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AD FAA-2014-0341

Airworthiness Directives; the Boeing Company Airplanes

Summary

We are superseding Airworthiness Directive (AD) 2014-03-06 for all the Boeing Company Model 737-100, -200, -200C, -300, -400, and -500 series airplanes. AD 2014-03-06 required repetitive inspections for cracking of the aft support fitting for the main landing gear (MLG) beam, and the rear spar upper chord and rear spar web in the area of rear spar station (RSS) 224.14; and repair if necessary. This AD clarifies two paragraph references. This AD was prompted by a determination that two paragraph references were in error. We are issuing this AD to detect and correct cracking of the aft support fitting for the main landing gear (MLG) beam, and the rear spar upper chord and rear spar web in the area of rear spar station (RSS) 224.14, which could grow and result in a fuel leak and possible fire.

Directive Details

AD Number

FAA-2014-0341

Document Number

2014-14475

Type

Rule

Publication Date

July 10, 2014

Effective Date

July 25, 2014

Affected Manufacturer

the Boeing Company

Criticality

routine

Emergency

No

Docket ID

Docket No. FAA-2014-0341

Topics

Air transportationAircraftAviation safetyIncorporation by referenceSafety

Official Documents

View all ADs for the Boeing Company →

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