Cessna Citation Mustang Flight Planning Guide

Cessna Citation Mustang · Flight Manual

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Overview

This Flight Planning Guide is specifically designed for the Cessna Citation Mustang (Model 510). It provides essential performance data derived from the Aircraft Flight Manual and Operating Manual. The guide is intended for pilots and aviation professionals to assist in evaluating the aircraft's performance capabilities. It includes critical information on takeoff, climb, cruise, descent performance, and reserve fuel calculations, ensuring that users can make informed decisions during flight planning. The data presented is subject to change and should not replace the FAA-approved Aircraft Flight Manual or Operating Manual.

Maximum Takeoff Weight: 8,645 lb (3,921 kg)
Takeoff Distance at Sea Level (Flaps 15°): 3,110 ft (948 m)
Rate of Climb (2 Engines): 3,010 ft/min (917 m/min)
Cruise Speed at 35,000 ft: 332 KTAS
VFR Fuel Reserve (Day): 291 lb

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Source

Originally published by www.cavok.at. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.

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Document details

Type: Flight Manual
Pages: 32
File size: 289 KB
Publisher: www.cavok.at

Specifications & performance

Extracted from this document.

Specifications

Engine (hp): 1,460
Height (ft): 13
Length (ft): 40
Wingspan (ft): 43
Engine model: PW-615F
Max speed (kt): 345
Cruise speed (kt): 320
Empty weight (lb): 5,350
Fuel capacity (gal): 384
Rate of climb (fpm): 3,010
Service ceiling (ft): 41,000
Max takeoff weight (lb): 8,645

Performance

Landing distance (ft): 2,380
Takeoff distance (ft): 3,110

V-speeds

VR: 89
VY: 97
VFE: 185

Weight & balance

Useful load (lb): 3,180
Max ramp weight (lb): 8,730
Baggage allowance (lb): 718
Basic empty weight (lb): 5,550
Max landing weight (lb): 8,000
Max takeoff weight (lb): 8,645

Documentation completeness

3/7

Most owners only have the POH. Here's the essential set for the Cessna Citation Mustang.

Pilot's Operating Handbook / AFM
Checklist
Maintenance Manual
Parts Catalog (IPC)
Systems & Wiring
Service Bulletins
Type Certificate (TCDS)

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In this document

Specifications

The specifications section outlines the general characteristics of the Cessna Citation Mustang, including its dimensions, weight limits, engine specifications, and performance metrics. The aircraft is powered by two Pratt & Whitney Canada PW-615F engines, each producing 1,460 lb of thrust. Key dimensions include a length of 40 ft 7 in (12.37 m), a height of 13 ft 5 in (4.09 m), and a wingspan of 43 ft 2 in (13.16 m). The maximum takeoff weight is 8,645 lb (3,921 kg) with a maximum fuel capacity of 2,580 lb (1,170 kg).

Takeoff Performance

This section details the takeoff performance of the Citation Mustang, including decision speeds, rotation speeds, and takeoff field lengths under various conditions. For instance, at sea level with flaps set to 15°, the takeoff distance for maximum takeoff weight (8,645 lb) is 3,110 ft (948 m). The guide emphasizes the importance of considering factors such as temperature, elevation, and aircraft weight when calculating takeoff distances.

Climb Performance

The climb performance section provides data on the aircraft's rate of climb under different weight conditions. The Citation Mustang can achieve a rate of climb of 3,010 ft/min (917 m/min) with two engines and 870 ft/min (265 m/min) with one engine. This section also includes information on cruise climb performance, detailing time, fuel, and distance to climb at various altitudes.

Cruise Performance

This section outlines the cruise speeds and fuel flow rates for the Citation Mustang at various altitudes. For example, at 35,000 ft, the aircraft can cruise at a speed of 332 KTAS with a fuel flow of 609 lb/hr. The guide provides detailed tables for both high-speed and long-range cruise performance, allowing pilots to optimize fuel efficiency during flight.

Reserve Fuel Calculations

The reserve fuel section outlines the fuel requirements for different flight scenarios, including VFR and IFR operations. For VFR flights at 15,000 ft, the reserve fuel requirement is 291 lb for day operations and 444 lb for night operations. IFR reserves are specified for alternate airports at various distances, ensuring pilots are prepared for unexpected diversions.

Safety notes

Always refer to the FAA-approved Aircraft Flight Manual for final performance data.
Ensure that all calculations consider current weather and runway conditions.

Full document text

1 T A B L E O F C O N T E N T S This Flight Planning Guide is published for the purpose of providing specific information for evaluating the performance of the Cessna Citation Mustang (Model 510). This guide is developed from data contained in the Citation Mustang Aircraft Flight Manual and Operating Manual. This document is not to be used in place of the FAA approved Aircraft Flight Manual or the Operating Manual. The data included herein does not constitute an offer and is subject to change without notice. Section Page Specifications ............................................................................................2 Takeoff Performance Decision, Rotation and Takeoff Safety Speeds ......................................4 Takeoff Field Length – Flaps 15°............................................................5 Takeoff Field Length – Flaps UP ..........................................................10 Climb Performance..................................................................................15 Cruise Performance High Speed Cruise................................................................................16 Long Range Cruise...............................................................................17 Descent Performance..............................................................................18 Reserve Fuel Calculations ......................................................................19 Holding Performance...............................................................................19 Landing Performance ..............................................................................20 Stall Speeds ............................................................................................24 Mission Planning Table ...........................................................................25 Revisions: FM-03, OM-00 2 S P E C I F I C A T I O N S General Certification Status 14 CFR Part 23 * Engines Manufacturer Pratt & Whitney Canada Model (2) PW-615F Thrust Output at S.L. (each) 1,460 lb 6.49 kN Flat Rating Temperature 77 °F 25 °C Overhaul Interval (TBO) 3,500 hours Exterior Dimensions Length 40 ft 7 in 12.37 m Height 13 ft 5 in 4.09 m Wing Span 43 ft 2 in 13.16 m Landing Gear Wheelbase 14 ft 4 in 4.37 m Landing Gear Tread 11 ft 10 in 3.61 m Cabin Dimensions (with typical interior installed) Length - overall 14 ft 9 in 4.50 m Length - excluding cockpit 9 ft 9 in 2.97 m Height 54 in 1.37 m Width 55 in 1.40 m Passenger Cabin Volume 144 ft 3 4.08 m3 Accommodations Passenger Seats 5 Baggage Capacity 63 ft 3 1.78 m3 718 lb 325 kg Pressurization Differential 8.3 psi 0.57 bar Sea Level Cabin to 21,280 ft 6,486 m 8,000 Foot Cabin at 41,000 ft 12,497 m Altitudes Certified Ceiling 41,000 ft 12,497 m Service Ceiling - 1 Engine (MTOW) 26,900 ft 8,199 m Typical Cruise Altitudes FL 350 - 390 * The Citation Mustang is certified under 14 CFR Part 23 Normal category rules but all takeoff and landing performance is based on 14 CFR Part 23 Commuter category rules. 3 S P E C I F I C A T I O N S Basic Performance Takeoff Distance, Sea Level, ISA, MTOW 3,110 ft 948 m Landing Distance, Sea Level, ISA, MLW 2,380 ft 725 m Rate of Climb - 2 Engines 3,010 ft/min 917 m/min Rate of Climb - 1 Engine 870 ft/min 265 m/min Typical Cruise Speeds 320 - 345 KTAS Airspeed Limitations Maximum Operating Limit MMO (27,120 ft / 8,266 m and above) M 0.63 Indicated VMO (Sea Level to 27,120 ft / 8,266 m) 250 KIAS 463 km/hr Maximum Flap Extended Speed (VFE) Takeoff & Approach (15°) 185 KIAS 343 km/hr Land (30°) 150 KIAS 278 km/hr Max Landing Gear Oper - Extending (V LO) 250 KIAS 463 km/hr Max Landing Gear Oper - Retracting (V LO) 185 KIAS 343 km/hr Max Landing Gear Extended Speed (V LE) 250 KIAS 463 km/hr Max. Speed Brake Operation Speed (VSB) No limit No limit Minimum Control Speed, Air (VMCA) Flaps - 0° 92 KIAS 170 km/hr Flaps - 15° 81 KIAS 150 km/hr Minimum Control Speed, Ground (V MCG) 73 KIAS 135 km/hr Certified Weights Maximum Ramp Weight 8,730 lb 3,960 kg Maximum Takeoff Weight 8,645 lb 3,921 kg Maximum Landing Weight 8,000 lb 3,629 kg Maximum Zero Fuel Weight 6,750 lb 3,062 kg Maximum Fuel Capacity (6.7 lb/gal) 2,580 lb 1,170 kg Basic Operating Weight Typically-Equipped Empty Weight 5,350 lb 2,427 kg Single Pilot & Furnishings 200 lb 91 kg Basic Operating Weight 5,550 lb 2,518 kg Payload Useful Payload and Fuel 3,180 lb 1,442 kg Maximum Payload 1,200 lb 544 kg Payload at Full Fuel 600 lb 272 kg 4 T A K E O F F P E R F O R M A N C E The Citation Mustang is certified to 14 CFR Part 23 Normal category rules. Cessna, however, elected to calculate all takeoff performance utilizing 14 CFR Part 23 Commuter category rules because of their higher standard of safety. Therefore, the takeoff distances reflected in the Aircraft Flight Manual and this guide are based on the greater of accelerate-stop distance, engine-out accelerate-go distance, or 115% of the all engine takeoff distance to a point 35 feet above the runway. These factors are incorporated into 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: 15° and UP. A flap setting of 15° is preferred to minimize runway length and runway speeds. In those situations where second segment climb requirements are too limiting for 15° of flaps, an UP flap setting is available. An UP flap setting requires greater runway length but provides greater second segment climb capability. A paved, level, dry runway with zero wind is assumed. Runway lengths

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shown are based on the aircraft's anti-ice systems being off and the cabin bleed air on. DECISION, ROTATION & TAKEOFF SAFETY SPEEDS Sea Level, Dry Runway, ISA, Zero Wind, Anti-Ice Off, KIAS Flaps 15° Setting Flaps UP Setting Takeoff Weight (lb) Decision Speed V1 Rotation Speed VR Safety Speed V2 Decision Speed V1 Rotation Speed VR Safety Speed V2 8,645 89 89 97 103 104 112 8,000 85 85 93 98 99 108 7,500 83 84 93 94 96 106 7,000 81 84 93 93 96 106 6,500 79 84 94 92 96 107 6,000 79 85 95 90 96 108 5 T A K E O F F P E R F O R M A N C E TAKEOFF FIELD LENGTH – FLAPS 15° (Over 35 Foot Screen Height) Dry Runway, Zero Wind, Anti-Ice Off, Cabin Bleed Air On Elevation = Sea Level Ambient Temp --------------------------------------- Takeoff Weight (lb) ---------------------------------------- °C / °F 8,645 8,000 7,500 7,000 6,500 6,000 0 / 32 2,990 2,500 2,320 2,220 2,130 2,160 10 / 50 3,070 2,570 2,390 2,290 2,190 2,210 15 / 59 3,110 2,610 2,420 2,320 2,220 2,240 20 / 68 3,150 2,640 2,460 2,360 2,260 2,270 25 / 77 3,190 2,680 2,490 2,390 2,290 2,300 30 / 86 3,380 2,810 2,520 2,410 2,310 2,240 35 / 95 3,820 3,130 2,690 2,420 2,300 2,200 40 / 104 4,440 3,550 3,020 2,570 2,310 2,190 45 / 113 — 4,170 3,460 2,900 2,440 2,190 50 / 122 — — 4,150 3,380 2,790 2,320 Climb Wght Temp Limits °C/°F 44/111 49/120 50/122 50/122 50/122 50/122 Field Length at Temp Limits (ft) 5,220 4,980 4,150 3,380 2,790 2,320 Elevation = 1,000 Feet Ambient Temp --------------------------------------- Takeoff Weight (lb) ---------------------------------------- °C / °F 8,645 8,000 7,500 7,000 6,500 6,000 0 / 32 3,070 2,570 2,390 2,290 2,190 2,220 5 / 41 3,110 2,600 2,420 2,320 2,230 2,250 10 / 50 3,150 2,640 2,460 2,360 2,260 2,280 15 / 59 3,200 2,680 2,500 2,390 2,290 2,310 20 / 68 3,240 2,730 2,530 2,430 2,330 2,340 25 / 77 3,390 2,830 2,560 2,450 2,350 2,310 30 / 86 3,810 3,130 2,700 2,460 2,350 2,240 35 / 95 4,370 3,520 3,000 2,560 2,350 2,230 40 / 104 5,230 4,050 3,390 2,860 2,410 2,240 45 / 113 — 4,950 3,990 3,280 2,730 2,270 Climb Wght Temp Limits °C/°F 40/104 45/113 47/117 47/117 47/117 47/117 Field Length at Temp Limits (ft) 5,230 4,950 4,330 3,510 2,890 2,390 6 T A K E O F F P E R F O R M A N C E TAKEOFF FIELD LENGTH – FLAPS 15° (Over 35 Foot Screen Height) Dry Runway, Zero Wind, Anti-Ice Off, Cabin Bleed Air On Elevation = 2,000 Feet Ambient Temp --------------------------------------- Takeoff Weight (lb) ---------------------------------------- °C / °F 8,645 8,000 7,500 7,000 6,500 6,000 0 / 32 3,150 2,640 2,460 2,360 2,260 2,280 5 / 41 3,190 2,680 2,500 2,400 2,300 2,310 10 / 50 3,240 2,730 2,540 2,430 2,330 2,350 15 / 59 3,280 2,770 2,580 2,470 2,370 2,380 20 / 68 3,390 2,850 2,610 2,500 2,390 2,360 25 / 77 3,810 3,140 2,720 2,510 2,390 2,290 30 / 86 4,360 3,530 3,010 2,580 2,400 2,280 35 / 95 5,160 4,030 3,380 2,860 2,430 2,280 40 / 104 — 4,760 3,880 3,230 2,690 2,290 45 / 113 — — 4,710 3,770 3,080 2,530 Climb Wght Temp Limits °C/°F 36/97 41/106 45/113 45/113 45/113 45/113 Field Length at Temp Limits (ft) 5,370 4,970 4,710 3,770 3,080 2,530 Elevation = 3,000 Feet Ambient Temp --------------------------------------- Takeoff Weight (lb) ---------------------------------------- °C / °F 8,645 8,000 7,500 7,000 6,500 6,000 -5 / 23 3,190 2,680 2,500 2,400 2,300 2,320 0 / 32 3,230 2,730 2,540 2,430 2,330 2,350 5 / 41 3,280 2,770 2,580 2,470 2,370 2,380 10 / 50 3,330 2,820 2,610 2,510 2,400 2,410 15 / 59 3,380 2,870 2,660 2,550 2,440 2,420 20 / 68 3,800 3,140 2,740 2,550 2,430 2,330 25 / 77 4,350 3,530 3,020 2,600 2,440 2,320 30 / 86 5,130 4,030 3,390 2,870 2,450 2,320 35 / 95 — 4,720 3,870 3,230 2,700 2,330 40 / 104 — — 4,570 3,690 3,030 2,510 Climb Wght Temp Limits °C/°F 31/88 37/99 42/108 43/109 43/109 43/109 Field Length at Temp Limits (ft) 5,340 5,090 4,960 4,090 3,300 2,700 7 T A K E O F F P E R F O R M A N C E TAKEOFF FIELD LENGTH – FLAPS 15° (Over 35 Foot Screen Height) Dry Runway, Zero Wind, Anti-Ice Off, Cabin Bleed Air On Elevation = 4,000 Feet Ambient Temp --------------------------------------- Takeoff Weight (lb) ---------------------------------------- °C / °F 8,645 8,000 7,500 7,000 6,500 6,000 -5 / 23 3,280 2,770 2,580 2,470 2,370 2,390 0 / 32 3,320 2,820 2,620 2,510 2,410 2,420 5 / 41 3,370 2,860 2,660 2,550 2,440 2,450 10 / 50 3,440 2,920 2,700 2,590 2,480 2,450 15 / 59 3,770 3,140 2,750 2,600 2,480 2,380 20 / 68 4,320 3,520 3,020 2,620 2,480 2,370 25 / 77 5,090 4,020 3,400 2,880 2,500 2,360 30 / 86 — 4,700 3,880 3,230 2,710 2,370 35 / 95 — — 4,530 3,690 3,040 2,520 40 / 104 — — — 4,320 3,460 2,820 Climb Wght Temp Limits °C/°F 27/81 33/91 38/100 40/104 40/104 40/104 Field Length at Temp Limits (ft) 5,510 5,260 5,090 4,320 3,460 2,820 Elevation = 5,000 Feet Ambient Temp --------------------------------------- Takeoff Weight (lb) ---------------------------------------- °C / °F 8,645 8,000 7,500 7,000 6,500 6,000 -10 / 14 3,320 2,810 2,620 2,510 2,410 2,420 -5 / 23 3,370 2,860 2,660 2,550 2,440 2,450 0 / 32 3,430 2,910 2,700 2,590 2,480 2,490 5 / 41 3,500 2,970 2,740 2,620 2,510 2,500 10 / 50 3,780 3,160 2,770 2,640 2,530 2,420 15 / 59 4,270 3,500 3,010 2,660 2,530 2,410 20 / 68 5,020 3,990 3,390 2,880 2,540 2,410 25 / 77 — 4,660 3,860 3,240 2,720 2,420 30 / 86 — — 4,490 3,670 3,040 2,520 35 / 95 — — — 4,270 3,450 2,820 Climb Wght Temp Limits °C/°F 23/73 29/84 34/93 38/100 38/100 38/100 Field Length at Temp Limits (ft) 5,640 5,410 5,230 4,770 3,760 3,030 8 T A K E O F F P E R F O R M A N C E TAKEOFF FIELD LENGTH – FLAPS 15° (Over 35 Foot Screen Height) Dry Runway, Zero Wind, Anti-Ice Off, Cabin Bleed Air On Elevation = 6,000 Feet Ambient Temp --------------------------------------- Takeoff Weight (lb) ---------------------------------------- °C / °F 8,645 8,000 7,500 7,000 6,500 6,000 -10 / 14 3,440 2,920 2,700 2,590 2,480 2,470 -5 / 23 3,500 2,970 2,750 2,630 2,520 2,510 0 / 32 3,570 3,020 2,790 2,670 2,560 2,540 5 / 41 3,790 3,200 2,820 2,690 2,580 2,480 10 / 50 4,230 3,480 3,010 2,710 2,580 2,460 15 / 59 4,840 3,900 3,320 2,840 2,590 2,460 20 / 68 — 4,530 3,790 3,190 2,690 2,460 25 / 77 — 5,430 4,380 3,620 3,010 2,520 30 / 86 — — 5,230 4,160 3,390 2,780 35 / 95 — — — 4,980 3,900 3,140 Climb Wght Temp Limits °C/°F 19/66 25/77 30/86 36/97 36/97 36/97 Field Length at Temp Limits (ft) 5,630 5,430 5,230 5,210 4,040 3,230 Elevation = 7,000 Feet Ambient Temp --------------------------------------- Takeoff Weight (lb) ---------------------------------------- °C / °F 8,645 8,000 7,500 7,000 6,500 6,000 -15 / 5 3,560 3,020 2,740 2,620 2,510 2,460 -10 / 14 3,630 3,070 2,790 2,660 2,550 2,490 -5 / 23 3,690 3,130 2,830 2,710 2,600 2,530 0 / 32 3,780 3,190 2,880 2,750 2,630 2,570 5 / 41 4,230 3,490 3,040 2,760 2,630 2,510 10 / 50 4,780 3,870 3,310 2,860 2,640 2,510 15 / 59 5,620 4,400 3,710 3,140 2,680 2,510 20 / 68 — 5,240 4,280 3,560 2,970 2,530 25 / 77 — — 5,050 4,070 3,340 2,760 30 / 86 — — — 4,800 3,820 3,090 Climb Wght Temp Limits °C/°F 16/61 22/72 27/81 32/90 33/91 33/91 Field Length at Temp Limits (ft) 5,870 5,680 5,460 5,210 4,200 3,340 9 T A K E O F F P E R F O R M A N C E TAKEOFF FIELD LENGTH – FLAPS 15° (Over 35 Foot Screen Height) Dry Runway, Zero Wind, Anti-Ice Off, Cabin Bleed Air On Elevation = 8,000 Feet Ambient Temp --------------------------------------- Takeoff Weight (lb) ---------------------------------------- °C / °F 8,645 8,000 7,500 7,000 6,500 6,000 -15 / 5 3,790 3,200 2,820 2,700 2,580 2,480 -10 / 14 3,850 3,250 2,870 2,740 2,620 2,520 -5 / 23 3,930 3,320 2,920 2,780 2,660 2,550 0 / 32 4,200 3,500 3,050 2,810 2,680 2,570 5 / 41 4,750 3,860 3,310 2,880 2,690 2,560 10 / 50 5,500 4,350 3,680 3,130 2,710 2,560 15 / 59 — 5,060 4,180 3,500 2,930 2,580 20 / 68 — — 4,920 4,010 3,310 2,740 25 / 77 — — — 4,660 3,750 3,050 30 / 86 — — — — 4,380 3,470 Climb Wght Temp Limits °C/°F 12/54 18/64 23/73 28/82 31/88 31/88 Field Length at Temp Limits (ft) 5,890 5,710 5,500 5,210 4,540 3,570 Elevation = 9,000 Feet Ambient Temp --------------------------------------- Takeoff Weight (lb) ---------------------------------------- °C / °F 8,645 8,000 7,500 7,000 6,500 6,000 -20 / -4 3,990 3,330 2,910 2,730 2,600 2,490 -15 / 5 4,050 3,390 2,970 2,780 2,650 2,540 -10 / 14 4,100 3,450 3,020 2,820 2,690 2,580 -5 / 23 4,210 3,540 3,090 2,860 2,730 2,610 0 / 32 4,740 3,870 3,330 2,900 2,740 2,610 5 / 41 5,460 4,340 3,680 3,140 2,760 2,610 10 / 50 — 4,990 4,150 3,480 2,930 2,630 15 / 59 — — 4,780 3,930 3,260 2,720 20 / 68 — — — 4,570 3,700 3,030 25 / 77 — — — 5,460 4,250 3,410 Climb Wght Temp Limits °C/°F 8/46 14/57 19/66 25/77 29/84 29/84 Field Length at Temp Limits (ft) 6,050 5,710 5,550 5,460 4,960 3,840 10 T A K E O F F P E R F O R M A N C E TAKEOFF FIELD LENGTH – FLAPS UP (Over 35 Foot Screen Height) Dry Runway, Zero Wind, Anti-Ice Off, Cabin Bleed Air On Elevation = Sea Level Ambient Temp --------------------------------------- Takeoff Weight (lb) ---------------------------------------- °C / °F 8,645 8,000 7,500 7,000 6,500 6,000 0 / 32 3,810 3,220 2,860 2,730 2,610 2,500 10 / 50 3,950 3,330 2,960 2,810 2,690 2,580 15 / 59 4,020 3,380 3,010 2,850 2,730 2,610 20 / 68 4,090 3,440 3,060 2,900 2,770 2,650 25 / 77 4,160 3,490 3,110 2,950 2,810 2,690 30 / 86 4,360 3,650 3,190 2,980 2,830 2,700 35 / 95 4,780 3,980 3,450 2,990 2,830 2,690 40 / 104 5,250 4,390 3,790 3,250 2,840 2,690 45 / 113 5,800 4,840 4,260 3,650 3,090 2,690 50 / 122 — 5,440 4,670 4,130 3,500 2,920 Climb Wght Temp Limits °C/°F 49/120 50/122 50/122 50/122 50/122 50/122 Field Length at Temp Limits (ft) 6,320 5,440 4,670 4,130 3,500 2,920 Elevation = 1,000 Feet Ambient Temp --------------------------------------- Takeoff Weight (lb) ---------------------------------------- °C / °F 8,645 8,000 7,500 7,000 6,500 6,000 0 / 32 3,940 3,320 2,960 2,810 2,690 2,580 5 / 41 4,020 3,380 3,010 2,860 2,730 2,610 10 / 50 4,090 3,440 3,060 2,900 2,770 2,650 15 / 59 4,160 3,500 3,110 2,950 2,810 2,690 20 / 68 4,240 3,560 3,160 3,000 2,850 2,730 25 / 77 4,410 3,700 3,220 3,030 2,880 2,760 30 / 86 4,830 4,020 3,480 3,040 2,880 2,750 35 / 95 5,260 4,400 3,790 3,270 2,890 2,740 40 / 104 5,760 4,820 4,230 3,600 3,050 2,750 45 / 113 6,410 5,400 4,630 4,090 3,440 2,880 Climb Wght Temp Limits °C/°F 45/113 47/117 47/117 47/117 47/117 47/117 Field Length at Temp Limits (ft) 6,410 5,670 4,810 4,250 3,630 3,020 11 T A K E O F F P E R F O R M A N C E TAKEOFF FIELD LENGTH – FLAPS UP (Over 35 Foot Screen Height) Dry Runway, Zero Wind, Anti-Ice Off, Cabin Bleed Air On Elevation = 2,000 Feet Ambient Temp --------------------------------------- Takeoff Weight (lb) ---------------------------------------- °C / °F 8,645 8,000 7,500 7,000 6,500 6,000 0 / 32 4,090 3,440 3,060 2,910 2,770 2,660 5 / 41 4,160 3,500 3,120 2,960 2,810 2,700 10 / 50 4,240 3,560 3,170 3,010 2,860 2,740 15 / 59 4,310 3,620 3,220 3,050 2,900 2,780 20 / 68 4,450 3,730 3,270 3,100 2,940 2,810 25 / 77 4,880 4,060 3,520 3,100 2,940 2,800 30 / 86 5,310 4,440 3,830 3,300 2,950 2,800 35 / 95 5,790 4,870 4,240 3,610 3,070 2,800 40 / 104 6,380 5,380 4,620 4,040 3,400 2,860 45 / 113 — 6,020 5,110 4,460 3,850 3,200 Climb Wght Temp Limits °C/°F 42/108 45/113 45/113 45/113 45/113 45/113 Field Length at Temp Limits (ft) 6,640 6,020 5,110 4,460 3,850 3,200 Elevation = 3,000 Feet Ambient Temp --------------------------------------- Takeoff Weight (lb) ---------------------------------------- °C / °F 8,645 8,000 7,500 7,000 6,500 6,000 -5 / 23 4,160 3,490 3,120 2,960 2,810 2,700 0 / 32 4,240 3,560 3,170 3,010 2,860 2,740 5 / 41 4,310 3,620 3,230 3,060 2,910 2,790 10 / 50 4,390 3,680 3,280 3,110 2,950 2,820 15 / 59 4,480 3,760 3,340 3,170 3,000 2,870 20 / 68 4,910 4,090 3,550 3,170 2,990 2,850 25 / 77 5,350 4,480 3,870 3,340 3,000 2,850 30 / 86 5,850 4,920 4,260 3,630 3,110 2,850 35 / 95 6,410 5,430 4,650 4,040 3,410 2,890 40 / 104 — 6,000 5,110 4,450 3,810 3,170 Climb Wght Temp Limits °C/°F 38/100 43/109 43/109 43/109 43/109 43/109 Field Length at Temp Limits (ft) 6,790 6,380 5,460 4,680 4,090 3,400 12 T A K E O F F P E R F O R M A N C E TAKEOFF FIELD LENGTH – FLAPS UP (Over 35 Foot Screen Height) Dry Runway, Zero Wind, Anti-Ice Off, Cabin Bleed Air On Elevation = 4,000 Feet Ambient Temp --------------------------------------- Takeoff Weight (lb) ---------------------------------------- °C / °F 8,645 8,000 7,500 7,000 6,500 6,000 -5 / 23 4,310 3,620 3,230 3,060 2,910 2,790 0 / 32 4,390 3,690 3,290 3,110 2,950 2,830 5 / 41 4,480 3,750 3,350 3,170 3,010 2,870 10 / 50 4,580 3,830 3,400 3,220 3,050 2,920 15 / 59 4,920 4,120 3,570 3,240 3,060 2,910 20 / 68 5,380 4,520 3,900 3,360 3,060 2,900 25 / 77 5,890 4,980 4,270 3,670 3,130 2,900 30 / 86 6,470 5,500 4,690 4,060 3,430 2,920 35 / 95 — 6,040 5,170 4,480 3,820 3,180 40 / 104 — — 5,730 4,850 4,240 3,550 Climb Wght Temp Limits °C/°F 33/91 39/102 40/104 40/104 40/104 40/104 Field Length at Temp Limits (ft) 6,850 6,530 5,730 4,850 4,240 3,550 Elevation = 5,000 Feet Ambient Temp --------------------------------------- Takeoff Weight (lb) ---------------------------------------- °C / °F 8,645 8,000 7,500 7,000 6,500 6,000 -10 / 14 4,390 3,680 3,290 3,120 2,960 2,830 -5 / 23 4,470 3,750 3,350 3,170 3,010 2,880 0 / 32 4,560 3,820 3,410 3,230 3,060 2,920 5 / 41 4,650 3,890 3,460 3,280 3,110 2,970 10 / 50 4,970 4,160 3,610 3,300 3,120 2,970 15 / 59 5,390 4,540 3,920 3,380 3,120 2,960 20 / 68 5,920 5,010 4,300 3,690 3,160 2,960 25 / 77 6,510 5,540 4,730 4,070 3,440 2,970 30 / 86 — 6,080 5,220 4,510 3,830 3,200 35 / 95 — 6,690 5,770 4,870 4,260 3,550 Climb Wght Temp Limits °C/°F 29/84 35/95 38/100 38/100 38/100 38/100 Field Length at Temp Limits (ft) 7,030 6,690 6,160 5,180 4,480 3,800 13 T A K E O F F P E R F O R M A N C E TAKEOFF FIELD LENGTH – FLAPS UP (Over 35 Foot Screen Height) Dry Runway, Zero Wind, Anti-Ice Off, Cabin Bleed Air On Elevation = 6,000 Feet Ambient Temp --------------------------------------- Takeoff Weight (lb) ---------------------------------------- °C / °F 8,645 8,000 7,500 7,000 6,500 6,000 -10 / 14 4,570 3,830 3,410 3,230 3,060 2,920 -5 / 23 4,660 3,890 3,470 3,290 3,110 2,970 0 / 32 4,750 3,980 3,530 3,340 3,170 3,020 5 / 41 5,010 4,210 3,650 3,380 3,190 3,030 10 / 50 5,410 4,560 3,940 3,400 3,190 3,020 15 / 59 5,870 4,990 4,280 3,680 3,210 3,020 20 / 68 6,480 5,520 4,730 4,040 3,440 3,030 25 / 77 7,150 6,060 5,210 4,500 3,790 3,180 30 / 86 — 6,670 5,760 4,860 4,240 3,510 35 / 95 — — 6,410 5,370 4,610 3,930 Climb Wght Temp Limits °C/°F 26/79 32/90 36/97 36/97 36/97 36/97 Field Length at Temp Limits (ft) 7,280 6,920 6,540 5,500 4,690 4,030 Elevation = 7,000 Feet Ambient Temp --------------------------------------- Takeoff Weight (lb) ---------------------------------------- °C / °F 8,645 8,000 7,500 7,000 6,500 6,000 -15 / 5 4,740 3,960 3,460 3,270 3,100 2,950 -10 / 14 4,820 4,040 3,520 3,330 3,150 3,000 -5 / 23 4,900 4,110 3,590 3,390 3,210 3,050 0 / 32 5,010 4,210 3,650 3,450 3,260 3,100 5 / 41 5,450 4,610 3,980 3,460 3,260 3,080 10 / 50 5,900 5,020 4,310 3,700 3,270 3,090 15 / 59 6,420 5,490 4,710 4,030 3,430 3,100 20 / 68 7,120 6,040 5,210 4,460 3,760 3,190 25 / 77 — 6,640 5,760 4,860 4,190 3,480 30 / 86 — — 6,370 5,360 4,600 3,880 Climb Wght Temp Limits °C/°F 22/72 28/82 33/91 33/91 33/91 33/91 Field Length at Temp Limits (ft) 8,010 7,030 6,770 5,710 4,840 4,170 14 T A K E O F F P E R F O R M A N C E TAKEOFF FIELD LENGTH – FLAPS UP (Over 35 Foot Screen Height) Dry Runway, Zero Wind, Anti-Ice Off, Cabin Bleed Air On Elevation = 8,000 Feet Ambient Temp --------------------------------------- Takeoff Weight (lb) ---------------------------------------- °C / °F 8,645 8,000 7,500 7,000 6,500 6,000 -15 / 5 5,010 4,210 3,650 3,380 3,190 3,030 -10 / 14 5,100 4,290 3,720 3,440 3,250 3,080 -5 / 23 5,190 4,380 3,790 3,500 3,300 3,130 0 / 32 5,470 4,640 4,000 3,540 3,330 3,150 5 / 41 5,920 5,060 4,340 3,730 3,350 3,150 10 / 50 6,440 5,500 4,730 4,050 3,440 3,160 15 / 59 7,200 6,010 5,200 4,420 3,750 3,180 20 / 68 — 6,630 5,770 4,870 4,160 3,460 25 / 77 — 7,290 6,350 5,360 4,590 3,840 30 / 86 — — — 5,940 5,020 4,300 Climb Wght Temp Limits °C/°F 18/64 25/77 29/84 31/88 31/88 31/88 Field Length at Temp Limits (ft) 8,510 7,290 6,870 6,080 5,130 4,380 Elevation = 9,000 Feet Ambient Temp --------------------------------------- Takeoff Weight (lb) ---------------------------------------- °C / °F 8,645 8,000 7,500 7,000 6,500 6,000 -20 / -4 5,220 4,400 3,810 3,420 3,230 3,060 -15 / 5 5,310 4,480 3,880 3,480 3,290 3,110 -10 / 14 5,390 4,570 3,950 3,550 3,350 3,170 -5 / 23 5,510 4,690 4,050 3,620 3,410 3,220 0 / 32 5,970 5,110 4,390 3,770 3,420 3,220 5 / 41 6,480 5,540 4,780 4,090 3,480 3,220 10 / 50 7,410 6,030 5,230 4,450 3,770 3,240 15 / 59 9,460 6,600 5,760 4,870 4,110 3,450 20 / 68 — 7,290 6,350 5,370 4,600 3,820 25 / 77 — — 6,980 5,930 4,990 4,270 Climb Wght Temp Limits °C/°F 15/59 21/70 26/79 29/84 29/84 29/84 Field Length at Temp Limits (ft) 9,460 7,430 7,130 6,500 5,470 4,600 15 C L I M B P E R F O R M A N C E CRUISE CLIMB ISA, Zero Wind, Anti-Ice Off Time, Fuel, and Distance To Climb * ----------------------------------- Takeoff Weight (lb) ----------------------------------- Pressure Altitude (ft) 8,645 8,000 7,500 7,000 6,500 15,000 Min Lb NM 6 119 18 5 108 17 5 100 15 4 92 14 4 84 13 21,000 Min Lb NM 9 166 29 8 151 26 7 139 24 7 128 22 6 117 20 25,000 Min Lb NM 11 199 38 10 180 35 9 166 32 8 152 29 8 139 27 27,000 Min Lb NM 12 216 44 11 195 39 10 179 36 9 165 33 8 151 30 29,000 Min Lb NM 13 232 49 12 209 44 11 193 40 10 177 37 9 161 34 31,000 Min Lb NM 15 248 55 13 223 49 12 205 45 11 188 41 10 172 37 33,000 Min Lb NM 16 265 61 14 238 54 13 218 50 12 199 45 11 182 41 35,000 Min Lb NM 18 283 68 16 253 60 15 231 55 13 211 50 12 193 45 37,000 Min Lb NM 20 302 76 18 269 67 16 246 61 15 224 55 13 204 50 39,000 Min Lb NM 22 326 87 20 288 76 18 262 69 16 238 62 15 216 56 41,000 Min Lb NM 27 359 105 23 312 89 20 282 79 18 255 70 16 230 63 * Based on the climb starting from sea level. 16 C R U I S E P E R F O R M A N C E HIGH SPEED CRUISE ISA, Anti-Ice Off Cruise Speed & Fuel Flow ----------------------------------- Cruise Weight (lb) ------------------------------------ Pressure Altitude (ft) 8,645 8,000 7,500 7,000 6,500 5,000 KTAS Lb/Hr 269 1,033 269 1,026 269 1,020 269 1,016 269 1,011 10,000 KTAS Lb/Hr 290 992 290 984 290 979 290 974 290 969 15,000 KTAS Lb/Hr 312 969 312 961 312 955 312 949 312 944 21,000 KTAS Lb/Hr 334 917 335 917 337 918 338 919 339 919 23,000 KTAS Lb/Hr 338 883 339 883 341 883 342 884 343 884 25,000 KTAS Lb/Hr 340 843 342 843 343 843 345 844 346 844 27,000 KTAS Lb/Hr 338 785 340 786 342 787 344 788 346 789 29,000 KTAS Lb/Hr 337 736 340 737 342 737 344 737 345 737 31,000 KTAS Lb/Hr 335 687 338 688 341 688 343 690 345 691 33,000 KTAS Lb/Hr 334 648 338 647 340 647 343 647 345 646 35,000 KTAS Lb/Hr 332 609 337 609 340 609 343 609 346 609 37,000 KTAS Lb/Hr 326 565 333 567 338 569 342 570 346 572 39,000 KTAS Lb/Hr 314 517 323 516 330 518 336 520 341 522 41,000 KTAS Lb/Hr 306 465 317 468 326 470 333 473 17 C R U I S E P E R F O R M A N C E LONG RANGE CRUISE ISA, Anti-Ice Off Cruise Speed & Fuel Flow ----------------------------------- Cruise Weight (lb) ------------------------------------ Pressure Altitude (ft) 8,645 8,000 7,500 7,000 6,500 5,000 KTAS Lb/Hr 218 788 210 741 205 712 200 683 195 654 10,000 KTAS Lb/Hr 238 761 230 718 224 687 219 662 211 626 15,000 KTAS Lb/Hr 253 716 245 678 238 646 232 618 224 586 21,000 KTAS Lb/Hr 275 671 266 635 259 606 252 579 246 553 23,000 KTAS Lb/Hr 281 654 275 626 267 595 258 563 250 534 25,000 KTAS Lb/Hr 285 631 281 607 276 584 267 553 257 521 27,000 KTAS Lb/Hr 288 609 284 583 280 563 273 537 265 510 29,000 KTAS Lb/Hr 291 586 287 561 284 543 280 523 273 499 31,000 KTAS Lb/Hr 294 567 290 541 287 523 283 504 279 483 33,000 KTAS Lb/Hr 300 555 293 523 289 503 286 484 282 465 35,000 KTAS Lb/Hr 310 550 300 514 294 488 289 467 285 447 37,000 KTAS Lb/Hr 317 542 314 519 307 493 295 460 289 436 39,000 KTAS Lb/Hr 320 508 319 493 317 477 301 438 41,000 KTAS Lb/Hr 324 466 323 453 18 D E S C E N T P E R F O R M 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 ------ End of Cruise Weight (lb) ------ ------ End of Cruise Weight (lb) ------ Pressure Altitude (ft) 8,000 7,000 6,000 8,000 7,000 6,000 15,000 Min Lb NM 5 21 23 5 26 22 5 32 22 8 58 34 8 63 34 8 68 34 25,000 Min Lb NM 8 37 40 8 45 40 8 55 40 13 97 61 13 105 61 13 113 61 27,000 Min Lb NM 9 41 44 9 49 44 9 59 44 14 105 66 14 113 66 14 121 66 29,000 Min Lb NM 10 45 48 10 54 48 10 64 48 15 114 73 15 122 73 15 131 73 31,000 Min Lb NM 10 49 52 10 58 52 10 69 52 16 122 78 16 130 78 16 139 78 33,000 Min Lb NM 11 52 56 11 62 56 11 73 56 17 128 84 17 137 84 17 146 84 35,000 Min Lb NM 12 55 61 12 65 60 12 76 60 18 134 90 18 143 90 18 153 90 37,000 Min Lb NM 13 60 66 13 69 65 12 80 64 19 139 96 19 149 96 19 158 96 39,000 Min Lb NM 14 64 72 14 73 71 13 83 70 20 144 102 20 153 102 20 163 102 41,000 Min Lb NM 15 68 78 15 77 77 14 88 75 21 148 108 21 158 108 21 167 108 * Based on descending to sea level. 19 R E S E R V E F U E L RESERVE FUEL ALLOWANCES Based on 3 Passengers, ISA, Zero Wind VFR Fuel Reserves (at 15,000 feet) Day (30 minutes) 291 lb Night (45 minutes) 444 lb IFR Fuel Reserves (Alternate plus 45 minutes at 15,000 feet) 100 Nautical Mile Alternate 729 lb 200 Nautical Mile Alternate 915 lb 300 Nautical Mile Alternate 1,056 lb NBAA IFR Reserves * 100 Nautical Mile Alternate 622 lb 200 Nautical Mile Alternate 805 lb 300 Nautical Mile Alternate 944 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. H O L D I N G P E R F O R M A N C E ISA, Anti-Ice Off, Speed Brakes Retracted, Gear & Flaps Up Holding Speed & Fuel Flow ----------------------------------- Pressure Altitude (ft) ------------------------------------ Weight (lb) KIAS S.L. 5,000 10,000 15,000 20,000 25,000 30,000 8,000 150 610 581 554 530 507 486 466 7,500 140 573 543 517 492 472 451 433 7,000 130 538 508 482 457 438 418 401 6,500 130 521 492 466 440 421 401 385 6,000 130 506 477 451 425 406 386 369 20 L A N D I N G P E R F O R M A N C E LANDING DISTANCE – ACTUAL (Distance from 50 Feet Above the Runway) Flaps Land, Dry Runway, Zero Wind, Anti-Ice On or Off Elevation = Sea Level Ambient Temp ------------------------------------------ Landing Weight (lb) -------------------------------------------- °C / °F * 8,645 8,000 7,500 7,000 6,500 6,000 0 / 32 2,440 2,290 2,170 2,060 1,960 1,850 10 / 50 2,510 2,350 2,220 2,110 2,000 1,890 15 / 59 2,550 2,380 2,250 2,130 2,020 1,910 20 / 68 2,580 2,410 2,280 2,160 2,050 1,940 25 / 77 2,620 2,440 2,310 2,190 2,070 1,960 30 / 86 2,660 2,470 2,340 2,210 2,090 1,980 35 / 95 2,690 2,510 2,370 2,240 2,120 2,000 40 / 104 2,730 2,540 2,400 2,270 2,140 2,020 45 / 113 — 2,580 2,430 2,300 2,170 2,050 50 / 122 — — 2,460 2,330 2,190 2,070 Lndg Wght Temp Limits °C/°F 44/111 49/120 50/122 50/122 50/122 50/122 VREF (KIAS) 98 94 91 88 85 82 Elevation = 1,000 Feet Ambient Temp ------------------------------------------ Landing Weight (lb) -------------------------------------------- °C / °F * 8,645 8,000 7,500 7,000 6,500 6,000 0 / 32 2,510 2,350 2,220 2,110 2,000 1,900 5 / 41 2,550 2,380 2,250 2,130 2,020 1,920 10 / 50 2,590 2,410 2,280 2,160 2,050 1,940 15 / 59 2,620 2,440 2,310 2,190 2,070 1,960 20 / 68 2,660 2,480 2,340 2,210 2,100 1,980 25 / 77 2,700 2,510 2,380 2,240 2,120 2,000 30 / 86 2,740 2,550 2,410 2,270 2,150 2,030 35 / 95 2,780 2,580 2,440 2,300 2,170 2,050 40 / 104 2,810 2,610 2,470 2,330 2,190 2,070 45 / 113 — 2,650 2,500 2,360 2,220 2,100 Lndg Wght Temp Limits °C/°F 41/106 46/115 47/117 47/117 47/117 47/117 VREF (KIAS) 98 94 91 88 85 82 * For use in an emergency. Maximum designed landing weight = 8,000 pounds (3,629 kg). 21 L A N D I N G P E R F O R M A N C E LANDING DISTANCE – ACTUAL (Distance from 50 Feet Above the Runway) Flaps Land, Dry Runway, Zero Wind, Anti-Ice On or Off Elevation = 2,000 Feet Ambient Temp ------------------------------------------ Landing Weight (lb) -------------------------------------------- °C / °F * 8,645 8,000 7,500 7,000 6,500 6,000 0 / 32 2,590 2,410 2,290 2,160 2,050 1,940 5 / 41 2,620 2,450 2,320 2,190 2,070 1,960 10 / 50 2,660 2,480 2,350 2,220 2,100 1,980 15 / 59 2,700 2,510 2,380 2,240 2,120 2,000 20 / 68 2,740 2,550 2,410 2,270 2,150 2,030 25 / 77 2,780 2,590 2,440 2,300 2,170 2,050 30 / 86 2,820 2,620 2,470 2,330 2,200 2,080 35 / 95 2,860 2,660 2,510 2,370 2,220 2,100 40 / 104 — 2,690 2,540 2,400 2,250 2,120 45 / 113 — — 2,570 2,420 2,280 2,150 Lndg Wght Temp Limits °C/°F 36/97 42/108 45/113 45/113 45/113 45/113 VREF (KIAS) 98 94 91 88 85 82 Elevation = 3,000 Feet Ambient Temp ------------------------------------------ Landing Weight (lb) -------------------------------------------- °C / °F * 8,645 8,000 7,500 7,000 6,500 6,000 -5 / 23 2,630 2,450 2,320 2,190 2,080 1,970 0 / 32 2,670 2,480 2,350 2,220 2,100 1,990 5 / 41 2,710 2,520 2,380 2,250 2,130 2,010 10 / 50 2,740 2,550 2,410 2,280 2,150 2,030 15 / 59 2,780 2,590 2,440 2,310 2,170 2,050 20 / 68 2,820 2,620 2,480 2,340 2,200 2,080 25 / 77 2,870 2,660 2,510 2,370 2,220 2,100 30 / 86 2,910 2,700 2,550 2,400 2,250 2,130 35 / 95 — 2,740 2,580 2,430 2,280 2,150 40 / 104 — — 2,610 2,460 2,310 2,180 Lndg Wght Temp Limits °C/°F 32/90 38/100 43/109 43/109 43/109 43/109 VREF (KIAS) 98 94 91 88 85 82 * For use in an emergency. Maximum designed landing weight = 8,000 pounds (3,629 kg). 22 L A N D I N G P E R F O R M A N C E LANDING DISTANCE – ACTUAL (Distance from 50 Feet Above the Runway) Flaps Land, Dry Runway, Zero Wind, Anti-Ice On or Off Elevation = 4,000 Feet Ambient Temp ------------------------------------------ Landing Weight (lb) -------------------------------------------- °C / °F * 8,645 8,000 7,500 7,000 6,500 6,000 -5 / 23 2,710 2,520 2,390 2,250 2,130 2,010 0 / 32 2,750 2,560 2,420 2,280 2,150 2,030 5 / 41 2,790 2,590 2,450 2,310 2,180 2,060 10 / 50 2,830 2,630 2,480 2,340 2,200 2,080 15 / 59 2,870 2,660 2,520 2,370 2,230 2,110 20 / 68 2,920 2,700 2,550 2,400 2,260 2,130 25 / 77 2,960 2,740 2,590 2,430 2,280 2,160 30 / 86 — 2,780 2,620 2,470 2,310 2,180 35 / 95 — — 2,660 2,500 2,340 2,200 40 / 104 — — — 2,530 2,370 2,230 Lndg Wght Temp Limits °C/°F 28/82 34/93 39/102 40/104 40/104 40/104 VREF (KIAS) 98 94 91 88 85 82 Elevation = 5,000 Feet Ambient Temp ------------------------------------------ Landing Weight (lb) -------------------------------------------- °C / °F * 8,645 8,000 7,500 7,000 6,500 6,000 -10 / 14 2,750 2,560 2,420 2,280 2,160 2,040 -5 / 23 2,800 2,600 2,450 2,320 2,180 2,060 0 / 32 2,830 2,630 2,490 2,350 2,210 2,090 5 / 41 2,880 2,670 2,520 2,380 2,230 2,110 10 / 50 2,920 2,710 2,560 2,410 2,260 2,130 15 / 59 2,970 2,750 2,590 2,440 2,290 2,160 20 / 68 3,010 2,790 2,620 2,470 2,320 2,180 25 / 77 — 2,830 2,660 2,500 2,350 2,210 30 / 86 — 2,870 2,700 2,540 2,380 2,230 35 / 95 — — 2,740 2,570 2,410 2,260 Lndg Wght Temp Limits °C/°F 24/75 30/86 35/95 38/100 38/100 38/100 VREF (KIAS) 98 94 91 88 85 82 * For use in an emergency. Maximum designed landing weight = 8,000 pounds (3,629 kg). 23 L A N D I N G P E R F O R M A N C E LANDING DISTANCE – ACTUAL (Distance from 50 Feet Above the Runway) Flaps Land, Dry Runway, Zero Wind, Anti-Ice On or Off Elevation = 6,000 Feet Ambient Temp ------------------------------------------ Landing Weight (lb) -------------------------------------------- °C / °F * 8,645 8,000 7,500 7,000 6,500 6,000 -10 / 14 2,850 2,650 2,500 2,360 2,220 2,100 -5 / 23 2,890 2,680 2,530 2,390 2,240 2,120 0 / 32 2,940 2,720 2,570 2,420 2,270 2,150 5 / 41 2,980 2,760 2,600 2,450 2,300 2,170 10 / 50 3,020 2,800 2,640 2,480 2,330 2,190 15 / 59 3,070 2,840 2,670 2,520 2,360 2,220 20 / 68 3,120 2,880 2,710 2,550 2,390 2,240 25 / 77 — 2,920 2,750 2,590 2,420 2,270 30 / 86 — — 2,790 2,620 2,450 2,300 35 / 95 — — — 2,650 2,480 2,320 Lndg Wght Temp Limits °C/°F 20/68 26/79 31/88 36/97 36/97 36/97 VREF (KIAS) 98 94 91 88 85 82 Elevation = 7,000 Feet Ambient Temp ------------------------------------------ Landing Weight (lb) -------------------------------------------- °C / °F * 8,645 8,000 7,500 7,000 6,500 6,000 -15 / 5 2,910 2,700 2,550 2,400 2,250 2,130 -10 / 14 2,950 2,740 2,580 2,430 2,280 2,160 -5 / 23 3,000 2,780 2,620 2,470 2,310 2,180 0 / 32 3,040 2,820 2,650 2,500 2,340 2,210 5 / 41 3,090 2,860 2,690 2,530 2,370 2,230 10 / 50 3,140 2,900 2,730 2,570 2,400 2,260 15 / 59 3,190 2,940 2,770 2,600 2,430 2,280 20 / 68 — 2,980 2,800 2,630 2,460 2,310 25 / 77 — — 2,840 2,670 2,500 2,340 30 / 86 — — — 2,700 2,530 2,360 Lndg Wght Temp Limits °C/°F 17/63 22/72 28/82 33/91 33/91 33/91 VREF (KIAS) 98 94 91 88 85 82 * For use in an emergency. Maximum designed landing weight = 8,000 pounds (3,629 kg). 24 L A N D I N G P E R F O R M A N C E LANDING DISTANCE – ACTUAL (Distance from 50 Feet Above the Runway) Flaps Land, Dry Runway, Zero Wind, Anti-Ice On or Off Elevation = 8,000 Feet Ambient Temp ------------------------------------------ Landing Weight (lb) -------------------------------------------- °C / °F * 8,645 8,000 7,500 7,000 6,500 6,000 -15 / 5 3,010 2,790 2,630 2,480 2,330 2,190 -10 / 14 3,060 2,830 2,670 2,510 2,360 2,220 -5 / 23 3,110 2,870 2,710 2,550 2,390 2,250 0 / 32 3,160 2,920 2,740 2,580 2,420 2,270 5 / 41 3,210 2,960 2,780 2,610 2,450 2,300 10 / 50 3,250 3,000 2,820 2,650 2,480 2,320 15 / 59 — 3,040 2,860 2,680 2,510 2,350 20 / 68 — — 2,900 2,720 2,540 2,380 25 / 77 — — — 2,760 2,580 2,400 30 / 86 — — — — 2,610 2,430 Lndg Wght Temp Limits °C/°F 13/55 19/66 24/75 29/84 31/88 31/88 VREF (KIAS) 98 94 91 88 85 82 * For use in an emergency. Maximum designed landing weight = 8,000 pounds (3,629 kg). S T A L L S P E E D S Zero Angle of Bank, Landing Gear Up or Down, Anti-Ice Off, KCAS Stall Speeds ---------------------- Flap Position ---------------------- Weight (lb) Land 15° Up 8,645 76 81 91 8,000 73 78 87 7,500 71 76 85 7,000 68 73 82 6,500 66 71 79 6,000 63 68 76 25 M I S S I O N P L A N N I N G CRITERIA The following mission planning table provides flight time and fuel burn statistics for selected distances and 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 60 pounds of fuel included in all fuel burn figures. NBAA IFR fuel reserves (100 nm) are considered in each case but are not included in the fuel burn figure. The mission planning table reflects cruise climb, high-speed cruise, and high-speed descent 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 6,000 - 15,000 100 - 199 14,000 - 28,000 200 - 299 27,000 - 35,000 300 - 499 33,000 - 37,000 500 - 999 35,000 - 39,000 1000 + 39,000 - 41,000 Wind Correction Factors * True Airspeed -------------- Headwinds (kt) -------------- --------------- Tailwinds (kt) --------------- (kt) 100 75 50 25 0 25 50 75 100 280 1.55 1.37 1.22 1.10 1.00 0.92 0.85 0.79 0.74 290 1.53 1.35 1.21 1.09 1.00 0.92 0.85 0.79 0.74 300 1.50 1.33 1.20 1.09 1.00 0.92 0.86 0.80 0.75 310 1.48 1.32 1.19 1.09 1.00 0.93 0.86 0.81 0.76 320 1.45 1.31 1.19 1.08 1.00 0.93 0.86 0.81 0.76 330 1.43 1.29 1.18 1.08 1.00 0.93 0.87 0.81 0.77 340 1.42 1.28 1.17 1.08 1.00 0.93 0.87 0.82 0.77 * Wind Correction Factor is calculated as KTAS divided by the sum of KTAS ± wind component 26 M I S S I O N P L A N N I N G FLIGHT TIME & FUEL BURN ------------------------------------------------- Cruise Altitude (ft) ------------------------------------------------- 15,000 25,000 27,000 29,000 31,000 Dist (nm) Time (min) Fuel (lb) Time (min) Fuel (lb) Time (min) Fuel (lb) Time (min) Fuel (lb) Time (min) Fuel (lb) 100 0:22 375 0:21 336 0:22 329 150 0:31 528 0:30 460 0:31 446 0:32 435 0:31 426 200 0:41 682 0:39 584 0:40 562 0:40 544 0:40 528 250 0:51 836 0:48 708 0:49 678 0:49 654 0:49 630 300 1:00 990 0:57 832 0:57 795 0:58 763 0:58 733 350 1:10 1,144 1:06 957 1:06 912 1:07 873 1:06 836 400 1:19 1,298 1:15 1,081 1:15 1,029 1:16 982 1:15 939 450 1:29 1,454 1:23 1,206 1:24 1,146 1:25 1,091 1:24 1,041 500 1:39 1,610 1:32 1,331 1:33 1,264 1:33 1,201 1:33 1,144 600 1:59 1,924 1:50 1,582 1:51 1,498 1:51 1,421 1:51 1,351 700 2:08 1,834 2:08 1,733 2:09 1,642 2:09 1,557 800 900 1,000 1,100 1,150 Assumptions: • Cruise climb • High-speed cruise • High-speed descent • ISA, zero winds enroute • Flight time includes climb, cruise and descent • Fuel burn includes 60 pounds for taxi and takeoff • Three passengers @ 200 pounds each, single pilot • NBAA IFR Reserves - 100 nm (622 lb) Reserves are not included in the fuel burn figures 27 FOR SELECTED DISTANCES ------------------------------------------------- Cruise Altitude (ft) ------------------------------------------------- 33,000 35,000 37,000 39,000 41,000 Time (min) Fuel (lb) Time (min) Fuel (lb) Time (min) Fuel (lb) Time (min) Fuel (lb) Time (min) Fuel (lb) Dist (nm) 100 0:32 418 0:32 412 0:33 409 150 0:40 514 0:41 503 0:42 494 0:42 482 0:43 477 200 0:49 611 0:50 594 0:51 579 0:51 562 0:52 551 250 0:58 707 0:59 685 0:59 665 1:00 641 1:01 625 300 1:07 804 1:08 776 1:08 751 1:09 721 1:11 699 350 1:16 901 1:17 867 1:17 836 1:18 801 1:20 774 400 1:25 998 1:26 959 1:26 923 1:28 881 1:29 849 450 1:33 1,096 1:35 1,051 1:35 1,009 1:37 962 1:39 925 500 1:51 1,292 1:52 1,235 1:53 1,182 1:55 1,124 1:58 1,076 600 2:09 1,487 2:10 1,420 2:11 1,355 2:14 1,286 2:17 1,229 700 2:27 1,684 2:28 1,605 2:29 1,530 2:32 1,450 2:37 1,383 800 2:45 1,880 2:46 1,791 2:47 1,705 2:50 1,614 2:56 1,539 900 3:06 1,881 3:09 1,779 3:16 1,696 1,000 3:36 1,854 1,100 3:46 1,932 1,150 28 M I S S I O N P L A N N I N G RANGE / PAYLOAD CAPABILITY NBAA IFR Reserves (100 nm), ISA, Zero Wind, High-Speed Cruise 0 200 400 600 800 1,000 1,200 1,400 0 200 400 600 800 1,000 1,200 1,400 NBAA IFR Range (nautical miles) Payload (pounds) Assumptions: Single Pilot Cruise at FL 410 2

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