A、 If the repair scheme must be changed,the approval of the design authority is hardly got.
B、 If the design authority need change the repair scheme,it can get the approval.
C、 If it is necessary to change the repair scheme,get the approval of the design authority.
答案：C
A、 If the repair scheme must be changed,the approval of the design authority is hardly got.
B、 If the design authority need change the repair scheme,it can get the approval.
C、 If it is necessary to change the repair scheme,get the approval of the design authority.
答案：C
A. The operational test of HFS-900D transceivers is an internal functions check of the HF transceiver and it is a BITE test.
B. The BITE test for the HFS-900D transceivers is the operation test that does the inner check of the HF transceiver.
C. The check of the internal functions of the HF transceiver is a BITE test related to HFS-900D transceivers.
A. If the brackets are not damaged,continue the procedure.
B. In the absence of damage to the brackets,recall the process.
C. When bracket damage occurs,recall the procedure.
A. After 10 flight cycles or 25 flight hours,which comes first,the rod end bearing shall be discarded if its wear is greater than 0.010 inch of diameter.
B. If the rod end bearing wear is greater than 0.010 inch in radial play,reject it within next 10 flight cycles or 25 flight hours whichever comes first.
C. Destroy the rod end bearing during 10 flight cycles or 25 flight hours when its wear is more than 0.010 inch of its radius,whichever comes first.
A. The manufacturer may set up steps and feedback the airworthy conditions discovered when complying.
B. The manufacturer may establish procedures to provide feedback on unairworthy conditions that were discovered when complying.
C. The manufacturer may establish procedures and comply regulations to provide feedback on unairworthy conditions.
A. 紧握住缸体。
B. 轻轻握住圆柱体。
C. 紧握住作动筒。
A. When the temperature is below zero,depressurize the water system.
B. If the temperature drops below zero,deflate the water system.
C. If the temperature decreases to less than zero,drain the water system.
A. Correct operation of the parts does not allow dents to occur.
B. Dents that have an influence on the correct operation of the parts are not allowed.
C. Dents can prevent correct operation of the parts,so they are not permitted.
A. The complexity and stringency of this test or check are different from the operation conditions of the unit.
B. The test or check will change in complexity and stringency no matter what the conditions under which the unit operates.
C. Such tests or checks will vary in complexity and stringency according to the conditions under which the unit functions.
A. 当飞机制造商选定的最大持续功率大于发动机型号数据单上的额定最大持续功率的时候,飞机型号数据单内列出来的最大持续功率表明是遵循了相应适航标准,同时这个数值也会呈现在《飞行员操作手册》中。
B. 当飞机制造商选定的最大连续功率小于发动机型号数据单上的额定最大连续功率时,飞机型号数据单内所列出的最大连续功率用以表明对相应适航标准的符合性,并应在《飞行员操作手册》中载明。
C. 当飞机制造商选定的最大持续功率小于发动机型号数据单上的额定最大持续功率的时候,发动机型号数据单内列出来的最大持续功率表明是遵循了相应适航标准,同时这个数值也会呈现在《飞行员操作手册》中。
D. B.当飞机制造商选定的最大连续功率小于发动机型号数据单上的额定最大连续功率时,飞机型号数据单内所列出的最大连续功率用以表明对相应适航标准的符合性,并应在《飞行员操作手册》中载明。
E. C.当飞机制造商选定的最大持续功率小于发动机型号数据单上的额定最大持续功率的时候,发动机型号数据单内列出来的最大持续功率表明是遵循了相应适航标准,同时这个数值也会呈现在《飞行员操作手册》中。
A. 描述飞机燃油系统时,应说明交替供油和燃油运输(如适用)。
B. 描述飞机燃油系统时,应提供交输供油和燃油传输(如适用)相关描述。
C. 描述飞机燃油系统时,应说明交叉供油和燃油传递(如适用)。
