(2)
Replace any damaged pitot-static probes, ref (AMM 34-11-11).
S 216-004-B00
(3)
Do a visual inspection of the fuselage skin around the pitot-static probes on the left and right sides of the airplane in Section 41. Fig. 601.
S 216-003-B00
NOTE: Look for damage or previous repairs.
____
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(4) If there is damage other than dents or bulges, do a repair as shown in SRM 53-10-01.
NOTE: When you do the repair, make sure that it is within the
____
limits shown in SRM 51-10-01.
S 226-006-B00
(5) If there are dents or bulges within the inspection area, check to see if you hav e one of the following condition:
(a)
Is there a dent or bulge that is beyond the limits shown in SRM 51-10-01.
(b)
Is the total number of dents and bulges on the airplane greater than 2.
NOTE: You can have a total of two dents or bulges on one side
____ of the airplae or you can have one dent or bulge on both sides of the airplane.
S 356-013-B00
(6) If you find any of the above conditions, repair the damage as shown in the SRM.
NOTE: If you cannot repair the damage then contact Boeing with the
____
following information:
-
the location of the damage.
-
the shape of the damage.
-
the orientation of the damage.
-
the height or depth of the damage.
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NOTE: You should measure the skin on the left and right sides of
____ the airplane as shown in Part II, Skin Measurement. To get the measurement tool contact Boeing. When you contact Boeing, you should also submit a purchase order for Technical Service Agreement (TSA). With a TSA, Boeing will analyze the measurement data and determine if the skin is within the limits necessary to RVSM.
If the analysis determines that the skin waviness is within the limits necessary for RVSM, Boeing will give an FAA form 8110-3 to the airline recommending approval.
S 216-026-B00
(7) If the inspection area has an external repair, or if the airplane has a flush repair that extends under a frame or stringer, see if you have one of the following conditions:
-Does the airplane have an external repair that is not within the limits shown in the SRM.
-Are the total number of repairs that are within, or extend into, the inspection area greater than 2.
NOTE: You can have a total of two repairs on one side of the
____ airplane or you can have one repair on both sides of the airplane.
NOTE: In step 2 above, do not count flush repairs that do not
____ extend under frames or stringers. Flush repairs that do not extend under frames or stringers do not make the skin bulge.
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(8) If you have any of the above conditions, you can remove the repairs and install new repairs with none of these conditions, or you can contact Boeing with the following information about the existing repairs.
-
the location of the repairs.
-
the shape of the repairs.
-
the orientation of the repairs.
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本文链接地址：737-300 400 500 AMM 飞机维护手册 结构 STRUCTURES(4)
