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S-14 AIRAILE
SPECIFICATIONS
42 HP
52 HP
65 HP
Wing Span
26 ft 4.5 in.
26 ft 4.5 in
Area
100 sq ft
Mean Chord
3 ft 9 in
Aspect.
6.98:1
Length.
18 ft 10 in
Height
7 ft.
7 ft
Cockpit Width
30 in
Headroom.
39 in
Legroom
42.5 in.
42.5 in
Number of Seats.
1
Doors
Landing Gear*.
F/TR
Baggage Volume **.
n/a.
n/a
Baggage Capacity.
Auxiliary Baggage Volume
Auxiliary Baggage Capacity
Fuel Capacity ***
9 gal US
POWER PLANT
447
503
582
Engine.
Rotax 447.
Rotax 503.
Rotax 582
Output
42 hp.
52 hp.
65 hp
Oil Capacity.
2.5 qts
Coolant Capacity.
4.4 qts
Propeller Diameter
68 in to 72 in.
68 in to 72 in
Propeller Type.
Wood
Gear Reduction.
1:2.58
Fuel G.P.H.
3.75 gal @ 85%
4.0 gal @ 85%
5.75 gal @ 85%
PERFORMANCE
Take Off Roll.
300 ft.
250 ft.
225 ft
Rate of Climb
600 fpm.
700 fpm.
900 fpm
Service Ceiling
12,000 ft
13,500 ft
15,000 ft
Cruise
75 mph
85 mph
95 mph
VNE.
120 mph
Stall Clean.
41 mph
43 mph
Stall Flaps.
36 mph
38 mph
Roll Rate.
94° /sec.
94° /sec
Glide Ratio
8:1.
8:1
Landing Roll
190 ft.
190 ft
Endurance.
2.4 hrs.
2.25 hrs.
1.56 hrs
Range.
180 miles
191 miles
148 miles
WEIGHTS AND LOADINGS
Gross Weight
675 lbs
750 lbs
775 lbs
Empty Weight
360 lbs
370 lbs
390 lbs
Useful Load.
315 lbs
380 lbs
385 lbs
Wing Loading
6.75 lbs.
7.5 lbs.
7.75 lbs
Power Loading
16.0 lbs.
14.4 lbs.
11.9 lbs
Limit Load Factors
+4 -2.
+4 -2
* F/TR = Fixed/Trike
** 50 lbs of baggage can be carried in the space available behind the seats.
*** Double the Range with a second optional wing tank.