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AD FAA-2014-0286

Airworthiness Directives; The Boeing Company Airplanes

Summary

We are adopting a new airworthiness directive (AD) for certain The Boeing Company Model 737-600 and -700 series airplanes. This AD was prompted by reports of cracking in the body station (STA) 727 bulkhead lower frame. This AD requires a detailed and open hole high frequency eddy current (HFEC) inspection of the left- and right-side lower frame webs and inner chords for cracking, and corrective actions and preventative modifications if necessary. This AD also provides for optional terminating action of the repetitive inspections, under certain conditions. We are issuing this AD to detect and correct cracking in a bulkhead lower frame web and inner chord, which could result in a severed frame and induced skin cracks, and could lead to rapid decompression of the fuselage.

Directive Details

AD Number

FAA-2014-0286

Document Number

2015-09805

Type

Rule

Publication Date

April 30, 2015

Effective Date

June 4, 2015

Affected Manufacturer

The Boeing Company

Criticality

important

Emergency

No

Docket ID

Docket No. FAA-2014-0286

Topics

Air transportationAircraftAviation safetyIncorporation by referenceSafety

Official Documents

View all ADs for The Boeing Company →

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