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Pitts Model 14
Specifications

The prototype of the Model 14 is currently under construction at Steen Aero Lab. Flight performance data is based on reasonable estimates until completion of flight testing.

PITTS MODEL 14 SPECIFICATIONS
Model 14 Notes
BASIC DIMENSIONS
Length ft
Height ft
Wing Span (Upper) ft 21.5
Wing Span (Lower) ft 20.5
PAYLOAD AND ACCOMODATIONS
Seats 2
Fuel Capacity US gal 35 (+18 optional)
Baggage Capacity lb 35
DETAILS
Upper Wing Airfoil NACA 23012 Symmetrical airfoils optional
Lower Wing Airfoil NACA 23012 Symmetrical airfoils optional
Upper Wing Sweep degrees 0 ** Swept upper wing option will be available.
Total Wing Area sq ft 157
WEIGHT
Empty Weight lb 1500
Max Aerobatic Weight lb 2000
Gross Weight lb 2250
Design Load Factor g +6/-4.5
Ultimate Load Factor g +9/-6
Wing Loading
(@ Acro Weight)
lb/sq ft 11.91
Wing Loading
(@ Gross Weight)
lb/sq ft 14.33
POWER
Power Requirements hp 360-400
Engine (Typical) Vendenyev M14P/
M14PF
Click here for more info about the M14P series engines
Power Loading
(@ Gross Weight)
lb/hp 6.25 (360hp)
5.63 (400hp)
Power Loading
(@ Acro Weight)
lb/hp 5.56 (360hp)
4.68 (400hp)
FLIGHT PERFORMANCE
Stall Speed (@ Gross Weight) TAS/mph 57-62 Estimated
Cruise Speed (75% power) mph 180 Estimated
Max Speed (Level Flight) mph 190 Estimated
Never-Exceed Speed (Vne) TAS/mph 235
Rate of Climb (Initial) ft/min 3500 Estimated
MISCELLANEOUS
Plans Price US Dollars See Note Plans for the Pitts Model 14 will not be available until after the prototype aircraft flies. However, you may Visit Our Online Store to order a FREE Pitts 14 Info-Pack.
Component Availability Coming soon!

Pitts 14 3-View Drawings
Pitts Model 14 3-Views Description Small Medium Large Printable
Model 14 400 x 250 800 x 500 1600 x 1000 PDF
        - Side 800 x 600 PDF
        - Top 800 x 600 PDF
        - Front 800 x 600 PDF
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