May 2010
TABLE OF CONTENTS This Flight Planning Guide is published for the purpose of providing specific information for evaluating the performance of the Cessna Corvalis TT. This guide is developed from data contained in the Cessna Corvalis TT Pilot's Operating Handbook. This document is not to be used in place of the FAA approved Pilot's Operating Handbook. The data included herein does not constitute an offer and is subject to change without notice. Section Page Specifications...2 Takeoff Performance Takeoff Speeds...4 Takeoff Field Length...5 Climb Performance...11 Cruise Performance...12 Descent Performance...13 Landing Performance...14 Stall Speeds...20 Mission Planning Wind Correction Factors...20 Flight Time & Fuel Burn...21 Range / Payload Capability...22 POH Revision Level/Date: I/10-22-2008 1
SPECIFICATIONS General Certification Status 14 CFR Part 23 Engine Manufacturer Model Thrust Output at S.L. (each) Overhaul Interval (TBO) Propeller Manufacturer Description Teledyne Continental TSIO-550-C 310 hp 2,000 hours Hartzell 3 blade, constant speed Exterior Dimensions Length 25 ft 4 in 7.72 m Height 9 ft 0 in 2.74 m Wing Span 35 ft 10 in 10.91 m Cabin Dimensions (with typical interior installed) Length 11 ft 8 in 3.54 m Height 49 in 1.24 m Width 49 in 1.24 m Accommodations Passenger Seats 4 Baggage Capacity 25 ft 3 0.7 m 3 120 lb 54 kg Altitudes Certified Ceiling 25,000 ft 7,620 m 2
SPECIFICATIONS Basic Performance Takeoff Distance - Sea Level, ISA, MTOW - Ground Roll 1,300 ft 396 m - To 50 feet 1,900 ft 579 m Landing Distance, Sea Level, ISA, MLW - Ground Roll 1,250 ft 381 m - From 50 feet 2,600 ft 792 m Rate of Climb 1,400 fpm 427 m Airspeed Limitations Maximum Operating Maneuvering Speed (V O ) 2,600 Pounds Gross Weight 135 KIAS 250 km/hr 3,600 Pounds Gross Weight 158 KIAS 293 km/hr Maximum Flap Extended Speed (V FE ) 117 KIAS 217 km/hr Maximum Structural Cruising Speed (V NO ) 181 KIAS 335 km/hr Never Exceed Speed (V NE ) 230 KIAS 426 km/hr Certified Weights Maximum Ramp Weight 3,600 lb 1,633 kg Maximum Takeoff Weight 3,600 lb 1,633 kg Maximum Landing Weight 3,420 lb 1,551 kg Maximum Zero Fuel Weight 3,300 lb 1,497 kg Maximum Fuel Capacity (6 lb/gal) 612 lb 278 kg Typically-Equipped Empty Weight 2,550 lb 1,157 kg Payload Useful Payload and Fuel 1,050 lb 476 kg Maximum Payload 750 lb 340 kg Payload at Full Fuel 438 lb 199 kg 3
TAKEOFF PERFORMANCE The Cessna Corvalis TT is certified to 14 CFR Part 23 Utility category rules. The takeoff distances reflected in the Pilot's Operating Handbook and this guide include both the ground roll and the distance to 50 feet above the surface. Flaps are in the takeoff position at 12. A paved, level, dry runway with zero wind is assumed. TAKEOFF SPEEDS Sea Level, Dry Runway, ISA, Zero Wind, KIAS Takeoff Weight (lb) Rotation Speed V R Speed at 50 ft 3,600 65 82 3,400 63 80 3,200 61 78 3,000 59 76 4
TAKEOFF PERFORMANCE SHORT FIELD TAKEOFF DISTANCE (in feet) FLAPS 12 Paved, Level, Dry Runway; Zero Wind Elevation = Sea Level Takeoff Weight Ambient Temp 3,600 lb 3,400 lb C / F Ground Roll To 50 ft Ground Roll To 50 ft -10 / 14 1,085 1,656 965 1,506-5 / 23 1,123 1,704 1,000 1,550 0 / 32 1,162 1,752 1,035 1,594 5 / 41 1,200 1,800 1,070 1,638 10 / 50 1,241 1,851 1,109 1,686 15 / 59 1,282 1,902 1,147 1,734 20 / 68 1,323 1,953 1,186 1,782 25 / 77 1,364 2,005 1,225 1,831 30 / 86 1,415 2,069 1,270 1,888 35 / 95 1,473 2,142 1,320 1,950 40 / 104 1,532 2,215 1,370 2,013 Takeoff Weight Ambient Temp 3,200 lb 3,000 lb C / F Ground Roll To 50 ft Ground Roll To 50 ft -10 / 14 845 1,356 725 1,206-5 / 23 877 1,396 753 1,242 0 / 32 908 1,435 782 1,277 5 / 41 940 1,475 810 1,313 10 / 50 976 1,520 844 1,355 15 / 59 1,013 1,566 878 1,398 20 / 68 1,049 1,611 912 1,440 25 / 77 1,085 1,657 946 1,483 30 / 86 1,125 1,706 980 1,525 35 / 95 1,167 1,758 1,013 1,567 40 / 104 1,208 1,810 1,047 1,608 5
TAKEOFF PERFORMANCE SHORT FIELD TAKEOFF DISTANCE (in feet) FLAPS 12 Paved, Level, Dry Runway; Zero Wind Elevation = 2,000 Feet Takeoff Weight Ambient Temp 3,600 lb 3,400 lb C / F Ground Roll To 50 ft Ground Roll To 50 ft -10 / 14 1,177 1,771 1,049 1,611-5 / 23 1,218 1,823 1,087 1,659 0 / 32 1,263 1,879 1,130 1,712 5 / 41 1,308 1,935 1,172 1,765 10 / 50 1,353 1,991 1,215 1,818 15 / 59 1,402 2,053 1,259 1,874 20 / 68 1,457 2,122 1,306 1,933 25 / 77 1,513 2,191 1,354 1,992 30 / 86 1,568 2,260 1,401 2,051 35 / 95 1,624 2,329 1,450 2,113 40 / 104 1,679 2,399 1,500 2,175 Takeoff Weight Ambient Temp 3,200 lb 3,000 lb C / F Ground Roll To 50 ft Ground Roll To 50 ft -10 / 14 921 1,451 793 1,291-5 / 23 956 1,495 825 1,331 0 / 32 996 1,545 863 1,378 5 / 41 1,036 1,595 900 1,425 10 / 50 1,076 1,645 938 1,472 15 / 59 1,116 1,695 973 1,516 20 / 68 1,155 1,744 1,004 1,555 25 / 77 1,195 1,793 1,036 1,595 30 / 86 1,234 1,843 1,067 1,634 35 / 95 1,276 1,896 1,103 1,679 40 / 104 1,321 1,951 1,141 1,726 6
TAKEOFF PERFORMANCE SHORT FIELD TAKEOFF DISTANCE (in feet) FLAPS 12 Paved, Level, Dry Runway; Zero Wind Elevation = 4,000 Feet Takeoff Weight Ambient Temp 3,600 lb 3,400 lb C / F Ground Roll To 50 ft Ground Roll To 50 ft -10 / 14 1,290 1,913 1,155 1,744-5 / 23 1,335 1,969 1,198 1,797 0 / 32 1,380 2,025 1,240 1,850 5 / 41 1,438 2,098 1,290 1,913 10 / 50 1,497 2,171 1,340 1,975 15 / 59 1,555 2,244 1,390 2,038 20 / 68 1,611 2,314 1,439 2,099 25 / 77 1,664 2,380 1,486 2,158 30 / 86 1,717 2,446 1,533 2,217 35 / 95 1,769 2,512 1,581 2,276 40 / 104 1,824 2,580 1,631 2,339 Takeoff Weight Ambient Temp 3,200 lb 3,000 lb C / F Ground Roll To 50 ft Ground Roll To 50 ft -10 / 14 1,020 1,575 885 1,406-5 / 23 1,060 1,625 923 1,453 0 / 32 1,100 1,675 960 1,500 5 / 41 1,142 1,727 993 1,542 10 / 50 1,183 1,779 1,027 1,583 15 / 59 1,225 1,831 1,060 1,625 20 / 68 1,267 1,883 1,094 1,668 25 / 77 1,308 1,935 1,131 1,713 30 / 86 1,350 1,988 1,167 1,758 35 / 95 1,392 2,040 1,203 1,803 40 / 104 1,438 2,097 1,245 1,856 7
TAKEOFF PERFORMANCE SHORT FIELD TAKEOFF DISTANCE (in feet) FLAPS 12 Paved, Level, Dry Runway; Zero Wind Elevation = 6,000 Feet Takeoff Weight Ambient Temp 3,600 lb 3,400 lb C / F Ground Roll To 50 ft Ground Roll To 50 ft -10 / 14 1,403 2,054 1,260 1,875-5 / 23 1,462 2,127 1,310 1,938 0 / 32 1,520 2,200 1,360 2,000 5 / 41 1,578 2,273 1,410 2,063 10 / 50 1,638 2,347 1,463 2,128 15 / 59 1,697 2,421 1,516 2,195 20 / 68 1,756 2,495 1,569 2,261 25 / 77 1,819 2,574 1,627 2,333 30 / 86 1,885 2,656 1,688 2,409 35 / 95 1,951 2,738 1,748 2,486 40 / 104 2,015 2,818 1,807 2,558 Takeoff Weight Ambient Temp 3,200 lb 3,000 lb C / F Ground Roll To 50 ft Ground Roll To 50 ft -10 / 14 1,117 1,696 973 1,517-5 / 23 1,158 1,748 1,007 1,558 0 / 32 1,200 1,800 1,040 1,600 5 / 41 1,242 1,852 1,073 1,642 10 / 50 1,288 1,909 1,113 1,691 15 / 59 1,334 1,968 1,153 1,741 20 / 68 1,381 2,027 1,194 1,792 25 / 77 1,434 2,092 1,241 1,851 30 / 86 1,490 2,163 1,293 1,916 35 / 95 1,546 2,233 1,344 1,980 40 / 104 1,599 2,299 1,391 2,039 8
TAKEOFF PERFORMANCE SHORT FIELD TAKEOFF DISTANCE (in feet) FLAPS 12 Paved, Level, Dry Runway; Zero Wind Elevation = 8,000 Feet Takeoff Weight Ambient Temp 3,600 lb 3,400 lb C / F Ground Roll To 50 ft Ground Roll To 50 ft -10 / 14 1,565 2,257 1,399 2,049-5 / 23 1,624 2,329 1,450 2,113 0 / 32 1,679 2,399 1,500 2,175 5 / 41 1,735 2,469 1,550 2,238 10 / 50 1,794 2,543 1,603 2,304 15 / 59 1,864 2,630 1,668 2,385 20 / 68 1,934 2,718 1,733 2,466 25 / 77 2,004 2,805 1,797 2,547 30 / 86 2,074 2,893 1,859 2,624 35 / 95 2,144 2,980 1,921 2,701 40 / 104 2,214 3,068 1,982 2,778 Takeoff Weight Ambient Temp 3,200 lb 3,000 lb C / F Ground Roll To 50 ft Ground Roll To 50 ft -10 / 14 1,232 1,840 1,066 1,632-5 / 23 1,276 1,896 1,103 1,679 0 / 32 1,321 1,951 1,141 1,726 5 / 41 1,365 2,006 1,179 1,774 10 / 50 1,412 2,065 1,221 1,826 15 / 59 1,472 2,140 1,276 1,895 20 / 68 1,532 2,215 1,331 1,964 25 / 77 1,591 2,288 1,384 2,030 30 / 86 1,644 2,355 1,429 2,086 35 / 95 1,697 2,422 1,474 2,143 40 / 104 1,751 2,488 1,519 2,199 9
TAKEOFF PERFORMANCE SHORT FIELD TAKEOFF DISTANCE (in feet) FLAPS 12 Paved, Level, Dry Runway; Zero Wind Elevation = 10,000 Feet Takeoff Weight Ambient Temp 3,600 lb 3,400 lb C / F Ground Roll To 50 ft Ground Roll To 50 ft -10 / 14 1,735 2,469 1,550 2,238-5 / 23 1,794 2,543 1,603 2,304 0 / 32 1,864 2,630 1,668 2,385 5 / 41 1,934 2,718 1,733 2,466 10 / 50 2,003 2,804 1,797 2,546 15 / 59 2,069 2,886 1,854 2,618 20 / 68 2,134 2,968 1,912 2,690 25 / 77 2,200 3,050 1,970 2,763 30 / 86 2,266 3,132 2,028 2,835 Takeoff Weight Ambient Temp 3,200 lb 3,000 lb C / F Ground Roll To 50 ft Ground Roll To 50 ft -10 / 14 1,365 2,006 1,179 1,774-5 / 23 1,412 2,065 1,221 1,826 0 / 32 1,472 2,140 1,276 1,895 5 / 41 1,532 2,215 1,331 1,964 10 / 50 1,590 2,288 1,383 2,029 15 / 59 1,640 2,350 1,426 2,082 20 / 68 1,690 2,413 1,468 2,135 25 / 77 1,740 2,475 1,510 2,188 30 / 86 1,790 2,538 1,552 2,240 10
CLIMB PERFORMANCE TIME, FUEL, AND DISTANCE TO CLIMB ISA, Zero Wind Pressure Time Fuel Distance Altitude (ft) (min) (gal) (nm) 2,000 1.4 0.9 3 4,000 2.9 1.9 5 6,000 4.3 2.8 8 8,000 5.7 3.7 11 10,000 7.1 4.6 14 12,000 8.6 5.6 17 14,000 10.0 6.5 21 16,000 11.5 7.5 24 18,000 13.0 8.5 28 20,000 14.6 9.5 32 22,000 16.4 10.7 36 24,000 18.4 11.9 42 25,000 19.5 12.7 45 11
CRUISE PERFORMANCE CRUISE SPEED & FUEL FLOW ISA Pressure Altitude (ft) 2,000 KTAS lb/hr 4,000 KTAS lb/hr 6,000 KTAS lb/hr 8,000 KTAS lb/hr 10,000 KTAS lb/hr 12,000 KTAS lb/hr 14,000 KTAS lb/hr 16,000 KTAS lb/hr 18,000 KTAS lb/hr 20,000 KTAS lb/hr 22,000 KTAS lb/hr 24,000 KTAS lb/hr 25,000 KTAS lb/hr Power Setting Best -50 Power LOP 55% 185 177 157 138 101 78 189 180 160 138 101 78 192 184 163 138 101 78 199 190 168 144 101 78 204 194 171 144 101 78 207 197 174 144 101 78 212 203 179 144 101 78 216 207 184 144 101 78 219 211 191 150 101 78 222 214 195 150 101 78 228 219 200 150 101 78 232 225 206 150 101 78 235 227 208 150 101 78 12
DESCENT PERFORMANCE TIME, FUEL, AND DISTANCE TO DESCEND ISA, Zero Wind Pressure Time Fuel Distance Altitude (ft) (min) (gal) (nm) 2,000 4 1 16 4,000 8 2 32 6,000 12 4 47 8,000 16 5 62 10,000 20 6 76 12,000 24 7 90 14,000 28 8 104 16,000 32 9 118 18,000 36 10 131 20,000 40 12 144 22,000 44 13 157 24,000 48 14 169 25,000 50 14 175 13
LANDING PERFORMANCE SHORT FIELD LANDING DISTANCE (in feet) FLAPS 40 Paved, Level, Dry Runway; Zero Wind Elevation = Sea Level Landing Weight Ambient Temp 3,420 lb 3,200 lb C / F Ground Roll From 50 ft Ground Roll From 50 ft -10 / 14 1,157 2,470 1,096 2,355-5 / 23 1,177 2,506 1,113 2,388 0 / 32 1,196 2,543 1,131 2,422 5 / 41 1,215 2,578 1,150 2,456 10 / 50 1,234 2,613 1,168 2,490 15 / 59 1,252 2,648 1,186 2,524 20 / 68 1,271 2,683 1,204 2,558 25 / 77 1,289 2,718 1,222 2,592 30 / 86 1,308 2,753 1,240 2,626 35 / 95 1,327 2,787 1,258 2,660 40 / 104 1,345 2,822 1,276 2,694 Landing Weight Ambient Temp 3,000 lb 2,800 lb C / F Ground Roll From 50 ft Ground Roll From 50 ft -10 / 14 1,034 2,240 973 2,125-5 / 23 1,050 2,270 987 2,152 0 / 32 1,067 2,301 1,002 2,180 5 / 41 1,084 2,333 1,019 2,211 10 / 50 1,102 2,366 1,036 2,243 15 / 59 1,119 2,400 1,053 2,275 20 / 68 1,137 2,433 1,070 2,307 25 / 77 1,155 2,466 1,087 2,339 30 / 86 1,172 2,499 1,105 2,372 35 / 95 1,190 2,532 1,122 2,404 40 / 104 1,208 2,565 1,139 2,436 14
LANDING PERFORMANCE SHORT FIELD LANDING DISTANCE (in feet) FLAPS 40 Paved, Level, Dry Runway; Zero Wind Elevation = 2,000 Feet Landing Weight Ambient Temp 3,420 lb 3,200 lb C / F Ground Roll From 50 ft Ground Roll From 50 ft -10 / 14 1,236 2,618 1,168 2,490-5 / 23 1,253 2,649 1,186 2,524 0 / 32 1,273 2,687 1,206 2,561 5 / 41 1,293 2,724 1,226 2,598 10 / 50 1,313 2,762 1,245 2,635 15 / 59 1,333 2,800 1,265 2,672 20 / 68 1,354 2,838 1,285 2,709 25 / 77 1,374 2,876 1,304 2,746 30 / 86 1,395 2,916 1,325 2,784 35 / 95 1,422 2,967 1,349 2,830 40 / 104 1,449 3,017 1,374 2,875 Landing Weight Ambient Temp 3,000 lb 2,800 lb C / F Ground Roll From 50 ft Ground Roll From 50 ft -10 / 14 1,100 2,363 1,032 2,236-5 / 23 1,120 2,400 1,053 2,276 0 / 32 1,139 2,436 1,072 2,311 5 / 41 1,158 2,472 1,091 2,346 10 / 50 1,177 2,508 1,109 2,380 15 / 59 1,196 2,544 1,128 2,415 20 / 68 1,216 2,579 1,146 2,450 25 / 77 1,235 2,615 1,165 2,485 30 / 86 1,254 2,652 1,184 2,520 35 / 95 1,276 2,693 1,203 2,556 40 / 104 1,298 2,734 1,222 2,592 15
LANDING PERFORMANCE SHORT FIELD LANDING DISTANCE (in feet) FLAPS 40 Paved, Level, Dry Runway; Zero Wind Elevation = 4,000 Feet Landing Weight Ambient Temp 3,420 lb 3,200 lb C / F Ground Roll From 50 ft Ground Roll From 50 ft -10 / 14 1,315 2,765 1,247 2,638-5 / 23 1,337 2,807 1,268 2,678 0 / 32 1,359 2,848 1,290 2,719 5 / 41 1,381 2,889 1,311 2,759 10 / 50 1,404 2,933 1,333 2,799 15 / 59 1,428 2,978 1,355 2,840 20 / 68 1,452 3,022 1,376 2,880 25 / 77 1,476 3,067 1,398 2,921 30 / 86 1,500 3,112 1,419 2,961 35 / 95 1,524 3,156 1,441 3,001 40 / 104 1,548 3,201 1,463 3,042 Landing Weight Ambient Temp 3,000 lb 2,800 lb C / F Ground Roll From 50 ft Ground Roll From 50 ft -10 / 14 1,179 2,511 1,111 2,383-5 / 23 1,200 2,550 1,131 2,422 0 / 32 1,221 2,589 1,152 2,460 5 / 41 1,242 2,628 1,172 2,498 10 / 50 1,262 2,666 1,190 2,532 15 / 59 1,281 2,702 1,207 2,564 20 / 68 1,300 2,738 1,224 2,596 25 / 77 1,320 2,774 1,241 2,628 30 / 86 1,339 2,810 1,258 2,660 35 / 95 1,358 2,846 1,275 2,692 40 / 104 1,378 2,883 1,293 2,724 16
LANDING PERFORMANCE SHORT FIELD LANDING DISTANCE (in feet) FLAPS 40 Paved, Level, Dry Runway; Zero Wind Elevation = 6,000 Feet Landing Weight Ambient Temp 3,420 lb 3,200 lb C / F Ground Roll From 50 ft Ground Roll From 50 ft -10 / 14 1,405 2,934 1,334 2,800-5 / 23 1,430 2,981 1,356 2,843 0 / 32 1,455 3,028 1,379 2,885 5 / 41 1,480 3,075 1,401 2,927 10 / 50 1,505 3,121 1,424 2,970 15 / 59 1,530 3,168 1,447 3,012 20 / 68 1,555 3,215 1,469 3,054 25 / 77 1,580 3,262 1,492 3,097 30 / 86 1,605 3,309 1,515 3,139 35 / 95 1,630 3,355 1,537 3,181 40 / 104 1,655 3,402 1,560 3,224 Landing Weight Ambient Temp 3,000 lb 2,800 lb C / F Ground Roll From 50 ft Ground Roll From 50 ft -10 / 14 1,262 2,667 1,191 2,533-5 / 23 1,282 2,705 1,209 2,566 0 / 32 1,303 2,742 1,226 2,600 5 / 41 1,323 2,780 1,244 2,633 10 / 50 1,343 2,818 1,262 2,667 15 / 59 1,363 2,856 1,280 2,700 20 / 68 1,384 2,894 1,298 2,734 25 / 77 1,404 2,932 1,316 2,767 30 / 86 1,424 2,970 1,334 2,800 35 / 95 1,444 3,008 1,351 2,834 40 / 104 1,465 3,046 1,369 2,867 17
LANDING PERFORMANCE SHORT FIELD LANDING DISTANCE (in feet) FLAPS 40 Paved, Level, Dry Runway; Zero Wind Elevation = 8,000 Feet Landing Weight Ambient Temp 3,420 lb 3,200 lb C / F Ground Roll From 50 ft Ground Roll From 50 ft -10 / 14 1,512 3,134 1,430 2,981-5 / 23 1,539 3,185 1,455 3,028 0 / 32 1,567 3,237 1,480 3,075 5 / 41 1,594 3,289 1,505 3,121 10 / 50 1,621 3,338 1,530 3,168 15 / 59 1,647 3,387 1,555 3,215 20 / 68 1,673 3,435 1,580 3,262 25 / 77 1,699 3,484 1,605 3,309 30 / 86 1,724 3,532 1,630 3,355 35 / 95 1,750 3,581 1,655 3,402 40 / 104 1,776 3,629 1,680 3,449 Landing Weight Ambient Temp 3,000 lb 2,800 lb C / F Ground Roll From 50 ft Ground Roll From 50 ft -10 / 14 1,348 2,828 1,267 2,675-5 / 23 1,371 2,870 1,287 2,712 0 / 32 1,393 2,912 1,306 2,749 5 / 41 1,416 2,954 1,326 2,786 10 / 50 1,439 2,998 1,349 2,828 15 / 59 1,463 3,043 1,372 2,872 20 / 68 1,487 3,088 1,395 2,915 25 / 77 1,511 3,133 1,418 2,958 30 / 86 1,536 3,179 1,441 3,002 35 / 95 1,560 3,224 1,464 3,045 40 / 104 1,584 3,269 1,487 3,088 18
LANDING PERFORMANCE SHORT FIELD LANDING DISTANCE (in feet) FLAPS 40 Paved, Level, Dry Runway; Zero Wind Elevation = 10,000 Feet Landing Weight Ambient Temp 3,420 lb 3,200 lb C / F Ground Roll From 50 ft Ground Roll From 50 ft -10 / 14 1,628 3,352 1,537 3,181-5 / 23 1,656 3,404 1,564 3,232 0 / 32 1,684 3,456 1,591 3,282 5 / 41 1,712 3,509 1,618 3,333 10 / 50 1,740 3,561 1,645 3,383 15 / 59 1,768 3,614 1,672 3,434 20 / 68 1,796 3,666 1,699 3,484 25 / 77 1,824 3,718 1,726 3,535 30 / 86 1,852 3,771 1,753 3,586 35 / 95 1,880 3,823 1,780 3,636 40 / 104 1,908 3,876 1,807 3,687 Landing Weight Ambient Temp 3,000 lb 2,800 lb C / F Ground Roll From 50 ft Ground Roll From 50 ft -10 / 14 1,446 3,011 1,355 2,841-5 / 23 1,472 3,060 1,380 2,887 0 / 32 1,498 3,108 1,405 2,934 5 / 41 1,524 3,157 1,430 2,981 10 / 50 1,550 3,206 1,455 3,028 15 / 59 1,576 3,254 1,480 3,075 20 / 68 1,602 3,303 1,505 3,121 25 / 77 1,628 3,352 1,530 3,168 30 / 86 1,654 3,400 1,555 3,215 35 / 95 1,680 3,449 1,580 3,262 40 / 104 1,706 3,498 1,605 3,309 19
STALL SPEEDS 3,600 lb, KCAS ---------------------- Flap Position ---------------------- Bank Angle Cruise 12 (Takeoff) 40 (Landing) 0 73 66 60 30 78 71 65 45 87 79 72 60 103 94 85 MISSION PLANNING 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 takeoff, climb, cruise, and descent. 45 minute fuel reserves are considered in each case but are not included in the fuel burn figure. The mission planning table reflects a power setting of -50 LOP. 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. Wind Correction Factors * True Airspeed -------------- Headwinds (kt) -------------- --------------- Tailwinds (kt) --------------- (kt) 100 75 50 25 0 25 50 75 100 160 2.67 1.88 1.45 1.19 1.00 0.86 0.76 0.68 0.62 170 2.43 1.79 1.42 1.17 1.00 0.87 0.77 0.69 0.63 180 2.25 1.71 1.38 1.16 1.00 0.88 0.78 0.71 0.64 190 2.11 1.65 1.36 1.15 1.00 0.88 0.79 0.72 0.66 200 2.00 1.60 1.33 1.14 1.00 0.89 0.80 0.73 0.67 210 1.91 1.56 1.31 1.14 1.00 0.89 0.81 0.74 0.68 220 1.83 1.52 1.29 1.13 1.00 0.90 0.81 0.75 0.69 230 1.77 1.48 1.28 1.12 1.00 0.90 0.82 0.75 0.70 * Wind Correction Factor is calculated as KTAS divided by the sum of KTAS ± wind component 20
MISSION PLANNING FLIGHT TIME & FUEL BURN FOR SELECTED DISTANCES ISA, zero wind, 45 Minute Reserves Dist (nm) ------------------------------------------------- Cruise Altitude (ft) ------------------------------------------------- Time (min) 5,000 10,000 15,000 20,000 25,000 Fuel (lb) Time (min) Fuel (lb) 100 0:32 63 0:30 71 Time (min) Fuel (lb) Time (min) Fuel (lb) Time (min) Fuel (lb) 200 1:05 118 1:01 123 1:01 129 1:02 144 300 1:38 174 1:32 175 1:30 178 1:30 192 1:32 201 400 2:10 229 2:03 227 1:59 227 1:58 239 1:58 246 500 2:43 285 2:34 279 2:29 276 2:26 286 2:24 290 600 3:16 340 3:05 331 2:58 326 2:54 333 2:51 335 700 3:49 396 3:36 383 3:27 375 3:22 380 3:17 379 800 4:22 451 4:07 435 3:56 424 3:50 427 3:44 424 900 4:55 507 4:38 487 4:26 474 4:18 475 4:10 468 1,000 5:09 539 4:55 523 4:46 522 4:37 513 1,092 5:01 554 21
MISSION PLANNING RANGE / PAYLOAD CAPABILITY ISA, zero wind, 45 Minute Reserves 800-50 LOP 55% Power 600 Payload (pounds) 400 200 0 0 200 400 600 800 1,000 1,200 1,400 Range (nautical miles) 22