TEMP °C
2200 RPM 2000 RPM
PWR
TRQ
LBFT
FUEL
FLOW
PPH
TAS
KTS
PWR
TRQ
LBFT
FUEL
FLOW
PPH
TAS
KTS
20 100% 1030 261 157 100% 1130 264 158
Rng 890 237 144 Rng 940 231 141
75% 770 216 128 75% 850 216 131
End 680 200 102 65% 740 198 110
End 720 196 99
10 100% 1150 282 165 100% 1260 288 166
Rng 890 235 143 75% 950 231 141
75% 860 230 139 Rng 940 229 140
65% 750 210 123 65% 820 211 127
End 680 198 99 End 710 193 97
0 100% 1260 303 170 100% 1380 312 171
75% 940 243 146 75% 1040 245 148
Rng 870 230 139 Rng 920 225 138
65% 820 220 132 65% 900 222 135
End 670 195 98
End 700 190 95
-9 100% 1350 323 174 100% 1490 335 175
75% 1010 254 151 75% 1120 258 153
Rng 880 231 139 65% 970 232 141
65% 880 230 138 Rng 910 222 135
End 660 193 95 End 690 188 95
-10 100% 1360 326 175 100% 1500 339 175
75% 1020 256 152 75% 1130 260 153
65% 890 231 139 65% 980 233 142
Rng 880 231 139 Rng 920 224 136
End 660 193 95 End 690 187 95
TEMP °C
2200 RPM 2000 RPM
PWR
TRQ
LBFT
FUEL
FLOW
PPH
TAS
KTS
PWR
TRQ
LBFT
FUEL
FLOW
PPH
TAS
KTS
-20 100% 1450 347 177 100% 1600 364 178
75% 1090 267 155 75% 1200 273 157
65% 940 240 143 65% 1040 243 145
Rng 900 231 138 Rng 880 216 131
End 660 190 89 End 680 184 94
-30 100% 1530 368 179 100% 1680 389 180
75% 1150 278 157 75% 1260 285 159
65% 990 248 145 65% 1090 252 148
Rng 850 223 132 Rng 880 214 130
End 650 188 87 End 680 182 93
-40 100% 1600 389 179 100% 1760 415 181
75% 1200 288 158 75% 1320 297 160
65% 1040 255 147 65% 1140 260 149
Rng 880 225 133 Rng 870 211 127
End 650 185 87 End 670 179 90
-50 100% 1670 413 180 100% 1830 444 181
75% 1250 299 159 75% 1380 310 161
65% 1080 263 148 65% 1190 270 150
Rng 900 228 133 Rng 870 209 126
End 640 183 86 End 660 177 88
CRUISE PERFORMANCE (Pressure Altitude 12,000 FT)
Conditions:
Weight
..................................................................................... 7255 pounds
Engine Inlet
...................................................................................NORMAL
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