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FPM –––– 941 1088 1250 1431 –––– –––– 832 982 1148 –––– –––– –––– –––– 805
MIN 18 16 15 14 12 20 18 16 15 14 –––– –––– 18 17 15
ISA NM 70 62 57 51 47 79 70 63 57 52 –––– –––– 71 64 58
LB 291 260 238 217 198 312 277 253 230 209 –––– –––– 270 245 222
FPM 1038 1235 1404 1591 1802 834 1021 1182 1359 1558 –––– –––– 866 1030 1211
MIN 15 13 12 11 10 17 15 14 12 11 19 17 15 14 13
ISA NM 56 50 45 41 38 64 56 51 46 42 74 65 58 53 47
-10°C LB 254 228 209 192 175 273 244 223 204 186 296 262 239 217 197
FPM 1177 1389 1571 1774 2001 908 1105 1274 1461 1670 667 856 1018 1196 1394
PRESSURE 41000 FEET
ALTITUDE ISA = -57°C = -70°F
MIN –––– –––– –––– –––– ––––
ISA NM –––– –––– –––– –––– ––––
+10°C LB –––– –––– –––– –––– ––––
FPM –––– –––– –––– –––– ––––
MIN –––– –––– –––– –––– ––––
ISA NM –––– –––– –––– –––– ––––
LB –––– –––– –––– –––– ––––
FPM –––– –––– –––– –––– ––––
MIN 23 20 18 16 14
ISA NM 89 76 68 60 54
-10°C LB 326 285 257 233 211
FPM 439 622 779 950 1139
51OM-00-01
CRUISE CLIMB SPEED - KIAS
PRESSURE ALTITUDE - FEET
0 5000 10000 15000 20000 25000 30000 35000 40000 41000
170 170 170 170 170 170 160 143 127 124
WIND EFFECT ON CLIMB DISTANCE - NM
(SUBTRACT FOR HEADWIND, ADD FOR TAILWIND)
CLIMB TIME WIND
(MIN) 25KTS 50KTS 100KTS
5 2 4 8
10 4 8 16
15 6 12 25
20 8 16 33
25 10 20 41
30 12 25 50
CITATION MUSTANG OPERATING MANUAL
8 510OM-00
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CITATION MUSTANG OPERATING MANUAL
510OM-00 9
CRUISE
Specific performance data are presented on the following pages for various combinations of fan
speeds, weights, temperature, altitudes and winds to enable the calculation of the cruise portion of
a range profile.
The various fan speeds presented provide the specific ranges between maximum cruise thrust
(maximum TAS) and the approximate maximum range thrust. It should be noted that reducing
thrust to maintain a constant indicated airspeed as the airplane weight decreases during cruise
results in a significant increase in range. The best range, however, results from decreasing thrust
to fly a constantly decreasing airspeed as airplane weight decreases per the values shown in the
tabulated data.
When the anti-ice systems are ON, increase the fuel flows and decrease the specific ranges that
are presented for each altitude by the percentage indicated. The cruise speeds will remain the
same for a given fan RPM (N1). The maximum allowable fan speeds with anti-ice systems ON are
presented on each chart for each altitude. Only fan speeds equal to or lower than these values
can be used. The one engine specific range data is presented for use in the event of an enroute
engine failure.
CITATION MUSTANG OPERATING MANUAL
10 510OM-00
CRUISE
5000 FEET
ANTI-ICE SYSTEMS OFF TWO ENGINES
FAN FUEL NAUTICAL MILES / 100 LBS FUEL
WT RAT PERCENT FLOW IND H E A D W I N D ZERO T A I L W I N D
LBS TEMP °C RPM LBS/HR KIAS MACH KTAS 100 KT 50 KT 25 KT WIND 25 KT 50 KT 100 KT
8645 ISA+20°C 35 (1) 83.4 1081 250 .41 279 16.6 21.2 23.5 25.8 28.1 30.4 35.1
25°C 34 80.6 1000 236 .390 264 16.4 21.4 23.9 26.4 28.9 31.4 36.4
33 78.0 933 224 .370 250 16.1 21.5 24.2 26.9 29.5 32.2 37.6
32 75.4 871 212 .350 237 15.7 21.5 24.3 27.2 30.1 33.0 38.7
32 (2) 73.6 830 203 .34 227 15.3 21.4 24.4 27.4 30.4 33.4 39.5
ISA+10°C 25 (1) 82.0 1057 250 .41 274 16.5 21.2 23.6 25.9 28.3 30.7 35.4
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