRSPEED MARKINGS Airspeed indicator markings, their color code and operational significance are shown in Figure 2--2. MARKING IAS SIGNIFICANCE Red band 20 KIAS – 59 KIAS Low speed awareness -- stall is imminent White band 59 KIAS – 110 KIAS Operating range with flaps fully extended Green band 66 KIAS – 173 KIAS Normal operating range Yellow band 174 KIAS -- 194 KIAS Caution range -- smooth air only Red band 194 KIAS and greater Lower limit of 195 KIAS is the maximum speed for all operations Figure 2-2 AIRSPEED INDICATOR MARKINGS The airspeed indicator is marked in IAS values. MOONEY M20TN SECTION II LIMITATIONS 2 -- 6 AIRPLANE FLIGHT MANUAL FAA APPROVED ORIGINAL ISSUE -- 12--22--2006 POWER PLANT LIMITATIONS Number of Engines 1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Engine Manufacturer Teledyne Continental Motors (TCM) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Engine Model Number TSIO--550--G (1B) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Recommended Time Between Overhaul 2000 Hours (Time in Service) . . . . . . . . . . . . . . . . . . . Engine Operating Limits for Takeoff and Continuous Operations: Maximum Recommended Cruise (For Leaning) 262 HP . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Maximum Continuous Power 280 BHP . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Maximum Continuous RPM 2500 RPM . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Maximum Recommended Continuous Cylinder Head Temperature . . . . . . . . . . . . . . . . . . 420 o F (215.6 o C) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Maximum Cylinder Head Temperature 460 o F (237.7 o C) . . . . . . . . . . . . . . . . . . . . . . . . . . . . Maximum Turbine Inlet Temperature (TIT) 1750 o F (954 o C)/1850 o F (1010 o C) for 30 Sec. . Maximum Oil Temperature 240 o F (116 o C) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Minimum Oil Temperature -- Takeoff 100 o F (38 o C) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Recommended Cruising Oil Temperature 170 o F--220 o F (76.7 o C--104.4 o C) . . . . . . . . . . . . . . Maximum Manifold Pressure 33.5 Inches of Hg . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Oil Pressure Normal Operating 30--100 PSI . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Minimum (IDLE ONLY) 10 PSI . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Maximum Allowable (Cold Oil) 100 PSI . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Oil Grades Recommended for Various Average Air Temperature Ranges Below 40 o F (4 o C) SAE 30, 10W30, 15W50 or 20W50 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Above 40 o F (4 o C) SAE 50, 15W50 or 20W50 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Fuel Grade (Color) 100LL (Blue) or 100 octane (Green) 1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Fuel Flow Normal Operations 7 to 32 GPH (27 to 121 LPH) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Maximum Allowable 32 GPH ( 121 LPH) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Number of Propellers 1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Propeller Manufacturer Hartzell . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Propeller Hub/Blade Model Number PHC--J3YF--1RF/F7693DF--2 . . . . . . . . . . . . . . . . . . . . . . . Number of Blades 3 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Propeller Diameter: Min 75 In. (190.5 cm.) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Max 76 In. (193.0 cm.) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Propeller Blade Angles @ 30.0 In. sta.: Low 16.5 Degrees +/-- 0.2 Degrees . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . High 38.0 Degrees +/-- 1.0 Degrees . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Propeller Operating Limits 2500 RPM . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 100LL fuel is calibrated at 5.82 lb/gal (0.69 Kg/liter) 100 octane fuel is calibrated at 6.0 lb. gal. (0.72 Kg/liter) MOONEY M20TN SECTION II LIMITATIONS FAA APPROVED 2 -- 7 AIRPLANE FLIGHT MANUAL ORIGINAL ISSUE -- 12--22--2006 POWER PLANT INSTRUMENT MARKINGS Power plant instrument markings and their color code significance are shown in the table below. NOTE: When an indication lies in the caution range, the legend for that display will change to the color of the caution range. When an indication lies in the upper or lower pro- hibited range, the legend for that display will change to the color of the prohibited range and will begin flashing as well. INDICATION Red arc / bar = Lower prohibited range Yellow arc / bar = Caution range Green arc / bar = Normal operating range Yellow arc / bar = Caution range Red arc / bar = Upper prohibited range Engine RPM -- -- 0 – 2500 -- 2500* Manifold Press. In. Hg -- -- 15 – 33.5 -- 33.5 Oil Temp o F -- -- 100 – 240 -- 240 Oil Press PSI 10 (Idle) 10 – 30 30 – 100 -- 100 (Cold) Cyl. Head Temp o F -- -- 240 – 460 -- 460 Turbine Inlet Temp. o F -- -- 1000 -- 1750 -- 1750 *To prevent nuisance alerts during normal takeoffs: the “RPM” data will not turn red or flash until the RPM exceeds 2540. MOONEY M20TN SECTION II LIMITATIONS 2 -- 8 AIRPLANE FLIGHT MANUAL FAA APPROVED ORIGINAL ISSUE -- 12--22--2006 FUEL LIMITATIONS --WARNING-- Takeoff maneuvers when the selected fuel tank contains less than 12 gallons (45.4 liters) of fuel have not been demonstrated. NOTE: Each fuel quantity gauge is calibrated to read zero only in coordinated level flight when remaining quantity of fuel can no longer be safely used. NOTE: An optional visual fuel quantity gauge is installed on top of each tank and is to be used as a reference for refueling tanks only. Standard Tanks (2) 47.5 U.S. Gal. each (179.8 liters) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Total Fuel Capacity -- Standard 95 U.S. Gal. (359.6 liters) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Usable Fuel 89 U.S. Gal. (336.9 liters) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Unusable Fuel: 6 U.S. Gal. (22.7 liters) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Fuel Grade (and color): 100LL (low lead) (blue) or 100 octane (green) is approved . . . . . . . . --CAUTION-- Ethylene glycol monomethyl ether (EGME) or other additives are not recom- mended due to potential deteriorating effects within the fuel system. Under cer- tain conditions of temperature and humidity, water can be present in fuel in suffi- cient quantities to create ice formations within the fuel system. To prevent this, add Anhydrous ISOPROPYL Alcohol to the fuel supply in quantities not to exceed 3% of total fuel volume per tank. WEIGHT LIMITS Maximum Weight -- Takeoff 3368 lb. (1528 Kg.) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Maximum Weight -- Landing 3200 lb. (1452 Kg) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Maximum Weight in Baggage Compartment 120 lb. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . (54.4 Kg.) @ Fus. Sta. 101.5 (253.7 cm.) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Maximum Weight in Rear Storage Area 10 lb. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . (4.54 Kg.) @ Fus. Sta. 131.0 (297.5 cm.) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Maximum Weight in Cargo Area (Rear seats folded down) 340 lbs. . . . . . . . . . . . . . . . . . . . . . . (154.2 KG) @ Fus. Sta. 70.7 (176.8 cm.) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CENTER OF GRAVITY LIMITS (GEAR DOWN) Most Forward Fus. Sta. 41.0 IN. (104.1 cm.) @ 2430 lb. (1102 Kg) . . . . . . . . . . . . . . . . . . . . . . . 16.79% MAC . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Intermediate Forward Fus. Sta. 44 IN. (111.7 cm.) @ 3300 lb. (1497 Kg) . . . . . . . . . . . . . . . . . 21.7% MAC . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Forward Gross Fus. Sta. 46.0 IN. (116.8 cm.) @ 3368 lb. (1528 Kg) . . . . . . . . . . . . . . . . . . . . . . 24.98% MAC . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Aft Gross Fus. Sta. 51.0 IN. (129.5 cm.) @ 3368 lb. (1528 Kg) . . . . . . . . . . . . . . . . . . . . . . . . . . 33.18% MAC . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . MAC (at Wing Sta. 94.85)(241 cm.) 61.00 In. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Datum (station zero) is 13 inches (32.5 cm.) aft of the centerline of the nose gear trunnion attach/ pivot bolts. MOONEY M20TN SECTION II LIMITATIONS FAA APPROVED 2 -- 9 AIRPLANE FLIGHT MANUAL ORIGINAL ISSUE -- 12--22--2006 MANEUVER LIMITS This airplane must be operated as a Normal Category airplane. Aerobatic maneuvers, including spins, are prohibited. NOTE: Up to 500 foot altitude loss may occur during stalls at maximum weight. FLIGHT LOAD FACTOR LIMITS Maximum Positive Load Factor Flaps Up +3.8 g. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Flaps Down (33 Degrees) +2.0 g. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Maximum Negative Load Factor Flaps Up --1.5 g. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Flaps Down 0.0 g. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FLIGHT CREW Pilot One . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Maximum passenger seating configuration Three . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OPERATING LIMITATIONS When aircraft is not equipped with an approved oxygen system and flight operations above 12,000 ft. are desired, this airplane must be: 1. Equipped with supplemental oxygen in accordance with FAR 23.1441 2. Operate in accordance with FAR 91.211 and, 3. Equipped with avionics in accordance with FAR 91 or FAR 135. ALTERNATOR OPERATING LIMITATIONS IS 94 AMPS. Above 30.5 inHg of manifold pressure only full rich mixture is permitted. At altitudes above 22,000 feet, power settings above 2300 RPM must be operated at 1675 o F TIT or richer. Above 12,000 ft. the minimum manifold pressure is 15 inHg and the minimum RPM is 2,000. KINDS OF OPERATION LIMITS This is a Normal Category airplane certified for VFR/IFR day or night operations when the re- quired equipment is installed and operational as specified in the KINDS OF OPERATION EQUIPMENT LIST and the applicable operating rules. Optional equipment installations may not be required to be operational. The pilot must determine that the applicable operating rules requirements for each kind of opera- tion are met. OPERATIONS IN KNOWN ICING CONDITIONS ARE PROHIBITED. MOONEY M20TN SECTION II LIMITATIONS 2 -- 10 AIRPLANE FLIGHT MANUAL FAA APPROVED ORIGINAL ISSUE -- 12--22--2006 KINDS OF OPERATION EQUIPMENT LIST The following equipment was approved during Type Certification and must be installed and op- erable for each kind of operation as specified. NOTE: The KINDS OF OPERATION EQUIPMENT list may not include all the equipment as required by applicable operating rules. KINDS OF OPERATION EQUIPMENT LIST SYSTEM or COMPONENT VFR DAY 1 VFR NIGHT IFR DAY IFR NIGHT AIRSPEED INDICATOR 1 1 1 1 ALTIMETER, SENSITIVE 1 1 1 1 MAGNETIC DIRECTION INDICATOR 1 1 1 1 PRIMARY FLIGHT DISPLAY 2 1 1 1 1 MULTI--FUNCTION DISPLAY -- -- 1 1 AUDIO PANEL -- -- 1 1 AIR DATA COMPUTER 1 1 1 1 ATTITUDE AND HEADING REFERENCE SYSTEM -- -- 1 1 GPS -- 1 2 2 LANDING GEAR POSITION INDICATOR 2 2 2 2 SEAT BELT & SHOULDER HARNESS FOR EACH OCCUPANT 3 1 1 1 1 OXYGEN MASK FOR EACH OCCUPANT 4 1 1 1 1 POSITION LIGHTS -- 3 -- 3 STROBE LIGHTS (ANTI--COLLISION) -- 3 -- 3 GYRO--HORIZON -- -- 1 1 LANDING LIGHT 5 -- 1 -- 1 INSTRUMENT LIGHTS (INTERNAL or GLARESHIELD) -- 1 -- 1 BATTERIES 2 2 2 2 FUEL BOOST PUMP 1 1 1 1 PILOT’S OPERATING HANDBOOK & AIRPLANE FLIGHT MANUAL 1 1 1 1 PITOT 5 -- -- 1 1 ELT 1 1 1 1 ALTERNATE STATIC SOURCE 5 -- -- 1 1 1 Equipment must be installed and operable for all operations 2 If the PFD is inoperative or removed for service, the MFD may be used as the PFD. The MFD display must be operated in PFD (reversionary) mode by depressing the reversionary button on the Audio Panel. When operating in reversionary mode the system is limited to DAY VFR operations only. 3 If inoperative for unoccupied seat(s), seat(s) must be placarded, “DO NOT OCCUPY” 4 Only required when the operating rules require use of oxygen 5 When required by the appropriate regulations MOONEY M20TN SECTION II LIMITATIONS FAA APPROVED 2 -- 11 AIRPLANE FLIGHT MANUAL ORIGINAL ISSUE -- 12--22--2006 TYPES OF OPERATION The airplane is approved for the following operations when equipped in accordance with FAR 91 or FAR 135. 1. Day V.F.R. 2. Night V.F.R 3. Day I.F.R. 4. Night I.F.R. 5. Non-Icing GENERAL G1000 System: 1. The GARMIN G1000 Cockpit Reference Guide for the M20TN Series aircraft, P/N 190--00450--01, Revision A or later approved revision must be immediately available to the flight crew. 2. The GARMIN G1000 must utilize the following or later FAA approved software versions: SYSTEM STATUS PAGE NAME SOFTWARE PART NUM- BER SOFTWARE VERSION GDC1--GIA1 006--B0261--03 2.05 GDC1 FPGA 006--C0055--00 01.05 GDL69 006--B0317--03 2.14.00 GEA1--GIA1 006--B0193--02 2.04 GEA1--GIA2 006--B0193--02 2.04 GIA1 006--B0190--13 2.08 GIA2 006--B0190--13 2.08 GMA1--GIA1 006--B0203--10 2.11 GMA1--GIA2 006--B0203--10 2.11 GMU1 006--B0224--00 2.01 GMU1 FPGA 006--C0048--00 2.00 GPS1 006--B0093--XX 3.01 GPS2 006--B0093--XX 3.01 GRS1--GIA1 006--B0223--02 2.03 GRS1--GIA2 006--B0223--02 2.03 GRS1 FPGA 006--B0049--00 2.00 GTX--GIA1 006--B0172--XX 4.02 GTX--GIA2 006--B0172--XX 4.02 MFD1 006--B0319--27 4.06 PFD1 006--B0319--27 4.06 The database version is displayed on the MFD power--up page immediately after system pow- er--up and must be acknowledged. The remaining system software versions can be verified on the AUX group sub--page 5, “AUX – SYSTEM STATUS.” 3. IFR enroute, oceanic and terminal navigation predicated upon the G1000 GPS Receiver is prohibited unless the pilot verifies the currency of the database or verifies each selected way- point for accuracy by reference to current approved data. MOONEY M20TN SECTION II LIMITATIONS 2 -- 12 AIRPLANE FLIGHT MANUAL FAA APPROVED ORIGINAL ISSUE -- 12--22--2006 4. Instrument approach navigation predicated upon the G1000 GPS Receiver must be accom- plished in accordance with approved instrument approach procedures that are retrieved from the GPS equipment database. The GPS equipment database must incorporate the cur- rent update cycle. a.) Instrument approaches utilizing the GPS receiver must be conducted in the approach mode and Receiver Autonomous Integrity Monitoring (RAIM) must be available at the Final Ap- proach Fix. b.) Accomplishment of ILS, LOC, LOC--BC, LDA, SDF, MLS or any other type of approach not approved for GPS overlay with the G1000 GPS receiver is not authorized. c.) Use of the G1000 VOR/ILS receiver to fly approaches not approved for GPS require VOR/ ILS navigation data to be valid on the PFD display. d.) When an alternate airport is required by the applicable operating rules, it must be served by an approach based on other than GPS navigation, the aircraft must have the operational equipment capable of using that navigation aid, and the required navigation aid must be op- erational. e.) VNAV information may be utilized for advisory information only. Use of VNAV information for Instrument Approach Procedures does not guarantee step--down fix altitude protection, or arrival at approach minimums in a normal position to land. VNAV also does not guarantee compliance with intermediate altitude constraints between the top of descent and the way- point where the VNAV path terminates in terminal or enroute operations. 5. If not previously defined, the following default settings must be made in the “SYSTEM SETUP” menu of the G1000 prior to operation (refer to Pilot’s Guide for procedure, if necessary). a.) DIS, SPD…..nm kt (sets navigation units to “nautical miles” and “knots”) b.) ALT, VS……..ft fpm (sets altitude units to “feet” and “feet per minute”) c.) MAP DATUM….WGS 84 (sets map datum to WGS--84, [see note below]) d.) POSITION……..deg--min (sets navigation grid units to decimal minutes) example: dd.mm.ss: 45_ 30’ 30” in decimal minutes are: 45_ 30.5’ NOTE: In some areas outside the United States, datums other than WGS--84 or NAD--83 may be used. If the G1000 is authorized for use by the appropriate Airworthiness author- ity, the required geodetic datum must be set in the G1000 prior to its use for naviga- tion. 6. Operation is prohibited north of 70 o N and south of 70 o S latitudes. In addition, operation is prohibited in the following two regions: a.) North of 65 o N between 75 o W and 120 o W longitude and b.) South of 55 o S between 120 o E and 165 o E longitude. --CAUTION-- CDI automatic source switching to the ILS on Nav 1 or 2 must be set to manual for instrument approaches conducted with the autopilot coupled. If the CDI navi- gation source is changed when autopilot is engaged in GPSS mode, the S- Tec 55x