1-2
PHYSICAL CHARACTERISTICS
3.
Key physical characteristics of the aircraft are detailed below.
Aircraft Dimensions and Weights
Length
28’ 6.5”
8.72m
Wingspan
39’ 7”
12.1m
Height (rudder)
8’ 0” ± 6”
2.4m ± 0.152m
Height (prop)
8’ 2” ± 2”
2.5m ± 0.05m
Prop diameter
78”
2.03m
Prop ground clearance
18” ± 2”
0.46m ± 0.05m
Length
28’ 6.5”
8.72m
Maximum Ramp Weight
3110 lbs
Maximum Takeoff Weight
3100 lbs
Maximum Landing Weight
2950 lbs
Basic Empty Weight
Approximately 1850 lbs
Useful Load
Approximately 1250 lbs
Figure 1-2 Dimensions and Weight
Fuel Tank Capacities
Total Fuel
Useable Fuel
USG
Litres
Pounds
USG
Litres
Pounds
Left Tank
40
151
240
37.5
142
225
Right Tank
40
151
240
37.5
142
225
TOTAL
80
303
480
75
284
450
Figure 1-3 Fuel Tank Capacities
CAUTION
Only 100LL AVGAS shall be used.
Oil Capacity
US Quarts
Litres
Weight
– lbs
Total capacity
12
11.4
22.2
Minimum for takeoff
9
8.5
17.5
Figure 1-4 Oil Capacity
CAUTION
Refer to the Aircraft Journey Log to confirm the type and grade of oil
in use.
Summary of Contents for 182
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