INTRODUCTION CESSNA
MODEL 162
GARMIN G300
U.S.
PERFORMANCE - SPECIFICATIONS
*SPEED:
Maximum at Sea Level . . . . . . . . . . . . . . 118 KNOTS (218.5 km/hr)
Cruise, 69% Power at 6000 Feet. . . . . . . 109 KNOTS (201.9 km/hr)
CRUISE: Recommended lean mixture with fuel allowance for engine
start, taxi, takeoff, climb and 30 minutes reserve.
RANGE:
69% Power at 6000 Feet. . . . . . . . . . . . . . . . . . . . .Range - 360 NM
24 Gallons Usable Fuel . . . . . . . . . . . . . . . . . . . Time - 3.30 HOURS
RATE OF CLIMB AT SEA LEVEL . . . . . . . . . . . 880 FPM (268.2 mpm)
SERVICE CEILING . . . . . . . . . . . . . . . . . . . . 14,625 FEET (4457.7 m)
TAKEOFF PERFORMANCE AT SEA LEVEL:
Ground Roll . . . . . . . . . . . . . . . . . . . . . . . . . . . .640 FEET (195.1 m)
Total Distance Over 50 Foot Obstacle. . . . . . .1138 FEET (346.9 m)
LANDING PERFORMANCE AT SEA LEVEL:
Ground Roll . . . . . . . . . . . . . . . . . . . . . . . . . . . .671 FEET (204.6 m)
Total Distance Over 50 Foot Obstacle. . . . . . .1369 FEET (417.3 m)
STALL SPEED:
Flaps UP, Power Idle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 41 KIAS
Flaps FULL, Power Idle. . . . . . . . . . . . . . . . . . . . . . . . . . . . 37 KIAS
* Speed performance is shown for airplanes not equipped
with the optional speed fairings. Airplanes equipped with
optional speed fairings will notice a increase in speeds by
approximately 2 knots. There is a corresponding difference
in range, while all other performance figures are
unchanged when speed fairings are installed.
The above performance figures are based on airplane weights at 1320
pounds (598.7 kg), standard atmospheric conditions, level, hard-
surfaced 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 and
numerous factors affecting flight performance.
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