C172R

C172R

C172R, the Skyhawk 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. It is certified to the requirements of U.S. FAA Federal Aviation Regulation Part 23 including day, night, VFR and IFR.

Dimensions:
˙	Baggage Door	Height (front)	22 in
		Height (rear)	21 in
		Width	15.3 in
˙	Cabin	Height (max)	48 in
		Length (firewall to aft baggage area)	142 in
		Width	39.5 in
˙	Cabin Door	Height (front)	40.5 in
		Height (rear)	39 in
		Width (top)	32.5 in
		Width (bottom)	37 in
˙	Wing	Span (overall)	36 ft 1 in
		Area	174 sq ft
˙	Baggage Allowance	120 lbs
˙	Landing Weight	Normal category	2,450 lbs
		Utility category	2,100 lbs
˙	Oil Capacity		8 qts
˙	Ramp Weight	Normal category	2,457 lbs
		Utility category	2,107 lbs
		Standard Empty Weight	1,620 lbs
˙	Takeoff Weight	Normal category	2,450 lbs
		Utility category	2,100 lbs

Performance:
All estimated performance data are based on airplane weights at 2,450 lbs; standard atmospheric conditions; level, hard-surface, dry runways; and no wind. They are calculated values derived from flight tests conducted by The Cessna Aircraft Company under carefully documented conditions and will vary with individual airplanes and numerous factors affecting flight performance.
Cruise at 60% power at 10,000 ft
	Time	6.6 hr
	Range	687 nm
Cruise at 80% power at 8,000 ft
	Time	4.8 hr
	Range	580 nm
Engine:
	Textron Lycoming IO-360-L2A		160 BHP at 2,400 RPM
Landing Performance
	Ground roll		550 ft
	Total distance over 50 ft obstacle		1,295 ft
Power Loading
	Propeller: Fixed Pitch, Diameter		75 in
	Rate of Climb at Sea Level		720 fpm
	Service Ceiling		13,500 ft
Speed
	Maximum at sea level		123 kts
	Cruise at 80% power at 8,000 ft		122 kts
Stall Speed, CAS
	Takeoff Performance	Ground Roll	945 ft
	Takeoff Performance	Total distance over 50 ft obstacle	1,685 ft
	Wing Loading		14.1 lb/sq ft