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Airworthiness directives › 2015-21-08

AD 2015-21-08 Airworthiness Directives; The Boeing Company Airplanes

Superseded. This directive was replaced by AD 2018-09-13. Work to the current one.
2015-11-12
2015-10-28
39-18301
FAA-2015-4205
Airframe
2018-09-13

Models named: 737-100, -200, -200C, -300, -400, -500 series. Read the applicability below — it usually turns on serial or part numbers too.

Applicability*9

This AD applies to The Boeing Company Model 737-100, -200, -200C, -300, -400, and -500 series airplanes, certificated in any category, as identified in Boeing Alert Service Bulletin 737-57A1326, dated September 22, 2015; except for Group 1, configuration 1, airplanes identified in Boeing Alert Service Bulletin 737-57A1326, dated September 22, 2015.

Compliance

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

Required actions

Except as provided by paragraph (h) of this AD, at the applicable time specified in paragraph 1.E., “Compliance,” of Boeing Alert Service Bulletin 737-57A1326, dated September 22, 2015: Do an eddy current inspection for any cracking in the inspar upper skin, and repair doublers and repair triplers, as applicable, and do all applicable related investigative and corrective actions, in accordance with the Accomplishment Instructions of Boeing Alert Service Bulletin 737-57A1326, dated September 22, 2015; except as provided by paragraph (h) of this AD. Do all applicable related investigative and corrective actions before further flight. Repeat the inspection thereafter at the applicable intervals specified in paragraph 1.E., “Compliance,” of Boeing Alert Service Bulletin 737-57A1326, dated September 22, 2015.

Unsafe condition

This AD was prompted by a report that an operator discovered a crack in the inspar upper skin at wing buttock line 157, just forward of the rear spar on the right wing. We are issuing this AD to detect and correct any cracking in the inspar upper skin and rear spar upper chord, which could result in the inability of the structure to carry limit load, or result in a fuel leak, which could prevent continued safe flight and landing.

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