clave 2

1) The changed data is identified... b) By a revision code on the left side of each new or changed page. wwwe.

2) Which document gives data on standards and vendor for materials used in the construction and repair of an airplane?. a) Boeing Materials Specification. fff.

3) Which document gives data on procedures and processes used in the manufacturing of Boeing airplanes?. b) Boeing Process Specification. fff.

4) A cold working process that is applied to aluminum and steels to improve their fatigue life is called... a) Shot Peening. fff.

5) Most of the sheet metal used in the structure of the airplane is... b) Aluminum alloy. aaa.

6) those fasteners that require destroyin part or all the fastener when removing it fasteners the airplane are classifiedas. c) Permanent fasteners. qqqq.

7) The distance from the center of the fastener hole to the nearest edge of the part is known as…. b) Edge Margin. ssss.

8) After a heavy landing…. a) An alignment check is often necessary. ccc.

9) What does BMS mean?. b) Boeing Material Specification. rrr.

10) What does BPS mean. b) Boeing Process Specification. hhhh.

11) Which is the page block for the repair information in the Boeing SRM?. a) Page Block 201-999. ttt.

12) What information do we find on page block 001-099?. a) Identification. yyy.

13) Where do we find information on allowable damages?. b) Page Block 101-199. uuuu.

14) The distance between two adjacent fasteners is…. a) Fasteners Pitch. iiii.

15) There are two basic formats of the SRM: the out-of-production airplanes are in the…. b) Old Format. pppp.

16) The standard numbering system for the Structural Repair Manuals conforms to ATA 100. This numbering system has…. c) Three elements with three numbers in each element. bbbbb.

17) Which chapter provides general information that is applicable to all chapters?. a) Chapter 51. nnnn.

18) Within the old format SRMs, the allowable damage data is provided. a) In the beginning of each chapter. mmmm.

19) In the SRM, figure 104…. a) Is from the Identification Block. dddd.

20) The normal revision time for SRMs is. Every 90 days for in-production airplanes. qqqq.