This Flight Planning Guide is published for the purpose of providing specific information for evaluating the performance of the Cessna Corvalis TT.
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- Nelson Collins
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1 May 2010
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3 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/
4 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 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 m lb 54 kg Altitudes Certified Ceiling 25,000 ft 7,620 m 2
5 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
6 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, , , ,
7 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, ,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, / 50 1,241 1,851 1,109 1, / 59 1,282 1,902 1,147 1, / 68 1,323 1,953 1,186 1, / 77 1,364 2,005 1,225 1, / 86 1,415 2,069 1,270 1, / 95 1,473 2,142 1,320 1, / 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 / , ,206-5 / , ,242 0 / , ,277 5 / , , / , , / 59 1,013 1, , / 68 1,049 1, , / 77 1,085 1, , / 86 1,125 1, , / 95 1,167 1,758 1,013 1, / 104 1,208 1,810 1,047 1,608 5
8 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, / 50 1,353 1,991 1,215 1, / 59 1,402 2,053 1,259 1, / 68 1,457 2,122 1,306 1, / 77 1,513 2,191 1,354 1, / 86 1,568 2,260 1,401 2, / 95 1,624 2,329 1,450 2, / 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 / , ,291-5 / , ,331 0 / , ,378 5 / 41 1,036 1, , / 50 1,076 1, , / 59 1,116 1, , / 68 1,155 1,744 1,004 1, / 77 1,195 1,793 1,036 1, / 86 1,234 1,843 1,067 1, / 95 1,276 1,896 1,103 1, / 104 1,321 1,951 1,141 1,726 6
9 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, / 50 1,497 2,171 1,340 1, / 59 1,555 2,244 1,390 2, / 68 1,611 2,314 1,439 2, / 77 1,664 2,380 1,486 2, / 86 1,717 2,446 1,533 2, / 95 1,769 2,512 1,581 2, / 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, ,406-5 / 23 1,060 1, ,453 0 / 32 1,100 1, ,500 5 / 41 1,142 1, , / 50 1,183 1,779 1,027 1, / 59 1,225 1,831 1,060 1, / 68 1,267 1,883 1,094 1, / 77 1,308 1,935 1,131 1, / 86 1,350 1,988 1,167 1, / 95 1,392 2,040 1,203 1, / 104 1,438 2,097 1,245 1,856 7
10 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, / 50 1,638 2,347 1,463 2, / 59 1,697 2,421 1,516 2, / 68 1,756 2,495 1,569 2, / 77 1,819 2,574 1,627 2, / 86 1,885 2,656 1,688 2, / 95 1,951 2,738 1,748 2, / 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, ,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, / 50 1,288 1,909 1,113 1, / 59 1,334 1,968 1,153 1, / 68 1,381 2,027 1,194 1, / 77 1,434 2,092 1,241 1, / 86 1,490 2,163 1,293 1, / 95 1,546 2,233 1,344 1, / 104 1,599 2,299 1,391 2,039 8
11 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, / 50 1,794 2,543 1,603 2, / 59 1,864 2,630 1,668 2, / 68 1,934 2,718 1,733 2, / 77 2,004 2,805 1,797 2, / 86 2,074 2,893 1,859 2, / 95 2,144 2,980 1,921 2, / 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, / 50 1,412 2,065 1,221 1, / 59 1,472 2,140 1,276 1, / 68 1,532 2,215 1,331 1, / 77 1,591 2,288 1,384 2, / 86 1,644 2,355 1,429 2, / 95 1,697 2,422 1,474 2, / 104 1,751 2,488 1,519 2,199 9
12 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, / 50 2,003 2,804 1,797 2, / 59 2,069 2,886 1,854 2, / 68 2,134 2,968 1,912 2, / 77 2,200 3,050 1,970 2, / 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, / 50 1,590 2,288 1,383 2, / 59 1,640 2,350 1,426 2, / 68 1,690 2,413 1,468 2, / 77 1,740 2,475 1,510 2, / 86 1,790 2,538 1,552 2,240 10
13 CLIMB PERFORMANCE TIME, FUEL, AND DISTANCE TO CLIMB ISA, Zero Wind Pressure Time Fuel Distance Altitude (ft) (min) (gal) (nm) 2, , , , , , , , , , , , ,
14 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%
15 DESCENT PERFORMANCE TIME, FUEL, AND DISTANCE TO DESCEND ISA, Zero Wind Pressure Time Fuel Distance Altitude (ft) (min) (gal) (nm) 2, , , , , , , , , , , , ,
16 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, / 50 1,234 2,613 1,168 2, / 59 1,252 2,648 1,186 2, / 68 1,271 2,683 1,204 2, / 77 1,289 2,718 1,222 2, / 86 1,308 2,753 1,240 2, / 95 1,327 2,787 1,258 2, / 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, ,125-5 / 23 1,050 2, ,152 0 / 32 1,067 2,301 1,002 2,180 5 / 41 1,084 2,333 1,019 2, / 50 1,102 2,366 1,036 2, / 59 1,119 2,400 1,053 2, / 68 1,137 2,433 1,070 2, / 77 1,155 2,466 1,087 2, / 86 1,172 2,499 1,105 2, / 95 1,190 2,532 1,122 2, / 104 1,208 2,565 1,139 2,436 14
17 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, / 50 1,313 2,762 1,245 2, / 59 1,333 2,800 1,265 2, / 68 1,354 2,838 1,285 2, / 77 1,374 2,876 1,304 2, / 86 1,395 2,916 1,325 2, / 95 1,422 2,967 1,349 2, / 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, / 50 1,177 2,508 1,109 2, / 59 1,196 2,544 1,128 2, / 68 1,216 2,579 1,146 2, / 77 1,235 2,615 1,165 2, / 86 1,254 2,652 1,184 2, / 95 1,276 2,693 1,203 2, / 104 1,298 2,734 1,222 2,592 15
18 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, / 50 1,404 2,933 1,333 2, / 59 1,428 2,978 1,355 2, / 68 1,452 3,022 1,376 2, / 77 1,476 3,067 1,398 2, / 86 1,500 3,112 1,419 2, / 95 1,524 3,156 1,441 3, / 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, / 50 1,262 2,666 1,190 2, / 59 1,281 2,702 1,207 2, / 68 1,300 2,738 1,224 2, / 77 1,320 2,774 1,241 2, / 86 1,339 2,810 1,258 2, / 95 1,358 2,846 1,275 2, / 104 1,378 2,883 1,293 2,724 16
19 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, / 50 1,505 3,121 1,424 2, / 59 1,530 3,168 1,447 3, / 68 1,555 3,215 1,469 3, / 77 1,580 3,262 1,492 3, / 86 1,605 3,309 1,515 3, / 95 1,630 3,355 1,537 3, / 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, / 50 1,343 2,818 1,262 2, / 59 1,363 2,856 1,280 2, / 68 1,384 2,894 1,298 2, / 77 1,404 2,932 1,316 2, / 86 1,424 2,970 1,334 2, / 95 1,444 3,008 1,351 2, / 104 1,465 3,046 1,369 2,867 17
20 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, / 50 1,621 3,338 1,530 3, / 59 1,647 3,387 1,555 3, / 68 1,673 3,435 1,580 3, / 77 1,699 3,484 1,605 3, / 86 1,724 3,532 1,630 3, / 95 1,750 3,581 1,655 3, / 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, / 50 1,439 2,998 1,349 2, / 59 1,463 3,043 1,372 2, / 68 1,487 3,088 1,395 2, / 77 1,511 3,133 1,418 2, / 86 1,536 3,179 1,441 3, / 95 1,560 3,224 1,464 3, / 104 1,584 3,269 1,487 3,088 18
21 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, / 50 1,740 3,561 1,645 3, / 59 1,768 3,614 1,672 3, / 68 1,796 3,666 1,699 3, / 77 1,824 3,718 1,726 3, / 86 1,852 3,771 1,753 3, / 95 1,880 3,823 1,780 3, / 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, / 50 1,550 3,206 1,455 3, / 59 1,576 3,254 1,480 3, / 68 1,602 3,303 1,505 3, / 77 1,628 3,352 1,530 3, / 86 1,654 3,400 1,555 3, / 95 1,680 3,449 1,580 3, / 104 1,706 3,498 1,605 3,309 19
22 STALL SPEEDS 3,600 lb, KCAS Flap Position Bank Angle Cruise 12 (Takeoff) 40 (Landing) 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) * Wind Correction Factor is calculated as KTAS divided by the sum of KTAS ± wind component 20
23 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: :30 71 Time (min) Fuel (lb) Time (min) Fuel (lb) Time (min) Fuel (lb) 200 1: : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : ,000 5: : : : ,092 5:
24 MISSION PLANNING RANGE / PAYLOAD CAPABILITY ISA, zero wind, 45 Minute Reserves LOP 55% Power 600 Payload (pounds) ,000 1,200 1,400 Range (nautical miles) 22
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