Airworthiness Directive · Amendment 39-9622 · Piper Aircraft Inc. Airplanes
Piper Aircraft Inc. Airplanes
This AD applies to Piper Aircraft Inc. PA-31, PA-31-300, PA-31-325, PA-31-350.
The models as the FAA's AD index lists them. The serial ranges, installed parts and exceptions are in the AD itself: read it at the FAA.
This amendment supersedes Airworthiness Directive (AD) 80-14-06, which currently requires the following on The New Piper Aircraft, Inc. (Piper) Models PA31, PA31-300, PA31-325, and PA31-350 airplanes: repetitively inspecting the outboard flap tracks, wing rib flanges, and the rear spar web at Wing Station (WS) 147.5 on each wing, and modifying the area at WS 147.5 on both wings if any cracks are found as terminating action for the repetitive inspection requirement. The Federal Aviation Administration's policy on aging commuter-class aircraft is to eliminate or, in certain instances, reduce the number of certain repetitive short-interval inspections when improved parts or modifications are available. This action retains the repetitive inspection requirement of AD 80-14-06, and requires modifying the area at WS 147.5 on both wings as terminating action for the repetitive inspection requirement. The actions specified in this AD are intended to prevent structural failure under certain load conditions caused by cracked areas at WS 147.5, which, if not detected and corrected, could result in loss of control of the airplane.
The aircraft, engines and makers this AD names, by the model designations in its text. A model listed here may still be outside the AD's serial ranges.
