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Airworthiness directives › 2014-08-08

AD 2014-08-08 Airworthiness Directives; the Boeing Company Airplanes

2014-06-03
2014-04-29
39-17832
FAA-2013-0837
Airframe
—

Models named: 737-200, -200C, -300, -400, -500 series. Read the applicability below — it usually turns on serial or part numbers too.

Applicability*9

(1) This AD applies to The Boeing Company Model 737-200, -200C, -300, -400, and -500 series airplanes, certificated in any category, without an airstair door cutout, as identified in Boeing Alert Service Bulletin 737-53A1329, dated June 4, 2013. (2) Installation of Supplemental Type Certificate (STC) ST01219SE ( http://rgl.faa.gov/Regulatory_and_Guidance_Library/rgstc.nsf/0/be866b732f6cf31086257b9700692796/$FILE/ST01219SE.pdf ) does not affect the ability to accomplish the actions required by this AD. Therefore, for airplanes on which STC ST01219SE is installed, a “change in product” alternative method of compliance (AMOC) approval request is not necessary to comply with the requirements of section 39.17 of the Federal Aviation Regulations (14 CFR 39.17).

Compliance

Comply with this AD within the compliance times specified, unless already done.

Required actions

Except as provided by paragraph (i)(1) of this AD, at the applicable times specified in paragraph 1.E., “Compliance,” of Boeing Alert Service Bulletin 737-53A1329, dated June 4, 2013, do the actions specified in paragraph (g)(1) or (g)(2) of this AD, as applicable. (1) For Group 1 airplanes, as identified in Boeing Alert Service Bulletin 737-53A1329, dated June 4, 2013: Except as provided by paragraph (i)(2) of this AD, inspect the lower corners of the forward entry doorway for cracking, using a method approved in accordance with the procedures specified in paragraph (j) of this AD. (2) For Group 2 and Group 3 airplanes, as identified in Boeing Alert Service Bulletin 737-53A1329, dated June 4, 2013: At the forward entry doorway lower forward and aft corners, as applicable, do an internal detailed inspection of the skin assembly and bear strap, an internal high frequency eddy current (HFEC) inspection of the bear strap, and external detailed and HFEC inspections of the skin assembly for cracking, in accordance with Part 2 of the Accomplishment Instructions of Boeing Alert Service Bulletin 737-53A1329, dated June 4, 2013. If no cracking is found during any inspection required by this paragraph: Except as provided by paragraph (i)(1) of this AD, repeat the applicable inspections at the applicable time specified in paragraph 1.E., “Compliance,” of Boeing Alert Service Bulletin 737-53A1329, dated June 4, 2013.

Unsafe condition

This AD was prompted by reports of cracking found in the skin at the lower aft corner of the forward entry doorway on airplanes that do not have an airstair door cutout. We are issuing this AD to detect and correct cracking in the lower corners of the forward entry doorway, which could lead to crack progression and consequent rapid decompression of the airplane.

Affected ADs

For The Boeing Company Model 737-300, -400, and -500 series airplanes: Certain requirements of AD 2008-09-13, Amendment 39-15494 (73 FR 24164, May 2, 2008), may be affected by certain requirements of this AD.

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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