Cessna 172S Nav III Information Manual

SECTION 6
WEIGHT AND BALANCE/EQUIPMENT LIST
CESSNA
MODEL 172SNAV III
CENTER-OF-GRAVITY LIIVIITS
Airplane C.G. Location - Millimeters Aft of Datum (FS 0.0)
875 925 975 1025 1075 1125 1175 1225
900 950 1000 1050 1100 1150 1200
2600
2500
Center-of-Gravity
Limits
2400
Maximum Takeoff Weight
2550 Pounds
1150
1100
1050
700
1500
34 35 36 37 38 39 40 41 42 43 44 45 46 47 48 49
Airplane C.G. Location - Inches Aft of Datum (FS 0.0)
|W Figure 6-8
6-16 U.S.
172SPHAUS-01

Cessna 172S Nav III Specifications

General

Manufacturer	Cessna
Model	172S Nav III
Engine	Lycoming IO-360-L2A
Horsepower	180 hp
Cruise Speed	124 knots (143 mph, 230 km/h)
Service Ceiling	13, 500 ft (4, 115 m)
Takeoff Distance (Ground Roll)	960 ft (293 m)
Landing Distance (Ground Roll)	575 ft (175 m)
Seating Capacity	4
Type	Single-engine, high-wing
Propeller	2-blade, constant-speed
Fuel Capacity	56 gallons
Wingspan	36 ft 1 in
Length	27 ft 2 in
Height	8 ft 11 in
Stall Speed	47 knots
Range	640 nautical miles
Rate of Climb	720 ft/min (3.7 m/s)
Avionics	Garmin G1000
Maximum Takeoff Weight	2, 550 lbs (1, 157 kg)