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 STC Update by Mike Keirnan Mgr Installations & Certification |
APPROVALS SINCE LAST NEWSLETTER
SYSTEM AIRCRAFT
20/30 Beech S35, V35, V35A, and V35B And The Above Models
When Modified By STC SA1035WE (Turbocharged Engine) (14V)
20/30 Beech A45 (T-34B, B-45) and D45 (T-34B) And The Above
Models When Modified By STC SA1450SW or STC SA1864SW
(Installation of 285 H.P. Engine Conversion)
20/30 Cessna 182E, 182F, 182G, 182H, 182J, 182K, 182L, 182M,
and 182N
20/30 Extra EA-300L
20/30 Navion A, B, D, E, F, G, & H When Modified By Palo Alto
Airport, Inc. or Symon's Engineering Horizontal Stabilizer
Angle of Incidence Change With or Without Tip Tanks And
The Above Models When Modified By 285 H.P. Engine Conversion
20/30 Piper PA-28-235, S/N 28-7310001 and Up
30 ALT Beech 35, A35, B35, C35, D35, E35, F35, and G35; and Model 35
When Modified Per SA1-460 (Auxiliary Wing Tip Fuel Tanks) (14V)
30 ALT Cessna 177B and 177RG (28V)
30 ALT Cessna 180, 180A, 180B, 180C, 180D, 180E, 180F, 180G, 180H,
180J, 180K (Landplane, Floatplane or Amphibian) & These Models
When Modified Per STC SA1705WE (Internal Tip Tanks) &/or
STC SA1435WE (Robertson STOL)
30 ALT Cessna 182, 182A, 182B, 182C, and 182D And These Models When
Modified Per STC SA1382WE (Robertson STOL) (14V)
30 ALT Cessna 182P, 182Q, F182P, F182Q
30 ALT Cessna R182, TR182, FR182 (28V)
30 ALT Cessna 185, 185A, 185B, 185C, 185D, A185E, A185F (Landplane,
Floatplane or Amphibian) & These Models When Modified per
STC SA2529WE (Internal Tip Tanks) &/or STC SA1441WE
(Robertson STOL) (14V)
30 ALT Cessna 190, 195, 195A, and 195B And These Models When Modified
Per STC SA2266WE (450 H.P. Engine Conversion) (14V)
30 ALT Cessna 401, 401A, 401B, 402A, 402B, 402C (28V)
30 ALT Piper PA-32-260, PA-32-300, and PA-32R-300 (14V)
30 ALT Piper PA-32-301, PA-32-301T, PA-32R-301, PA-32R-301T (28V)
40/50 Piper PA-31-325 & The Above Model When Modified Per STC SA00048SE
(Vortex Generator System) (28V)
60-2 Extra EA-300L
PROJECTS IN PROCESS SINCE LAST NEWSLETTER
SYSTEM AIRCRAFT
20/30 Beech H35, J35, K35, M35, N35, and P35
20/30 Beech V35B And The Above Model When Modified By STC SA1035WE
(Turbocharged Engine) (28V)
20/30 Cessna 210L, T210L, 210M, T210M, 210N, T210N, 210R, T210R;
210L, T210L, 210M, T210M When Modified Per STC SA1525WE
(Robertson STOL); T210L When Modified Per STC SA2689SW
(RAM Modification); 210N, T210N When Modified Per STC SA1756NW
(Robertson STOL)
30 ALT Beech H35, J35, K35, M35, N35, and P35
30 ALT Beech A45 (T-34B, B-45) and D45 (T-34B) And The Above Models
When Modified By STC SA1450SW or STC SA1864SW (Installation of
285 H.P. Engine Conversion)
30 ALT Cessna 182E, 182F, 182G, 182H, 182J, 182K, 182L, 182M, 182N
30 ALT Cessna 210L, T210L, 210M, T210M, 210N, T210N, 210R, T210R; 210L,
T210L, 210M, T210M When Modified Per STC SA1525WE (Robertson STOL);
T210L When Modified Per STC SA2689SW (RAM Modification); 210N,
T210N When Modified Per STC SA1756NW (Robertson STOL)
30 ALT Piper PA-28-235, S/N 28-7310001 & Up
40/50 Navion A, B, D, E, F, G, & H When Modified By Palo Alto Airport, Inc.
or Symon's Engineering Horizontal Stabilizer Angle of Incidence Change
With or Without Tip Tanks And The Above Models When Modified By 285
H.P. Engine Conversion
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