Summary
We are adopting a new airworthiness directive (AD) for all Boeing Model 737-300, -400, and -500 series airplanes. This AD requires repetitive inspections for discrepancies of the fuse pins of the inboard and outboard midspar fittings of the nacelle strut, and corrective actions if necessary. This AD results from a report of corrosion damage of the chrome runout on the head side found on all four midspar fuse pins of the nacelle strut. Additionally, a large portion of the chrome plate was missing from the corroded area of the shank. We are issuing this AD to detect and correct discrepancies of the fuse pins of the inboard and outboard midspar fittings of the nacelle strut, which could result in reduced structural integrity of the fuse pins and consequent loss of the strut and separation of the engine from the airplane.
Directive Details
AD Number
FAA-2008-0357
Document Number
E8-23658
Type
Rule
Publication Date
October 9, 2008
Effective Date
November 13, 2008
Affected Manufacturer
Boeing Model 737-300, -400, and -500 Series
Criticality
important
Emergency
No
Docket ID
Docket No. FAA-2008-0357
Topics
Official Documents
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