Altitude loss of more than 100 feet and pitch below the horizon of more than thirty degrees during recovery from stalls should be added.
答案解析
解析:
题干的核心内容是:
- 在恢复失速过程中,
- 高度损失超过100英尺,
- 俯仰角度低于地平线30度,
- 这些数据应被记录和增加。
### 选项解析
**A. 从失速状态恢复期间,应增加超过100英尺的高度损失和低于地平线30度的俯仰角。**
这个选项在表达上略显模糊,不够准确。虽然它提到需要增加高度损失和俯仰角度,但没有清楚地说明这些数据是如何被应用的,容易造成理解上的混淆。
**B. 应增加高度损失超过100英尺和俯仰操纵(低头)超过30度的失速改出数据。**
这个选项正确地描述了应记录和增加的数据类型,并明确了这些数据是用来补充失速恢复过程中的记录。这是标准的飞行操作要求中对失速恢复过程的要求,确保飞行员在失速恢复中保持足够的安全裕度。
**C. 应增加从失速恢复过程中超过100英尺的高度损失和超过30度的地平面以下俯仰。**
这个选项的表达也有一定的准确性,但“地平面以下”这样的表述可能让人混淆,因为“地平面以下”并不是标准的飞行术语。标准的描述应该是“低于地平线”,并且这个选项的表达方式不如B选项清晰。
### 进一步解析与例子
假设你正在进行一次飞行训练,教练告诉你在进行失速恢复的过程中,你的任务是记录和评估恢复过程中的高度损失和俯仰角度。如果你在失速恢复的过程中高度损失超过100英尺,同时俯仰角度低于地平线30度,这些数据会被用来帮助改进飞行操作和训练。
**联想与例子:**
想象你正在开车下坡,车速很快,突然你要刹车。你刹车的过程就像是飞机的失速恢复。假设你看到车速表突然下滑了100公里/小时,同时车头的俯仰角度(即车头是否抬起或压低)低于水平面30度。你需要记录下这些数据,以确保你知道在刹车过程中你车辆的表现。飞行中类似,飞行员需要确保在失速恢复过程中,任何可能的飞行参数都要准确记录,以避免未来的操作中出现安全问题。
### 总结
综上所述,**选项B**是最准确的。它明确地表示在失速恢复过程中需要记录和增加的数据类型,以及这些数据的应用方法。通过准确记录这些数据,飞行员可以确保在实际飞行中能够安全地恢复失速,避免可能的危险情况。
相关知识点:
失速改出增加数据要记全
相关题目
The intensity of the LCD backlighting is obtained from the aircraft dimming bus and a measurement of the ambient light in the cockpit. The ambient light is sensed by a photodiode on the front bezel.
Accumulator, in a computer, is a special storage register associated with the arithmetic logic unit, used for holding the results of a computation or data transfer.
Some tanks are called trim tanks because as well as storing fuel, they are also used to trim the aircraft.
For a quick passenger and crew evacuation in case of emergency, all these main entry doors can also be used as emergency exit doors.
This is a scheduled maintenance task to see if the battery charger and battery pack for the integrated standby flight display are operational.
When there are several words in English for the same thing (synonyms), STE permits one of these synonyms to the exclusion of the others.
An aircraft has five main structural units which consist of the fuselage, the wings, the stabilizers, the flight control surfaces and the landing gears.
The airspeeds which may enhance the safety of operations shall be provided as a preface to the Normal Procedures Section.
It is understood that compliance with the above can in some instances cause duplication of test procedures, which is acceptable.
The inspection/check portion shall provide information and procedure necessary to gain access to and inspection or check of a system, a unit, or an area.
