Airworthiness Directive

AD 2014-15-01 Amendment 39-17903

Federal Aviation Administration · 14 CFR part 39

FR document
2014-17053
Amendment
39-17903
Published
2014-07-23
Models covered
1
Last live check
Not yet re-verified
AD

2014-15-01

FR doc 2014-17053

AD 2014-15-01Published 2014-07-23Effective 2014-08-27

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.

Full official 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.

Applies to 1 model in our index