N61942-extN61942 is a 2008 Cessna Skyhawk SP equipped with the Garmin G1000 NAV III glass cockpit. The G1000 integrates all primary flight, engine and sensor, and navigation data to provide an intuitive display of all the information you’ll need.

Real-time, flight-critical information is presented on two colorful 10.4-inch active-matrix LCD displays – bringing new levels of safety and confidence to your flight. N61942 is the newest addition to the fleet, for a total of five Skyhawks of which three are G1000 equipped.

If you’d like more information specific to N61942, check out the Pilot Downloads page.

All information herein applies to the Skyhawk SP (Model 172S).

The Skyhawk SP aircraft is an all-metal, single-engine piston, high-wing monoplane with a four-person seating capacity including a crew of one or two. Suitable allowance for luggage is provided.

N61942-cockpitThe Model 172S is certified to the requirements of U.S. FAA Federal Aviation Regulation Part 23 through amendment 23-6, including day, night, VFR and IFR.

Performance
All estimated performance data are based on airplane weights at 2,550 pounds; standard atmospheric conditions; level, hard-surface, dry runways; and no wind. They are calculated values derived from flight tests conducted by Cessna Aircraft Company under carefully documented conditions and will vary with individual airplanes, pilots, and numerous factors affecting flight performance.

English Metric
Cruise (45% power @ 10000′)
range 638nm 1182km
duration 6.72hr
Cruise (75% power @8500′)
range 518nm 959km
duration 4.26hr
Engine: Textron Lycoming IO-360-L2A
180 BHP @ 2700 RPM
Propeller: 2 blade fixed pitch diameter: 76in. 1.93m
Rate of climb (sea level): 730ft/min 223m/min
Service Ceiling: 14000′ 4267m
Speed
Max at sea level 126kts. 233kph
Cruise (75% power @ 8500′) 124kts 230kph
Stall Speed, CAS
Flaps Up, power off 53kts 98kph
Flaps Down, power off 48kts 89kph
Takeoff Performance 960ft 293m
Total distance over 50′ obstacle 1630ft 497m
Landing Performance
Ground Roll 575′ 175m
Total distance over 50′ obstacle 1335′ 407m
Wing Loading 14.7lb/sq. ft. 71.8kgm/sq. m.
Power Loading 14.2lb/hp 6.4kg/hp
The Skyhawk SP aircraft is an all-metal, single-engine piston, high-wing monoplane with a four-person seating capacity including a crew of one or two. Suitable allowance for luggage is provided.The Model 172S is certified to the requirements of U.S. FAA Federal Aviation Regulation Part 23 through amendment 23-6, including day, night, VFR and IFR.Performance
All estimated performance data are based on airplane weights at 2,550 pounds; standard atmospheric conditions; level, hard-surface, dry runways; and no wind. They are calculated values derived from flight tests conducted by Cessna Aircraft Company under carefully documented conditions and will vary with individual airplanes, pilots, and numerous factors affecting flight performance.

English Metric
Cruise (45% power @ 10000′)
range 638nm 1182km
duration 6.72hr
Cruise (75% power @8500′)
range 518nm 959km
duration 4.26hr
Engine: Textron Lycoming IO-360-L2A
180 BHP @ 2700 RPM
Propeller: 2 blade fixed pitch diameter: 76in. 1.93m
Rate of climb (sea level): 730ft/min 223m/min
Service Ceiling: 14000′ 4267m
Speed
Max at sea level 126kts. 233kph
Cruise (75% power @ 8500′) 124kts 230kph
Stall Speed, CAS
Flaps Up, power off 53kts 98kph
Flaps Down, power off 48kts 89kph
Takeoff Performance 960ft 293m
Total distance over 50′ obstacle 1630ft 497m
Landing Performance
Ground Roll 575′ 175m
Total distance over 50′ obstacle 1335′ 407m
Wing Loading 14.7lb/sq. ft. 71.8kgm/sq. m.
Power Loading 14.2lb/hp 6.4kg/hp