CESSNA 172N

G-GYAV

VITAL STATISTICS

Performance

	Knots		Knots			Knots
Vx	59	Va	97 Note 1	Rotate		65
Vy	79	Va	89 Note 2	Cruise at 2300 rpm		100
Vno	128	Vsi	47	Best angle of glide		65
Vne	160	Vso	41	Short finals (flaps down)		60
Vfe	85			Crosswind limit		15

Note 1: at max weight

Note 2: at 1950 lbs

Weight and Balance

	Pounds	Kilograms	Max fwd C of G	Max aft C of G
MAUW	2307	1047	38.50 ins	47.3 ins
Aerobatic	1653	750	2000lbs 38.50 ins	40.5 ins
SEW			Datum is the firewall
BEW	1550	704
Max landing weight	2300	1044	Lever arm	39.46 ins
Useful load	757	344	Wing span	36 ft
Max baggage weight	120	55	Wing loading	13.2 lbs/ft2

Fuel and Endurance

	US gallons	Litres	Endurance hrs	With Reserves 0.75 hrs
Fuel 100 LL	43	156
Useable fuel	40	145	5.0	4.25
Usage at 2300 rpm	8USG/hr	29l/hr

Aircraft

Tyres			Electrics
Nosewheel	5.00 x 5	31 p.s.i	Alternator	28V 60A
Main wheels	6.00 x 6	29 p.s.i.	Battery	24V 25A
Oil
	6 US quarts	5.7 litres	25-100 psi normal	100-245oF
Propeller			Flaps
	McCauley	75 ins	Variable 0-40o

Short Field Takeoff

1       Set Flaps UP	4     Climb at  59 knots to clear obstacles
2       Rotate at 52 knots	5     Normal climb attitude at  75 knots
3       Fly level to 59 knots	6     Normal ground run 220m @ISA ,sea level, max wt

Compass Variation

Recalibrated April 2007