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Airworthiness directives › 2012-04-09

AD 2012-04-09 Airworthiness Directives; The Boeing Company Airplanes

2012-04-10
2012-03-06
39-16965
FAA-2008-0107
Airframe
—

Models named: 747-100, 747-100B, 747-100B SUD, 747-200B, 747-200C, 747-200F, 747-300, 747-400, 747-400D, 747-400F. Read the applicability below — it usually turns on serial or part numbers too.

Applicability*9

This AD applies to The Boeing Company Model 747-100, 747-100B, 747-100B SUD, 747-200B, 747-200C, 747-200F, 747-300, 747-400, 747-400D, 747-400F, 747SP, and 747SR series airplanes; certificated in any category; as identified in Boeing Service Bulletin 747-53A2563, Revision 4, dated May 6, 2010.

Compliance

You are responsible for having the actions required by this AD performed within the compliance times specified, unless the actions have already been done.

Required actions

At the applicable times specified in Tables 1 through 21 and Table 25 in paragraph 1.E., “Compliance,” of Boeing Service Bulletin 747-53A2563, Revision 4, dated May 6, 2010, except as provided in paragraph (h) of this AD, do detailed inspections for scribe lines of affected lap and butt splices, wing-to-body fairing locations, and external repair and cutout reinforcement areas, and do all applicable related investigative and corrective actions, by accomplishing all actions specified in the Accomplishment Instructions of Boeing Service Bulletin 747-53A2563, Revision 4, dated May 6, 2010, except as provided by paragraph (i) of this AD. Note 1 to paragraph (g) of this AD: The inspection exemptions noted in paragraph 1.E., “Compliance,” of Boeing Service Bulletin 747-53A2563, Revision 4, dated May 6, 2010, apply to this AD, provided that the operator meets the requirements stated in each applicable exemption.

Unsafe condition

This AD results from reports of scribe lines found at lap joints and butt joints, around external doublers and antennas, and at locations where external decals had been cut. We are issuing this AD to detect and correct scribe lines, which can develop into fatigue cracks in the skin and cause sudden decompression of the airplane.

Affected ADs

None.

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The directive text above is reproduced from the Federal Register, a work of the United States government and in the public domain. The separation into applicability, compliance and required actions is TrackAD's.*1