CITATION LONGITUDE FLIGHT PLANNING GUIDE

Two flap settings are shown for the aircraft: Flaps 2 (15°) and Flaps 1 (7°). Flaps 2 is preferred to minimize runway length and runway speeds. In those situations where second segment climb requirements are too limiting for Flaps 2, a Flaps 1 setting is available. Flaps 1 requires greater runway length but provides equal or greater second segment climb capability. A paved, level, dry runway with zero wind is assumed. Runway lengths shown are based on the aircraft’s anti-ice systems being off and the cabin bleed air on. DECISION, ROTATION & TAKEOFF SAFETY SPEEDS (KIAS) Sea Level, Dry Runway, ISA, Zero Wind, Anti-Ice Off Flaps 2 Setting Flaps 1 Setting Takeoff Weight (lb) Decision Speed V1 Rotation Speed VR Safety Speed V2 Decision Speed V1 Rotation Speed VR Safety Speed V2 39500 123 126 136 128 130 142 38500 121 124 134 126 128 140 37500 118 122 133 123 126 138 36500 115 120 131 121 123 137 34500 110 115 128 115 119 133 31500 103 110 123 107 112 127 29500 98 106 120 101 107 123 25500 90 100 117 96 105 123 5 CITATION LONGITUDE TAKEOFF PERFORMANCE TAKEOFF FIELD LENGTH – FEET; FLAPS 2 (Over 35 Foot Screen Height) Dry Runway, Zero Wind, Anti-Ice Off, Cabin Bleed Air On Elevation = Sea Level Ambient Temp °C / °F ----------------------------------------- Takeoff Weight (lb) ------------------------------------------- 39,500 38,500 37,500 36,500 34,500 31,500 29,500 25,500 0 / 32 4590 4360 4150 3940 3560 3080 2760 2320 10 / 50 4740 4500 4290 4070 3680 3180 2850 2390 15 / 59 4810 4580 4360 4140 3740 3230 2890 2430 20 / 68 4890 4650 4420 4200 3790 3280 2940 2460 25 / 77 4960 4720 4490 4260 3850 3300 2980 2500 30 / 86 5110 4860 4620 4390 3960 3420 3060 2560 35 / 95 5410 5140 4890 4630 4150 3580 3190 2620 40 / 104 5780 5480 5210 4930 4410 3740 3340 2640 45 / 113 6160 5830 5530 5240 4690 3920 3480 2750 50 / 122 6720 6290 5910 5590 4980 4160 3650 2870 Climb Wght Temp Limits °C/°F 50/122 50/122 50/122 50/122 50/122 50/122 50/122 50/122 Field Length at Temp Limits (ft) 6720 6290 5910 5590 4980 4160 3650 2870 Elevation = 1,000 Feet Ambient Temp °C / °F ----------------------------------------- Takeoff Weight (lb) ------------------------------------------- 39,500 38,500 37,500 36,500 34,500 31,500 29,500 25,500 0 / 32 4730 4500 4280 4070 3670 3180 2850 2390 10 / 50 4890 4650 4420 4200 3790 3280 2940 2470 15 / 59 4960 4720 4490 4270 3850 3330 2980 2500 20 / 68 5040 4790 4560 4330 3910 3380 3030 2540 25 / 77 5150 4900 4660 4420 3990 3450 3090 2590 30 / 86 5450 5180 4920 4670 4200 3620 3230 2670 35 / 95 5810 5510 5230 4960 4440 3780 3370 2680 40 / 104 6190 5870 5580 5280 4720 3960 3520 2780 45 / 113 6730 6300 5950 5630 5020 4200 3690 2900 48 / 118 7110 6640 6230 5860 5220 4360 3800 2980 Climb Wght Temp Limits °C/°F 48/118 48/118 48/118 48/118 48/118 48/118 48/118 48/118 Field Length at Temp Limits (ft) 7110 6640 6230 5860 5220 4360 3800 2980 6 CITATION LONGITUDE TAKEOFF PERFORMANCE TAKEOFF FIELD LENGTH – FEET; FLAPS 2 (Over 35 Foot Screen Height) Dry Runway, Zero Wind, Anti-Ice Off, Cabin Bleed Air On Elevation = 2,000 Feet Ambient Temp °C / °F ----------------------------------------- Takeoff Weight (lb) ------------------------------------------- 39,500 38,500 37,500 36,500 34,500 31,500 29,500 25,500 0 / 32 4890 4650 4420 4200 3800 3280 2940 2470 10 / 50 5050 4800 4570 4340 3920 3390 3030 2550 15 / 59 5120 4870 4640 4400 3980 3440 3080 2580 20 / 68 5210 4950 4710 4470 4040 3490 3120 2620 25 / 77 5480 5210 4950 4690 4230 3650 3260 2720 30 / 86 5850 5550 5280 5000 4480 3830 3410 2740 35 / 95 6240 5920 5610 5320 4750 4010 3560 2810 40 / 104 6740 6320 5990 5670 5060 4230 3730 2940 45 / 113 7390 6900 6460 6060 5400 4500 3920 3070 46 / 115 7530 7030 6580 6150 5470 4560 3970 3100 Climb Wght Temp Limits °C/°F 46/115 46/115 46/115 46/115 46/115 46/115 46/115 46/115 Field Length at Temp Limits (ft) 7530 7030 6580 6150 5470 4560 3970 3100 Elevation = 3,000 Feet Ambient Temp °C / °F ----------------------------------------- Takeoff Weight (lb) ------------------------------------------- 39,500 38,500 37,500 36,500 34,500 31,500 29,500 25,500 -10 / 14 4880 4640 4410 4190 3790 3280 2940 2470 0 / 32 5040 4790 4560 4330 3920 3390 3030 2550 10 / 50 5210 4950 4710 4480 4040 3490 3130 2630 15 / 59 5290 5030 4790 4540 4100 3550 3180 2670 20 / 68 5520 5250 4990 4730 4270 3680 3290 2760 25 / 77 5880 5580 5310 5030 4500 3860 3440 2790 30 / 86 6290 5960 5660 5360 4790 4050 3610 2850 35 / 95 6760 6360 6040 5710 5100 4270 3780 2970 40 / 104 7390 6910 6480 6100 5440 4530 3960 3110 44 / 111 7990 7440 6960 6500 5730 4770 4150 3220 Climb Wght Temp Limits °C/°F 44/111 44/111 44/111 44/111 44/111 44/111 44/111 44/111 Field Length at Temp Limits (ft) 7990 7440 6960 6500 5730 4770 4150 3220 7 CITATION LONGITUDE TAKEOFF PERFORMANCE TAKEOFF FIELD LENGTH – FEET; FLAPS 2 (Over 35 Foot Screen Height) Dry Runway, Zero Wind, Anti-Ice Off, Cabin Bleed Air On Elevation = 4,000 Feet Ambient Temp °C / °F ----------------------------------------- Takeoff Weight (lb) ------------------------------------------- 39,500 38,500 37,500 36,500 34,500 31,500 29,500 25,500 -10 / 14 5030 4780 4550 4320 3910 3380 3020 2550 0 / 32 5200 4940 4710 4470 4040 3490 3130 2630 10 / 50 5370 5100 4860 4620 4170 3610 3230 2710 15 / 59 5570 5290 5030 4780 4310 3720 3330 2790 20 / 68 5920 5620 5340 5070 4540 3900 3480 2840 25 / 77 6330 6000 5700 5400 4830 4090 3640 2880 30 / 86 6780 6410 6090 5760 5140 4300 3820 3010 35 / 95 7400 6920 6500 6150 5480 4570 4010 3140 40 / 104 8140 7580 7090 6620 5850 4870 4240 3280 42 / 108 8500 7890 7360 6860 6010 4990 4340 3350 Climb Wght Temp Limits °C/°F 42/108 42/108 42/108 42/108 42/108 42/108 42/108 42/108 Field Length at Temp Limits (ft) 8500 7890 7360 6860 6010 4990 4340 3350 Elevation = 5,000 Feet Ambient Temp °C / °F ----------------------------------------- Takeoff Weight (lb) ------------------------------------------- 39,500 38,500 37,500 36,500 34,500 31,500 29,500 25,500 -10 / 14 5200 4950 4710 4480 4040 3490 3130 2630 0 / 32 5380 5120 4870 4630 4180 3610 3230 2720 5 / 41 5470 5200 4950 4700 4250 3670 3280 2760 10 / 50 5640 5360 5100 4840 4370 3770 3370 2830 15 / 59 5980 5680 5390 5120 4590 3950 3520 2890 20 / 68 6360 6040 5740 5440 4860 4130 3680 2910 25 / 77 6810 6460 6130 5800 5180 4340 3860 3040 30 / 86 7430 6960 6560 6200 5530 4620 4060 3180 35 / 95 8140 7590 7110 6640 5900 4910 4270 3330 40 / 104 9070 8400 7810 7270 6330 5230 4550 3480 Climb Wght Temp Limits °C/°F 40/104 40/104 40/104 40/104 40/104 40/104 40/104 40/104 Field Length at Temp Limits (ft) 9070 8400 7810 7270 6330 5230 4550 3480 8 CITATION LONGITUDE TAKEOFF PERFORMANCE TAKEOFF FIELD LENGTH – FEET; FLAPS 2 (Over 35 Foot Screen Height) Dry Runway, Zero Wind, Anti-Ice Off, Cabin Bleed Air On Elevation = 6,000 Feet Ambient Temp °C / °F ----------------------------------------- Takeoff Weight (lb) ------------------------------------------- 39,500 38,500 37,500 36,500 34,500 31,500 29,500 25,500 -10 / 14 5240 4990 4750 4510 4110 3560 3190 2730 0 / 32 5450 5190 4940 4690 4270 3690 3310 2820 5 / 41 5710 5430 5160 4900 4430 3830 3420 2870 10 / 50 6060 5760 5470 5190 4650 4010 3580 2920 15 / 59 6450 6120 5810 5510 4930 4190 3740 2960 20 / 68 6890 6530 6200 5870 5240 4400 3910 3090 25 / 77 7470 7000 6620 6270 5590 4670 4110 3230 30 / 86 8210 7660 7170 6710 5970 4970 4330 3370 35 / 95 9100 8440 7860 7320 6400 5300 4600 3530 38 / 100 9800 9030 8370 7760 6710 5510 4780 3640 Climb Wght Temp Limits °C/°F 38/100 38/100 38/100 38/100 38/100 38/100 38/100 38/100 Field Length at Temp Limits (ft) 9800 9030 8370 7760 6710 5510 4780 3640 Elevation = 7,000 Feet Ambient Temp °C / °F ----------------------------------------- Takeoff Weight (lb) ------------------------------------------- 39,500 38,500 37,500 36,500 34,500 31,500 29,500 25,500 -10 / 14 5470 5200 4950 4700 4280 3700 3310 2820 0 / 32 5860 5570 5300 5030 4530 3910 3500 2890 5 / 41 6160 5850 5560 5280 4730 4060 3630 2940 10 / 50 6540 6210 5900 5590 5000 4260 3790 3010 15 / 59 6970 6600 6270 5940 5310 4460 3970 3130 20 / 68 7520 7060 6700 6340 5660 4720 4160 3270 25 / 77 8250 7700 7210 6780 6030 5030 4380 3420 30 / 86 9130 8480 7900 7370 6470 5360 4660 3580 35 / 95 - - 9490 8780 8130 7000 5730 4970 3760 36 / 97 - - 9740 8990 8310 7140 5830 5030 3800 Climb Wght Temp Limits °C/°F 33/91 36/97 36/97 36/97 36/97 36/97 36/97 36/97 Field Length at Temp Limits (ft) 9844 9740 8990 8310 7140 5830 5030 3800 9 CITATION LONGITUDE TAKEOFF PERFORMANCE TAKEOFF FIELD LENGTH – FEET; FLAPS 2 (Over 35 Foot Screen Height) Dry Runway, Zero Wind, Anti-Ice Off, Cabin Bleed Air On Elevation = 8,000 Feet Ambient Temp °C / °F ----------------------------------------- Takeoff Weight (lb) ------------------------------------------- 39,500 38,500 37,500 36,500 34,500 31,500 29,500 25,500 -20 / -4 5520 5250 4990 4740 4300 3720 3330 2810 -10 / 14 5880 5590 5320 5050 4540 3920 3510 2890 0 / 32 6310 5990 5700 5410 4850 4150 3700 2960 5 / 41 6650 6310 5990 5680 5090 4320 3850 3050 10 / 50 7070 6700 6360 6030 5390 4530 4030 3180 15 / 59 7570 7140 6770 6410 5720 4780 4220 3320 20 / 68 8290 7750 7270 6860 6110 5090 4430 3470 25 / 77 9160 8510 7940 7410 6530 5420 4710 3630 30 / 86 - - 9480 8790 8150 7070 5790 5020 3810 34 / 93 - - - - 9680 8910 7600 6180 5310 3960 Climb Wght Temp Limits °C/°F 29/84 32/90 34/93 34/93 34/93 34/93 34/93 34/93 Field Length at Temp Limits (ft) 10064 10015 9680 8910 7600 6180 5310 3960 Elevation = 9,000 Feet Ambient Temp °C / °F ----------------------------------------- Takeoff Weight (lb) ------------------------------------------- 39,500 38,500 37,500 36,500 34,500 31,500 29,500 25,500 -20 / -4 5940 5650 5370 5100 4580 3950 3530 2880 -10 / 14 6330 6020 5730 5430 4870 4170 3720 2960 0 / 32 6800 6460 6140 5820 5210 4410 3930 3120 5 / 41 7180 6810 6470 6130 5480 4600 4090 3230 10 / 50 7650 7250 6880 6510 5810 4860 4290 3370 15 / 59 8350 7810 7350 6940 6180 5150 4490 3520 20 / 68 9190 8550 7990 7470 6600 5480 4770 3680 25 / 77 10270 9480 8800 8180 7130 5840 5080 3860 30 / 86 - - - - 9900 9110 7780 6330 5440 4060 32 / 90 - - - - - - 9590 8120 6550 5620 4150 Climb Wght Temp Limits °C/°F 25/77 28/82 30/86 32/90 32/90 32/90 32/90 32/90 Field Length at Temp Limits (ft) 10270 10266 9900 9590 8120 6550 5620 4150 10 CITATION LONGITUDE TAKEOFF PERFORMANCE TAKEOFF FIELD LENGTH – FEET; FLAPS 1 (Over 35 Foot Screen Height) Dry Runway, Zero Wind, Anti-Ice Off, Cabin Bleed Air On Elevation = Sea Level Ambient Temp °C / °F ----------------------------------------- Takeoff Weight (lb) ------------------------------------------- 39,500 38,500 37,500 36,500 34,500 31,500 29,500 25,500 0 / 32 4850 4620 4390 4180 3770 3210 2870 2540 10 / 50 5010 4770 4540 4320 3890 3310 2960 2620 15 / 59 5090 4850 4610 4390 3950 3360 3010 2660 20 / 68 5170 4920 4680 4460 4010 3420 3050 2700 25 / 77 5250 5000 4750 4520 4070 3470 3090 2740 30 / 86 5400 5150 4890 4650 4190 3560 3180 2810 35 / 95 5710 5440 5160 4910 4410 3730 3320 2870 40 / 104 6080 5780 5490 5210 4680 3940 3480 2870 45 / 113 6510 6150 5820 5530 4950 4170 3660 2870 50 / 122 7040 6630 6240 5880 5260 4420 3870 2990 Climb Wght Temp Limits °C/°F 50/122 50/122 50/122 50/122 50/122 50/122 50/122 50/122 Field Length at Temp Limits (ft) 7040 6630 6240 5880 5260 4420 3870 2990 Elevation = 1,000 Feet Ambient Temp °C / °F ----------------------------------------- Takeoff Weight (lb) ------------------------------------------- 39,500 38,500 37,500 36,500 34,500 31,500 29,500 25,500 0 / 32 5000 4770 4530 4310 3890 3310 2960 2620 10 / 50 5170 4920 4680 4460 4010 3420 3050 2710 15 / 59 5250 5000 4750 4520 4080 3470 3100 2750 20 / 68 5330 5080 4830 4600 4140 3520 3140 2790 25 / 77 5450 5190 4930 4690 4230 3600 3210 2840 30 / 86 5760 5480 5210 4950 4450 3770 3360 2930 35 / 95 6120 5820 5520 5250 4710 3970 3510 2940 40 / 104 6550 6190 5870 5570 5000 4200 3690 2940 45 / 113 7060 6660 6260 5920 5310 4450 3900 3020 48 / 118 7410 6980 6560 6170 5510 4620 4040 3110 Climb Wght Temp Limits °C/°F 48/118 48/118 48/118 48/118 48/118 48/118 48/118 48/118 Field Length at Temp Limits (ft) 7410 6980 6560 6170 5510 4620 4040 3110 11 CITATION LONGITUDE TAKEOFF PERFORMANCE TAKEOFF FIELD LENGTH – FEET; FLAPS 1 (Over 35 Foot Screen Height) Dry Runway, Zero Wind, Anti-Ice Off, Cabin Bleed Air On Elevation = 2,000 Feet Ambient Temp °C / °F ----------------------------------------- Takeoff Weight (lb) ------------------------------------------- 39,500 38,500 37,500 36,500 34,500 31,500 29,500 25,500 0 / 32 5170 4920 4680 4460 4020 3420 3050 2710 10 / 50 5340 5090 4840 4600 4150 3530 3150 2800 15 / 59 5420 5170 4910 4680 4210 3580 3200 2840 20 / 68 5510 5250 4990 4750 4270 3640 3250 2880 25 / 77 5790 5520 5240 4980 4480 3800 3390 2990 30 / 86 6160 5870 5570 5290 4750 4010 3550 3000 35 / 95 6570 6230 5920 5620 5320 4240 3720 3010 40 / 104 7090 6690 6300 5970 5650 4490 3940 3060 45 / 113 7690 7240 6800 6400 6020 4770 4170 3200 46 / 115 7820 7360 6910 6500 6110 4830 4230 3230 Climb Wght Temp Limits °C/°F 46/115 46/115 46/115 46/115 46/115 46/115 46/115 46/115 Field Length at Temp Limits (ft) 7820 7360 6910 6500 6110 4830 4230 3230 Elevation = 3,000 Feet Ambient Temp °C / °F ----------------------------------------- Takeoff Weight (lb) ------------------------------------------- 39,500 38,500 37,500 36,500 34,500 31,500 29,500 25,500 -10 / 14 5160 4910 4670 4450 4010 3410 3050 2710 0 / 32 5330 5080 4830 4600 4140 3530 3150 2800 10 / 50 5510 5250 4990 4750 4280 3640 3250 2890 15 / 59 5600 5330 5070 4830 4350 3700 3300 2930 20 / 68 5840 5560 5280 5020 4520 3840 3420 3030 25 / 77 6210 5910 5610 5330 4790 4040 3590 3060 30 / 86 6610 6290 5960 5670 5080 4270 3760 3070 35 / 95 7130 6730 6350 6020 5390 4530 3970 3090 40 / 104 7720 7260 6830 6430 5730 4810 4210 3240 44 / 111 8260 7760 7280 6840 6050 5050 4420 3360 Climb Wght Temp Limits °C/°F 44/111 44/111 44/111 44/111 44/111 44/111 44/111 44/111 Field Length at Temp Limits (ft) 8260 7760 7280 6840 6050 5050 4420 3360 12 CITATION LONGITUDE TAKEOFF PERFORMANCE TAKEOFF FIELD LENGTH – FEET; FLAPS 1 (Over 35 Foot Screen Height) Dry Runway, Zero Wind, Anti-Ice Off, Cabin Bleed Air On Elevation = 4,000 Feet Ambient Temp °C / °F ----------------------------------------- Takeoff Weight (lb) ------------------------------------------- 39,500 38,500 37,500 36,500 34,500 31,500 29,500 25,500 -10 / 14 5320 5070 4820 4590 4130 3520 3140 2800 0 / 32 5510 5250 4990 4750 4270 3640 3250 2890 10 / 50 5690 5420 5150 4900 4410 3760 3350 2980 15 / 59 5890 5610 5330 5070 4560 3880 3460 3070 20 / 68 6250 5950 5650 5370 4830 4070 3630 3120 25 / 77 6660 6340 6010 5710 5120 4310 3800 3130 30 / 86 7170 6770 6400 6080 5440 4570 4010 3140 35 / 95 7750 7300 6870 6480 5780 4850 4250 3270 40 / 104 8430 7920 7420 6990 6180 5150 4500 3440 42 / 108 8740 8200 7680 7210 6370 5280 4610 3500 Climb Wght Temp Limits °C/°F 42/108 42/108 42/108 42/108 42/108 42/108 42/108 42/108 Field Length at Temp Limits (ft) 8740 8200 7680 7210 6370 5280 4610 3500 Elevation = 5,000 Feet Ambient Temp °C / °F ----------------------------------------- Takeoff Weight (lb) ------------------------------------------- 39,500 38,500 37,500 36,500 34,500 31,500 29,500 25,500 -10 / 14 5510 5250 4990 4830 4350 3700 3300 2940 0 / 32 5700 5430 5160 4910 4420 3770 3360 2990 5 / 41 5790 5520 5250 4990 4500 3830 3420 3030 10 / 50 5970 5680 5400 5140 4620 3930 3500 3110 15 / 59 6310 6010 5710 5430 4880 4120 3670 3180 20 / 68 6710 6380 6060 5750 5160 4350 3840 3190 25 / 77 7200 6800 6450 6130 5490 4610 4050 3210 30 / 86 7810 7360 6930 6550 5850 4900 4290 3320 35 / 95 8450 7950 7460 7040 6230 5200 4550 3470 40 / 104 9260 8670 8110 7610 6730 5530 4830 3650 Climb Wght Temp Limits °C/°F 40/104 40/104 40/104 40/104 40/104 40/104 40/104 40/104 Field Length at Temp Limits (ft) 9260 8670 8110 7610 6730 5530 4830 3650 13 CITATION LONGITUDE TAKEOFF PERFORMANCE TAKEOFF FIELD LENGTH – FEET; FLAPS 1 (Over 35 Foot Screen Height) Dry Runway, Zero Wind, Anti-Ice Off, Cabin Bleed Air On Elevation = 6,000 Feet Ambient Temp °C / °F ----------------------------------------- Takeoff Weight (lb) ------------------------------------------- 39,500 38,500 37,500 36,500 34,500 31,500 29,500 25,500 -10 / 14 5560 5300 5040 4800 4320 3700 3310 3000 0 / 32 5780 5510 5240 4990 4490 3840 3430 3100 5 / 41 6050 5760 5470 5210 4690 3990 3550 3160 10 / 50 6400 6100 5790 5510 4950 4180 3720 3210 15 / 59 6800 6470 6140 5830 5230 4410 3900 3240 20 / 68 7260 6880 6530 6200 5550 4670 4100 3260 25 / 77 7860 7410 7000 6610 5910 4960 4340 3360 30 / 86 8540 8030 7550 7130 6310 5270 4610 3520 35 / 95 9330 8740 8180 7690 6800 5600 4890 3700 38 / 100 9900 9250 8640 8090 7130 5850 5070 3830 Climb Wght Temp Limits °C/°F 38/100 38/100 39/102 40/104 40/104 40/104 40/104 40/104 Field Length at Temp Limits (ft) 9900 9250 8640 8090 7130 5850 5070 3830 Elevation = 7,000 Feet Ambient Temp °C / °F ----------------------------------------- Takeoff Weight (lb) ------------------------------------------- 39,500 38,500 37,500 36,500 34,500 31,500 29,500 25,500 -10 / 14 5790 5520 5250 5000 4500 3850 3440 3100 0 / 32 6200 5900 5610 5340 4810 4080 3640 3180 5 / 41 6510 6190 5890 5600 5030 4250 3780 3230 10 / 50 6900 6560 6230 5920 5310 4480 3960 3290 15 / 59 7340 6970 6610 6270 5620 4730 4150 3320 20 / 68 7930 7490 7070 6680 5980 5020 4400 3410 25 / 77 8610 8100 7630 7200 6380 5330 4660 3570 30 / 86 9390 8810 8250 7780 6880 5670 4950 3750 35 / 95 10360 9680 9020 8440 7440 6110 5270 3970 36 / 97 10590 9880 9200 8600 7560 6200 5340 4020 Climb Wght Temp Limits °C/°F 36/97 36/97 36/97 36/97 36/97 36/97 36/97 36/97 Field Length at Temp Limits (ft) 10590 9880 9200 8600 7560 6200 5340 4020 14 CITATION LONGITUDE TAKEOFF PERFORMANCE TAKEOFF FIELD LENGTH – FEET; FLAPS 1 (Over 35 Foot Screen Height) Dry Runway, Zero Wind, Anti-Ice Off, Cabin Bleed Air On Elevation = 8,000 Feet Ambient Temp °C / °F ----------------------------------------- Takeoff Weight (lb) ------------------------------------------- 39,500 38,500 37,500 36,500 34,500 31,500 29,500 25,500 -20 / 4 5840 5560 5290 5040 4540 3870 3460 3090 -10 / 14 6220 5920 5630 5360 4820 4090 3650 3180 0 / 32 6660 6340 6020 5730 5150 4350 3860 3250 5 / 41 7010 6670 6330 6020 5400 4550 4020 3310 10 / 50 7440 7070 6710 6370 5710 4810 4220 3380 15 / 59 8010 7580 7150 6760 6050 5080 4460 3450 20 / 68 8670 8180 7710 7280 6450 5400 4720 3620 25 / 77 9450 8860 8320 7850 6950 5730 5010 3800 30 / 86 10390 9710 9070 8500 7510 6160 5330 4020 34 / 93 - - 10560 9820 9160 8020 6570 5660 4220 Climb Wght Temp Limits °C/°F 33/91 34/93 34/93 34/93 34/93 34/93 34/93 34/93 Field Length at Temp Limits (ft) 11125 10560 9820 9160 8020 6570 5660 4220 Elevation = 9,000 Feet Ambient Temp °C / °F ----------------------------------------- Takeoff Weight (lb) ------------------------------------------- 39,500 38,500 37,500 36,500 34,500 31,500 29,500 25,500 -20 / -4 6280 5980 5690 5410 4870 4120 3680 3170 -10 / 14 6690 6370 6050 5750 5180 4370 3880 3250 0 / 32 7170 6820 6480 6160 5530 4670 4110 3330 5 / 41 7560 7190 6820 6480 5810 4890 4290 3390 10 / 50 8110 7680 7250 6860 6150 5160 4520 3510 15 / 59 8750 8270 7800 7370 6530 5470 4790 3680 20 / 68 9510 8930 8410 7940 7020 5800 5070 3850 25 / 77 10420 9750 9110 8570 7580 6220 5390 4060 30 / 86 - - 10810 10050 9370 8220 6740 5800 4320 32 / 90 - - 11330 10500 9770 8510 6970 6000 4430 Climb Wght Temp Limits °C/°F 29/84 32/90 32/90 32/90 32/90 32/90 32/90 32/90 Field Length at Temp Limits (ft) 11636 11330 10500 9770 8510 6970 6000 4430 15 CITATION LONGITUDE CLIMB PERFORMANCE CRUISE CLIMB - 270 KIAS / M 0.80 ISA, Zero Wind, Anti-Ice Off Time, Fuel and Distance To Climb * Pressure Altitude (ft) --------------------------------------- Takeoff Weight (lb) ----------------------------------------- 39,500 38,000 36,000 33,000 30,000 26,000 15,000 Min 3 3 3 3 2 2 Lb 316 303 285 259 233 200 NM 16 15 14 13 12 10 25,000 Min 6 6 6 5 5 4 Lb 548 524 491 445 399 342 NM 35 33 31 28 25 21 31,000 Min 9 9 8 7 7 6 Lb 718 684 640 576 516 439 NM 55 52 49 44 39 33 33,000 Min 11 10 9 8 7 6 Lb 786 748 698 628 561 476 NM 64 61 57 51 45 38 35,000 Min 12 12 11 10 8 7 Lb 866 821 765 685 611 517 NM 76 72 67 59 53 44 37,000 Min 14 13 12 11 9 8 Lb 941 891 827 739 656 554 NM 89 83 77 68 60 50 39,000 Min 16 15 14 12 11 9 Lb 1023 965 892 792 701 590 NM 103 97 89 78 68 57 41,000 Min 18 17 16 14 12 10 Lb 1126 1055 970 855 752 629 NM 124 115 104 90 78 64 43,000 Min 23 21 19 16 14 11 Lb 1275 1179 1069 930 811 672 NM 157 143 127 107 91 74 45,000 Min 96** 49** 23 19 16 13 Lb 3571 2069 1220 1030 882 721 NM 725 363 164 132 109 86 * Based on the climb starting from sea level. ** Step climb required - includes cruise portion. 16 CITATION LONGITUDE CLIMB PERFORMANCE MAX RATE CLIMB - 270 KIAS / M 0.76 ISA, Zero Wind, Anti-Ice Off Time, Fuel and Distance To Climb * Pressure Altitude (ft) --------------------------------------- Takeoff Weight (lb) ----------------------------------------- 39,500 38,000 36,000 33,000 30,000 26,000 15,000 Min 3 3 3 3 2 2 Lb 316 303 285 259 233 200 NM 16 15 14 13 12 10 25,000 Min 6 6 6 5 5 4 Lb 548 524 491 445 399 342 NM 35 33 31 28 25 21 31,000 Min 9 9 8 7 7 6 Lb 718 684 640 576 516 439 NM 55 52 49 44 39 33 33,000 Min 11 10 9 8 7 6 Lb 785 747 698 627 560 476 NM 64 61 57 51 45 38 35,000 Min 12 11 10 9 8 7 Lb 846 800 746 669 597 506 NM 73 69 64 57 50 42 37,000 Min 13 12 11 10 9 8 Lb 900 853 793 710 632 534 NM 82 77 71 63 56 47 39,000 Min 15 14 13 11 10 8 Lb 969 916 849 757 671 566 NM 94 88 81 71 63 52 41,000 Min 17 16 14 13 11 9 Lb 1054 992 915 810 715 600 NM 110 103 94 82 71 59 43,000 Min 20 19 17 15 13 10 Lb 1172 1090 996 873 765 637 NM 136 124 111 95 82 67 45,000 Min 96** 50** 21 17 15 12 Lb 3572 2069 1113 953 824 680 NM 726 364 139 114 96 77 * Based on the climb starting from sea level. ** Step climb required - includes cruise portion. 17 CITATION LONGITUDE Cruise Speed & Fuel Flow Pressure Altitude (ft) --------------------------------------- Cruise Weight (lb) ----------------------------------------- 39,000 38,000 36,000 34,000 32,000 29,000 29,000 KTAS 492 492 492 492 492 492 Lb/Hr 2916 2896 2857 2819 2789 2747 31,000 KTAS 492 492 492 492 492 492 Lb/Hr 2823 2799 2752 2708 2668 2613 33,000 KTAS 487 487 487 487 487 487 Lb/Hr 2658 2627 2573 2524 2478 2416 35,000 KTAS 483 483 483 483 483 483 Lb/Hr 2523 2491 2420 2358 2306 2236 37,000 KTAS 481 481 481 481 481 481 Lb/Hr 2403 2369 2306 2241 2172 2090 39,000 KTAS 481 481 481 481 481 481 Lb/Hr 2335 2295 2215 2147 2084 1981 41,000 KTAS 476 477 480 481 481 481 Lb/Hr 2119 2122 2126 2075 1999 1901 43,000 KTAS 462 466 473 477 480 481 Lb/Hr 1887 1894 1904 1910 1915 1825 45,000 KTAS - - - - - - 466 473 479 Lb/Hr - - - - - - 1702 1712 1722 * Maximum Cruise Thrust The following tables present cruise performance in ISA conditions for the Citation Longitude. The fuel flow shown is total fuel for both engines. • Maximum Speed Cruise is limited by MMO (M0.84) or available cruise thrust • Constant Mach Cruise at M0.82 • Constant Mach Cruise at M0.80 CRUISE PERFORMANCE MAXIMUM SPEED CRUISE * ISA, Anti-Ice Off 18 CITATION LONGITUDE CRUISE PERFORMANCE HIGH SPEED CRUISE - M0.82* ISA, Anti-Ice Off Cruise Speed & Fuel Flow Pressure Altitude (ft) --------------------------------------- Cruise Weight (lb) ----------------------------------------- 39,000 38,000 36,000 34,000 32,000 29,000 5,000 KTAS 310 310 310 310 310 310 Lb/Hr 2541 2529 2506 2484 2464 2435 10,000 KTAS 372 372 372 372 372 372 Lb/Hr 2979 2968 2948 2928 2910 2885 15,000 KTAS 400 400 400 400 400 400 Lb/Hr 2887 2876 2855 2835 2817 2791 21,000 KTAS 437 437 437 437 437 437 Lb/Hr 2812 2796 2766 2740 2718 2687 25,000 KTAS 463 463 463 463 463 463 Lb/Hr 2816 2800 2769 2741 2716 2682 27,000 KTAS 478 478 478 478 478 478 Lb/Hr 2834 2817 2785 2756 2730 2693 29,000 KTAS 486 486 486 486 486 486 Lb/Hr 2822 2808 2770 2733 2703 2664 31,000 KTAS 480 480 480 480 480 480 Lb/Hr 2627 2605 2576 2536 2498 2455 33,000 KTAS 476 476 476 476 476 476 Lb/Hr 2445 2441 2393 2351 2311 2272 35,000 KTAS 471 471 471 471 471 471 Lb/Hr 2260 2235 2188 2145 2105 2048 37,000 KTAS 469 469 469 469 469 469 Lb/Hr 2146 2119 2064 2014 1969 1910 39,000 KTAS 469 469 469 469 469 469 Lb/Hr 2058 2028 1976 1921 1868 1798 41,000 KTAS 469 469 469 469 469 469 Lb/Hr 1991 1954 1896 1840 1787 1706 43,000 KTAS 462 466 469 469 469 469 Lb/Hr 1887 1894 1843 1771 1713 1630 45,000 KTAS - - - - - - 466 469 469 Lb/Hr - - - - - - 1702 1654 1564 * Max Cruise Thrust for Limit Airspeed, M0.82 Cruise or Thrust for Maximum Range (approximate). 19 CITATION LONGITUDE CRUISE PERFORMANCE INTERMEDIATE SPEED CRUISE - M0.80 * ISA, Anti-Ice Off Cruise Speed & Fuel Flow Pressure Altitude (ft) --------------------------------------- Cruise Weight (lb) ----------------------------------------- 39,000 38,000 36,000 34,000 32,000 29,000 5,000 KTAS 310 310 310 310 310 310 Lb/Hr 2541 2529 2506 2484 2464 2435 10,000 KTAS 372 372 372 372 372 372 Lb/Hr 2979 2968 2948 2928 2910 2885 15,000 KTAS 400 400 400 400 400 400 Lb/Hr 2887 2876 2855 2835 2817 2791 21,000 KTAS 437 437 437 437 437 437 Lb/Hr 2812 2796 2766 2740 2718 2687 25,000 KTAS 463 463 463 463 463 463 Lb/Hr 2816 2800 2769 2741 2716 2682 27,000 KTAS 478 478 478 478 478 478 Lb/Hr 2834 2817 2785 2756 2730 2767 29,000 KTAS 473 473 473 473 473 473 Lb/Hr 2635 2633 2596 2561 2530 2499 31,000 KTAS 468 468 468 468 468 468 Lb/Hr 2430 2411 2400 2363 2329 2297 33,000 KTAS 464 464 464 464 464 464 Lb/Hr 2282 2254 2213 2178 2143 2129 35,000 KTAS 460 460 460 460 460 460 Lb/Hr 2144 2120 2070 2026 1988 1935 37,000 KTAS 457 457 457 457 457 457 Lb/Hr 2039 2013 1960 1911 1863 1804 39,000 KTAS 457 457 457 457 457 457 Lb/Hr 1959 1931 1877 1827 1773 1701 41,000 KTAS 457 457 457 457 457 457 Lb/Hr 1891 1863 1807 1751 1698 1619 43,000 KTAS 459 458 457 457 457 457 Lb/Hr 1861 1814 1745 1686 1631 1575 45,000 KTAS - - - - - - 457 457 457 Lb/Hr - - - - - - 1632 1573 1488 * Max Cruise Thrust for Limit Airspeed, M0.80 Cruise or Thrust for Maximum Range (approximate). 20 CITATION LONGITUDE Time, Fuel and Distance To Descend * High Speed - 3,000 FPM Normal - 2,000 FPM Pressure Altitude (ft) ------ Start of Descent Weight (lb) ------ ------ Start of Descent Weight (lb) ------ 35,000 30,000 25,000 35,000 30,000 25,000 15,000 Min 8 7 7 8 8 8 Lb 114 111 107 149 146 155 NM 37 35 32 42 40 40 21,000 Min 10 9 9 12 11 11 Lb 145 148 150 221 223 237 NM 51 48 46 63 60 60 25,000 Min 11 10 10 14 13 13 Lb 166 172 177 268 273 290 NM 60 58 55 77 75 74 33,000 Min 14 13 13 18 17 17 Lb 214 225 235 369 376 398 NM 81 79 76 108 106 106 35,000 Min 14 14 13 18 18 18 Lb 226 237 248 392 400 423 NM 86 84 81 116 114 114 37,000 Min 15 14 14 20 19 19 Lb 236 248 260 414 421 444 NM 92 89 87 124 122 122 39,000 Min 16 15 15 20 20 20 Lb 245 257 269 433 440 463 NM 97 95 92 132 130 129 41,000 Min 16 16 15 22 21 21 Lb 253 265 278 450 458 481 NM 102 100 97 140 138 137 43,000 Min 17 17 16 22 22 22 Lb 263 275 287 467 474 497 NM 108 106 103 148 145 145 45,000 Min 18 17 17 24 23 23 Lb 273 285 297 483 489 512 NM 115 112 109 155 153 153 * Based on descending to sea level. DESCENT PERFORMANCE HIGH SPEED & NORMAL DESCENT ISA, Zero Wind, Anti-Ice Off, Speed Brakes Retracted, Gear & Flaps Up 21 CITATION LONGITUDE RESERVE FUEL RESERVE FUEL ALLOWANCES Based on 4 Passengers, ISA, Zero Wind VFR Fuel Reserves (at 5,000 feet) Day (30 minutes) 616 lb Night (45 minutes) 924 lb IFR Fuel Reserves (Alternate plus 45 minutes at 5,000 feet) 100 Nautical Mile Alternate 1,541 lb 200 Nautical Mile Alternate 1,971 lb 300 Nautical Mile Alternate 2,309 lb NBAA IFR Reserves * 100 Nautical Mile Alternate 1,457 lb 200 Nautical Mile Alternate 1,883 lb 300 Nautical Mile Alternate 2,217 lb *NBAA IFR Reserves are defined as the amount of fuel for the following profile: - A 5 minute approach at sea level - Climb to 5,000 feet - A 5 minute hold at 5,000 feet - Climb to cruise altitude for the diversion to the alternate airport - Cruise at long range cruise power - Descend to sea level - Land with 30 minutes of holding fuel at 5,000 feet. HOLDING PERFORMANCE ISA, Anti-Ice Off, Speed Brakes Retracted, Gear & Flaps Up Holding Speed (KIAS) & Fuel Flow (lb/hr) Weight (lb) ------------------------------------- Pressure Altitude (ft) --------------------------------------- Speed S.L. 5,000 10,000 15,000 20,000 25,000 30,000 38,000 194 1740 1642 1586 1538 1491 1467 1456 36,000 188 1670 1568 1512 1466 1420 1399 1377 33,000 179 1568 1459 1403 1359 1314 1293 1260 30,000 170 1469 1352 1298 1254 1211 1188 1158 27,000 160 1370 1245 1194 1150 1108 1084 1055 24,000 160 1310 1193 1133 1089 1037 1012 986 22 CITATION LONGITUDE LANDING PERFORMANCE LANDING DISTANCE - FEET (ACTUAL DISTANCE); FLAPS FULL (Distance from 50 Feet Above the Runway) Dry Runway, Zero Wind, Anti-Ice On or Off Elevation = Sea Level Ambient Temp °C / °F ----------------------------------------- Landing Weight (lb) ------------------------------------------- 33500 31500 29500 27500 26500 25500 24500 23500 0 / 32 3040 2890 2730 2580 2510 2440 2380 2300 10 / 50 3120 2970 2800 2650 2580 2510 2440 2360 15 / 59 3170 3010 2840 2690 2610 2540 2470 2390 20 / 68 3210 3050 2870 2720 2650 2570 2500 2420 25 / 77 3250 3090 2910 2760 2680 2600 2530 2450 30 / 86 3290 3130 2950 2790 2710 2640 2560 2480 35 / 95 3330 3170 2980 2820 2750 2670 2600 2510 40 / 104 3370 3210 3020 2860 2780 2700 2620 2540 45 / 113 3420 3250 3060 2900 2810 2740 2660 2580 50 / 122 3460 3290 3100 2930 2850 2770 2690 2610 Lndg Wght Temp Limits °C/°F 50/122 50/122 50/122 50/122 50/122 50/122 50/122 50/122 VREF (KIAS) 125 121 116 112 110 108 106 104 Elevation = 1,000 Feet Ambient Temp °C / °F ----------------------------------------- Landing Weight (lb) ------------------------------------------- 33500 31500 29500 27500 26500 25500 24500 23500 0 / 32 3120 2970 2800 2650 2580 2510 2440 2360 10 / 50 3210 3050 2880 2730 2650 2580 2500 2420 15 / 59 3250 3100 2910 2760 2680 2610 2540 2460 20 / 68 3300 3140 2950 2800 2720 2640 2570 2490 25 / 77 3340 3180 2990 2830 2750 2680 2600 2520 30 / 86 3380 3220 3030 2870 2790 2710 2630 2550 35 / 95 3430 3260 3060 2900 2820 2740 2660 2580 40 / 104 3470 3300 3100 2940 2860 2780 2700 2310 45 / 113 3510 3340 3140 2980 2890 2810 2730 2640 48 / 118 3540 3370 3170 3000 2910 2830 2750 2660 Lndg Wght Temp Limits °C/°F 48/118 48/118 48/118 48/118 48/118 48/118 48/118 48/118 VREF (KIAS) 125 121 116 112 110 108 106 104 23 CITATION LONGITUDE Elevation = 2,000 Feet Ambient Temp °C / °F ----------------------------------------- Landing Weight (lb) ------------------------------------------- 33500 31500 29500 27500 26500 25500 24500 23500 0 / 32 3210 3050 2880 2730 2650 2580 2500 2420 10 / 50 3300 3140 2960 2800 2720 2640 2570 2490 15 / 59 3340 3180 3000 2840 2760 2680 2600 2520 20 / 68 3390 3230 3030 2870 2790 2710 2640 2560 25 / 77 3430 3260 3070 2910 2830 2750 2670 2590 30 / 86 3480 3310 3110 2950 2860 2780 2700 2620 35 / 95 3520 3350 3150 2980 2900 2820 2740 2650 40 / 104 3570 3390 3190 3020 2940 2850 2770 2680 45 / 113 3610 3440 3230 3060 2970 2890 2810 2720 46 / 115 3620 3440 3240 3070 2980 2900 2810 2720 Lndg Wght Temp Limits °C/°F 46/115 46/115 46/115 46/115 46/115 46/115 46/115 46/115 VREF (KIAS) 125 121 116 112 110 108 106 104 Elevation = 3,000 Feet Ambient Temp °C / °F ----------------------------------------- Landing Weight (lb) ------------------------------------------- 33500 31500 29500 27500 26500 25500 24500 23500 -10 / 14 3210 3050 2870 2720 2650 2580 2500 2420 0 / 32 3300 3140 2960 2800 2720 2650 2570 2490 10 / 50 3390 3230 3040 2880 2800 2720 2640 2560 15 / 59 3440 3270 3080 2910 2830 2750 2670 2590 20 / 68 3480 3310 3120 2950 2870 2790 2710 2620 25 / 77 3530 3360 3160 2990 2910 2820 2740 2660 30 / 86 3580 3400 3200 3030 2940 2860 2780 2690 35 / 95 3620 3440 3240 3070 2980 2890 2810 2720 40 / 104 3670 3490 3280 3100 3020 2930 2850 2760 44 / 111 3700 3520 3310 3140 3050 2960 2870 2790 Lndg Wght Temp Limits °C/°F 44/111 44/111 44/111 44/111 44/111 44/111 44/111 44/111 VREF (KIAS) 125 121 116 112 110 108 106 104 LANDING PERFORMANCE LANDING DISTANCE - FEET (ACTUAL DISTANCE); FLAPS FULL (Distance from 50 Feet Above the Runway) Dry Runway, Zero Wind, Anti-Ice On or Off 24 CITATION LONGITUDE LANDING PERFORMANCE LANDING DISTANCE - FEET (ACTUAL DISTANCE); FLAPS FULL (Distance from 50 Feet Above the Runway) Dry Runway, Zero Wind, Anti-Ice On or Off Elevation = 4,000 Feet Ambient Temp °C / °F ----------------------------------------- Landing Weight (lb) ------------------------------------------- 33500 31500 29500 27500 26500 25500 24500 23500 -10 / 14 3300 3140 2960 2800 2720 2640 2570 2490 0 / 32 3400 3230 3040 2880 2800 2720 2640 2560 10 / 50 3490 3320 3120 2960 2870 2790 2710 2630 15 / 59 3540 3370 3170 3000 2910 2830 2750 2660 20 / 68 3590 3410 3210 3030 2950 2870 2790 2700 25 / 77 3630 3450 3250 3070 2990 2900 2820 2730 30 / 86 3680 3500 3290 3110 3020 2940 2850 2770 35 / 95 3720 3540 3330 3150 3060 2980 2890 2800 40 / 104 3770 3590 3370 3190 3100 3010 2930 2830 42 / 108 3790 3610 3390 3210 3120 3030 2940 2850 Lndg Wght Temp Limits °C/°F 42/108 42/108 42/108 42/108 42/108 42/108 42/108 42/108 VREF (KIAS) 125 121 116 112 110 108 106 104 Elevation = 5,000 Feet Ambient Temp °C / °F ----------------------------------------- Landing Weight (lb) ------------------------------------------- 33500 31500 29500 27500 26500 25500 24500 23500 -10 / 14 3400 3230 3040 2880 2810 2730 2650 2570 0 / 32 3500 3330 3130 2970 2880 2800 2720 2640 5 / 41 3550 3370 3170 3010 2920 2840 2760 2670 10 / 50 3600 3420 3220 3050 2960 2880 2800 2710 15 / 59 3640 3460 3260 3090 3000 2920 2830 2750 20 / 68 3690 3510 3300 3130 3040 2960 2870 2780 25 / 77 3740 3560 3350 3170 3080 2990 2910 2810 30 / 86 3790 3610 3390 3210 3120 3030 2940 2850 35 / 95 3840 3650 3430 3250 3160 3070 2980 2890 40 / 104 3890 3690 3470 3290 3200 3110 3020 2920 Lndg Wght Temp Limits °C/°F 40/104 40/104 40/104 40/104 40/104 40/104 40/104 40/104 VREF (KIAS) 125 121 116 112 110 108 106 104 25 CITATION LONGITUDE LANDING PERFORMANCE LANDING DISTANCE - FEET (ACTUAL DISTANCE); FLAPS FULL (Distance from 50 Feet Above the Runway) Dry Runway, Zero Wind, Anti-Ice On or Off Elevation = 6,000 Feet Ambient Temp °C / °F ----------------------------------------- Landing Weight (lb) ------------------------------------------- 33500 31500 29500 27500 26500 25500 24500 23500 -10 / 14 3500 3330 3140 2970 2890 2810 2730 2640 0 / 32 3600 3430 3230 3050 2970 2890 2810 2720 5 / 41 3650 3480 3270 3100 3010 2930 2840 2750 10 / 50 3700 3520 3320 3140 3050 2970 2880 2790 15 / 59 3760 3570 3360 3180 3090 3010 2920 2830 20 / 68 3810 3620 3410 3220 3130 3040 2960 2860 25 / 77 3850 3670 3450 3260 3170 3080 3000 2900 30 / 86 3910 3710 3490 3310 3210 3120 3030 2940 35 / 95 3960 3760 3540 3350 3250 3160 3070 2970 38 / 100 3990 3790 3560 3370 3280 3180 3090 3000 Lndg Wght Temp Limits °C/°F 38/100 38/100 38/100 38/100 38/100 38/100 38/100 38/100 VREF (KIAS) 125 121 116 112 110 108 106 104 Elevation = 7,000 Feet Ambient Temp °C / °F ----------------------------------------- Landing Weight (lb) ------------------------------------------- 33500 31500 29500 27500 26500 25500 24500 23500 -10 / 14 3610 3430 3230 3060 2980 2890 2810 2720 0 / 32 3710 3530 3320 3150 3060 2970 2890 2800 5 / 41 3770 3580 3370 3190 3100 3020 2930 2830 10 / 50 3820 3630 3420 3230 3140 3050 2970 2870 15 / 59 3870 3680 3460 3280 3190 3090 3010 2910 20 / 68 3920 3730 3510 3320 3230 3140 3040 2950 25 / 77 3970 3780 3550 3360 3270 3180 3080 2990 30 / 86 4030 3830 3600 3410 3310 3220 3120 3020 35 / 95 4080 3880 3650 3450 3350 3250 3160 3060 36 / 97 4090 3890 3650 3460 3360 3260 3170 3070 Lndg Wght Temp Limits °C/°F 36/97 36/97 36/97 36/97 36/97 36/97 36/97 36/97 VREF (KIAS) 125 121 116 112 110 108 106 104 26 CITATION LONGITUDE LANDING PERFORMANCE LANDING DISTANCE - FEET (ACTUAL DISTANCE); FLAPS FULL (Distance from 50 Feet Above the Runway) Dry Runway, Zero Wind, Anti-Ice On or Off Elevation = 8,000 Feet Ambient Temp °C / °F ----------------------------------------- Landing Weight (lb) ------------------------------------------- 33500 31500 29500 27500 26500 25500 24500 23500 -10 / 14 3720 3540 3330 3150 3060 2980 2890 2800 -5 / 23 3770 3590 3380 3200 3110 3020 2930 2840 0 / 32 3830 3640 3430 3240 3150 3060 2980 2880 5 / 41 3880 3690 3470 3290 3200 3100 3020 2920 10 / 50 3930 3740 3520 3330 3240 3150 3050 2960 15 / 59 3990 3790 3570 3380 3280 3190 3100 3000 20 / 68 4040 3850 3620 3420 3320 3230 3140 3040 25 / 77 4100 3890 3660 3460 3370 3270 3180 3080 30 / 86 4150 3950 3710 3510 3410 3310 3220 3120 34 / 93 4190 3990 3750 3540 3440 3350 3250 3150 Lndg Wght Temp Limits °C/°F 34/93 34/93 34/93 34/93 34/93 34/93 34/93 34/93 VREF (KIAS) 125 121 116 112 110 108 106 104 STALL SPEEDS Zero Angle of Bank, Landing Gear Up or Down Stall Speeds (KCAS) Weight (lb) ----------------------------------------- Flap Position ------------------------------------------- Flaps FULL Flaps 2 Flaps 1 UP 33500 102 111 116 129 31500 98 107 112 125 29500 94 103 108 120 27500 91 99 104 116 26500 90 98 102 114 25500 88 96 100 111 24500 86 94 98 109 23500 84 92 96 107 27 CITATION LONGITUDE MISSION PLANNING CRITERIA The following mission planning table provides flight time and fuel burn estimates for selected distances and cruise altitudes. Flight time represents the time for the climb, cruise and descent portion of the mission. No allowance has been added for taxi, takeoff, approach, or ATC procedures. Fuel burn represents the total amount of fuel consumed for taxi, takeoff, climb, cruise, and descent. There is a taxi and takeoff allowance of 200 pounds of fuel included in all fuel burn figures. NBAA IFR fuel reserves (200 nm) are considered in each case but are not included in the fuel burn figure. Each distance and altitude combination is based on the aircraft departing at the minimum takeoff weight required to complete the mission. The mission planning table reflects the 270 knots / M 0.76 climb, M0.82 cruise and high-speed descent (3,000 fpm) schedules. Standard day conditions are assumed with zero wind enroute. The effects of wind can be determined from the wind correction factors table below. Apply the wind correction factor to the zero wind flight time and fuel burn to estimate the impact of wind. Typical cruise altitudes for various distances are: Distance (nm) Typical Cruise Altitude (ft) 0 - 99 4,000 - 10,000 100 - 199 9,000 - 22,000 200 - 299 21,000 - 30,000 300 - 499 29,000 - 41,000 500 - 999 37,000 - 43,000 1,000 + 41,000 - 45,000 Wind Correction Factors * True Airspeed ------------ Headwinds (kt) ------------ ------------ Tailwinds (kt) ----------- (kt) 100 75 50 25 0 25 50 75 100 360 1.38 1.26 1.16 1.07 1.00 0.93 0.88 0.83 0.78 380 1.36 1.25 1.15 1.07 1.00 0.94 0.88 0.84 0.79 400 1.33 1.23 1.14 1.06 1.00 0.94 0.89 0.84 0.80 420 1.31 1.22 1.13 1.06 1.00 0.94 0.89 0.85 0.81 440 1.29 1.21 1.13 1.06 1.00 0.95 0.90 0.85 0.81 460 1.28 1.19 1.12 1.06 1.00 0.95 0.90 0.86 0.82 480 1.26 1.19 1.12 1.05 1.00 0.95 0.91 0.86 0.83 * Wind Correction Factor is calculated as KTAS divided by the sum of KTAS ± wind component. 28 CITATION LONGITUDE ----------------------------------------------- Cruise Altitude (ft) ----------------------------------------------- 25,000 29,000 31,000 33,000 35,000 Dist (nm) Time (min) Fuel (lb) Time (min) Fuel (lb) Time (min) Fuel (lb) Time (min) Fuel (lb) Time (min) Fuel (lb) 200 0:30 1438 0:30 1390 0:30 1353 0:30 1326 0:30 1296 300 0:43 2018 0:42 1939 0:43 1864 0:42 1802 0:43 1730 400 0:56 2599 0:54 2488 0:55 2376 0:55 2279 0:55 2166 500 1:09 2181 1:07 3039 1:08 2890 1:08 2757 1:08 2603 600 1:22 3764 1:19 3591 1:20 3404 1:20 3237 1:21 3041 700 1:35 4351 1:32 4145 1:33 3920 1:33 3718 1:34 3481 800 1:48 4940 1:44 4703 1:45 4441 1:46 4202 1:46 3923 1,000 2:14 6125 2:08 5826 2:10 5490 2:11 5182 2:12 4811 1,200 2:40 7319 2:33 6958 2:35 6549 2:36 6171 2:37 5706 1,400 3:06 8516 2:58 8100 3:00 7618 3:01 7166 3:03 6608 1,600 3:32 9710 3:23 9234 3:25 8686 3:27 8168 3:28 7520 1,800 3:58 10911 3:47 10373 3:50 9752 3:52 9161 3:54 8440 2,000 4:12 11517 4:15 10824 4:17 10158 4:20 9367 2,200 4:41 11902 4:43 11161 4:45 10302 2,400 5:08 12167 5:11 11245 2,600 5:36 12196 2,800 3,000 3,200 3,275 MISSION PLANNING FLIGHT TIME & FUEL BURN Assumptions: • 270 KIAS / M 0.76 climb • M0.82 cruise • High-speed descent (3,000 fpm) • ISA, zero winds enroute • Flight time includes climb, cruise and descent • Fuel burn includes 200 pounds for taxi and takeoff • NBAA IFR Reserves – 200 nm (1,883 lb) Reserves are not included in the fuel burn figures • Four passengers @ 200 pounds each • Aircraft BOW of 23,600 pounds (includes 2 crew at 200 pounds each) 29 CITATION LONGITUDE FOR SELECTED DISTANCES ----------------------------------------------- Cruise Altitude (ft) ----------------------------------------------- 37,000 39,000 41,000 43,000 45,000 Time (min) Fuel (lb) Time (min) Fuel (lb) Time (min) Fuel (lb) Time (min) Fuel (lb) Time (min) Fuel (lb) Dist (nm) 0:30 1273 0:30 1260 0:30 1251 0:30 1244 0:31 1244 200 0:43 1678 0:43 1640 0:43 1610 0:43 1586 0:44 1570 300 0:56 2085 0:56 2022 0:56 1972 0:56 1929 0:57 1899 400 1:09 2494 1:09 2406 1:09 2334 1:09 2275 1:09 2230 500 1:21 2904 1:22 2792 1:21 2699 1:22 2622 1:22 2562 600 1:34 3316 1:35 3179 1:34 3066 1:35 2971 1:35 2896 700 1:47 3729 1:47 3567 1:47 3434 1:48 3322 1:48 3233 800 2:13 4562 2:13 4351 2:13 4176 2:13 4031 2:14 3911 1,000 2:38 5402 2:39 5142 2:38 4927 2:39 4749 2:39 4600 1,200 3:04 6249 3:04 5940 3:04 5686 3:05 5477 3:05 5317 1,400 3:29 7104 3:30 6748 3:30 6454 3:30 6213 3:31 6050 1,600 3:55 7967 3:56 7564 3:56 7230 3:56 6958 3:56 6792 1,800 4:21 8837 4:21 8389 4:21 8016 4:22 7713 4:22 7543 2,000 4:46 9713 4:47 9222 4:46 8814 4:47 8477 4:47 8303 2,200 5:12 10598 5:13 10064 5:12 9624 5:13 9250 5:13 9072 2,400 5:38 11491 5:39 10917 5:38 10444 5:38 10032 5:39 9851 2,600 6:03 12392 6:04 11779 6:04 11275 6:04 10825 6:04 10641 2,800 6:29 12117 6:30 11650 6:30 11457 3,000 6:56 12491 6:56 12296 3,200 7:06 12617 3,275 © 2019 Textron Aviation Inc. 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