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