135.  The aircraft engines, the APU or a ground air source can supply compressed air to the pneumatic system. The distribution system supplies the compressed air from the different sources to the user systems.飛機(jī)發(fā)動(dòng)機(jī)、APU、地面氣源能夠向氣動(dòng)系統(tǒng)提供增壓空氣。分配系統(tǒng)將不同來源的增壓空氣提供到用戶系統(tǒng)

136.  The aircraft pressure sensor delivers an electric analog signal representative of

aircraft pressure. This analog signal is converted to digital information to be processed by the digital section.飛機(jī)壓力傳感器發(fā)送一個(gè)代表飛機(jī)外壓力的模擬電子信號(hào)。這個(gè)模擬信號(hào)轉(zhuǎn)換為數(shù)字信息,并由數(shù)字部分進(jìn)行處理。

137.  The aircraft wing is a continuous structure which goes through the fuselage between Frames 36 and 42. The center wing is part of the fuselage and gives attachment points for the outer wings.飛機(jī)機(jī)翼是一個(gè)連續(xù)的結(jié)構(gòu)體，通過機(jī)身隔框 36和42之間。中央翼是機(jī)身的一部分，為外側(cè)機(jī)翼提供安裝點(diǎn)。

138.  The APU engine is located in the aft end of the fuselage, behind the pressure bulkhead and below the horizontal stabilizer. The APU engine is completely enclosed in a titanium shroud.APU發(fā)動(dòng)機(jī)安裝于機(jī)身尾部、壓力隔板后面及水平安定面下方。APU發(fā)動(dòng)機(jī)被完全地封進(jìn)一個(gè)鈦防護(hù)罩中。

139.  The APU usually takes its fuel supply from the LH engine-feed line, but when the cross-feed valve is open, the RH engine-feed line can also supply the APU with fuel.APU通常從左發(fā)動(dòng)機(jī)供油管路獲得燃油，如果交輸活門打開，右發(fā)動(dòng)機(jī)供油管路也可以供應(yīng) APU燃油。

140.  The basic yaw control is hydro-mechanical as well as the alternate horizontal stabilizer

control, thus providing the ability to keep the aircraft in flight during a temporary complete loss of electrical power.基本的偏航操縱是液壓機(jī)械式，如同備用水平安定面操縱。因此，當(dāng)飛機(jī)電力突然完全消失，飛機(jī)仍然具有保持飛行的能力。

141.  The Bulk cargo compartment has tie down/ attachment points for the door nets and for the nets and straps which keep the bulk cargo in place.散裝貨艙安裝有連接門網(wǎng)和散貨固定網(wǎng)及束帶的系留點(diǎn)。