EASA AD US-2020-26-16
Feb 9, 2021NOT ADOPTED - EASA DECISION ATTACHED
The Federal Aviation Administration (FAA) Final Rule titled Airworthiness Directive 2020-26-16 addresses certain Piper Aircraft, Inc. models including PA-28-151, PA-28-161, PA-28-181, PA-28-235, PA-28R-180, PA-28R-200, PA-28R-201, PA-28R-201T, PA-28RT-201, PA-28RT-201T, PA-32-260, PA-32-300, PA-32R-300, PA-32RT-300, and PA-32RT-300T airplanes. This directive responds to a safety concern involving wing separation caused by fatigue cracking in the lower main wing spar cap. It mandates inspections and potential replacement of affected wing spars to ensure continued airworthiness.
- Piper Aircraft PA-28 (Archer)
- Piper Aircraft PA-28 (Cadet)
- Piper Aircraft PA-28 (Cherokee)
- Piper Aircraft PA-28 (Warrior)
- Piper Aircraft PA-28R (Arrow)
- Piper Aircraft PA-32 (Cherokee Six)
- Piper Aircraft PA-32R (Lance)
- Piper PA-28-151
- Piper PA-28-161
- Piper PA-28-181
- Piper PA-28-235
- Piper PA-28R-180
- Piper PA-28R-200
- Piper PA-28R-201
- Piper PA-28R-201T
- Piper PA-28RT-201
- Piper PA-28RT-201T
- Piper PA-32-260
- Piper PA-32-300
- Piper PA-32R-300
- Piper PA-32RT-300
- Piper PA-32RT-300T