96-20-08
FR doc 96-24886 · 61 FR 50999AD 96-20-08Published 1996-09-30Effective 1996-11-14
Requires repetitively inspecting acrylic cabin and cockpit side windows for cracks on certain Fairchild Aircraft SA26, SA226, and SA227 series airplanes, and, if cracks are found that exceed certain limitations, replacing that window.
Supersedes an earlier directive that is not in our index. See the official text.
Full official abstract
This amendment supersedes AD 93-19-06, which currrently requires repetitively inspecting acrylic cabin and cockpit side windows for cracks on certain Fairchild Aircraft SA26, SA226, and SA227 series airplanes, and, if cracks are found that exceed certain limitations, replacing that window. This action maintains the requirement of repetitively inspecting the cabin and cockpit side windows, and adds a life limit for the single-pane cockpit side windows. Acrylic window failures on the affected airplanes prompted this action. The actions specified by this AD are intended to prevent acrylic cabin or cockpit side window failures, which could result in airframe damage and decompression injuries.
More directives for Fairchild SA226/SA227 Metro
- AD 2021-01-02 Airworthiness Directives; M7 Aerospace LLC Airplanes Effective 2021-02-26
- AD 2017-07-01 Airworthiness Directives; M7 Aerospace LLC Models Airplanes Effective 2017-05-05
- AD 2016-25-12 Airworthiness Directives; M7 Aerospace LLC Effective 2017-01-12
- AD 2016-15-02 Airworthiness Directives; M7 Aerospace LLC Airplanes Effective 2016-08-26
- AD 2016-10-01 Airworthiness Directives; M7 Aerospace LLC Airplanes Effective 2016-06-15
