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The Cessna model 162 is
an all-metal, single engine piston,
high-wing monoplane with a two-person
seating capacity including the pilot.
Suitable allowance for luggage is provided
aft of the seats. The 162 will be equipped
per FAR 91.205 to meet both Day and Night
VFR flight requirements. Cessna's worldwide
network of authorized service centers
provides a complete source for all servicing
needs.
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Dimensions |
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Overall Height |
8.3 ft |
2.53 m |
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Overall Length |
22.8
ft |
6.95 m |
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Wing
Span |
30 ft |
9.14 m |
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Wing
Area |
120 sq
ft |
11.15
sq m |
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Wing
Loading |
11
lb/sq ft |
53.7
kg/sq m |
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Cabin
- Width (at the shoulder) |
44 in |
1.12 m |
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Maximum Seating Capacity |
2 |
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Design
Weights And Capabilities |
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Maximum Gross Weight |
1,320 lb |
598.7 kg |
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Standard Empty Weight |
830 lb |
376.5 kg |
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Maximum Useful Load |
490 lb |
222.3 kg |
Maximum Baggage Weight
(no parachute) |
50 lb |
22.7 kg |
Maximum Baggage Weight
(w/optional parachute) |
25 lb |
11.3 kg |
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Usable
Fuel |
24 U.S. gal |
90.8 L |
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Power
Plant |
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Engine: Teledyne Continental |
0-200D |
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Horsepower at 2,800 rpm |
100 bhp |
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Propeller: Composite, Two-Blade, Fixed
Pitch |
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Performance
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Speed – Maximum at Sea Level |
118 ktas/136 mph**
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Cruise Speed
(77% Power at 6,000 ft) |
112 ktas/129 mph* |
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Maximum Range and Endurance
(at 6,000 ft) |
470 nm/5.8 hrs* |
870 km |
Cruise Range and Endurance
(77% Power at 6,000 ft) |
390 nm/3.4 hrs** |
722 km |
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Maximum Climb Rate at Sea Level |
890 fpm |
271 mpm |
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Service Ceiling |
15,500 ft |
4,724 m |
Takeoff Performance at Sea Level
Total Distance Ground Roll |
770 ft |
235 m |
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Total Distance Over 50-ft Obstacle |
1,250 ft |
381 m |
Landing Distance at Sea Level
Total Distance Ground Roll |
420 ft |
128 m |
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Total Distance Over 50-ft Obstacle |
1,040 ft |
317 m |
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