Specifications
Cardinal Specs
'68 177
'69 177A
'70-'74 177B
'75-'78 177B
1971 RG
1972-1978 RG
Interior Comparision
Other Cessnas
172 A
172 B
172 C
172 D-H
172 I Skyhawk
172 K Hawk XP
172 K-L Skyhawk
172 K-L
172 M Float
172 M Float 2
172 M Skyhawk
172 N Hawk 100
172 N-P Hawk 100
172 O Cutlass
172 P II Skyhawk
172 RG II Cutlass
182 A-D
182 E-H
182 J-M Skylane
182 N Skylane
182 P-Q
182 Q II
182
R 172 K Hawk XP
R182 RG II Skylane
R182 RG Turbo Skylane
T-182 Q II Turbo Skylane
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Cessna Aircraft Aircraft Performance Specifications
Notice : Data is provided as a guide "at users risk" and is not intended for flight planning purposes! Consult the relevant Pilots Operating Handbook prior to flight.
R 172 K Hawk XP | CESSNA AIRCRAFT CORPORATION | 1977 Model had a takeoff ground run of 850 ft. |
General Information | |
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Engine Type: | Piston | |
Engine Make: | Continental 195hp
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Power (HP or Lbs Thrust): | 195 |
Engine TBO: | 1500 | |
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S P E E D S | | MPH | KTS | KPH |
Maximum Cruising Speed | | 152 | 132 | 244 |
Recommended Cruising Speed | | 149 | 129 | 238 |
Stalling Speed | | 54 | 46 | 85 |
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F U E L C A P A C I T Y | | Lbs | US Gals | Litres |
Standard Fuel | | 343 | 52 | 196 |
Long Range Version | | 448 | 68 | 257 |
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W E I G H T S | | | US Lbs | Kilos |
Gross Weight | | | 2550 | 1156 |
Empty Weight | | | 1572 | 712 |
Max Useful Load | | | 978 | 443 |
Max Useful w/Full Fuel | | | 635 | 287 |
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R A N G E | | SM | NM | KM | Hrs |
Max Range - Std Cruise | | 656 | 569 | 1053 | 4.4 |
C E I L I N G S | | Feet | Meters |
Max Service Ceiling | | 17000 | 5181 |
Max Engine Out Ceiling | | 0 | 0 |
C L I M B R A T E S | | Feet P/Min | Meters P/Min |
Max Climb, Sea Level, Gross Weight | | 870 | 265 |
Max Climb, Engine Out, Sea Level, Gross Weight | | 0 | 0 |
T A K E O F F & L A N D I N G D I S T A N C E S | | Feet | Meters |
TakeOff Ground Roll, Sea Level, Gross Weight | | 800 | 243 |
TakeOff Over 50ft/15meter Obstacle, Sea Level, Gross Weight | | 1360 | 414 |
Landing Ground Roll, Sea Level, Gross Weight | | 635 | 193 |
Landing Over 50ft/15meter Obstacle, Sea Level, Gross Weight | | 1345 | 409 |
A I R C R A F T D I M E N S I O N S | | Feet | Meters |
Cabin Width (at shoulder) | | 39.5 inches | |
Fuselage Length (approx.) | | 27.2 | 8.29 |
Fuselage (usually tail section) Height (approx.) | | 8.1 | 2.47 |
Total Wingspan (approx.) | | 35.1 | 10.7 |
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