airworthiness · Rule · Final rule. · Published 2014-07-23 · Effective 2014-08-27 · 79 FR 42660
Document
Document number
2014-17053
Federal Register citation
79 FR 42660
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
M7 Aerospace LLC
Publication date
2014-07-23
Effective date
2014-08-27
FAA docket
Docket No. FAA-2014-0308
Abstract
We are adopting a new airworthiness directive (AD) for M7 Aerospace LLC Models SA227-AT, SA227-AC, SA227-BC, SA227-CC, and SA227- DC airplanes equipped with a bayonet shear pin main cabin door latching mechanism. This AD was prompted by fatigue cracks found in the internal door surround doubler, the fuselage external skin, and the door corner fittings at the fuselage upper forward corner of the main cabin door cutout. This AD requires repetitively inspecting the four corners of the main cabin door cutout for cracks, making necessary repairs, and reporting inspection results to M7 Aerospace LLC. We are issuing this AD to correct the unsafe condition on these products.