CRUISE PERFORMANCE (Pressure Altitude 24,000 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% 800 191 133 100% 880 198 132
End 780 188 122 End 870 195 124
-20 100% 860 206 149 100% 950 215 150
Rng 860 205 148 Rng 920 209 145
End 770 185 122 End 850 191 122
-30 100% 920 220 156 100% 1010 232 157
Rng 840 201 145 Rng 900 204 143
End 760 182 118 End 830 187 118
-33 100% 930 223 158 100% 1020 236 159
Rng 830 199 143 Rng 900 203 142
End 750 181 117 End 830 186 117
-40 100% 970 235 161 100% 1060 250 162
Rng 820 196 141 Rng 890 202 141
End 740
178 115 End 810 183 115
-50 100% 1020 254 166 100% 1130 274 167
Rng 810 193 139 Rng 870 197 138
75% 770 184 130 75% 840 191 133
End 730 175 111 End 790 178 111
CRUISE PERFORMANCE (Pressure Altitude 25,000 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
-20 100% 820 196 140 100% 900 205 140
End 790 188 121 End 870 196 124
-30 100% 870 210 151 100% 960 221 151
Rng 840 202 146 Rng 910 206 143
End 770 185 120 End 850 192 122
-35 100% 900 216 154 100% 980 228 155
Rng 850 203 146 Rng 900 206 143
End 770 183 121 End 840 190 119
-40 100% 920 224 157 100% 1010 238 158
Rng 830 199 143 Rng 900 206 143
End 760 181 118 End 830 187 118
-50 100% 980 243 163 100% 1080 262 164
Rng 810 194 139 Rng 880 201 139
End 740
178 115 End 810 183 115