A、 System test contain part of the adjustment specifications and tolerances.
B、 System test is required to maintain a unit performance at its lowest design specifications.
C、 System test may cover other tests, such as operational test.
答案：C
A、 System test contain part of the adjustment specifications and tolerances.
B、 System test is required to maintain a unit performance at its lowest design specifications.
C、 System test may cover other tests, such as operational test.
答案：C
A. An alphanumeric identifier is an assembly of characters and numbers. It can recognize something.
B. An symbolic-numeric identifier is an assembly of symbols and numbers. It can identifies something.
C. An alphanumeric identifier is a combination of letters and numbers that identifies something.
A. The CFM56-7 is a high roadway, dual rotor, axial flow turbofan engine. The start valve is a butterfly shutoff valve;
B. The CFM56-7 is a high aisle, dual rotor, axial flow turbofan engine. The start valve is a butterfly shut down valve;
C. The CFM56-7 is a high bypass, dual rotor, axial flow turbofan engine. The start valve is a butterfly shutoff valve;
A. ASSEMBLE
B. INSTALL
C. REMOVE
A. Functional check L VHF radio found static interference and noise.
B. Functional check of L VHF radio shown turbulence and static noise.
C. Functional check of L VHF radio revealed interference of static with noise.
A. 该程序应在飞机最后一次运行之后至少2小时完成。这将确保记录的减震支柱数值是准确的。
B. 该程序应在飞机最后一次运行后2小时之内完成。这将确保记录的减震支柱数值是准确的。
C. 应在飞机至少运行2小时,最后再完成该程序,这将确保记录的减震支柱数值是准确的
A. Artificial feel used in flight control system, its direction is opposition to pilot’s movement.
B. Artificial feel force is inversely proportional to the aerodynamic loads acting on the control surfaces.
C. Artificial feel in aircraft flight control system is used in manual flight control of the aircraft.
A. 通过最少两个全循环操作副翼,并操作至其最大行程
B. 至少完整操作副翼两个全循环至其最大行程
C. 操作副翼最小两个单位,至其最大行程
A. That portion of the system within the aircraft which connects external electrical power to the aircraft＇s electrical system.
B. That portion of the system within the aircraft which connects service electrical power to the aircraft＇s electrical system.
C. That portion of the system within the aircraft which connects integral electrical power to the aircraft＇s electrical system.
A. 从右侧页面开始记录每个部分
B. 每个部分都要从右侧页面开始
C. 每个部分都写在右侧页面上
A. 与本规范的符合性相关的重要意见应予以公布。
B. 对于和本规范相抵触的重大意见应予以公布。
C. 应发布符合本规范的重要议题。
