General Description
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| All estimated
performance data are based on airplane weights at 3,100 pounds; standard
atmospheric conditions; level, hard-surface, 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, pilots, and numerous other factors affecting
flight performance. |
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Specifications
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English |
Metric |
Baggage Door
Height (front)
Height (rear)
Width
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22"
20.5"
15.8"
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0.56 m
0.52 m
0.40 m
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Cabin
Height (max)
Length (firewall to aft baggage area)
Width
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48.5"
134"
42"
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1.23 m
3.40 m
1.07 m
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Cabin
Door
Height (front)
Height (rear)
Width (top)
Width (bottom)
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41"
38.5"
32"
36.5"
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1.04 m
0.98 m
0.81 m
0.93 m
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Overall
Height (max)
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9'4"
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2.84 m
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Overall
Length
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29'0"
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8.84 m
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Wing
Span (overall)
Area |
36'0"
174 sq ft |
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10.97 m
16.2 sq m |
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Design Weights and Capacities
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English |
Metric |
Baggage
Allowance
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200 lbs
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91 kg
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Fuel
Capacity
Total capacity
Total usable
Total capacity each tank
Total usable capacity each tank
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92.0 gal
87.0 gal
46.0 gal
43.5 gal
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348.2 liters
329.3 liters
174.1 liters
164.6 liters
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Maximum Landing
Weight
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2,950 lbs
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1,338 kg
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Maximum
Useful Load
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1,017 lbs
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461.3 kg
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Oil
Capacity
Sump
Total capacity
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8 qts
9 qts
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7.5 liters
8.5 liters
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Maximum Ramp
Weight
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3,112 lbs
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1,412 kg
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Standard
Empty Weight
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2,095 lbs
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950.3 kg
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Maximum Takeoff
Weight
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3,100 lbs
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1,406 kg
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Notes: 1.
Standard empty weight based upon: a) 0.6 mil primer on all
details, 0.6 mil primer on all exterior surfaces and 2.0 mil
paint on all exterior surfaces. b) Engineering defined standard
aircraft. |
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