Engineers Flying Club - Oklahoma City

Garmin GNS430 GPS/NAV/COM	Apollo MX20 MFD
Garmin GMA340 Audio Panel	BF Goodrich WX500 Stormscope
Garmin GTX327 Mode A/C Transponder	Bendix-King KX125 NAV/COM
Garmin GTX327 Mode A/C Transponder	Bendix-King KX125 NAV/COM
Garmin WX500 Stormscope Interface	KI525 HSI Slaved HSI/Gyro
S-TEC 40 Single Axis Autopilot	KRA-10 Radar Altimeter
Standard ADF with RMI	Electric Aileron Trim & Indicator
Standby Vacuum System	Alternate Static Source/System
Shadin Mini-Flow Fuel Mgmt. System	Volt/Amp Meter
Elec. Int'l US-8A Engine Analyzer	Flint-Aero Aux/tip Tanks (23 gals. Additional useable fuel) with Elect. fuel pumps and indicators

AIRFRAME:	Aluminum
	Wingspan	36 ft 0 in
	Wing area	174 sq ft
	Length	26 ft 11 in
	Height	8 ft 10 in
	Gross Weight	2550 lbs
	Useful Load	1015 lbs
	Basic Empty Weight	1535 lbs
	Fuel Capacity	48 gal. with std tanks 23 gals. in aux tanks
PROPELLER:	Sensenich Fixed Pitch	2 blades	76 in. Diameter
ENGINE:	Lycoming	O-360	180 HP @ 2700 rpm
			Power-Flow Exhaust System
PERFORMANCE:	Never Exceed Speed (Vne)	160 kts
	Cruise Speed (75% power)	125 kts
	Maximum Range	470 nm
		Aux Tanks 225 nm
		Total Range (71 Gals) 695 nm
	Rate of Climb (Sea Level)	730 fpm
	Service Ceiling	14,000 ft
	Stall Speed (flaps up)	50 kts
	Stall Speed (flaps extended)	44 kts
	Best Rate of Climb (Vy)	91 mph
	Best Angle of Climb (Vx)	65 mph
	Landing (over 50' obstacle)	1335 ft
	Takeoff (over 50' obstacle)	1630 ft
	Wing loading	13.2 lbs/sq ft
	Power loading	14.2 lbs/hp

N61571, 1975 Cessna 172M Skyhawk