SA01058SE
Installation of vortex generators on the wings and tail surfaces of the above model aircraft in accordance with Drawing Package MA2165, Revision IR, dated February 14, 2002, and Installation Manual MA2166, Revision IR, dated February 25, 2002, or later FAA approved revision of either of these documents. Held by Micro Aerodynamics INC, which holds 77 approved modifications in all. Last revised February 28, 2002. System: airframe structure.
What it applies to
- Kind of product
- Aircraft
- Design holder
- The Cessna Aircraft Company; The Cessna Aircraft Company; The Cessna Aircraft Company
- Models
- 210R, P210R, T210R
- Type certificates
- 3A21, 3A21, 3A21
- On this site
- Cessna 210 Centurion 1,526 registered
Cessna P210 Pressurized Centurion 443 registered
Cessna T210 Turbo Centurion 1,284 registered - The FAA's record
- On the FAA's site
What an approved modification is
A supplemental type certificate is the FAA's approval of a change to a certified design: a new engine or propeller, avionics, an autopilot, floats, a parachute, a larger fuel tank, an ice-protection kit. The company holding it may sell the kit and the paperwork to owners of the listed models; the modification then becomes part of that aircraft's record. The FAA's list says what was approved and for which models, not how many aircraft carry it.
Source: FAA supplemental type certificates (Dynamic Regulatory System). Register counts from the FAA register of October 7, 2026.