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| APPROVALS SINCE THE LAST NEWSLETTER |
| System |
Aircraft |
| 20/30 |
Cessna models 210D, 210E, 210F, and T210F and these models when modified per STC SA1525WE (Robertson STOL) or STC SA1048CE (Horton STOL) (14V) |
| 30 ALT |
Cessna models 210D, 210E, 210F, and T210F and these models when modified per STC SA1525WE (Robertson STOL) or STC SA1048CE (Horton STOL) (14V) |
| 20/30 |
Cessna models 310, 310A, 310B, and 310C (28V) |
| 20/30 |
Beech models C23 and C24R (28V) |
| 55X |
1. Commander Aircraft models 112, 112B, 112TC, 112TCA, 114, and 114A; 2. Commander Aircraft models 112 and 112B when modified per STC SE5203NM (turbocharger/ intercooler) and STC SA5202NM (installation of modified engine) and STC SA00499SE (three blade propeller) and/ or STC SA2677CE (Horton flap gap seals); 3. Commander Aircraft models 112TC, 112TCA, and 114 when modified per STC SA2677CE (Horton flap gap seals) (14V) |
| 55X |
Beech models 3N, 3NM, 3TM, JRB-6, D18S, E18S, E18S-9700, G18S, H18, C-45G, TC-45G, C-45H, TC-45H, and TC-45J (SNB-5) and these models when modified by Hamilton gross weight increase and models D18S, E18S, E18S-9700, G18S, H18, C-45G, TC-45G, C-45H, TC-45H, and TC-45J (SNB-5) when modified by Volpar tri-gear installation (28V) |
| 55X |
Piper models PA-24 (PA-24-180), PA-24-250, and PA-24-260 and the above models when modified in accordance with STC SA4-1351 or STC SA4-1235 as applicable (wing tip tanks) and PA-24-400 (14V) |
| 55X |
Cessna models 335, 340, and 340A and models 340 and 340A when modified per STC SE4327SW (RAM engine conversion) (28V) |
| 55X |
Cessna models 210G, T210G, 210H, T210H, 210J, T210J, 210K, and T210K and models T210G, T210H, T210J, and T210K when modified per STC SA2689SW (RAM modification) and all of the above models when modified per STC SA1525WE (Robertson STOL) or STC SA1048CE (Horton STOL) or STC SA966CE (Horton STOL) (14V) |
| 55X |
Piper models PA-32-260, PA-32-300, and PA-32R-300 (14V) |
| 55X |
Mooney models M20L, M20M, M20R, and M20S (28V) |
| 55X |
Cessna models 182E, 182F, 182G, 182H, 182J, 182K, 182L, 182M, and 182N and the above models when modified per STC SA1382WE (Robertson STOL) (14V) |
| 55X |
Piper models PA-28-151, PA-28-161, PA-28-181, PA-28-236, and PA-28-201T (14V) |
| 55X |
Cessna models 210D, 210E, 210F, and T210F and these models when modified per STC SA1525WE (Robertson STOL) (14V) |
| 55X |
Cessna models 210, 210A, 210B, and 210C (14V) |
| 55X |
Piper models PA-23-250 and PA-E23-250, S/N 27-2000 through S/N 27-7554172 and the above models when equipped with approved turbocharged engines (250 H.P.) and/or wing tip tanks per STC SA1480WE (28V) |
| 55X |
Cessna model T303 (28V) |
| 55X |
Mooney models M20F, M20G, and M20J (14V) |
| 55X |
Mooney model M20J (28V) |
| 55X |
Piper models PA-28-140, PA-28-150, PA-28-160, PA-28-180; and PA-28-235, S/N 28-10003 through S/N 28-11393 and S/N 28-7110001 through S/N 28-7210023 (14V) |
| 55X |
Piper models PA-28-161, PA-28-181, PA-28-201T, and PA-28-236 (28V) |
| 55X |
Piper model PA-44-180 (14V) |
| 55X |
Piper models PA-32-301, PA-32-301T, PA-32R-301 and PA-32R-301T (28V) |
| 55X |
Piper models PA-34-200, PA-34-200T, and PA-34-220T (28V) |
| 55X |
Piper models PA-28R-180, PA-28R-200, PA-28R-201, and PA-28R-201T (14V) |
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