Airworthiness Directives; Boeing Model 727, 727-100C, 727-200F, and 727C Series Airplanes
airworthiness · Rule · Final rule. · Published 2004-02-18 · Effective 2004-03-24 · 69 FR 7550
Document
Document number
04-3130
Federal Register citation
69 FR 7550
Type
Rule
Action
Final rule.
Category
airworthiness
Publication date
2004-02-18
Effective date
2004-03-24
FAA docket
Docket No. 2003-NM-191-AD
Abstract
This amendment adopts a new airworthiness directive (AD), applicable to certain Boeing Model 727, 727-100C, 727-200F, and 727C series airplanes, that requires repetitive open-hole high frequency eddy current inspections for cracks in the fuselage skin, strap (bearstrap), and doubler at the forward and aft hinge fittings for the main deck cargo door, and repair of any cracks found. This action is necessary to detect and correct such cracks, which could reach critical crack length and result in rapid decompression of the airplane. This action is intended to address the identified unsafe condition.