 |
Pilatus P.3-05 Swiss Air Force tandem two seat Intermediate Trainer, Lycoming GO-435-C&D 260 Hp, Vne 316 mph, max cruise 170 mph, sea level rate of climb 1,378 ft/min., ventral fin keel prevents flat spins |
|
 |
Pilatus P.3-05 Swiss Air Force Intermediate Trainer, Lycoming GO-435-C&D 260 Hp |
|
 |
Pilatus P.3-05 Swiss Air Force Intermediate Trainer, Lycoming GO-435-C&D 260 Hp, wing strobe light, nav light & landing light |
|
 |
Pilatus P.3-05 Swiss Air Force Intermediate Trainer, Lycoming GO-435-C&D 260 Hp, tri-blade constant speed prop |
|
 |
Pilatus P.3-05 Swiss Air Force Intermediate Trainer, Lycoming GO-435-C&D 260 Hp, first flight of prototype P.3 1953. Designed to replace Bucker 1.133 JUNGMEISTER and T-6 TEXAN in Swiss Air Force. Production commenced 1956. |
|
 |
Pilatus P.3-05 Swiss Air Force Intermediate Trainer, Lycoming GO-435-C&D 260 Hp, cowl |
|
 |
Pilatus P.3-05 Swiss Air Force Intermediate Trainer, Lycoming GO-435-C&D 260 Hp, Vne 316 mph, early recip engine forerunner of Pilatus P.7 and P.9 |
|
 |
Pilatus P.3-05 Swiss Air Force Intermediate Trainer, Lycoming GO-435-C&D 260 Hp, empennage, note ventral fin keel prevents flat spins |
|
 |
Pilatus P.3-05 Swiss Air Force Intermediate Trainer, Lycoming GO-435-C&D 260 Hp, warning on wing |
|
 |
Pilatus P.3-05 Swiss Air Force Intermediate Trainer, Lycoming GO-435-C&D 260 Hp, warning on wing |
|
 |
Pilatus P.3-05 Swiss Air Force Intermediate Trainer, Lycoming GO-435-C&D 260 Hp, warning on horizontal stabilizer |
|
 |
Pilatus P.3-05 Swiss Air Force Intermediate Trainer, Lycoming GO-435-C&D 260 Hp, Vne 316 mph |
|
