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Airworthiness directives › 2012-09-14

AD 2012-09-14 Airworthiness Directives; The Boeing Company Airplanes

2012-06-21
2012-05-17
39-17049
FAA-2012-0105
Airframe
—

Models named: 777-200, -200LR, -300, -300ER, 777F 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, -200LR, -300, -300ER, and 777F series airplanes; certificated in any category; as identified in Boeing Alert Service Bulletin 777-52A0038, Revision 1, dated June 24, 2010.

Compliance

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

Required actions

At the applicable times specified in paragraph 1.E., “Compliance,” of Boeing Alert Service Bulletin 777-52A0038, Revision 1, dated June 24, 2010, except as specified in paragraph (i) of this AD: Do a detailed inspection for fractured and/or missing latch pin retention bolts of the latch pin fittings of the lower sill of the forward large cargo door, and do all applicable related investigative and corrective actions, in accordance with the Accomplishment Instructions of Boeing Alert Service Bulletin 777-52A0038, Revision 1, dated June 24, 2010, except as provided by paragraph (h) of this AD. Do all applicable related investigative and corrective actions at the applicable times specified in paragraph 1.E., “Compliance,” of Boeing Alert Service Bulletin 777-52A0038, Revision 1, dated June 24, 2010. Repeat the inspection thereafter at the applicable time specified in paragraph 1.E., “Compliance,” of Boeing Alert Service Bulletin 777-52A0038, Revision 1, dated June 24, 2010, except as specified in paragraph (j) of this AD.

Unsafe condition

This AD was prompted by reports of fractured and missing latch pin retention bolts that secure the latch pins on the forward cargo door. We are issuing this AD to detect and correct fractured and missing latch pin retention bolts, which could result in potential separation of the cargo door from the airplane and catastrophic 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