CRUISE PERFORMANCE (Pressure Altitude 19,000 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% 830 206 143 100% 910 209 144
End 740 189 113 End 810 190 113
0 100% 920 222 154 100% 1010 228 155
Rng 870 213 149 Rng 920 210 144
End 730 186 111 End 790 186 111
-10 100% 1010 241 162 100% 1110 249 163
Rng 850 208 144 Rng 900 206 142
75% 750 190 128 75% 830 192 130
End 720 183 109 End 780 183 110
-20 100% 1080 257 167 100% 1180 269 168
Rng 840 204 142 Rng 910 206 142
75% 810 199 138 75% 890 203 139
End 700 180 105 65% 770 181 115
End 760 179 108
-23 100%
1090 261 168 100% 1200 274 169
Rng 830 203 141 75% 900 205 141
75% 820 201 139 Rng 890 203 140
65% 710 180 114 65% 780 183 120
End 700 179 105 End 760 178 108
-30 100% 1140 274 170 100% 1250 289 171
75% 850 207 143 75% 940 213 145
Rng 820 201 139 Rng 880 200 138
65% 740 185 125 65% 810 188 128
End 700 177 105 End 750 176 106
-40 100% 1200 291 172 100% 1320 310 173
75% 900 216 147 75% 990 223 149
Rng 830 202 139 65% 860 195 134
65% 780 192 131 Rng 850 194 133
End 690 174 104 End 730 173 102
-50 100% 1260 312 174 100% 1390 336 175
75% 940 226 150
75% 1040 234 152
65% 820 199 136 65% 900 204 138
Rng 810 197 134 Rng 840 191 131
End 680 172 102 End 720 169 100