编辑“︁Ae-45”︁（章节）

==性能==
Ae-45有光滑，淚珠狀的[[機身]]，圓形及加長玻璃為飛行員提供良好視野，採用低單翼設計；[[起落架]]能收回但尾輪不能。

{{Aircraft specifications
<!-- if you do not understand how to use this template, please ask at [[Wikipedia talk:WikiProject Aircraft]] -->
|plane or copter?=<!-- options: plane/copter --> plane
|jet or prop?=<!-- options: jet/prop/both/neither --> prop
<!-- Now, fill out the specs. Please include units where appropriate (main comes first, alt in parentheses). If an item doesn't apply leave it blank. For instructions on using |more general=, |more performance=, |power original=, and |thrust original= see [[Template talk:Aircraft specifications]]. -->
|ref=
|crew= 1
|capacity= 3-4
|length main=7.54 米
|length alt= 24 尺 9 英寸
|span main= 12.60 米
|span alt= 46 尺 7 英寸
|height main= 2.30 米
|height alt= 7 尺 7 英寸
|area main= 17.09 米²
|area alt= 184 尺²
|airfoil=
|empty weight main= 960 公斤
|empty weight alt= 2,112 磅
|loaded weight main= 1,510 公斤
|loaded weight alt= 3,322 磅
|useful load main= <!--kg-->
|useful load alt= <!--lb-->
|max takeoff weight main= 1,600 公斤
|max takeoff weight alt= 3,527 磅
|more general=
|engine (prop)= Walter Minor-III
|type of prop= 4-cylinder inline engine
|number of props=2
|power main= 77 kW
|power alt= 105 hp
|power original=
|max speed main= 270 公里/時
|max speed alt= 146 海里, 168 英里
|cruise speed main= <!--km/h-->
|cruise speed alt= <!--knots,mph-->
|never exceed speed main= <!--km/h-->
|never exceed speed alt= <!--knots,mph-->
|stall speed main= <!--km/h-->
|stall speed alt= <!--knots,mph-->
|range main= 1,600 公里
|range alt= 864 海里, 1,000 英里
|ceiling main= 4,400 米
|ceiling alt= 14,400 尺
|climb rate main= 300 米/分鐘
|climb rate alt= 984 尺/分鐘
|loading main= 88 kg/米²
|loading alt= 18 磅/尺²
|thrust/weight=<!--a unitless ratio-->
|power/mass main= 0.08 kW/公斤
|power/mass alt= 0.05 hp/磅
|more performance=
|armament=
|avionics=
}}