FAA Issues AD For Piper GA Airplanes | Aero-News Network
Aero-News Network
RSS icon RSS feed
podcast icon MP3 podcast
Subscribe Aero-News e-mail Newsletter Subscribe

** Airborne/NBAA2014 10.22.14 ** HD iPad-Friendly -- Airborne/NBAA2014 10.22.14 **
** Airborne/NBAA2014 10.21.14 ** HD iPad-Friendly -- Airborne/NBAA2014 10.21.14 **
** Airborne/NBAA2014 10.20.14 ** HD iPad-Friendly -- Airborne/NBAA2014 10.20.14 **

Tue, Feb 05, 2013

FAA Issues AD For Piper GA Airplanes

Will Require The Inspection Of Stabilator Control Cables In Cherokee, Cherokee Six, Seneca, And Seminole Models

The FAA has published in the Federal Register an AD for Piper PA-28, PA-32, PA-34, and PA-44 airplanes. The FAA said AD was prompted by reports of control cable assembly failures that may lead to failure of the horizontal stabilator control system and could result in loss of pitch control.

The AD requires inspections of the stabilator control system and replacement of parts as necessary. We are issuing this AD to correct the unsafe condition on these products. In the discussion posted on the Federal Register Monday, the FAA said that according to NTSB Chair Deborah Hersman, two special airworthiness information bulletins (SAIBs) have been issued that recommend inspecting the entire surface of each cable terminal, turnbuckle, or other cable fittings for corrosion or cracking. Within the past 2 years, the NTSB has investigated two accidents and one incident involving Piper airplanes where control cable assembly failures due to stress corrosion cracking led to failures of the horizontal stabilator control system. She stated that the fact these events continue to occur more than 10 years after the SAIBs were issued shows that the SAIBs were not effective. The NTSB supports the need for this AD.

Piper investigated the possibility of using a commercial product called "scotch-brite" to remove surface corrosion and found it to be acceptable. The FAA said it will change this AD to reference the revised Piper Aircraft, Inc. Mandatory Service Bulletin No. 1245A, dated November 28, 2012, which incorporated cleaning agents and scotch-brite.

The inspection is expected to cost individual owners of the airplanes about $425 according to an estimate provided by the FAA. If it is determined that the stabilator control system needs to be replaced, that repair is estimated to cost the individual owner $1,458 in parts and labor.

The AD is effective March 11.

(Pictured above Piper Cherokee 6. Below (L-R) Piper Seneca, Cherokee, Seminole)

FMI: www.faa.gov


Advertisement

More News

Airborne at NBAA-10.22.14: Legacy 500, Universal InSight, BendixKing AeroWave

Also: GE Honda, Sagem's Active SideStick, Syberjet Update, Techno Aerospace Knows How to Party The FAA handed over certification papers for Embraer's Legacy 500 executive jet durin>[...]

ANN's Daily Aero-Linx (10.24.14)

Homebuilt Homepage: Clubs And Newsletters This page lists Homebuilt related Clubs and Newsletters.>[...]

ANN's Daily Aero-Term (10.24.14): Phase Separation – Aviation Fuel

Phase separation is when a combined liquid separates into two different liquids and may occur when autogas is used for aviation fuel.>[...]

Aero-News: Quote Of The Day (10.24.14)

“I’m excited and humbled by the trust that the ALPA Board of Directors has placed in me with this election.” Source: ALPA President-Elect Tim Canoll.>[...]

ANN FAQ: Q&A 101

A Few Questions AND Answers To Help You Get MORE Out of ANN!>[...]

blog comments powered by Disqus



Advertisement

Advertisement

Podcasts

Advertisement

© 2007 - 2014 Web Development & Design by Pauli Systems, LC