Beechcraft Musketeer Sport III A23-19 Pilot Operating Handbook page 124

SectionV
Performance
BEECHCRAFT Sport III
Musketeer A23-19, 19A
Gross
W
t
1500
1510
1520
1530
1540
1550
1560
1570
1580
1590
1600
1610
1620
1630
1640
1650
1660
1670
GROSS WEIGHT MOMENT LIMITS
(UTILITY CATEGORY)
(ACROBATIC CATEGORY- 19A)
Min.
Max.
Min.
Max.
Min .
Mo m.
M om.
Gross M om. M om. Gross Mo m.
100
100
W
t
100
100
W
t
100
1617 1710
1680 1811
1915
1860 2017
1628 1721
1690 1822
1927
1870 2029
1639
1733 1700 1833
1938 1880 2042
1649
1744
1710 1843
1949 1890 2055
1660
1756
1720 1854
1961
1900 2068
1671
1767
1730 1865
1972
1910 2081
1682
1778 1740 1876
1984 1920 2094
1692 1790
1750 1887
1995
1930 2107
1703
1801
1760 1897 2006 1940 2120
1714
1813 1770 1908
2018 1950 2133
1725
1824 1780 1919
2029 1960 2145
1736
1835 1790 1930
2041 1970 2158
1746
1847 1800 1940
2052 1980 2172
1757
1858 1810 1953 2063 1990 2185
1768 1870 1820 1966 2075 2000 2198
1779
1881 1830 1978
2086 2010 2211
1789
1892 1840 1991
2098 2020 2224
1800
1904 1850 2004
2109 2030 2237
Max.
Mo m.
100
2120
2132
2143
2155
2166
2177
2189
2200
2212
2223
2234
2246
2257
2269
2280
2291
2303
2314
The above weight and moment limits are based on the following
weight and center o f gravity limit data :
UTILIT Y CATEGORY
&
ACROBATIC CATEGORY
WEIGHT CONDITION FWD CG LIM IT AFT CG LIMIT
2030 lbs (max take·off or 1and1ngl
110.2 114 .0
1800 1 bsorless 1078 114 .0
6-14
October 1979