C I TAT I O N LO N G I T U D E FLIGHT PLANNING GUIDE CITATION LONGITUDE TAB L E O F C ON T E N TS This Flight Planning Guide is published for the purpose of evaluating the performance of the Cessna Citation Longitude (Model 700 - 0001 & on). This guide is developed from data contained in the Citation Longitude Aircraft Flight Manual and Electronic Operating Manual. This document is not to be used in place of the FAA approved Aircraft Flight Manual or the Electronic Operating Manual. The data included herein does not constitute an offer and is subject to change without notice. Section Page Specifications............................................................................................................... 2 Takeoff Performance.................................................................................................. 4 Decision, Rotation & Takeoff Safety Speeds (KIAS)........................................ 4 Takeoff Field Length – Flaps 2............................................................................. 5 Takeoff Field Length – Flaps 1.............................................................................10 Climb Performance ...................................................................................................15 Cruise Performance .................................................................................................. 17 Max Speed Cruise.................................................................................................. 17 Constant Mach Cruise - M0.82 ...........................................................................18 Constant Mach Cruise - M0.80............................................................................19 Descent Performance .............................................................................................20 Reserve Fuel Calculations ......................................................................................21 Holding Performance ...............................................................................................21 Landing Performance...............................................................................................22 Stall Speeds................................................................................................................26 Mission Planning Table ........................................................................................... 27 Revisions: FM-00, PP-00 1 CITATION LONGITUDE SPEC I F I CAT I ON S General Certification Status Engines Manufacturer Model Thrust Output at S.L. (each) Flat Rating Temperature Overhaul Interval (TBO) Exterior Dimensions Length Height Wing Span Landing Gear Wheelbase Landing Gear Tread 14 CFR Part 25 Honeywell (2) HTF7700L 7,665 lb 34.1 kN 93 °F 34 °C On Condition 73 ft 2 in 19 ft 5 in 68 ft 11 in 31 ft 7 in 9 ft 8 in 22.30 m 5.991 m 21.00 m 9.62 m 2.95 m Internal Dimensions (with typical interior installed) Length - overall * 35 ft 5 in Length - excluding cockpit 25 ft 2 in Height 72 in Width 77 in Passenger Cabin Volume 755 ft3 10.79 m 7.67 m 1.83 m 1.95 m 21.38 m3 * Forward pressure bulkhead to aft pressure bulkhead Accommodations Passenger Seats – maximum Baggage Capacity 112 ft3 1,115 lb Pressurization Differential (nominal) 9.66 (±0.1) psi Sea Level Cabin to 26,816 ft Cabin Altitude at Certified Ceiling (45,000 ft) 5,950 ft Altitudes Certified Ceiling Service Ceiling - 1 Engine (MTOW) Typical Cruise Altitudes 2 12 3.17 m3 506 kg 0.67 bar 8,174 m 1,814 m 45,000 ft 13,716 m 28,420 ft 8,662 m FL 350 - 450 CITATION LONGITUDE SPEC I F I CAT I ON S Basic Performance Takeoff Distance, Sea Level, ISA, MTOW Landing Distance, Sea Level, ISA, MLW Rate of Climb - 2 Engines Rate of Climb - 1 Engine Typical Cruise Speeds 4,810 ft 1,466 m 3,170 ft 966 m 4,310 ft/min 1,314 m/min 1,330 ft/min 405 m/min 448-483 ktas 830-895 km/hr Airspeed Limitations Maximum Operating Limit MMO (29,375 ft / 8,953 m and above) M 0.84 Indicated VMO (8,000 ft to 29,375 ft / 8,953 m) 325 KIAS 602 km/hr VMO (Below 8,000 ft / 2,438 m) Linear Variation from 305 KIAS\565 km/hr (8,000 ft) to 290 KIAS\537 km/hr (at SL) Maximum Flap Extended Speed (VFE) Partial Flaps – 1 Position Partial Flaps – 2 Position Full Flaps – FULL Position Max Landing Gear Extended Speed (VLE) Max Landing Gear Operating Speed (VLO) Max. Speedbrake Extension Speed (VSB) Minimum Control Speed, Air (VMCA) Flaps - 1 Flaps - 2 250 KIAS 230 KIAS 180 KIAS 230 KIAS 230 KIAS No limit 463 km/hr 426 km/hr 333 km/hr 426 km/hr 426 km/hr No limit 100 KIAS 96 KIAS 185 km/hr 178 km/hr Certified Weights Maximum Ramp Weight Maximum Takeoff Weight Maximum Landing Weight Maximum Zero Fuel Weight Maximum Usable Fuel Capacity (6.7 lb/gal) 39,700 lb 39,500 lb 33,500 lb 26,000 lb 14,500 lb 18,008 kg 17,917 kg 15,195 kg 11,793 kg 6,577 kg Basic Operating Weight Typically-Equipped Empty Weight 2 Crew & Stores Basic Operating Weight (BOW) 23,200 lb 400 lb 23,600 lb 10,523 kg 181 kg 10,705 kg 16,100 lb 2,400 lb 1,600 lb 7,303 kg 1,089 kg 726 kg Payload Useful Load (Payload and Fuel) Maximum Payload Payload with Full Fuel 3 CITATION LONGITUDE TAK EO F F P E RF O RM A N C E 14 CFR Part 25 takeoff field lengths are shown on the following pages. Part 25 (through Amendment 25-139, 25-141, and 25-143) defines takeoff distance as the greater of single-engine accelerate-stop, multi-engine accelerate-stop, accelerate-go with one engine inoperative, or 115% of the all engine takeoff distance to a point 35 feet above the runway. These factors are reflected in the takeoff field lengths presented. Second segment climb limitations are presented at the bottom of each takeoff field length table. Second segment climb refers to the ability of the aircraft to meet certain climb rates after takeoff with one engine inoperative. Second segment climb limitations are a function of temperature, elevation and aircraft weight. 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 4 Takeoff Weight (lb) Decision Speed 39500 38500 37500 36500 34500 31500 29500 25500 123 121 118 115 110 103 98 90 V1 Rotation Speed VR 126 124 122 120 115 110 106 100 Flaps 1 Setting Safety Speed Decision Speed 136 134 133 131 128 123 120 117 128 126 123 121 115 107 101 96 V2 V1 Rotation Speed VR 130 128 126 123 119 112 107 105 Safety Speed V2 142 140 138 137 133 127 123 123 CITATION LONGITUDE TAK EO F F P E RF O RM A N C E 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 0 / 32 10 / 50 15 / 59 20 / 68 25 / 77 30 / 86 35 / 95 40 / 104 45 / 113 50 / 122 Climb Wght Temp Limits °C/°F Field Length at Temp Limits (ft) ----------------------------------------- Takeoff Weight (lb) ------------------------------------------- 39,500 4590 4740 4810 4890 4960 5110 5410 5780 6160 6720 38,500 4360 4500 4580 4650 4720 4860 5140 5480 5830 6290 37,500 4150 4290 4360 4420 4490 4620 4890 5210 5530 5910 36,500 3940 4070 4140 4200 4260 4390 4630 4930 5240 5590 34,500 3560 3680 3740 3790 3850 3960 4150 4410 4690 4980 31,500 3080 3180 3230 3280 3300 3420 3580 3740 3920 4160 29,500 2760 2850 2890 2940 2980 3060 3190 3340 3480 3650 25,500 2320 2390 2430 2460 2500 2560 2620 2640 2750 2870 50/122 50/122 50/122 50/122 50/122 50/122 50/122 50/122 6720 6290 5910 5590 4980 4160 3650 2870 Elevation = 1,000 Feet Ambient Temp °C / °F 0 / 32 10 / 50 15 / 59 20 / 68 25 / 77 30 / 86 35 / 95 40 / 104 45 / 113 48 / 118 Climb Wght Temp Limits °C/°F Field Length at Temp Limits (ft) ----------------------------------------- Takeoff Weight (lb) ------------------------------------------- 39,500 4730 4890 4960 5040 5150 5450 5810 6190 6730 7110 38,500 4500 4650 4720 4790 4900 5180 5510 5870 6300 6640 37,500 4280 4420 4490 4560 4660 4920 5230 5580 5950 6230 36,500 4070 4200 4270 4330 4420 4670 4960 5280 5630 5860 34,500 3670 3790 3850 3910 3990 4200 4440 4720 5020 5220 31,500 3180 3280 3330 3380 3450 3620 3780 3960 4200 4360 29,500 2850 2940 2980 3030 3090 3230 3370 3520 3690 3800 25,500 2390 2470 2500 2540 2590 2670 2680 2780 2900 2980 48/118 48/118 48/118 48/118 48/118 48/118 48/118 48/118 7110 6640 6230 5860 5220 4360 3800 2980 5 CITATION LONGITUDE TAK EO F F P E RF O RM A N C E 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 0 / 32 10 / 50 15 / 59 20 / 68 25 / 77 30 / 86 35 / 95 40 / 104 45 / 113 46 / 115 Climb Wght Temp Limits °C/°F Field Length at Temp Limits (ft) ----------------------------------------- Takeoff Weight (lb) ------------------------------------------- 39,500 4890 5050 5120 5210 5480 5850 6240 6740 7390 7530 38,500 4650 4800 4870 4950 5210 5550 5920 6320 6900 7030 37,500 4420 4570 4640 4710 4950 5280 5610 5990 6460 6580 36,500 4200 4340 4400 4470 4690 5000 5320 5670 6060 6150 34,500 3800 3920 3980 4040 4230 4480 4750 5060 5400 5470 31,500 3280 3390 3440 3490 3650 3830 4010 4230 4500 4560 29,500 2940 3030 3080 3120 3260 3410 3560 3730 3920 3970 25,500 2470 2550 2580 2620 2720 2740 2810 2940 3070 3100 46/115 46/115 46/115 46/115 46/115 46/115 46/115 46/115 7530 7030 6580 6150 5470 4560 3970 3100 Elevation = 3,000 Feet Ambient Temp °C / °F -10 / 14 0 / 32 10 / 50 15 / 59 20 / 68 25 / 77 30 / 86 35 / 95 40 / 104 44 / 111 Climb Wght Temp Limits °C/°F Field Length at Temp Limits (ft) 6 ----------------------------------------- Takeoff Weight (lb) ------------------------------------------- 39,500 4880 5040 5210 5290 5520 5880 6290 6760 7390 7990 38,500 4640 4790 4950 5030 5250 5580 5960 6360 6910 7440 37,500 4410 4560 4710 4790 4990 5310 5660 6040 6480 6960 36,500 4190 4330 4480 4540 4730 5030 5360 5710 6100 6500 34,500 3790 3920 4040 4100 4270 4500 4790 5100 5440 5730 31,500 3280 3390 3490 3550 3680 3860 4050 4270 4530 4770 29,500 2940 3030 3130 3180 3290 3440 3610 3780 3960 4150 25,500 2470 2550 2630 2670 2760 2790 2850 2970 3110 3220 44/111 44/111 44/111 44/111 44/111 44/111 44/111 44/111 7990 7440 6960 6500 5730 4770 4150 3220 CITATION LONGITUDE TAK EO F F P E RF O RM A N C E 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 -10 / 14 0 / 32 10 / 50 15 / 59 20 / 68 25 / 77 30 / 86 35 / 95 40 / 104 42 / 108 Climb Wght Temp Limits °C/°F Field Length at Temp Limits (ft) ----------------------------------------- Takeoff Weight (lb) ------------------------------------------- 39,500 5030 5200 5370 5570 5920 6330 6780 7400 8140 8500 38,500 4780 4940 5100 5290 5620 6000 6410 6920 7580 7890 37,500 4550 4710 4860 5030 5340 5700 6090 6500 7090 7360 36,500 4320 4470 4620 4780 5070 5400 5760 6150 6620 6860 34,500 3910 4040 4170 4310 4540 4830 5140 5480 5850 6010 31,500 3380 3490 3610 3720 3900 4090 4300 4570 4870 4990 29,500 3020 3130 3230 3330 3480 3640 3820 4010 4240 4340 25,500 2550 2630 2710 2790 2840 2880 3010 3140 3280 3350 42/108 42/108 42/108 42/108 42/108 42/108 42/108 42/108 8500 7890 7360 6860 6010 4990 4340 3350 Elevation = 5,000 Feet Ambient Temp °C / °F -10 / 14 0 / 32 5 / 41 10 / 50 15 / 59 20 / 68 25 / 77 30 / 86 35 / 95 40 / 104 Climb Wght Temp Limits °C/°F Field Length at Temp Limits (ft) ----------------------------------------- Takeoff Weight (lb) ------------------------------------------- 39,500 5200 5380 5470 5640 5980 6360 6810 7430 8140 9070 38,500 4950 5120 5200 5360 5680 6040 6460 6960 7590 8400 37,500 4710 4870 4950 5100 5390 5740 6130 6560 7110 7810 36,500 4480 4630 4700 4840 5120 5440 5800 6200 6640 7270 34,500 4040 4180 4250 4370 4590 4860 5180 5530 5900 6330 31,500 3490 3610 3670 3770 3950 4130 4340 4620 4910 5230 29,500 3130 3230 3280 3370 3520 3680 3860 4060 4270 4550 25,500 2630 2720 2760 2830 2890 2910 3040 3180 3330 3480 40/104 40/104 40/104 40/104 40/104 40/104 40/104 40/104 9070 8400 7810 7270 6330 5230 4550 3480 7 CITATION LONGITUDE TAK EO F F P E RF O RM A N C E 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 -10 / 14 0 / 32 5 / 41 10 / 50 15 / 59 20 / 68 25 / 77 30 / 86 35 / 95 38 / 100 Climb Wght Temp Limits °C/°F Field Length at Temp Limits (ft) ----------------------------------------- Takeoff Weight (lb) ------------------------------------------- 39,500 5240 5450 5710 6060 6450 6890 7470 8210 9100 9800 38,500 4990 5190 5430 5760 6120 6530 7000 7660 8440 9030 37,500 4750 4940 5160 5470 5810 6200 6620 7170 7860 8370 36,500 4510 4690 4900 5190 5510 5870 6270 6710 7320 7760 34,500 4110 4270 4430 4650 4930 5240 5590 5970 6400 6710 31,500 3560 3690 3830 4010 4190 4400 4670 4970 5300 5510 29,500 3190 3310 3420 3580 3740 3910 4110 4330 4600 4780 25,500 2730 2820 2870 2920 2960 3090 3230 3370 3530 3640 38/100 38/100 38/100 38/100 38/100 38/100 38/100 38/100 9800 9030 8370 7760 6710 5510 4780 3640 Elevation = 7,000 Feet Ambient Temp °C / °F -10 / 14 0 / 32 5 / 41 10 / 50 15 / 59 20 / 68 25 / 77 30 / 86 35 / 95 36 / 97 Climb Wght Temp Limits °C/°F Field Length at Temp Limits (ft) 8 ----------------------------------------- Takeoff Weight (lb) ------------------------------------------- 39,500 5470 5860 6160 6540 6970 7520 8250 9130 --- 38,500 5200 5570 5850 6210 6600 7060 7700 8480 9490 9740 37,500 4950 5300 5560 5900 6270 6700 7210 7900 8780 8990 36,500 4700 5030 5280 5590 5940 6340 6780 7370 8130 8310 34,500 4280 4530 4730 5000 5310 5660 6030 6470 7000 7140 31,500 3700 3910 4060 4260 4460 4720 5030 5360 5730 5830 29,500 3310 3500 3630 3790 3970 4160 4380 4660 4970 5030 25,500 2820 2890 2940 3010 3130 3270 3420 3580 3760 3800 33/91 36/97 36/97 36/97 36/97 36/97 36/97 36/97 9844 9740 8990 8310 7140 5830 5030 3800 CITATION LONGITUDE TAK EO F F P E RF O RM A N C E 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 -20 / -4 -10 / 14 0 / 32 5 / 41 10 / 50 15 / 59 20 / 68 25 / 77 30 / 86 34 / 93 Climb Wght Temp Limits °C/°F Field Length at Temp Limits (ft) ----------------------------------------- Takeoff Weight (lb) ------------------------------------------- 39,500 5520 5880 6310 6650 7070 7570 8290 9160 --- 38,500 5250 5590 5990 6310 6700 7140 7750 8510 9480 -- 37,500 4990 5320 5700 5990 6360 6770 7270 7940 8790 9680 36,500 4740 5050 5410 5680 6030 6410 6860 7410 8150 8910 34,500 4300 4540 4850 5090 5390 5720 6110 6530 7070 7600 31,500 3720 3920 4150 4320 4530 4780 5090 5420 5790 6180 29,500 3330 3510 3700 3850 4030 4220 4430 4710 5020 5310 25,500 2810 2890 2960 3050 3180 3320 3470 3630 3810 3960 29/84 32/90 34/93 34/93 34/93 34/93 34/93 34/93 10064 10015 9680 8910 7600 6180 5310 3960 Elevation = 9,000 Feet Ambient Temp °C / °F -20 / -4 -10 / 14 0 / 32 5 / 41 10 / 50 15 / 59 20 / 68 25 / 77 30 / 86 32 / 90 Climb Wght Temp Limits °C/°F Field Length at Temp Limits (ft) ----------------------------------------- Takeoff Weight (lb) ------------------------------------------- 39,500 5940 6330 6800 7180 7650 8350 9190 10270 --- 38,500 5650 6020 6460 6810 7250 7810 8550 9480 --- 37,500 5370 5730 6140 6470 6880 7350 7990 8800 9900 -- 36,500 5100 5430 5820 6130 6510 6940 7470 8180 9110 9590 34,500 4580 4870 5210 5480 5810 6180 6600 7130 7780 8120 31,500 3950 4170 4410 4600 4860 5150 5480 5840 6330 6550 29,500 3530 3720 3930 4090 4290 4490 4770 5080 5440 5620 25,500 2880 2960 3120 3230 3370 3520 3680 3860 4060 4150 25/77 28/82 30/86 32/90 32/90 32/90 32/90 32/90 10270 10266 9900 9590 8120 6550 5620 4150 9 CITATION LONGITUDE TAK EO F F P E RF O RM A N C E 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 0 / 32 10 / 50 15 / 59 20 / 68 25 / 77 30 / 86 35 / 95 40 / 104 45 / 113 50 / 122 Climb Wght Temp Limits °C/°F Field Length at Temp Limits (ft) ----------------------------------------- Takeoff Weight (lb) ------------------------------------------- 39,500 4850 5010 5090 5170 5250 5400 5710 6080 6510 7040 38,500 4620 4770 4850 4920 5000 5150 5440 5780 6150 6630 37,500 4390 4540 4610 4680 4750 4890 5160 5490 5820 6240 36,500 4180 4320 4390 4460 4520 4650 4910 5210 5530 5880 34,500 3770 3890 3950 4010 4070 4190 4410 4680 4950 5260 31,500 3210 3310 3360 3420 3470 3560 3730 3940 4170 4420 29,500 2870 2960 3010 3050 3090 3180 3320 3480 3660 3870 25,500 2540 2620 2660 2700 2740 2810 2870 2870 2870 2990 50/122 50/122 50/122 50/122 50/122 50/122 50/122 50/122 7040 6630 6240 5880 5260 4420 3870 2990 Elevation = 1,000 Feet Ambient Temp °C / °F 0 / 32 10 / 50 15 / 59 20 / 68 25 / 77 30 / 86 35 / 95 40 / 104 45 / 113 48 / 118 Climb Wght Temp Limits °C/°F Field Length at Temp Limits (ft) 10 ----------------------------------------- Takeoff Weight (lb) ------------------------------------------- 39,500 5000 5170 5250 5330 5450 5760 6120 6550 7060 7410 38,500 4770 4920 5000 5080 5190 5480 5820 6190 6660 6980 37,500 4530 4680 4750 4830 4930 5210 5520 5870 6260 6560 36,500 4310 4460 4520 4600 4690 4950 5250 5570 5920 6170 34,500 3890 4010 4080 4140 4230 4450 4710 5000 5310 5510 31,500 3310 3420 3470 3520 3600 3770 3970 4200 4450 4620 29,500 2960 3050 3100 3140 3210 3360 3510 3690 3900 4040 25,500 2620 2710 2750 2790 2840 2930 2940 2940 3020 3110 48/118 48/118 48/118 48/118 48/118 48/118 48/118 48/118 7410 6980 6560 6170 5510 4620 4040 3110 CITATION LONGITUDE TAK EO F F P E RF O RM A N C E 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 0 / 32 10 / 50 15 / 59 20 / 68 25 / 77 30 / 86 35 / 95 40 / 104 45 / 113 46 / 115 Climb Wght Temp Limits °C/°F Field Length at Temp Limits (ft) ----------------------------------------- Takeoff Weight (lb) ------------------------------------------- 39,500 5170 5340 5420 5510 5790 6160 6570 7090 7690 7820 38,500 4920 5090 5170 5250 5520 5870 6230 6690 7240 7360 37,500 4680 4840 4910 4990 5240 5570 5920 6300 6800 6910 36,500 4460 4600 4680 4750 4980 5290 5620 5970 6400 6500 34,500 4020 4150 4210 4270 4480 4750 5320 5650 6020 6110 31,500 3420 3530 3580 3640 3800 4010 4240 4490 4770 4830 29,500 3050 3150 3200 3250 3390 3550 3720 3940 4170 4230 25,500 2710 2800 2840 2880 2990 3000 3010 3060 3200 3230 46/115 46/115 46/115 46/115 46/115 46/115 46/115 46/115 7820 7360 6910 6500 6110 4830 4230 3230 Elevation = 3,000 Feet Ambient Temp °C / °F -10 / 14 0 / 32 10 / 50 15 / 59 20 / 68 25 / 77 30 / 86 35 / 95 40 / 104 44 / 111 Climb Wght Temp Limits °C/°F Field Length at Temp Limits (ft) ----------------------------------------- Takeoff Weight (lb) ------------------------------------------- 39,500 5160 5330 5510 5600 5840 6210 6610 7130 7720 8260 38,500 4910 5080 5250 5330 5560 5910 6290 6730 7260 7760 37,500 4670 4830 4990 5070 5280 5610 5960 6350 6830 7280 36,500 4450 4600 4750 4830 5020 5330 5670 6020 6430 6840 34,500 4010 4140 4280 4350 4520 4790 5080 5390 5730 6050 31,500 3410 3530 3640 3700 3840 4040 4270 4530 4810 5050 29,500 3050 3150 3250 3300 3420 3590 3760 3970 4210 4420 25,500 2710 2800 2890 2930 3030 3060 3070 3090 3240 3360 44/111 44/111 44/111 44/111 44/111 44/111 44/111 44/111 8260 7760 7280 6840 6050 5050 4420 3360 11 CITATION LONGITUDE TAK EO F F P E RF O RM A N C E 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 -10 / 14 0 / 32 10 / 50 15 / 59 20 / 68 25 / 77 30 / 86 35 / 95 40 / 104 42 / 108 Climb Wght Temp Limits °C/°F Field Length at Temp Limits (ft) ----------------------------------------- Takeoff Weight (lb) ------------------------------------------- 39,500 5320 5510 5690 5890 6250 6660 7170 7750 8430 8740 38,500 5070 5250 5420 5610 5950 6340 6770 7300 7920 8200 37,500 4820 4990 5150 5330 5650 6010 6400 6870 7420 7680 36,500 4590 4750 4900 5070 5370 5710 6080 6480 6990 7210 34,500 4130 4270 4410 4560 4830 5120 5440 5780 6180 6370 31,500 3520 3640 3760 3880 4070 4310 4570 4850 5150 5280 29,500 3140 3250 3350 3460 3630 3800 4010 4250 4500 4610 25,500 2800 2890 2980 3070 3120 3130 3140 3270 3440 3500 42/108 42/108 42/108 42/108 42/108 42/108 42/108 42/108 8740 8200 7680 7210 6370 5280 4610 3500 Elevation = 5,000 Feet Ambient Temp °C / °F -10 / 14 0 / 32 5 / 41 10 / 50 15 / 59 20 / 68 25 / 77 30 / 86 35 / 95 40 / 104 Climb Wght Temp Limits °C/°F Field Length at Temp Limits (ft) 12 ----------------------------------------- Takeoff Weight (lb) ------------------------------------------- 39,500 5510 5700 5790 5970 6310 6710 7200 7810 8450 9260 38,500 5250 5430 5520 5680 6010 6380 6800 7360 7950 8670 37,500 4990 5160 5250 5400 5710 6060 6450 6930 7460 8110 36,500 4830 4910 4990 5140 5430 5750 6130 6550 7040 7610 34,500 4350 4420 4500 4620 4880 5160 5490 5850 6230 6730 31,500 3700 3770 3830 3930 4120 4350 4610 4900 5200 5530 29,500 3300 3360 3420 3500 3670 3840 4050 4290 4550 4830 25,500 2940 2990 3030 3110 3180 3190 3210 3320 3470 3650 40/104 40/104 40/104 40/104 40/104 40/104 40/104 40/104 9260 8670 8110 7610 6730 5530 4830 3650 CITATION LONGITUDE TAK EO F F P E RF O RM A N C E 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 -10 / 14 0 / 32 5 / 41 10 / 50 15 / 59 20 / 68 25 / 77 30 / 86 35 / 95 38 / 100 Climb Wght Temp Limits °C/°F Field Length at Temp Limits (ft) ----------------------------------------- Takeoff Weight (lb) ------------------------------------------- 39,500 5560 5780 6050 6400 6800 7260 7860 8540 9330 9900 38,500 5300 5510 5760 6100 6470 6880 7410 8030 8740 9250 37,500 5040 5240 5470 5790 6140 6530 7000 7550 8180 8640 36,500 4800 4990 5210 5510 5830 6200 6610 7130 7690 8090 34,500 4320 4490 4690 4950 5230 5550 5910 6310 6800 7130 31,500 3700 3840 3990 4180 4410 4670 4960 5270 5600 5850 29,500 3310 3430 3550 3720 3900 4100 4340 4610 4890 5070 25,500 3000 3100 3160 3210 3240 3260 3360 3520 3700 3830 38/100 38/100 39/102 40/104 40/104 40/104 40/104 40/104 9900 9250 8640 8090 7130 5850 5070 3830 Elevation = 7,000 Feet Ambient Temp °C / °F -10 / 14 0 / 32 5 / 41 10 / 50 15 / 59 20 / 68 25 / 77 30 / 86 35 / 95 36 / 97 Climb Wght Temp Limits °C/°F Field Length at Temp Limits (ft) ----------------------------------------- Takeoff Weight (lb) ------------------------------------------- 39,500 5790 6200 6510 6900 7340 7930 8610 9390 10360 10590 38,500 5520 5900 6190 6560 6970 7490 8100 8810 9680 9880 37,500 5250 5610 5890 6230 6610 7070 7630 8250 9020 9200 36,500 5000 5340 5600 5920 6270 6680 7200 7780 8440 8600 34,500 4500 4810 5030 5310 5620 5980 6380 6880 7440 7560 31,500 3850 4080 4250 4480 4730 5020 5330 5670 6110 6200 29,500 3440 3640 3780 3960 4150 4400 4660 4950 5270 5340 25,500 3100 3180 3230 3290 3320 3410 3570 3750 3970 4020 36/97 36/97 36/97 36/97 36/97 36/97 36/97 36/97 10590 9880 9200 8600 7560 6200 5340 4020 13 CITATION LONGITUDE TAK EO F F P E RF O RM A N C E 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 -20 / 4 -10 / 14 0 / 32 5 / 41 10 / 50 15 / 59 20 / 68 25 / 77 30 / 86 34 / 93 Climb Wght Temp Limits °C/°F Field Length at Temp Limits (ft) ----------------------------------------- Takeoff Weight (lb) ------------------------------------------- 39,500 5840 6220 6660 7010 7440 8010 8670 9450 10390 -- 38,500 5560 5920 6340 6670 7070 7580 8180 8860 9710 10560 37,500 5290 5630 6020 6330 6710 7150 7710 8320 9070 9820 36,500 5040 5360 5730 6020 6370 6760 7280 7850 8500 9160 34,500 4540 4820 5150 5400 5710 6050 6450 6950 7510 8020 31,500 3870 4090 4350 4550 4810 5080 5400 5730 6160 6570 29,500 3460 3650 3860 4020 4220 4460 4720 5010 5330 5660 25,500 3090 3180 3250 3310 3380 3450 3620 3800 4020 4220 33/91 34/93 34/93 34/93 34/93 34/93 34/93 34/93 11125 10560 9820 9160 8020 6570 5660 4220 Elevation = 9,000 Feet Ambient Temp °C / °F -20 / -4 -10 / 14 0 / 32 5 / 41 10 / 50 15 / 59 20 / 68 25 / 77 30 / 86 32 / 90 Climb Wght Temp Limits °C/°F Field Length at Temp Limits (ft) 14 ----------------------------------------- Takeoff Weight (lb) ------------------------------------------- 39,500 6280 6690 7170 7560 8110 8750 9510 10420 --- 38,500 5980 6370 6820 7190 7680 8270 8930 9750 10810 11330 37,500 5690 6050 6480 6820 7250 7800 8410 9110 10050 10500 36,500 5410 5750 6160 6480 6860 7370 7940 8570 9370 9770 34,500 4870 5180 5530 5810 6150 6530 7020 7580 8220 8510 31,500 4120 4370 4670 4890 5160 5470 5800 6220 6740 6970 29,500 3680 3880 4110 4290 4520 4790 5070 5390 5800 6000 25,500 3170 3250 3330 3390 3510 3680 3850 4060 4320 4430 29/84 32/90 32/90 32/90 32/90 32/90 32/90 32/90 11636 11330 10500 9770 8510 6970 6000 4430 CITATION LONGITUDE CLIM B P E R F O RM A N C E CRUISE CLIMB - 270 KIAS / M 0.80 ISA, Zero Wind, Anti-Ice Off Time, Fuel and Distance To Climb * --------------------------------------- Takeoff Weight (lb) ----------------------------------------- Pressure Altitude (ft) 15,000 25,000 31,000 33,000 35,000 37,000 39,000 41,000 43,000 45,000 Min Lb NM Min Lb NM Min Lb NM Min Lb NM Min Lb NM Min Lb NM Min Lb NM Min Lb NM Min Lb NM Min Lb NM 39,500 3 316 16 6 548 35 9 718 55 11 786 64 12 866 76 14 941 89 16 1023 103 18 1126 124 23 1275 157 96** 3571 725 38,000 3 303 15 6 524 33 9 684 52 10 748 61 12 821 72 13 891 83 15 965 97 17 1055 115 21 1179 143 49** 2069 363 36,000 3 285 14 6 491 31 8 640 49 9 698 57 11 765 67 12 827 77 14 892 89 16 970 104 19 1069 127 23 1220 164 33,000 3 259 13 5 445 28 7 576 44 8 628 51 10 685 59 11 739 68 12 792 78 14 855 90 16 930 107 19 1030 132 30,000 2 233 12 5 399 25 7 516 39 7 561 45 8 611 53 9 656 60 11 701 68 12 752 78 14 811 91 16 882 109 26,000 2 200 10 4 342 21 6 439 33 6 476 38 7 517 44 8 554 50 9 590 57 10 629 64 11 672 74 13 721 86 * Based on the climb starting from sea level. ** Step climb required - includes cruise portion. 15 CITATION LONGITUDE CLIM B P E R F O RM A N C E MAX RATE CLIMB - 270 KIAS / M 0.76 ISA, Zero Wind, Anti-Ice Off Time, Fuel and Distance To Climb * --------------------------------------- Takeoff Weight (lb) ----------------------------------------- Pressure Altitude (ft) 15,000 25,000 31,000 33,000 35,000 37,000 39,000 41,000 43,000 45,000 Min Lb NM Min Lb NM Min Lb NM Min Lb NM Min Lb NM Min Lb NM Min Lb NM Min Lb NM Min Lb NM Min Lb NM 39,500 3 316 16 6 548 35 9 718 55 11 785 64 12 846 73 13 900 82 15 969 94 17 1054 110 20 1172 136 96** 3572 726 38,000 3 303 15 6 524 33 9 684 52 10 747 61 11 800 69 12 853 77 14 916 88 16 992 103 19 1090 124 50** 2069 364 36,000 3 285 14 6 491 31 8 640 49 9 698 57 10 746 64 11 793 71 13 849 81 14 915 94 17 996 111 21 1113 139 33,000 3 259 13 5 445 28 7 576 44 8 627 51 9 669 57 10 710 63 11 757 71 13 810 82 15 873 95 17 953 114 30,000 2 233 12 5 399 25 7 516 39 7 560 45 8 597 50 9 632 56 10 671 63 11 715 71 13 765 82 15 824 96 * Based on the climb starting from sea level. ** Step climb required - includes cruise portion. 16 26,000 2 200 10 4 342 21 6 439 33 6 476 38 7 506 42 8 534 47 8 566 52 9 600 59 10 637 67 12 680 77 CITATION LONGITUDE CRUI SE P E R F ORM A N C E 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 MAXIMUM SPEED CRUISE * ISA, Anti-Ice Off Cruise Speed & Fuel Flow Pressure Altitude (ft) 29,000 KTAS Lb/Hr 31,000 KTAS Lb/Hr 33,000 KTAS Lb/Hr 35,000 KTAS Lb/Hr 37,000 KTAS Lb/Hr 39,000 KTAS Lb/Hr 41,000 KTAS Lb/Hr 43,000 KTAS Lb/Hr 45,000 KTAS Lb/Hr --------------------------------------- Cruise Weight (lb) ----------------------------------------- 39,000 492 2916 492 2823 487 2658 483 2523 481 2403 481 2335 476 2119 462 1887 --- 38,000 492 2896 492 2799 487 2627 483 2491 481 2369 481 2295 477 2122 466 1894 --- 36,000 492 2857 492 2752 487 2573 483 2420 481 2306 481 2215 480 2126 473 1904 --- 34,000 492 2819 492 2708 487 2524 483 2358 481 2241 481 2147 481 2075 477 1910 466 1702 32,000 492 2789 492 2668 487 2478 483 2306 481 2172 481 2084 481 1999 480 1915 473 1712 29,000 492 2747 492 2613 487 2416 483 2236 481 2090 481 1981 481 1901 481 1825 479 1722 * Maximum Cruise Thrust 17 CITATION LONGITUDE CRUI SE P E R F ORM A N C E HIGH SPEED CRUISE - M0.82* ISA, Anti-Ice Off Cruise Speed & Fuel Flow --------------------------------------- Cruise Weight (lb) ----------------------------------------- Pressure Altitude (ft) 5,000 10,000 15,000 21,000 25,000 27,000 29,000 31,000 33,000 35,000 37,000 39,000 41,000 43,000 45,000 KTAS Lb/Hr KTAS Lb/Hr KTAS Lb/Hr KTAS Lb/Hr KTAS Lb/Hr KTAS Lb/Hr KTAS Lb/Hr KTAS Lb/Hr KTAS Lb/Hr KTAS Lb/Hr KTAS Lb/Hr KTAS Lb/Hr KTAS Lb/Hr KTAS Lb/Hr KTAS Lb/Hr 39,000 310 2541 372 2979 400 2887 437 2812 463 2816 478 2834 486 2822 480 2627 476 2445 471 2260 469 2146 469 2058 469 1991 462 1887 --- 38,000 310 2529 372 2968 400 2876 437 2796 463 2800 478 2817 486 2808 480 2605 476 2441 471 2235 469 2119 469 2028 469 1954 466 1894 --- 36,000 310 2506 372 2948 400 2855 437 2766 463 2769 478 2785 486 2770 480 2576 476 2393 471 2188 469 2064 469 1976 469 1896 469 1843 --- 34,000 310 2484 372 2928 400 2835 437 2740 463 2741 478 2756 486 2733 480 2536 476 2351 471 2145 469 2014 469 1921 469 1840 469 1771 466 1702 32,000 310 2464 372 2910 400 2817 437 2718 463 2716 478 2730 486 2703 480 2498 476 2311 471 2105 469 1969 469 1868 469 1787 469 1713 469 1654 29,000 310 2435 372 2885 400 2791 437 2687 463 2682 478 2693 486 2664 480 2455 476 2272 471 2048 469 1910 469 1798 469 1706 469 1630 469 1564 * Max Cruise Thrust for Limit Airspeed, M0.82 Cruise or Thrust for Maximum Range (approximate). 18 CITATION LONGITUDE CRUI SE P E R F ORM A N C E INTERMEDIATE SPEED CRUISE - M0.80 * ISA, Anti-Ice Off Cruise Speed & Fuel Flow --------------------------------------- Cruise Weight (lb) ----------------------------------------- Pressure Altitude (ft) 5,000 10,000 15,000 21,000 25,000 27,000 29,000 31,000 33,000 35,000 37,000 39,000 41,000 43,000 45,000 KTAS Lb/Hr KTAS Lb/Hr KTAS Lb/Hr KTAS Lb/Hr KTAS Lb/Hr KTAS Lb/Hr KTAS Lb/Hr KTAS Lb/Hr KTAS Lb/Hr KTAS Lb/Hr KTAS Lb/Hr KTAS Lb/Hr KTAS Lb/Hr KTAS Lb/Hr KTAS Lb/Hr 39,000 310 2541 372 2979 400 2887 437 2812 463 2816 478 2834 473 2635 468 2430 464 2282 460 2144 457 2039 457 1959 457 1891 459 1861 --- 38,000 310 2529 372 2968 400 2876 437 2796 463 2800 478 2817 473 2633 468 2411 464 2254 460 2120 457 2013 457 1931 457 1863 458 1814 --- 36,000 310 2506 372 2948 400 2855 437 2766 463 2769 478 2785 473 2596 468 2400 464 2213 460 2070 457 1960 457 1877 457 1807 457 1745 --- 34,000 310 2484 372 2928 400 2835 437 2740 463 2741 478 2756 473 2561 468 2363 464 2178 460 2026 457 1911 457 1827 457 1751 457 1686 457 1632 32,000 310 2464 372 2910 400 2817 437 2718 463 2716 478 2730 473 2530 468 2329 464 2143 460 1988 457 1863 457 1773 457 1698 457 1631 457 1573 29,000 310 2435 372 2885 400 2791 437 2687 463 2682 478 2767 473 2499 468 2297 464 2129 460 1935 457 1804 457 1701 457 1619 457 1575 457 1488 * Max Cruise Thrust for Limit Airspeed, M0.80 Cruise or Thrust for Maximum Range (approximate). 19 CITATION LONGITUDE DESC ENT P E RF O RM A N C E HIGH SPEED & NORMAL DESCENT ISA, Zero Wind, Anti-Ice Off, Speed Brakes Retracted, Gear & Flaps Up Time, Fuel and Distance To Descend * High Speed - 3,000 FPM Normal - 2,000 FPM ------ Start of Descent Weight (lb) ------ Pressure Altitude (ft) 15,000 21,000 25,000 33,000 35,000 37,000 39,000 41,000 43,000 45,000 Min Lb NM Min Lb NM Min Lb NM Min Lb NM Min Lb NM Min Lb NM Min Lb NM Min Lb NM Min Lb NM Min Lb NM 35,000 8 114 37 10 145 51 11 166 60 14 214 81 14 226 86 15 236 92 16 245 97 16 253 102 17 263 108 18 273 115 * Based on descending to sea level. 20 30,000 7 111 35 9 148 48 10 172 58 13 225 79 14 237 84 14 248 89 15 257 95 16 265 100 17 275 106 17 285 112 25,000 7 107 32 9 150 46 10 177 55 13 235 76 13 248 81 14 260 87 15 269 92 15 278 97 16 287 103 17 297 109 ------ Start of Descent Weight (lb) ------ 35,000 8 149 42 12 221 63 14 268 77 18 369 108 18 392 116 20 414 124 20 433 132 22 450 140 22 467 148 24 483 155 30,000 8 146 40 11 223 60 13 273 75 17 376 106 18 400 114 19 421 122 20 440 130 21 458 138 22 474 145 23 489 153 25,000 8 155 40 11 237 60 13 290 74 17 398 106 18 423 114 19 444 122 20 463 129 21 481 137 22 497 145 23 512 153 CITATION LONGITUDE RESE RVE F U E L RESERVE FUEL ALLOWANCES Based on 4 Passengers, ISA, Zero Wind VFR Fuel Reserves (at 5,000 feet) Day (30 minutes) Night (45 minutes) 616 lb 924 lb IFR Fuel Reserves (Alternate plus 45 minutes at 5,000 feet) 100 Nautical Mile Alternate 200 Nautical Mile Alternate 300 Nautical Mile Alternate 1,541 lb 1,971 lb 2,309 lb NBAA IFR Reserves * 100 Nautical Mile Alternate 200 Nautical Mile Alternate 300 Nautical Mile Alternate 1,457 lb 1,883 lb 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. HOLD I NG P E RF O RM A N C E ISA, Anti-Ice Off, Speed Brakes Retracted, Gear & Flaps Up Holding Speed (KIAS) & Fuel Flow (lb/hr) ------------------------------------- Pressure Altitude (ft) --------------------------------------Weight (lb) 38,000 36,000 33,000 30,000 27,000 24,000 Speed 194 188 179 170 160 160 S.L. 1740 1670 1568 1469 1370 1310 5,000 10,000 15,000 20,000 25,000 30,000 1642 1586 1538 1491 1467 1456 1568 1512 1466 1420 1399 1377 1459 1403 1359 1314 1293 1260 1352 1298 1254 1211 1188 1158 1245 1194 1150 1108 1084 1055 1193 1133 1089 1037 1012 986 21 CITATION LONGITUDE LAN DI NG P E RF O RM A N C E 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 0 / 32 10 / 50 15 / 59 20 / 68 25 / 77 30 / 86 35 / 95 40 / 104 45 / 113 50 / 122 Lndg Wght Temp Limits °C/°F VREF (KIAS) ----------------------------------------- Landing Weight (lb) ------------------------------------------- 33500 3040 3120 3170 3210 3250 3290 3330 3370 3420 3460 31500 2890 2970 3010 3050 3090 3130 3170 3210 3250 3290 29500 2730 2800 2840 2870 2910 2950 2980 3020 3060 3100 27500 2580 2650 2690 2720 2760 2790 2820 2860 2900 2930 26500 2510 2580 2610 2650 2680 2710 2750 2780 2810 2850 25500 2440 2510 2540 2570 2600 2640 2670 2700 2740 2770 24500 2380 2440 2470 2500 2530 2560 2600 2620 2660 2690 23500 2300 2360 2390 2420 2450 2480 2510 2540 2580 2610 50/122 50/122 50/122 50/122 50/122 50/122 50/122 50/122 125 121 116 112 110 108 106 104 Elevation = 1,000 Feet Ambient Temp °C / °F 0 / 32 10 / 50 15 / 59 20 / 68 25 / 77 30 / 86 35 / 95 40 / 104 45 / 113 48 / 118 Lndg Wght Temp Limits °C/°F VREF (KIAS) 22 ----------------------------------------- Landing Weight (lb) ------------------------------------------- 33500 3120 3210 3250 3300 3340 3380 3430 3470 3510 3540 31500 2970 3050 3100 3140 3180 3220 3260 3300 3340 3370 29500 2800 2880 2910 2950 2990 3030 3060 3100 3140 3170 27500 2650 2730 2760 2800 2830 2870 2900 2940 2980 3000 26500 2580 2650 2680 2720 2750 2790 2820 2860 2890 2910 25500 2510 2580 2610 2640 2680 2710 2740 2780 2810 2830 24500 2440 2500 2540 2570 2600 2630 2660 2700 2730 2750 23500 2360 2420 2460 2490 2520 2550 2580 2310 2640 2660 48/118 48/118 48/118 48/118 48/118 48/118 48/118 48/118 125 121 116 112 110 108 106 104 CITATION LONGITUDE LAN DI NG P E RF O RM A N C E LANDING DISTANCE - FEET (ACTUAL DISTANCE); FLAPS FULL (Distance from 50 Feet Above the Runway) Dry Runway, Zero Wind, Anti-Ice On or Off Elevation = 2,000 Feet Ambient Temp °C / °F 0 / 32 10 / 50 15 / 59 20 / 68 25 / 77 30 / 86 35 / 95 40 / 104 45 / 113 46 / 115 Lndg Wght Temp Limits °C/°F VREF (KIAS) ----------------------------------------- Landing Weight (lb) ------------------------------------------- 33500 3210 3300 3340 3390 3430 3480 3520 3570 3610 3620 31500 3050 3140 3180 3230 3260 3310 3350 3390 3440 3440 29500 2880 2960 3000 3030 3070 3110 3150 3190 3230 3240 27500 2730 2800 2840 2870 2910 2950 2980 3020 3060 3070 26500 2650 2720 2760 2790 2830 2860 2900 2940 2970 2980 25500 2580 2640 2680 2710 2750 2780 2820 2850 2890 2900 24500 2500 2570 2600 2640 2670 2700 2740 2770 2810 2810 23500 2420 2490 2520 2560 2590 2620 2650 2680 2720 2720 46/115 46/115 46/115 46/115 46/115 46/115 46/115 46/115 125 121 116 112 110 108 106 104 Elevation = 3,000 Feet Ambient Temp °C / °F -10 / 14 0 / 32 10 / 50 15 / 59 20 / 68 25 / 77 30 / 86 35 / 95 40 / 104 44 / 111 Lndg Wght Temp Limits °C/°F VREF (KIAS) ----------------------------------------- Landing Weight (lb) ------------------------------------------- 33500 3210 3300 3390 3440 3480 3530 3580 3620 3670 3700 31500 3050 3140 3230 3270 3310 3360 3400 3440 3490 3520 29500 2870 2960 3040 3080 3120 3160 3200 3240 3280 3310 27500 2720 2800 2880 2910 2950 2990 3030 3070 3100 3140 26500 2650 2720 2800 2830 2870 2910 2940 2980 3020 3050 25500 2580 2650 2720 2750 2790 2820 2860 2890 2930 2960 24500 2500 2570 2640 2670 2710 2740 2780 2810 2850 2870 23500 2420 2490 2560 2590 2620 2660 2690 2720 2760 2790 44/111 44/111 44/111 44/111 44/111 44/111 44/111 44/111 125 121 116 112 110 108 106 104 23 CITATION LONGITUDE LAN DI NG P E RF O RM A N C E 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 -10 / 14 0 / 32 10 / 50 15 / 59 20 / 68 25 / 77 30 / 86 35 / 95 40 / 104 42 / 108 Lndg Wght Temp Limits °C/°F VREF (KIAS) ----------------------------------------- Landing Weight (lb) ------------------------------------------- 33500 3300 3400 3490 3540 3590 3630 3680 3720 3770 3790 31500 3140 3230 3320 3370 3410 3450 3500 3540 3590 3610 29500 2960 3040 3120 3170 3210 3250 3290 3330 3370 3390 27500 2800 2880 2960 3000 3030 3070 3110 3150 3190 3210 26500 2720 2800 2870 2910 2950 2990 3020 3060 3100 3120 25500 2640 2720 2790 2830 2870 2900 2940 2980 3010 3030 24500 2570 2640 2710 2750 2790 2820 2850 2890 2930 2940 23500 2490 2560 2630 2660 2700 2730 2770 2800 2830 2850 42/108 42/108 42/108 42/108 42/108 42/108 42/108 42/108 125 121 116 112 110 108 106 104 Elevation = 5,000 Feet Ambient Temp °C / °F -10 / 14 0 / 32 5 / 41 10 / 50 15 / 59 20 / 68 25 / 77 30 / 86 35 / 95 40 / 104 Lndg Wght Temp Limits °C/°F VREF (KIAS) 24 ----------------------------------------- Landing Weight (lb) ------------------------------------------- 33500 3400 3500 3550 3600 3640 3690 3740 3790 3840 3890 31500 3230 3330 3370 3420 3460 3510 3560 3610 3650 3690 29500 3040 3130 3170 3220 3260 3300 3350 3390 3430 3470 27500 2880 2970 3010 3050 3090 3130 3170 3210 3250 3290 26500 2810 2880 2920 2960 3000 3040 3080 3120 3160 3200 25500 2730 2800 2840 2880 2920 2960 2990 3030 3070 3110 24500 2650 2720 2760 2800 2830 2870 2910 2940 2980 3020 23500 2570 2640 2670 2710 2750 2780 2810 2850 2890 2920 40/104 40/104 40/104 40/104 40/104 40/104 40/104 40/104 125 121 116 112 110 108 106 104 CITATION LONGITUDE LAN DI NG P E RF O RM A N C E 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 -10 / 14 0 / 32 5 / 41 10 / 50 15 / 59 20 / 68 25 / 77 30 / 86 35 / 95 38 / 100 Lndg Wght Temp Limits °C/°F VREF (KIAS) ----------------------------------------- Landing Weight (lb) ------------------------------------------- 33500 3500 3600 3650 3700 3760 3810 3850 3910 3960 3990 31500 3330 3430 3480 3520 3570 3620 3670 3710 3760 3790 29500 3140 3230 3270 3320 3360 3410 3450 3490 3540 3560 27500 2970 3050 3100 3140 3180 3220 3260 3310 3350 3370 26500 2890 2970 3010 3050 3090 3130 3170 3210 3250 3280 25500 2810 2890 2930 2970 3010 3040 3080 3120 3160 3180 24500 2730 2810 2840 2880 2920 2960 3000 3030 3070 3090 23500 2640 2720 2750 2790 2830 2860 2900 2940 2970 3000 38/100 38/100 38/100 38/100 38/100 38/100 38/100 38/100 125 121 116 112 110 108 106 104 Elevation = 7,000 Feet Ambient Temp °C / °F ----------------------------------------- Landing Weight (lb) ------------------------------------------- -10 / 14 0 / 32 5 / 41 10 / 50 15 / 59 20 / 68 25 / 77 30 / 86 35 / 95 36 / 97 33500 3610 3710 3770 3820 3870 3920 3970 4030 4080 4090 31500 3430 3530 3580 3630 3680 3730 3780 3830 3880 3890 29500 3230 3320 3370 3420 3460 3510 3550 3600 3650 3650 27500 3060 3150 3190 3230 3280 3320 3360 3410 3450 3460 26500 2980 3060 3100 3140 3190 3230 3270 3310 3350 3360 25500 2890 2970 3020 3050 3090 3140 3180 3220 3250 3260 24500 2810 2890 2930 2970 3010 3040 3080 3120 3160 3170 23500 2720 2800 2830 2870 2910 2950 2990 3020 3060 3070 Lndg Wght Temp Limits °C/°F 36/97 36/97 36/97 36/97 36/97 36/97 36/97 36/97 125 121 116 112 110 108 106 104 VREF (KIAS) 25 CITATION LONGITUDE LAN DI NG P E RF O RM A N C E 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 -10 / 14 -5 / 23 0 / 32 5 / 41 10 / 50 15 / 59 20 / 68 25 / 77 30 / 86 34 / 93 Lndg Wght Temp Limits °C/°F VREF (KIAS) ----------------------------------------- Landing Weight (lb) ------------------------------------------- 33500 3720 3770 3830 3880 3930 3990 4040 4100 4150 4190 31500 3540 3590 3640 3690 3740 3790 3850 3890 3950 3990 29500 3330 3380 3430 3470 3520 3570 3620 3660 3710 3750 27500 3150 3200 3240 3290 3330 3380 3420 3460 3510 3540 26500 3060 3110 3150 3200 3240 3280 3320 3370 3410 3440 25500 2980 3020 3060 3100 3150 3190 3230 3270 3310 3350 24500 2890 2930 2980 3020 3050 3100 3140 3180 3220 3250 23500 2800 2840 2880 2920 2960 3000 3040 3080 3120 3150 34/93 34/93 34/93 34/93 34/93 34/93 34/93 34/93 125 121 116 112 110 108 106 104 STAL L S P EE D S Zero Angle of Bank, Landing Gear Up or Down Stall Speeds (KCAS) ----------------------------------------- Flap Position ------------------------------------------Weight (lb) 33500 31500 29500 27500 26500 25500 24500 23500 26 Flaps FULL 102 98 94 91 90 88 86 84 Flaps 2 111 107 103 99 98 96 94 92 Flaps 1 116 112 108 104 102 100 98 96 UP 129 125 120 116 114 111 109 107 CITATION LONGITUDE MISS I O N P L A N N IN G 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 True Airspeed (kt) 360 380 400 420 440 460 480 Wind Correction Factors * ------------ Headwinds (kt) ------------ 100 1.38 1.36 1.33 1.31 1.29 1.28 1.26 75 1.26 1.25 1.23 1.22 1.21 1.19 1.19 50 1.16 1.15 1.14 1.13 1.13 1.12 1.12 25 1.07 1.07 1.06 1.06 1.06 1.06 1.05 0 1.00 1.00 1.00 1.00 1.00 1.00 1.00 ------------ Tailwinds (kt) ----------- 25 0.93 0.94 0.94 0.94 0.95 0.95 0.95 50 0.88 0.88 0.89 0.89 0.90 0.90 0.91 75 0.83 0.84 0.84 0.85 0.85 0.86 0.86 * Wind Correction Factor is calculated as KTAS divided by the sum of KTAS ± wind component. 100 0.78 0.79 0.80 0.81 0.81 0.82 0.83 27 CITATION LONGITUDE MISS I O N P L A N N IN G FLIGHT TIME & FUEL BURN ----------------------------------------------- Cruise Altitude (ft) ----------------------------------------------- 25,000 Dist (nm) 200 300 400 500 600 700 800 1,000 1,200 1,400 Time (min) Fuel (lb) 29,000 Time (min) Fuel (lb) 31,000 Time (min) Fuel (lb) 33,000 Time (min) Fuel (lb) 35,000 Time (min) Fuel (lb) 0:30 1438 0:30 1390 0:30 1353 0:30 1326 0:30 1296 0:43 2018 0:42 1939 0:43 1864 0:42 1802 0:43 1730 0:56 2599 0:54 2488 0:55 2376 0:55 2279 0:55 2166 1:09 2181 1:07 3039 1:08 2890 1:08 2757 1:08 2603 1:22 3764 1:19 3591 1:20 3404 1:20 3237 1:21 3041 1:35 4351 1:32 4145 1:33 3920 1:33 3718 1:34 3481 1:48 4940 1:44 4703 1:45 4441 1:46 4202 1:46 3923 2:14 6125 2:08 5826 2:10 5490 2:11 5182 2:12 4811 2:40 7319 2:33 6958 2:35 6549 2:36 6171 2:37 5706 3:06 8516 2:58 8100 3:00 7618 3:01 7166 3:03 6608 1,800 3:32 9710 3:23 9234 3:25 8686 3:27 8168 3:28 7520 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 1,600 2,800 3,000 3,200 3,275 28 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) CITATION LONGITUDE FOR SELECTED DISTANCES ----------------------------------------------- Cruise Altitude (ft) ----------------------------------------------- 37,000 Time (min) Fuel (lb) 39,000 Time (min) Fuel (lb) 41,000 Time (min) Fuel (lb) 43,000 Time (min) Fuel (lb) 45,000 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 29 U.S. + 1.844.44.TXTAV | INTERNATIONAL +1.316.517.8270 | TXTAV.COM © 2019 Textron Aviation Inc. 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