CRUISE PERFORMANCE (Pressure Altitude 16,000 FT)
Conditions:
Weight
..................................................................................... 7255 pounds
Engine Inlet
...................................................................................NORMAL
TEMP
°C
2200 RPM 2000 RPM
PWR
TRQ
LBFT
FUEL
FLOW
PPH
TAS
KTS
PWR
TRQ
LBFT
FUEL
FLOW
PPH
TAS
KTS
10 100% 960 238 156 100% 1060 242 157
Rng 890 223 148 Rng 930 217 144
75% 720 194 119 75% 790 195 123
End 700 190 105 End 760 189 108
0 100% 1060 255 163 100% 1160 262 164
Rng 860 217 144 Rng 920 216 142
75% 790 205 134 75% 870 207 136
End 690 188 104 65% 760 187 113
End 750 186 106
-10 100% 1160 276 170 100% 1270 287 170
75% 870 217 143 75% 950 220 145
Rng 850 214 141 Rng 910 212 140
65% 750 196 126 65% 830 198 129
End 690 185 104 End 730 183 102
-17 100% 1210
288 172 100% 1330 301 173
75% 910 224 146 75% 1000 228 148
Rng 840 212 139 Rng 890 207 137
65% 780 201 131 65% 860 204 134
End 680 183 101 End 730 180 101
-20 100% 1230 295 173 100% 1360 309 174
75% 920 227 148 75% 1020 232 150
Rng 850 213 140 Rng 890 208 137
65% 800 204 133 65% 880 206 136
End 680 182 100 End 720 179 100
-30 100% 1300 314 175 100% 1430 332 176
75% 980 237 151 75% 1080 243 153
Rng 850 212 138 65% 930 215 140
65% 850 211 138 Rng 870 203 133
End 670 180 98 End 710 176 97
-40 100% 1370 333 177 100% 1500 356 178
75% 1030 246 154 75%
1130 254 155
65% 890 218 141 65% 980 223 143
Rng 850 210 136 Rng 860 201 132
End 670 177 95 End 700 173 95
-50 100% 1430 356 178 100% 1580 384 179
75% 1080 257 156 75% 1180 267 157
65% 930 226 143 65% 1030 232 146
Rng 820 204 131 Rng 820 193 126
End 660 175 93 End 690 170 94
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