2021-25-11
FR doc 2021-27510 · 86 FR 72186AD 2021-25-11Published 2021-12-21Effective 2022-01-25
Requires the actions in the revised service information.
Supersedes an earlier directive that is not in our index. See the official text.
Full official abstract
The FAA is superseding Airworthiness Directive (AD) 78-02-03, which applied to all Piper Aircraft, Inc. (Piper) Model PA-23-250 airplanes. AD 78-02-03 required repetitively inspecting the stabilator tip tube and weight assemblies for cracks, inspecting for missing rivets and screws, replacing the forward rib/horn assemblies, and reinforcing the mounting. Since AD 78-02-03 was issued, Piper developed a newly-designed stabilator, which is not subject to the unsafe condition, and revised its service information. This AD retains the actions of AD 78-02-03, but reduces the applicability and requires the actions in the revised service information. The FAA is issuing this AD to address the unsafe condition on these products.
More directives for Piper PA-23 Apache/Aztec
- AD 2017-15-05 Airworthiness Directives; Piper Aircraft, Inc. Airplanes Effective 2017-08-28
- AD 2015-24-05 Airworthiness Directives; Piper Aircraft, Inc. Airplanes Effective 2016-01-12
- AD 2009-13-06 R1 Airworthiness Directives; Piper Aircraft, Inc. Airplanes Effective 2011-11-03
- AD 2009-13-06 Airworthiness Directives; Piper Aircraft, Inc. PA-23, PA-31, and PA-42 S... Effective 2009-07-24
- AD 2005-01-10 Airworthiness Directives; The New Piper Aircraft, Inc. Models PA-23-235,... Effective 2005-02-22
