Need help?Do you have a question about the Rans S-19 VENTERRA and is the answer not in the manual?
Guidance on using the S-19 assembly manuals and general assembly advice.
Contact details and support information for RANS.
Steps for FAA registration, obtaining an N-number, and compliance.
Procedures and checklists for final inspection and obtaining airworthiness.
Requirements and procedures for the mandatory test flight period.
Explains the necessity and goals of the flight test period.
An overview of the RANS S-19 and general assembly preparation.
Step-by-step instructions for assembling the vertical stabilizer.
Detailed instructions for assembling the aircraft rudder.
Procedures for assembling the aircraft stabilator.
Instructions for assembling the anti-servo and trim tab components.
Procedures for balancing the stabilator, including lead pouring.
Explanation of RANS engineering drawing classification and numbering.
Cross-reference for rivets and details on airframe bolts.
Forms for aircraft ownership affidavit and eligibility statement.
FAA form to apply for a U.S. airworthiness certificate.
General| Engine | Rotax 912ULS |
|---|---|
| Height | 2.13 m (7 ft 0 in) |
| Maximum Takeoff Weight / Gross Weight | 1320 lbs |
| Cruise Speed | 138 mph (222 km/h, 120 knots) |
| Fuel Capacity | 100 L (26 US gal; 22 imp gal) |
| Powerplant | Rotax 912ULS |
| Stall Speed | 72 km/h (45 mph, 39 kn) |
| Rate of Climb | 5.1 m/s (1, 000 ft/min) |
To Next Page
