Airworthiness Directives; Boeing Model 737-600, -700, -700C, -800, and -900 Series Airplanes
airworthiness · Rule · Final rule. · Published 2008-06-11 · Effective 2008-07-16 · 73 FR 32991
Document
Document number
E8-12761
Federal Register citation
73 FR 32991
Type
Rule
Action
Final rule.
Category
airworthiness
Publication date
2008-06-11
Effective date
2008-07-16
FAA docket
Docket No. FAA-2007-29333
Abstract
We are adopting a new airworthiness directive (AD) for certain Boeing Model 737-600, -700, -700C, -800, and -900 series airplanes. This AD requires various repetitive inspections to detect cracks along the chemically milled steps of the fuselage skin or missing or loose fasteners in the area of the preventative modification or repairs, replacement of the time-limited repair with the permanent repair if applicable, and applicable corrective actions if necessary, which would end certain repetitive inspections. This AD results from a fatigue test that revealed numerous cracks in the upper skin panel at the chemically milled step above the lap joint. We are issuing this AD to detect and correct such fatigue-related cracks, which could result in the crack tips continuing to turn and grow to the point where the skin bay flaps open, causing decompression of the airplane.