STC# |
Date of Drawing Issue |
Package |
Aircraft Types |
SA4913NM* |
3-30-90 |
SP4000 |
Cessna 402C, 402C R/STOL, 414A, 414A R/STOL, 414AW, 421C, 421CW, 421C R/STOL, 421C w/Turbine engines, 425 |
SA4937NM* |
5-11-90 |
SP6000 |
Cessna 421B (Without STOL) |
SA4948NM* |
6-19-90 |
SP8000 |
Cessna 340, 340A (Without STOL) |
SA4951NM |
6-28-90 |
SP5000 |
PA 60-600, 601, 601P, 602P, 700P |
SA5114NM* |
1-23-91 |
SP7000 |
Cessna 337, P337B, T337B, 337C, T337C, 337D, T337D, 337E, T337E, 337F, T337F, 337G, T337G, 337H, P337H, T337H, T337H-SP. All approved with STOL kits from Robertson, Horton, Bush. |
SA5196NM* |
10-23-91 |
SP9000 |
Piper PA-46-310P, PA-46-350P |
SA5777NM* |
10-5-92 |
SP10000 |
Beechcraft 58 Series |
SA00007SE* |
7-28-93 |
SP11000 |
Beechcraft 60, A60, B60 (With and without Boundary Layer Research vortex generator kit STC #SA5761NM) installed) |
SA00001SE* |
6-9-93 |
SP12000 |
Cessna 414 (Without STOL) |
SA00215SE* |
7-7-95 |
SP13000 |
Cessna 310R/T310R (Must be installed only in conjunction with vortex generators manufactured by Micro AeroDynamics STC #SA4980NM or STC #SA5668NM; or by Aeronautical Testing Service, STC #5163NM) |