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
Official Documents
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