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Airworthiness directives › 2016-09-01

AD 2016-09-01 Airworthiness Directives; The Boeing Company Airplanes

Superseded. This directive was replaced by AD 2022-06-07. Work to the current one.
2016-06-06
2016-05-02
39-18499
FAA-2015-1428
Airframe
2022-06-07

Models named: 777-200, -300 series. Read the applicability below — it usually turns on serial or part numbers too.

Applicability*9

This AD applies to The Boeing Company Model 777-200 and -300 series airplanes, certificated in any category, as identified in Boeing Alert Service Bulletin 777-53A0075, Revision 1, dated December 14, 2015.

Compliance

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

Required actions

At the times specified in table 1 of paragraph 1.E., “Compliance,” of Boeing Alert Service Bulletin 777-53A0075, Revision 1, dated December 14, 2015, except as provided in paragraph (j)(1) of this AD: Do a detailed inspection and high frequency eddy current (HFEC) inspections for cracking of the left and right side forward outer chords of the STA 2370 pivot bulkhead, and do all applicable related investigative and corrective actions, in accordance with the Accomplishment Instructions of Boeing Alert Service Bulletin 777-53A0075, Revision 1, dated December 14, 2015, except as provided in paragraph (j)(2) of this AD. Do all applicable related investigative and corrective actions before further flight. Repeat the inspections thereafter at the applicable intervals specified in table 1 of paragraph 1.E., “Compliance,” of Boeing Alert Service Bulletin 777-53A0075, Revision 1, dated December 14, 2015, until the modification specified in paragraph (i) of this AD is done.

Unsafe condition

This AD was prompted by reports of fatigue cracking of the forward outer chord of the station (STA) 2370 pivot bulkhead. We are issuing this AD to detect and correct fatigue cracking of the outer flanges of the left and right side forward outer chords of the STA 2370 pivot bulkhead, which could result in a severed forward outer chord and consequent loss of horizontal stabilizer control.

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