GRT / Paul Dye Constant Speed Hartzell BA O-360-A1A, 180 HP, 8.5:1 Jan 2006 167180 1682000 1692100 1702200 1712300 1722400 1732500 1742600 1752700 1760 1770 17821.600046 17921.000044 18020.300041 18119.800039 18219.200037 18318.900036 18418.600035 18518.200033 1860 1870 18826.700066 18926.000063 19025.200060 19124.600058 19223.900055 19323.500053 19423.200052 19522.700050 1960 1970 1982000 1994000 2006000 2018000 20210000 20312000 20414000 2050 2060 2070 2082.300000 2094.599998 2106.899996 2119.099998 21211.400007 21313.700016 21416.000025 2150 2160 2170 Carl Morgan - Lycoming Curve C-12850 - IO-360-B Constant Speed Hartzell BA 7496 TMX IOF-360 180 hp (vertical FI) March 2008 167180 1682000 1692100 1702200 1712300 1722400 1732500 1742600 1752700 1760 1770 17821.700047 17921.100044 18020.600042 18120.100040 18219.700039 18319.200037 18418.900036 18518.600035 1860 1870.100000 18827.400068 18926.600065 19026.100063 19125.400061 19224.700058 19324.200056 19423.600054 19523.200052 1960 1970.100000 1982000 1994000 2006000 2018000 20210000 20312000 20414000 2050 2060 2070 2082.300000 2094.599998 2106.899996 2119.099998 21211.400007 21313.700016 21416.000025 2150 2160 2170 Ted Chang - Lycoming Curve 11260-A revised 1997 Sensenich FP propeller O320-D2A, 160 hp 8.5:1 Feb 2007 1682000 1692100 1702200 1712300 1722400 1732500 1742600 1750 1760 1770 17823.200052 17922.500050 18021.200045 18120.100040 18219.500038 18319.200037 18419.000036 1850.000000 1860.000000 1870.000000 18828.800074 18927.500069 19025.800062 19124.200056 19223.500053 19323.100052 19422.600050 1950.000000 1960.000000 1970.000000 1982000 1994000 2005000 2016000 2027000 2038000 2049000 20510000 20612000 20714000 2085.999997 2097.999996 21010.000002 21112.000010 21215.000021 21315.000021 21416.000025 21518.000032 21622.000048 21722.000048 Ted Chang - Lycoming Curve 13381 published 2000 Sensenich FP propeller O320-D2A, 160 hp 8.5:1 Feb 2007 1682000 1692100 1702200 1712300 1722400 1732500 1742600 1750 1760 1770 17823 17922.5 18021.8 18121.2 18220.5 18320.2 18419.7 1850.000000 1860.000000 1870.000000 18828.5 18927.5 19026.8 19126.0 19225.2 19324.5 19424 1950.000000 1960.000000 1970.000000 1982000 1994000 2005000 2016000 2027000 2038000 2049000 20510000 20612000 20714000 2084 2099 21015 21113 21216 21315 21418 21518 21623 21727 Craig Woolston - (Rated 312HP)MT-Propeller, constant speed, MTV-9V 3 blade prop Continental IO-550-N-16B - 312 HPApril 2007 167312 1681900 1692000 1702100 1712200 1722300 1732400 1742500 1752600 1762700 1770 17819.000036 17918.800035 18019.000036 18119.000036 18219.400038 18319.200037 18419.300037 18518.800035 18618.900036 1870 18823.300053 18923.200052 19023.400053 19123.500053 19223.700054 19323.400053 19423.500053 19523.100052 19623.100052 1970 1982000 1994000 2006000 2018000 20210000 20312000 2040 2050 2060 2070 20813.400015 20919.600039 21025.800062 21132.100082 21238.299988 21344.599892 2140 2150 2160 2170 John Ferguson / GRT Unknown Rotax 912S 100hp Estimated Mar 2008 167100 1684300 1694510 1704730 1714940 1725160 1735370 1745560 1755800 1760 1770 17822.7 17921.9 18021.2 18120.5 18219.7 18319.1 18418.6 18518.3 1860 1870 18827.6 18926.8 19026.0 19125.1 19224.2 19323.6 19423.0 19522.5 1960 1970 1982000 1994000 2006000 2018000 20210000 20312000 20414000 2050 2060 2070 2083.7 2095 2107.5 2119.4 21213.8 21314.4 21418.1 2150 2160 2170