3031.封面标题应为“飞行员操作手册”或“飞行员操作手册和 FAA 批准的飞机飞行手册”。

2665.超过此速度时不要放出或收上起落架。

A. Do not extend or retract landing gear above this speed.

B. Do not expand or retract landing gear at this speed.

C. Do not put down or retract landing gear by more than this speed.

673.设备清单应包含所有必需的或可选的设备。

A. The equipment list shall contain all required or optional equipment.

B. All required equipment and facilities should be included in this list.

C. Only optional equipment is described in this equipment list.

2793.The adjustment/test description shall provide instructions for accomplishment of a test or check to assure the integrity as an operational component of a system,subsystem or unit assembly.Such tests or checks will vary in complexity and stringency according to the conditions under which the unit functions.It is not intended that a complex functional test of a complete system and its attendant closer tolerances be performed if the unit replaced reactiviates the system and operates within the confines of a go-no-go specification .

A. 在调试/测试的描述中应提供完成测试或检查的说明,以确保作为一个系统、子系统组件、工作部件的完整性。这样的测试或检查将根据部件运行的条件而在复杂度和严格度上有所不同。如果更换的部件使系统重新启动并在“是/否"规范的限制范围内运行,就不需要进行完整系统的复杂功能测试和更严格的容限测试。

B. 在调试/测试的描述中应提供完成测试或检查的说明,以确保作为一个系统、子系统或组件的一个工作部件的完整性。这样的测试或检查将根据部件运行的条件而在复杂度和严格度上有所不同。如果更换的部件使系统重新启动并在“是/否”规范的限制范围内运行,就不需对整个系统做复杂的功能测试和更严格的容限测试。

C. 在调试/测试的描述中应提供完成测试或检查的说明,以确保作为一个系统、子系统组件、工作部件的完整性。这样的测试或检查将根据部件运行的条件而在复杂度和严格度上有所不同。如果更换的部件使系统重新启动并在“是/否"规范的限制范围内运行,就不需要对整个系统做复杂的功能测试和进一步的容限测试。

2908.在此期间使用经济型功率设置可能会对发动机的寿命有损害。

A. During this period,if you use economy power settings,the engine may be damaged."

B. The use of economy power settings during this period may be detrimental to the engine life."

C. The use of economy power settings during this period may reproduce the engine life."

2093.The indications must agree with the values in the table.

A. 显示器必须与表中的数值一致。

B. 根据显示要求必须与台架上的活门保持相同。

C. 显示结果必须与表中的数值一致。

1886.If you push the LSK that is adjacent to EXIT,then the BITE will take you out of BITE test and put the airplane back to its usual condition.

A. After pressing the LSK next to EXIT,the BITE will take you out of BITE test and the airplane will return to its normal condition.

B. The BITE will continue the BITE test and the airplane will go back to its usual condition when you push the LSK next to EXIT.

C. The BITE will proceed the BITE test and the airplane will go back to its normal configuration after releasing the LSK that is adjacent to EXIT.

6.These parts can easily bend,break or become incorrectly aligned.

A. 这些部件很容易弯曲、断裂或不正确地对齐。

B. 这些部件很容易焊接、损坏或不正确地对齐。

C. 这些部件很容易焊接、断裂或不正确地装配。

2928.充过电的电容器就像一个辅助电瓶。

A. The charged resister acts as a primary battery.

B. The discharged resister acts as a secondary battery.

C. The charged capacitor behaves as a secondary battery.

2865.All of the cracked lugs had two flanged bushings installed in the lug hole per Service Bulletin 2243 or in production to eliminate an earlier problem of migration of straight sleeve bushings into the mating clevises of the stabilizer.

A. 按照服务公告 2243,所有开裂的接耳都有两个凸缘衬套安装在接耳孔中,或者在生产时解决直衬套与安定面配合 U 型槽失配的早期问题。

B. 根据服务公告 2243 或在生产中,所有出现裂纹的接耳都在接耳孔中安装了两个凸缘衬套,以消除直衬套移入到安定面的配合 U 型槽中的早期问题。

C. 根据服务通告 2243,在生产过程中给所有出现裂纹的接耳孔中都安装了两个凸缘衬套,解决了之前直衬套游移到安定面配合 U 型槽的问题。

D. B.根据服务公告 2243 或在生产中,所有出现裂纹的接耳都在接耳孔中安装了两个凸缘衬套,以消除直衬套移入到安定面的配合 U 型槽中的早期问题。

E. C.根据服务通告 2243,在生产过程中给所有出现裂纹的接耳孔中都安装了两个凸缘衬套,解决了之前直衬套游移到安定面配合 U 型槽的问题。

1849.系统的这个部分能够消除或阻止所有翼型表面积冰,包括机翼和尾翼的翼面部分。

A. The portion of the systemis used to eliminate or prevent the formation of ice on all airfoil surfaces,including wings and airfoil sections of the empennage.

B. The portion of the systemis used to dispel or get rid of ice gathering on some aircraft surfaces,including wings and empennage surfaces.

C. The portion of the system is used to eliminate or forbid ice forming on outside parts of all airfoils,including the airfoils of wings and empennage.