Cessna 510 Mustang FP Guide

T A B L E O F C O NT E NT S  Thi  This Flig Flight P lanning Gui Guide is publish she ed for the purpose of providing specific information for evaluating the performance of the Cessna Citation Mustang (Model 510).  Thi  This guide is developed from data contained in the Cita Citation Must Musta ang 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  The data included herein does no not const stiitute an offer and is subject to change without notice. Section

Page

Specifi pecificat cation ions s .......................... ....................................... .......................... .......................... .......................... .......................... ..............2 .2  Tak  Takeoff P erformance Decision, Decision, Rot R otat ation ion and and Take Takeoff off Safe Safetty Spe S peed eds s ....................... ................................... ...............4 ...4  Tak  Takeoff Fiel Field Len Length – Fl F laps 15° ....................... .................................. ...................... ...................... ...............5 ....5  Tak  Takeoff Fiel Field Len Length – Fl F laps UP .... ...... .... .... .... .... .... .... .... .... .... .... .... .... .... .... .... .... .... .... .... .... .... .... .... .... .... .... ..1 10 Climb Performance..................................................................................15 Cruise ruise P erform erformance ance High Speed Cruise................................................................................16 Long Range Cruise...............................................................................17 Descent Performance..............................................................................18 Reserve eserve F uel uel Calculat alculation ions s ........................ ..................................... ......................... ......................... ..................... ........19 19 Holding Performance...............................................................................19 Landin Landing g P erform erforman ance ce............. .......................... .......................... .......................... .......................... .......................... .............20 20 Stall all Speeds eeds ....................... .................................. ....................... ....................... ...................... ....................... ....................... ............24 .24 Mission P lanni lanning ng Table ......................... ...................................... .......................... ......................... ........................ ............25 25

Revisions: Revisions: FM-07(AH), FM-07(AH), PP P P -01

1

SPECIFICATIONS 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 23 *

Pratt & Whitney Canada (2) PW-615F 1,460 lb 6.49 kN 77 °F 25 °C 3,500 hours

40 ft 7 in 13 ft 5 in 43 ft 2 in 14 ft 4 in 11 ft 10 in

12.37 m 4.09 m 13.16 m 4.37 m 3.61 m

Cabin Dimensions (with typical interior installed) Length - overall 14 ft 9 in Length - excluding cockpit 9 ft 9 in Height 54 in Width 55 in 3 Passenger Cabin Volume 144 ft Accommodations Passenger Seats Baggage Capacity

3

4.50 m 2.97 m 1.37 m 1.40 m 3 4.08 m

5

3

63 ft 718 lb

1.78 m 325 kg

Pressurization Differential Sea Level Cabin to 8,000 Foot Cabin at

8.3 psi 21,280 ft 41,000 ft

0.57 bar 6,486 m 12,497 m

Altitudes Certified Ceiling Service Ceiling - 1 Engine (MTOW)  Typical Cruise Altitudes

41,000 ft 12,497 m 26,900 ft 8,199 m FL 330 - 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.

2

SPECIFICATIONS 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 Airspeed Limitations Maximum Operating Limit MMO (27,120 ft / 8,266 m and above) VMO (Sea Level to 27,120 ft / 8,266 m) Maximum Flap Extended Speed (VFE )  Takeoff & Approach (15°) Land (30°) Max Landing Gear Extended Speed (VLE) Max Landing Gear Oper - Extending (VLO) Max Landing Gear Oper - Retracting (VLO) Max. Speed Brake Operation Speed (VSB) Minimum Control Speed, Air (VMCA) Flaps - 0° Flaps - 15° Minimum Control Speed, Ground (V MCG)

3,110 ft 948 m 2,380 ft 725 m 3,010 ft/min 917 m/min 870 ft/min 265 m/min 320-345 ktas 593-639 km/hr

M 0.63 Indicated 250 KIAS 463 km/hr 185 KIAS 150 KIAS 250 KIAS 250 KIAS 185 KIAS No limit

343 km/hr 278 km/hr 463 km/hr 463 km/hr 343 km/hr No limit

92 KIAS 81 KIAS 73 KIAS

170 km/hr 150 km/hr 135 km/hr

Certified Weights Maximum Ramp Weight Maximum Takeoff Weight Maximum Landing Weight Maximum Zero Fuel Weight Maximum Fuel Capacity (6.7 lb/gal)

8,730 lb 8,645 lb 8,000 lb 6,750 lb 2,580 lb

3,960 kg 3,921 kg 3,629 kg 3,062 kg 1,170 kg

Basic Operating Weight  Typically-Equipped Empty Weight Single Pilot & Furnishings Basic Operating Weight

5,375 lb 200 lb 5,575 lb

2,438 kg 91 kg 2,529 kg

Payload Useful Payload and Fuel Maximum Payload Payload at Full Fuel

3,155 lb 1,175 lb 575 lb

1,431 kg 533 kg 261 kg

3

T A K E O F F P E R F OR 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 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  Takeoff  Weight (lb)

8,645 8,000 7,500 7,000 6,500 6,000

4

Decision Speed

Rotation Speed

V1 89 85 82 81 79 79

VR 89 85 84 84 84 84

Safety Speed

V2 97 93 93 94 94 95

Flaps UP Settin g Decision Speed

Rotation Speed

Safety Speed

V1 102 97 94 93 91 89

VR 104 99 95 95 95 95

V2 112 108 106 106 107 108

T A K E O F F P E R F OR 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 °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) ----------------------------------------

8,645 2,990 3,070 3,110 3,150 3,190 3,380 3,820 4,440 — —

8,000 2,500 2,580 2,610 2,650 2,690 2,810 3,130 3,550 4,170 —

7,500 2,350 2,420 2,450 2,490 2,520 2,550 2,700 3,020 3,460 4,150

7,000 2,240 2,310 2,340 2,380 2,410 2,430 2,450 2,570 2,900 3,390

6,500 2,160 2,220 2,250 2,280 2,310 2,320 2,330 2,340 2,440 2,790

6,000 2,210 2,270 2,300 2,330 2,360 2,300 2,210 2,210 2,220 2,320

44/111

49/120

50/122

50/122

50/122

50/122

5,230

4,990

4,150

3,390

2,790

2,320

Elevation = 1,000 Feet Ambient Temp °C

/

°F

0 / 32 5 / 41 10 / 50 15 / 59 20 / 68 25 / 77 30 / 86 35 / 95 40 / 104 45 / 113 Climb Wght Temp Limits °C/°F Field Length at  Temp Limits (ft)

--------------------------------------- Takeoff Weight (lb) ----------------------------------------

8,645 3,070 3,110 3,150 3,200 3,240 3,390 3,810 4,370 5,240 —

8,000 2,580 2,610 2,650 2,690 2,730 2,840 3,130 3,520 4,050 4,960

7,500 2,420 2,450 2,490 2,530 2,560 2,600 2,700 3,000 3,390 3,990

7,000 2,310 2,340 2,380 2,410 2,450 2,480 2,490 2,570 2,860 3,290

6,500 2,230 2,260 2,290 2,320 2,350 2,360 2,370 2,380 2,420 2,730

6,000 2,280 2,310 2,340 2,370 2,400 2,370 2,270 2,250 2,260 2,280

40/104

45/113

47/117

47/117

47/117

47/117

5,240

4,960

4,330

3,510

2,890

2,390

5

T A K E O F F P E R F OR 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 °C

/

°F

0 / 32 5 / 41 10 / 50 15 / 59 20 / 68 25 / 77 30 / 86 35 / 95 40 / 104 45 / 113 Climb Wght Temp Limits °C/°F Field Length at  Temp Limits (ft)

--------------------------------------- Takeoff Weight (lb) ----------------------------------------

8,645 3,150 3,190 3,240 3,280 3,390 3,810 4,360 5,160 — —

8,000 2,650 2,690 2,740 2,780 2,860 3,140 3,530 4,030 4,760 —

7,500 2,490 2,530 2,570 2,600 2,640 2,720 3,010 3,380 3,880 4,710

7,000 2,380 2,410 2,450 2,490 2,520 2,540 2,590 2,860 3,230 3,770

6,500 2,290 2,330 2,360 2,390 2,410 2,410 2,420 2,450 2,690 3,080

6,000 2,350 2,380 2,410 2,440 2,420 2,320 2,290 2,300 2,320 2,530

36/97

41/106

45/113

45/113

45/113

45/113

5,370

4,970

4,710

3,770

3,080

2,530

Elevation = 3,000 Feet Ambient Temp °C

/

°F

-5 / 23 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)

6

--------------------------------------- Takeoff Weight (lb) ----------------------------------------

8,645 3,190 3,230 3,280 3,330 3,390 3,800 4,350 5,130 — —

8,000 2,690 2,740 2,780 2,830 2,880 3,140 3,530 4,030 4,720 —

7,500 2,530 2,570 2,610 2,650 2,690 2,740 3,020 3,400 3,870 4,570

7,000 2,410 2,450 2,490 2,530 2,570 2,580 2,610 2,870 3,230 3,690

6,500 2,330 2,360 2,400 2,430 2,450 2,450 2,460 2,490 2,700 3,030

6,000 2,380 2,410 2,450 2,480 2,480 2,380 2,340 2,340 2,360 2,510

31/88

37/99

42/108

43/109

43/109

43/109

5,340

5,100

4,960

4,090

3,300

2,700

T A K E O F F P E R F OR 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 °C

/

°F

-5 / 23 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) ----------------------------------------

8,645 3,280 3,330 3,380 3,450 3,770 4,320 5,090 — — —

8,000 2,780 2,830 2,870 2,930 3,140 3,520 4,020 4,700 — —

7,500 2,610 2,650 2,690 2,730 2,760 3,020 3,400 3,880 4,530 —

7,000 2,490 2,530 2,570 2,600 2,630 2,650 2,880 3,240 3,690 4,320

6,500 2,400 2,430 2,470 2,490 2,500 2,510 2,530 2,710 3,040 3,460

6,000 2,450 2,480 2,520 2,520 2,440 2,380 2,390 2,400 2,520 2,820

27/81

33/91

38/100

40/104

40/104

40/104

5,510

5,260

5,090

4,320

3,460

2,820

Elevation = 5,000 Feet Ambient Temp °C

/

-10 / -5 / 0/ 5/ 10 / 15 / 20 / 25 / 30 / 35 /

°F

14 23 32 41 50 59 68 77 86 95

Climb Wght Temp Limits °C/°F Field Length at  Temp Limits (ft)

--------------------------------------- Takeoff Weight (lb) ----------------------------------------

8,645 3,320 3,380 3,440 3,510 3,780 4,270 5,020 — — —

8,000 2,820 2,870 2,920 2,980 3,170 3,500 4,000 4,660 — —

7,500 2,650 2,690 2,740 2,770 2,810 3,010 3,390 3,860 4,490 —

7,000 2,530 2,570 2,610 2,640 2,670 2,700 2,880 3,240 3,680 4,280

6,500 2,430 2,470 2,510 2,530 2,550 2,560 2,580 2,720 3,040 3,450

6,000 2,480 2,520 2,560 2,570 2,490 2,430 2,430 2,440 2,520 2,820

23/73

29/84

34/93

38/100

38/100

38/100

5,640

5,410

5,230

4,780

3,760

3,030

7

T A K E O F F P E R F OR 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 °C

/

-10 / -5 / 0/ 5/ 10 / 15 / 20 / 25 / 30 / 35 /

°F

14 23 32 41 50 59 68 77 86 95

Climb Wght Temp Limits °C/°F Field Length at  Temp Limits (ft)

--------------------------------------- Takeoff Weight (lb) ----------------------------------------

8,645 3,450 3,510 3,580 3,790 4,230 4,840 — — — —

8,000 2,930 2,980 3,030 3,200 3,480 3,900 4,530 5,430 — —

7,500 2,740 2,780 2,820 2,860 3,020 3,320 3,790 4,380 5,230 —

7,000 2,610 2,650 2,700 2,720 2,750 2,850 3,190 3,620 4,160 4,980

6,500 2,500 2,540 2,580 2,600 2,600 2,620 2,700 3,010 3,390 3,910

6,000 2,540 2,580 2,610 2,550 2,480 2,480 2,490 2,520 2,780 3,140

19/66

25/77

30/86

36/97

36/97

36/97

5,630

5,430

5,230

5,210

4,040

3,230

Elevation = 7,000 Feet Ambient Temp °C

/

-15 / -10 / -5 / 0/ 5/ 10 / 15 / 20 / 25 / 30 /

°F

5 14 23 32 41 50 59 68 77 86

Climb Wght Temp Limits °C/°F Field Length at  Temp Limits (ft)

8

--------------------------------------- Takeoff Weight (lb) ----------------------------------------

8,645 3,570 3,640 3,700 3,790 4,230 4,790 5,620 — — —

8,000 3,030 3,080 3,140 3,200 3,490 3,870 4,400 5,240 — —

7,500 2,780 2,820 2,870 2,920 3,050 3,310 3,710 4,280 5,050 —

7,000 2,640 2,690 2,730 2,780 2,800 2,860 3,140 3,560 4,070 4,800

6,500 2,530 2,570 2,610 2,650 2,650 2,670 2,700 2,970 3,340 3,820

6,000 2,530 2,570 2,600 2,640 2,530 2,530 2,540 2,560 2,760 3,090

16/61

22/72

27/81

32/90

33/91

33/91

5,870

5,680

5,460

5,210

4,200

3,340

T A K E O F F P E R F OR 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 °C

/

-15 / -10 / -5 / 0/ 5/ 10 / 15 / 20 / 25 / 30 /

°F

5 14 23 32 41 50 59 68 77 86

Climb Wght Temp Limits °C/°F Field Length at  Temp Limits (ft)

--------------------------------------- Takeoff Weight (lb) ----------------------------------------

8,645 3,800 3,860 3,940 4,200 4,750 5,500 — — — —

8,000 3,210 3,260 3,330 3,510 3,860 4,350 5,060 — — —

7,500 2,860 2,910 2,960 3,060 3,310 3,680 4,180 4,920 — —

7,000 2,720 2,770 2,810 2,840 2,890 3,130 3,500 4,010 4,660 —

6,500 2,600 2,640 2,680 2,700 2,720 2,750 2,930 3,310 3,750 4,380

6,000 2,550 2,590 2,620 2,580 2,580 2,590 2,610 2,740 3,050 3,470

12/54

18/64

23/73

28/82

31/88

31/88

5,900

5,710

5,500

5,220

4,540

3,580

Elevation = 9,000 Feet Ambient Temp °C

/

-20 / -15 / -10 / -5 / 0/ 5/ 10 / 15 / 20 / 25 /

°F

-4 5 14 23 32 41 50 59 68 77

Climb Wght Temp Limits °C/°F Field Length at  Temp Limits (ft)

--------------------------------------- Takeoff Weight (lb) ----------------------------------------

8,645 3,990 4,050 4,110 4,230 4,740 5,460 — — — —

8,000 3,340 3,400 3,460 3,550 3,870 4,340 4,990 — — —

7,500 2,920 2,970 3,020 3,100 3,340 3,680 4,150 4,780 — —

7,000 2,760 2,810 2,850 2,890 2,930 3,140 3,480 3,930 4,570 5,460

6,500 2,620 2,670 2,710 2,750 2,770 2,800 2,940 3,260 3,700 4,260

6,000 2,530 2,570 2,610 2,640 2,630 2,640 2,660 2,730 3,030 3,410

8/46

14/57

19/66

25/77

29/84

29/84

6,060

5,720

5,560

5,460

4,960

3,840

9

T A K E O F F P E R F OR 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 °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) ----------------------------------------

8,645 3,820 3,960 4,030 4,100 4,170 4,370 4,790 5,260 5,880 —

8,000 3,220 3,340 3,390 3,450 3,500 3,660 3,990 4,390 4,850 5,530

7,500 2,870 2,970 3,020 3,070 3,120 3,200 3,460 3,790 4,260 4,670

7,000 2,730 2,820 2,860 2,910 2,960 2,980 3,000 3,260 3,650 4,130

6,500 2,610 2,690 2,730 2,780 2,810 2,830 2,840 2,850 3,090 3,500

6,000 2,500 2,580 2,620 2,660 2,700 2,710 2,700 2,700 2,700 2,920

49/120

50/122

50/122

50/122

50/122

50/122

6,530

5,530

4,670

4,130

3,500

2,920

Elevation = 1,000 Feet Ambient Temp °C

/

°F

0 / 32 5 / 41 10 / 50 15 / 59 20 / 68 25 / 77 30 / 86 35 / 95 40 / 104 45 / 113 Climb Wght Temp Limits °C/°F Field Length at  Temp Limits (ft)

10

--------------------------------------- Takeoff Weight (lb) ----------------------------------------

8,645 3,960 4,030 4,100 4,170 4,250 4,430 4,840 5,270 5,830 6,480

8,000 3,330 3,390 3,450 3,510 3,570 3,710 4,030 4,400 4,840 5,470

7,500 2,970 3,020 3,070 3,120 3,170 3,230 3,490 3,800 4,230 4,630

7,000 2,820 2,860 2,910 2,960 3,010 3,040 3,050 3,280 3,600 4,090

6,500 2,690 2,740 2,780 2,820 2,860 2,890 2,890 2,900 3,060 3,440

6,000 2,580 2,620 2,660 2,700 2,740 2,760 2,750 2,750 2,760 2,880

45/113

47/117

47/117

47/117

47/117

47/117

6,480

5,760

4,820

4,250

3,630

3,020

T A K E O F F P E R F OR 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 °C

/

°F

0 / 32 5 / 41 10 / 50 15 / 59 20 / 68 25 / 77 30 / 86 35 / 95 40 / 104 45 / 113 Climb Wght Temp Limits °C/°F Field Length at  Temp Limits (ft)

--------------------------------------- Takeoff Weight (lb) ----------------------------------------

8,645 4,090 4,170 4,250 4,320 4,470 4,890 5,310 5,860 6,460 —

8,000 3,450 3,510 3,570 3,630 3,740 4,070 4,450 4,880 5,440 6,100

7,500 3,070 3,130 3,180 3,230 3,280 3,530 3,840 4,240 4,620 5,180

7,000 2,920 2,970 3,020 3,060 3,110 3,110 3,310 3,610 4,040 4,460

6,500 2,780 2,820 2,870 2,910 2,940 2,940 2,950 3,080 3,400 3,850

6,000 2,660 2,710 2,750 2,790 2,820 2,810 2,800 2,810 2,870 3,200

42/108

45/113

45/113

45/113

45/113

45/113

6,790

6,100

5,180

4,460

3,850

3,200

Elevation = 3,000 Feet Ambient Temp °C

/

°F

-5 / 23 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) ----------------------------------------

8,645 4,170 4,250 4,320 4,410 4,500 4,920 5,360 5,900 6,500 —

8,000 3,500 3,570 3,630 3,690 3,770 4,100 4,490 4,940 5,480 6,080

7,500 3,130 3,180 3,240 3,290 3,350 3,560 3,880 4,260 4,650 5,160

7,000 2,970 3,020 3,070 3,120 3,170 3,180 3,350 3,640 4,040 4,450

6,500 2,820 2,870 2,910 2,960 3,010 3,000 3,010 3,110 3,410 3,810

6,000 2,710 2,750 2,790 2,830 2,880 2,860 2,850 2,860 2,900 3,170

38/100

43/109

43/109

43/109

43/109

43/109

6,910

6,480

5,530

4,680

4,090

3,400

11

T A K E O F F P E R F OR 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 °C

/

°F

-5 / 23 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) ----------------------------------------

8,645 4,320 4,410 4,490 4,590 4,940 5,390 5,940 6,560 — —

8,000 3,630 3,690 3,760 3,840 4,130 4,530 4,990 5,520 6,120 —

7,500 3,240 3,300 3,350 3,410 3,580 3,910 4,280 4,700 5,180 5,810

7,000 3,070 3,120 3,180 3,230 3,250 3,370 3,680 4,060 4,480 4,850

6,500 2,920 2,960 3,010 3,060 3,060 3,060 3,140 3,430 3,820 4,240

6,000 2,800 2,840 2,880 2,920 2,920 2,910 2,910 2,930 3,180 3,550

33/91

39/102

40/104

40/104

40/104

40/104

6,920

6,580

5,810

4,850

4,240

3,550

Elevation = 5,000 Feet Ambient Temp °C

/

-10 / -5 / 0/ 5/ 10 / 15 / 20 / 25 / 30 / 35 /

°F

14 23 32 41 50 59 68 77 86 95

Climb Wght Temp Limits °C/°F Field Length at  Temp Limits (ft)

12

--------------------------------------- Takeoff Weight (lb) ----------------------------------------

8,645 4,400 4,480 4,570 4,660 4,980 5,400 5,930 6,600 — —

8,000 3,690 3,760 3,830 3,900 4,170 4,550 5,030 5,550 6,150 6,750

7,500 3,300 3,360 3,420 3,470 3,620 3,930 4,310 4,750 5,230 5,850

7,000 3,130 3,180 3,240 3,290 3,310 3,390 3,700 4,070 4,510 4,880

6,500 2,970 3,020 3,070 3,120 3,130 3,130 3,170 3,450 3,830 4,260

6,000 2,840 2,880 2,930 2,980 2,980 2,970 2,970 2,980 3,200 3,550

29/84

35/95

38/100

38/100

38/100

38/100

7,100

6,750

6,250

5,240

4,480

3,800

T A K E O F F P E R F OR 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 °C

/

-10 / -5 / 0/ 5/ 10 / 15 / 20 / 25 / 30 / 35 /

°F

14 23 32 41 50 59 68 77 86 95

Climb Wght Temp Limits °C/°F Field Length at  Temp Limits (ft)

--------------------------------------- Takeoff Weight (lb) ----------------------------------------

8,645 4,580 4,670 4,760 5,020 5,420 5,880 6,550 7,220 — —

8,000 3,840 3,900 3,990 4,220 4,580 5,000 5,530 6,120 6,740 —

7,500 3,420 3,480 3,540 3,660 3,950 4,300 4,740 5,230 5,830 6,480

7,000 3,230 3,290 3,350 3,390 3,410 3,690 4,050 4,500 4,870 5,430

6,500 3,070 3,120 3,170 3,200 3,200 3,210 3,450 3,790 4,240 4,610

6,000 2,930 2,980 3,020 3,040 3,030 3,030 3,040 3,190 3,510 3,930

26/79

32/90

36/97

36/97

36/97

36/97

7,610

7,020

6,590

5,550

4,690

4,030

Elevation = 7,000 Feet Ambient Temp °C

/

-15 / -10 / -5 / 0/ 5/ 10 / 15 / 20 / 25 / 30 /

°F

5 14 23 32 41 50 59 68 77 86

Climb Wght Temp Limits °C/°F Field Length at  Temp Limits (ft)

--------------------------------------- Takeoff Weight (lb) ----------------------------------------

8,645 4,750 4,830 4,910 5,020 5,460 5,910 6,480 7,480 — —

8,000 3,970 4,050 4,120 4,230 4,620 5,040 5,500 6,090 6,730 —

7,500 3,470 3,530 3,600 3,660 3,990 4,320 4,720 5,230 5,810 6,460

7,000 3,280 3,340 3,400 3,460 3,470 3,710 4,040 4,460 4,880 5,410

6,500 3,110 3,160 3,220 3,270 3,270 3,280 3,440 3,760 4,190 4,600

6,000 2,960 3,010 3,060 3,100 3,090 3,090 3,100 3,190 3,480 3,880

22/72

28/82

33/91

33/91

33/91

33/91

8,380

7,090

6,850

5,780

4,820

4,170

13

T A K E O F F P E R F OR 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 °C

/

-15 / -10 / -5 / 0/ 5/ 10 / 15 / 20 / 25 / 30 /

°F

5 14 23 32 41 50 59 68 77 86

Climb Wght Temp Limits °C/°F Field Length at  Temp Limits (ft)

--------------------------------------- Takeoff Weight (lb) ----------------------------------------

8,645 5,020 5,110 5,200 5,480 5,940 6,480 7,530 — — —

8,000 4,220 4,300 4,390 4,650 5,070 5,510 6,020 6,710 7,340 —

7,500 3,660 3,730 3,800 4,010 4,360 4,740 5,210 5,780 6,430 —

7,000 3,380 3,450 3,510 3,550 3,740 4,060 4,430 4,890 5,370 6,020

6,500 3,200 3,260 3,310 3,340 3,350 3,450 3,760 4,160 4,590 4,970

6,000 3,040 3,090 3,140 3,160 3,160 3,170 3,190 3,460 3,840 4,300

18/64

25/77

29/84

31/88

31/88

31/88

8,860

7,340

6,930

6,160

5,060

4,380

Elevation = 9,000 Feet Ambient Temp °C

/

-20 / -15 / -10 / -5 / 0/ 5/ 10 / 15 / 20 / 25 /

°F

-4 5 14 23 32 41 50 59 68 77

Climb Wght Temp Limits °C/°F Field Length at  Temp Limits (ft)

14

--------------------------------------- Takeoff Weight (lb) ----------------------------------------

8,645 5,230 5,310 5,400 5,520 5,980 6,510 7,680 9,810 — —

8,000 4,410 4,490 4,580 4,700 5,130 5,550 6,040 6,670 7,370 —

7,500 3,820 3,890 3,960 4,060 4,400 4,790 5,250 5,770 6,420 7,050

7,000 3,430 3,490 3,560 3,630 3,780 4,100 4,460 4,880 5,390 6,000

6,500 3,230 3,300 3,360 3,420 3,430 3,490 3,780 4,120 4,600 4,960

6,000 3,070 3,120 3,180 3,230 3,220 3,230 3,240 3,460 3,820 4,270

15/59

21/70

26/79

29/84

29/84

29/84

9,810

7,480

7,180

6,580

5,420

4,600

CLIMB PERFORMANCE 170 KIAS / M 0.44 CLIMB ISA, Zero Wind, Anti-Ice Off  Time, Fuel, and Distance To Climb * ----------------------------------- Takeoff Weight (lb) -----------------------------------

Pressure Altitude (ft)

15,000

21,000

25,000

27,000

29,000

31,000

33,000

35,000

37,000

39,000

41,000

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 Min Lb NM

8,645 6 119 18 9 166 29 11 199 38 12 216 44 13 232 49 15 248 55 16 265 61 18 283 68 20 302 76 22 326 87 27 359 105

8,000 5 108 17 8 151 26 10 180 35 11 195 39 12 209 44 13 223 49 14 238 54 16 253 60 18 269 67 20 288 76 23 312 89

7,500 5 100 15 7 139 24 9 166 32 10 179 36 11 193 40 12 205 45 13 218 50 15 231 55 16 246 61 18 262 69 20 282 79

7,000 4 92 14 7 128 22 8 152 29 9 165 33 10 177 37 11 188 41 12 199 45 13 211 50 15 224 55 16 238 62 18 255 70

6,500 4 84 13 6 117 20 8 139 27 8 151 30 9 161 34 10 172 37 11 182 41 12 193 45 13 204 50 15 216 56 16 230 63

* Based on the climb starting from sea level.

15

CRUISE PERFORMANCE HIGH SPEED CRUISE ISA, Anti-Ice Off  Cruis e 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 40,000 41,000

16

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

8,645 269 1,033 290 992 312 969 333 917 340 843 338 785 337 736 335 687 334 648 332 609 326 565 314 517 302 490

8,000 269 1,026 290 984 312 961 335 917 342 843 340 786 340 737 338 688 338 647 337 609 333 567 323 516 316 491 305 465

7,500 269 1,020 290 979 312 955 337 918 344 843 342 787 342 737 341 688 340 647 340 609 338 569 330 518 324 492 317 468

7,000 269 1,016 290 974 312 949 338 919 345 844 344 788 344 737 343 690 343 647 343 609 342 570 336 520 331 495 326 470

6,500 269 1,011 290 969 312 944 339 919 346 844 346 789 345 737 345 691 345 646 346 609 346 572 341 522 337 497 333 473

CRUISE PERFORMANCE LONG RANGE CRUISE ISA, Anti-Ice Off  Cruis e 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 40,000 41,000

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

8,645 218 788 238 761 253 716 275 671 285 632 289 609 291 586 294 567 300 555 310 550 317 542 314 517 302 490

8,000 210 742 230 718 245 678 266 635 281 607 284 583 287 562 290 541 293 523 300 515 314 519 320 508 316 491 305 465

7,500 205 713 224 687 238 646 259 607 276 584 280 563 284 543 287 523 289 503 294 488 307 493 319 493 322 486 317 468

7,000 200 683 219 662 232 618 252 579 267 553 273 537 280 523 283 504 286 484 289 467 295 460 317 477 321 473 324 466

6,500 195 654 211 626 224 586 246 553 257 521 265 510 273 499 279 483 282 465 285 447 289 436 301 438 316 453 323 453

17

DESCENT PERFORMANCE HIGH SPEED & NORMAL DESCENT ISA, Zero Wind, Anti-Ice Off, Speed Brakes Retracted, Gear & Flaps Up Time, Fuel, and Dist ance To Descend * High Speed – 3,000 FPM Normal – 2,000 FPM Pressure Altitude (ft)

15,000

25,000

27,000

29,000

31,000

33,000

35,000

37,000

39,000

41,000

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

------ End of Cruise Weight (lb) ------

------ End of Cruise Weight (lb) ------

8,000 5 21 23 8 37 40 9 41 44 10 45 48 10 49 52 11 52 56 12 55 61 13 60 66 14 64 72 15 68 78

8,000 8 58 34 13 97 61 14 105 66 15 114 73 16 122 78 17 128 84 18 134 90 19 139 96 20 144 102 21 148 108

* Based on descending to sea level.

18

7,000 5 26 22 8 45 40 9 49 44 10 54 48 10 58 52 11 62 56 12 65 60 13 69 65 14 73 71 15 77 77

6,000 5 32 22 8 55 40 9 59 44 10 64 48 10 69 52 11 73 56 12 76 60 12 80 64 13 83 70 14 88 75

7,000 8 63 34 13 105 61 14 113 66 15 122 73 16 130 78 17 137 84 18 143 90 19 149 96 20 153 102 21 158 108

6,000 8 68 34 13 113 61 14 121 66 15 131 73 16 139 78 17 146 84 18 153 90 19 158 96 20 163 102 21 167 108

RESERVE FUEL RESERVE FUEL ALL OWANCES Based on 1 Pilot / 3 Passengers, ISA, Zero Wind VFR Fuel Reserves (at 15,000 feet) Day (30 minutes) Night (45 minutes)

292lb 445 lb

IFR Fuel Reserves (Alternate plus 45 minutes at 15,000 feet) 100 Nautical Mile Alternate 739 lb 200 Nautical Mile Alternate 933 lb 300 Nautical Mile Alternate 1,078 lb NBAA IFR Reserves * 100 Nautical Mile Alternate 200 Nautical Mile Alternate 300 Nautical Mile Alternate

634 lb 826 lb 968 lb

*NBAA IFR Reserves are defined as the amount of fuel for the following profile: - A 5 minute approach at sea level - Climb to 5,000 feet - A 5 minute hold at 5,000 feet - Climb to cruise altitude for the diversion to the alternate airport - Cruise at long range cruise power - Descend to sea level - Land with 30 minutes of holding fuel at 5,000 feet.

HOLDING PERFORMANCE ISA, Anti-Ice Off, Speed Brakes Retracted, Gear & Flaps Up Holding Speed & Fuel Flow ----------------------------------- Pressure Altitude (ft) -----------------------------------Weight (lb)

8,000 7,500 7,000 6,500 6,000

KIAS 150 140 130 130 130

S.L. 613 574 539 523 508

5,000 10,000 15,000 20,000 25,000 30,000 583 557 532 509 488 468 545 519 494 474 453 434 510 484 459 439 419 403 494 467 442 423 403 386 479 452 426 407 388 371

19

L A N D I N G P E R F OR 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 °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) --------------------------------------------

* 8,645 2,440 2,510 2,550 2,580 2,620 2,660 2,690 2,730 — —

8,000 2,290 2,350 2,380 2,410 2,440 2,470 2,510 2,540 2,580 —

7,500 2,170 2,220 2,250 2,280 2,310 2,340 2,370 2,400 2,430 2,460

7,000 2,060 2,110 2,130 2,160 2,190 2,210 2,240 2,270 2,300 2,330

6,500 1,960 2,000 2,020 2,050 2,070 2,090 2,120 2,140 2,170 2,190

6,000 1,850 1,890 1,910 1,940 1,960 1,980 2,000 2,020 2,050 2,070

44/111

49/120

50/122

50/122

50/122

50/122

98

94

91

88

85

82

Elevation = 1,000 Feet Ambient Temp °C

/

°F

0 / 32 5 / 41 10 / 50 15 / 59 20 / 68 25 / 77 30 / 86 35 / 95 40 / 104 45 / 113 Lndg Wght Temp Limits °C/°F

VREF

(KIAS)

------------------------------------------ Landing Weight (lb) --------------------------------------------

* 8,645 2,510 2,550 2,590 2,620 2,660 2,700 2,740 2,780 2,810 —

8,000 2,350 2,380 2,410 2,440 2,480 2,510 2,550 2,580 2,610 2,650

7,500 2,220 2,250 2,280 2,310 2,340 2,380 2,410 2,440 2,470 2,500

7,000 2,110 2,130 2,160 2,190 2,210 2,240 2,270 2,300 2,330 2,360

6,500 2,000 2,020 2,050 2,070 2,100 2,120 2,150 2,170 2,190 2,220

6,000 1,900 1,920 1,940 1,960 1,980 2,000 2,030 2,050 2,070 2,100

41/106

46/115

47/117

47/117

47/117

47/117

98

94

91

88

85

82

* For use in an emergency. Maximum designed landing weight =8,000 pounds (3,629 kg).

20

L A N D I N G P E R F OR 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 °C

/

°F

0 / 32 5 / 41 10 / 50 15 / 59 20 / 68 25 / 77 30 / 86 35 / 95 40 / 104 45 / 113 Lndg Wght Temp Limits °C/°F

VREF

(KIAS)

------------------------------------------ Landing Weight (lb) --------------------------------------------

* 8,645 2,590 2,620 2,660 2,700 2,740 2,780 2,820 2,860 — —

8,000 2,410 2,450 2,480 2,510 2,550 2,590 2,620 2,660 2,690 —

7,500 2,290 2,320 2,350 2,380 2,410 2,440 2,470 2,510 2,540 2,570

7,000 2,160 2,190 2,220 2,240 2,270 2,300 2,330 2,370 2,400 2,420

6,500 2,050 2,070 2,100 2,120 2,150 2,170 2,200 2,220 2,250 2,280

6,000 1,940 1,960 1,980 2,000 2,030 2,050 2,080 2,100 2,120 2,150

36/97

42/108

45/113

45/113

45/113

45/113

98

94

91

88

85

82

Elevation = 3,000 Feet Ambient Temp °C

/

°F

-5 / 23 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)

------------------------------------------ Landing Weight (lb) --------------------------------------------

* 8,645 2,630 2,670 2,710 2,740 2,780 2,820 2,870 2,910 — —

8,000 2,450 2,480 2,520 2,550 2,590 2,620 2,660 2,700 2,740 —

7,500 2,320 2,350 2,380 2,410 2,440 2,480 2,510 2,550 2,580 2,610

7,000 2,190 2,220 2,250 2,280 2,310 2,340 2,370 2,400 2,430 2,460

6,500 2,080 2,100 2,130 2,150 2,170 2,200 2,220 2,250 2,280 2,310

6,000 1,970 1,990 2,010 2,030 2,050 2,080 2,100 2,130 2,150 2,180

32/90

38/100

43/109

43/109

43/109

43/109

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 OR 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 °C

/

°F

-5 / 23 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)

------------------------------------------ Landing Weight (lb) --------------------------------------------

* 8,645 2,710 2,750 2,790 2,830 2,870 2,920 2,960 — — —

8,000 2,520 2,560 2,590 2,630 2,660 2,700 2,740 2,780 — —

7,500 2,390 2,420 2,450 2,480 2,520 2,550 2,590 2,620 2,660 —

7,000 2,250 2,280 2,310 2,340 2,370 2,400 2,430 2,470 2,500 2,530

6,500 2,130 2,150 2,180 2,200 2,230 2,260 2,280 2,310 2,340 2,370

6,000 2,010 2,030 2,060 2,080 2,110 2,130 2,160 2,180 2,200 2,230

28/82

34/93

39/102

40/104

40/104

40/104

98

94

91

88

85

82

Elevation = 5,000 Feet Ambient Temp °C

/

-10 / -5 / 0/ 5/ 10 / 15 / 20 / 25 / 30 / 35 /

°F

14 23 32 41 50 59 68 77 86 95

Lndg Wght Temp Limits °C/°F

VREF

(KIAS)

------------------------------------------ Landing Weight (lb) --------------------------------------------

* 8,645 2,750 2,800 2,830 2,880 2,920 2,970 3,010 — — —

8,000 2,560 2,600 2,630 2,670 2,710 2,750 2,790 2,830 2,870 —

7,500 2,420 2,450 2,490 2,520 2,560 2,590 2,620 2,660 2,700 2,740

7,000 2,280 2,320 2,350 2,380 2,410 2,440 2,470 2,500 2,540 2,570

6,500 2,160 2,180 2,210 2,230 2,260 2,290 2,320 2,350 2,380 2,410

6,000 2,040 2,060 2,090 2,110 2,130 2,160 2,180 2,210 2,230 2,260

24/75

30/86

35/95

38/100

38/100

38/100

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 OR 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 °C

/

-10 / -5 / 0/ 5/ 10 / 15 / 20 / 25 / 30 / 35 /

°F

14 23 32 41 50 59 68 77 86 95

Lndg Wght Temp Limits °C/°F

VREF

(KIAS)

------------------------------------------ Landing Weight (lb) --------------------------------------------

* 8,645 2,850 2,890 2,940 2,980 3,020 3,070 3,120 — — —

8,000 2,650 2,680 2,720 2,760 2,800 2,840 2,880 2,920 — —

7,500 2,500 2,530 2,570 2,600 2,640 2,670 2,710 2,750 2,790 —

7,000 2,360 2,390 2,420 2,450 2,480 2,520 2,550 2,590 2,620 2,650

6,500 2,220 2,240 2,270 2,300 2,330 2,360 2,390 2,420 2,450 2,480

6,000 2,100 2,120 2,150 2,170 2,190 2,220 2,240 2,270 2,300 2,320

20/68

26/79

31/88

36/97

36/97

36/97

98

94

91

88

85

82

Elevation = 7,000 Feet Ambient Temp °C

/

-15 / -10 / -5 / 0/ 5/ 10 / 15 / 20 / 25 / 30 /

°F

5 14 23 32 41 50 59 68 77 86

Lndg Wght Temp Limits °C/°F

VREF

(KIAS)

------------------------------------------ Landing Weight (lb) --------------------------------------------

* 8,645 2,910 2,950 3,000 3,040 3,090 3,140 3,190 — — —

8,000 2,700 2,740 2,780 2,820 2,860 2,900 2,940 2,980 — —

7,500 2,550 2,580 2,620 2,650 2,690 2,730 2,770 2,800 2,840 —

7,000 2,400 2,430 2,470 2,500 2,530 2,570 2,600 2,630 2,670 2,700

6,500 2,250 2,280 2,310 2,340 2,370 2,400 2,430 2,460 2,500 2,530

6,000 2,130 2,160 2,180 2,210 2,230 2,260 2,280 2,310 2,340 2,360

17/63

22/72

28/82

33/91

33/91

33/91

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 OR 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 °C

/

-15 / -10 / -5 / 0/ 5/ 10 / 15 / 20 / 25 / 30 /

------------------------------------------ Landing Weight (lb) --------------------------------------------

°F

5 14 23 32 41 50 59 68 77 86

* 8,645 3,010 3,060 3,110 3,160 3,210 3,250 — — — —

8,000 2,790 2,830 2,870 2,920 2,960 3,000 3,040 — — —

7,500 2,630 2,670 2,710 2,740 2,780 2,820 2,860 2,900 — —

7,000 2,480 2,510 2,550 2,580 2,610 2,650 2,680 2,720 2,760 —

6,500 2,330 2,360 2,390 2,420 2,450 2,480 2,510 2,540 2,580 2,610

6,000 2,190 2,220 2,250 2,270 2,300 2,320 2,350 2,380 2,400 2,430

13/55

19/66

24/75

29/84

31/88

31/88

98

94

91

88

85

82

Lndg Wght Temp Limits °C/°F

VREF

(KIAS)

* For use in an emergency. Maximum designed landing weight =8,000 pounds (3,629 kg).

S T A L L S P EE D S Stall Warning-Normal, Zero Angle of Bank, Landing Gear Up or Down, Anti-Ice Off, KCAS Stall Speeds ---------------------- Flap Position ---------------------Weight (lb)

8,645 8,000 7,500 7,000 6,500 6,000

24

Land 76 73 71 68 66 63

15° 81 78 76 73 71 68

Up 91 87 85 82 79 76

MI SSION PL A N N IN 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 170 KIAS / M 0.44 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: Typical Cruise Altitude (ft) Distance (nm) 0 - 99 6,000 - 15,000 100 - 199 14,000 - 26,000 200 - 299 25,000 - 34,000 300 - 499 33,000 - 38,000 500 - 899 36,000 - 40,000 901 + 39,000 - 41,000 Wind Corr ection Factors *  True Airspeed (kt)

280 290 300 310 320 330 340

-------------- Headwinds (kt) --------------

100 1.55 1.53 1.50 1.48 1.45 1.43 1.42

75 1.37 1.35 1.33 1.32 1.31 1.29 1.28

50 1.22 1.21 1.20 1.19 1.19 1.18 1.17

25 1.10 1.09 1.09 1.09 1.08 1.08 1.08

--------------- Tailwinds (kt) ---------------

0 1.00 1.00 1.00 1.00 1.00 1.00 1.00

25 0.92 0.92 0.92 0.93 0.93 0.93 0.93

* Wind Correction Factor is calculated as KTAS divided by the sum of KTAS

50 0.85 0.85 0.86 0.86 0.86 0.87 0.87 ±

75 0.79 0.79 0.80 0.81 0.81 0.81 0.82

100 0.74 0.74 0.75 0.76 0.76 0.77 0.77

wind component

25

MI SSION PL A N N IN G FLIGHT TIME & FUEL BURN ------------------------------------------------- Cruise Altitude (ft) -------------------------------------------------

15,000 Dist (nm)

 Time (min)

Fuel (lb)

25,000  Time (min)

Fuel (lb)

27,000  Time (min)

Fuel (lb)

29,000  Time (min)

Fuel (lb)

31,000  Time (min)

Fuel (lb)

100

0:22

375

0:22

336

0:22

330

150

0:31

529

0:30

460

0:31

446

0:31

436

0:31

426

200

0:41

683

0:39

584

0:40

562

0:40

545

0:40

528

250

0:51

837

0:48

708

0:49

678

0:49

654

0:49

631

300

1:00

990

0:57

832

0:58

795

0:58

764

0:58

733

350

1:10 1,144

1:06

956

1:06

912

1:07

873

1:07

836

400

1:20 1,299

1:15 1,080

1:15 1,030

1:16

982

1:16

939

450

1:29 1,455

1:23 1,205

1:24 1,147

1:25 1,092

1:25 1,042

500

1:39 1,611

1:32 1,329

1:33 1,264

1:33 1,201

1:33 1,145

600

1:50 1,579

1:51 1,499

1:51 1,422

1:51 1,351

700

2:08 1,831

2:08 1,734

2:09 1,643

2:09 1,558

800 900 1,000 1,100 1,123

26

Assumptions: • 170 KIAS / M 0.44 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 (634 lb) Reserves are not included in the fuel burn figures

FOR SELECTED DISTANCES ------------------------------------------------- Cruise Altitude (ft) -------------------------------------------------

33,000  Time (min)

Fuel (lb)

35,000  Time (min)

Fuel (lb)

37,000  Time (min)

Fuel (lb)

39,000  Time (min)

Fuel (lb)

41,000  Time (min)

Fuel (lb)

Dist (nm)

100 0:32

419

0:32

413

0:33

409

150

0:40

515

0:41

503

0:42

494

0:42

483

0:43

477

200

0:49

611

0:50

594

0:51

580

0:51

562

0:52

551

250

0:58

708

0:59

685

0:59

666

1:00

642

1:01

626

300

1:07

805

1:08

777

1:08

751

1:09

722

1:11

700

350

1:16

902

1:17

868

1:17

837

1:19

802

1:20

775

400

1:25

999

1:26

960

1:26

923

1:28

883

1:30

851

450

963

1:39

926

500

1:33 1,097

1:35 1,052

1:35 1,010

1:37

1:51 1,293

1:52 1,237

1:53 1,183

1:55 1,125

1:58 1,078

600

2:09 1,489

2:10 1,421

2:11 1,357

2:14 1,288

2:18 1,231

700

2:27 1,685

2:28 1,606

2:29 1,531

2:32 1,452

2:37 1,386

800

2:45 1,881

2:46 1,792

2:48 1,707

2:51 1,616

2:57 1,542

900

3:06 1,883

3:09 1,781

3:16 1,699 1,000 3:37 1,859 1,100 3:41 1,896 1,123

27

MI SSION PL A N N IN G RANGE / PAYLOAD CAPABILITY NBAA IFR Reserves (100 nm), ISA, Zero Wind, High-Speed Cruise 1,200

1,000

        )       s         d       n       u       o       p         (

   d   a   o    l   y   a    P

800

600

400

200

0 0

200

400

600

800

1,000

NBAA IFR Range (nautical miles)

Assumptions: Single Pilot Cruise at FL 410

28

1,200

1,400