SA01299SE
Installation of vortex generators on the wings and tail surfaces of the above model aircraft in accordance with Micro AeroDynamics , Inc. Drawing Package Document MA2191, Revision IR, dated September 17, 2003, and Installation Manual MA2192, Revision IR, dated October 27, 2003, or later FAA approved revision to either of these documents. Held by Micro Aerodynamics INC, which holds 77 approved modifications in all. Last revised November 14, 2003. System: airframe structure.
What it applies to
- Kind of product
- Aircraft
- Design holder
- The New Piper Aircraft Inc.; The New Piper Aircraft Inc.; The New Piper Aircraft Inc.
- Models
- PA-24, PA-24-250, PA-24-260
- Type certificates
- 1A15, 1A15, 1A15
- On this site
- Piper PA-24 Comanche 2,428 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.