ジェット旅客機の進入時の推力設定に関する一覚書
1992 年 40 巻 457 号 p. 92-102
詳細
1992 年 40 巻 457 号 p. 92-102
A method of thrust control is shown for jetliner during approach. With this method, pilot can reduce airspeed deviation even or less compared with the operation under ATS (auto throttle system). In this way, airspeed can be controlled with adequate thrust change, without extra acceleration or deceleration. Flight record is shown to substantiate this.
