Pitts S1
Specifications / 3-views
|
PITTS S1-C AND S1-SS SPECIFICATIONS
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
S1-C |
|
|
|
S1-SS |
|
|
|
Notes |
|
|
BASIC DIMENSIONS |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
Length |
|
ft |
|
|
|
15.46 |
|
|
|
15.46 |
|
|
|
Will vary slightly with engine/prop installation |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
Height |
|
ft |
|
|
|
6.29 |
|
|
|
|
|
|
|
All S1-C specs are for the new, updated CAD plans. |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
Wing Span (Upper) |
|
ft |
|
|
|
17.33 |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
Wing Span (Lower) |
|
ft |
|
|
|
15.5 |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
PAYLOAD AND ACCOMODATIONS |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
Seats |
|
|
|
|
|
1 |
|
|
|
1 |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
Fuel Capacity |
|
US gal |
|
|
|
19 |
|
|
|
19 |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
Baggage Capacity |
|
lb |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
DETAILS |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
Upper Wing Airfoil |
|
|
|
|
|
NACA 632015 |
|
|
|
NACA 632A015 |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
Lower Wing Airfoil |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
Upper Wing Sweep |
|
degrees |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
Upper Wing Area |
|
sq ft |
|
|
|
50.03 |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
Lower Wing Area |
|
sq ft |
|
|
|
48.44 |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
Total Wing Area |
|
sq ft |
|
|
|
98.47 |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
Stabilizer/Elevator Area |
|
sq ft |
|
|
|
15.45 |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
Fin/Rudder Area |
|
sq ft |
|
|
|
7.84 |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
WEIGHT |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
Empty Weight |
|
lb |
|
|
|
650 (125hp)
720 (180hp) |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
Acro Weight |
|
lb |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
Gross Weight |
|
lb |
|
|
|
1150 |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
Design Load Factor |
|
g |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
Ultimate Load Factor |
|
g |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
Wing Loading
(@ Acro Weight) |
|
lb/sq ft |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
Wing Loading
(@ Gross Weight) |
|
lb/sq ft |
|
|
|
10.67 (@ 1050lb)
11.68 (@ 1150lb) |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
POWER |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
Power Requirements |
|
hp |
|
|
|
85-180 |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
Engine (Typical) |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
Power Loading
(@ Acro Weight) |
|
lb/hp |
|
|
|
X.XX (125hp)
X.XX (180hp) |
|
|
|
X.XX (125hp)
X.XX (180hp) |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
FLIGHT PERFORMANCE |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
Stall Speed (@ Gross Weight) |
|
TAS/mph |
|
|
|
57 |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
Cruise Speed (75% power) |
|
mph |
|
|
|
154 |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
Max Speed (Level Flight) |
|
mph |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
Never-Exceed Speed (Vne) |
|
TAS/mph |
|
|
|
203 |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
Rate of Climb (Initial) |
|
ft/min |
|
|
|
1750 (125hp)
2650 (180hp) |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
Ceiling (@ Gross Weight) |
|
ft MSL |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
Ceiling (@ Acro Weight) |
|
ft MSL |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
Roll Rate |
|
degrees/s |
|
|
|
180 |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
MISCELLANEOUS |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
Plans Price |
|
US Dollars |
|
|
|
original $125
enhanced CAD $250
(* See Note 1) |
|
|
|
$100
(** Supplemental Plans)
(** See Note 2) |
|
|
|
Plus shipping and handling
* NOTE 1: All specifications for S1-C are for the updated CAD plans version. The CAD plans are highly recommended for all new projects. Please note that the CAD plans were drawn using CAD software, but are printed on paper. They are NOT available in electronic format.
** NOTE 2: S1-SS plans are SUPPLEMENTAL to the S1-C Plans and show ONLY the new SS wing construction. You must have a full set of S1-C plans AND the S1-SS Supplemental plans in order to build a Pitts S1-SS.
Purchase Plans Online! |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
Component Availability |
|
|
|
|
|
Extensive |
|
|
|
Extensive |
|
|
|
|
|
|
Pitts S1-C
– Front
– Side
– Top
(Click for Printable PDF)