Airworthiness Directives; Boeing Model 747-100, 747-100B, 747-100B SUD, 747-200B, 747-200C, 747-200F, 747-300, 747-400, 747SR, and 747SP Series Airplanes
airworthiness · Rule · Final rule. · Published 2009-03-16 · Effective 2009-04-20 · 74 FR 11013
Document
Document number
E9-4973
Federal Register citation
74 FR 11013
Type
Rule
Action
Final rule.
Category
airworthiness
Publication date
2009-03-16
Effective date
2009-04-20
FAA docket
Docket No. FAA-2008-1072
Abstract
We are adopting a new airworthiness directive (AD) for certain Boeing Model 747-100, 747-100B, 747-100B SUD, 747-200B, 747-200C, 747- 200F, 747-300, 747-400, 747SR, and 747SP series airplanes. This AD requires inspecting for skin cracks at the shear tie end fastener locations of the fuselage frames, and repairing cracks if necessary. This AD results from a wide-spread fatigue damage assessment of Model 747 airplanes. We are issuing this AD to detect and correct cracks in the fuselage skin that can propagate and grow, resulting in a loss of structural integrity and a sudden decompression of the airplane during flight.