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 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 To view PDF files, you need to have the free Adobe Acrobat Reader installed.

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