Such failure could lead to loss of control of the airplane. This could result in cracking and failure of the main landing gear lower side brace. The actions specified by the proposed AD are intended to correct damage or cracks in the main landing gear lower side brace at the upper bolt lug where the upper and lower side braces connect. The proposed AD is the result of several reports of cracking of the main landing gear lower side brace at the upper bolt lug discovered on preflight inspection. The proposed AD would require you to replace both of the existing main landing gear lower side brace assemblies with parts of improved design. This document proposes to adopt a new airworthiness directive (AD) that would apply to all Aerostar Aircraft Corporation (Aerostar) Models PA-60-600, PA-60-601, PA-60-601P, PA-60-602P and PA-60-700P airplanes. Would this proposed AD involve a significant rule or regulatory action?įederal Aviation Administration, DOT.Would this proposed AD impact relations between Federal and State governments?.What would be the cost impact of the proposed AD on owners/operators of the affected airplanes?.How many airplanes would the proposed AD impact?.The FAA's Determination and an Explanation of the Provisions of the Proposed AD.What are the provisions of this service bulletin?.Is there service information that applies to this subject?.What are the consequences if the condition is not corrected?.How can I be sure FAA receives my comment?.Are there any specific portions of the proposed AD I should pay attention to?.This repetition of headings to form internal navigation links Headings within the legal text of Federal Register documents. This table of contents is a navigational tool, processed from the Provide legal notice to the public or judicial notice to the courts. Rendition of the daily Federal Register on does not Until the ACFR grants it official status, the XML Legal research should verify their results against an official edition of
#AEROSTAR 601P X PLANE CRACK PDF#
The official SGML-based PDF version on, those relying on it for The material on is accurately displayed, consistent with While every effort has been made to ensure that Regulatory information on with the objective ofĮstablishing the XML-based Federal Register as an ACFR-sanctioned The OFR/GPO partnership is committed to presenting accurate and reliable Register (ACFR) issues a regulation granting it official legal status.įor complete information about, and access to, our official publications Informational resource until the Administrative Committee of the Federal This prototype edition of theĭaily Federal Register on will remain an unofficial Each document posted on the site includes a link to theĬorresponding official PDF file on. The documents posted on this site are XML renditions of published Federal Register, and does not replace the official print version or the official It is not an official legal edition of the Federal In production between 19, the 700P has more powerful engines, a higher max takeoff weight and optional extra fuel capacity.This site displays a prototype of a “Web 2.0” version of the dailyįederal Register. The PA-60-700P was the last Aerostar version, and just 25 were built. When Piper transferred production to its new Vero Beach, Florida factory in early 1982, only the 602P was in production, and this was redesignated the PA-60-602P. Piper continued production of the 600A, 601B and 601P at Ted Smith's Santa Maria plant, and introduced the 602P with low compression TIO-540-AA1A5 engines. Smith bought the line back again in 1972, and his new company Ted R Smith and Associates resumed Aerostar manufacture, including of the improved 601B with the same span wings as on the 601P, until Piper acquired the Aerostar line in March 1978. By this time Butler Aviation had acquired the production rights of the Aerostar in 1970, producing a small number as Butler Aerostars. The turbocharged Aerostar 601 followed the 600 into production shortly afterwards, while the turbocharged and pressurised 601P went into production in 1972. The prototype was powered by 120kW (160hp) Lycoming IO-320s, but the Aerostar was placed into production from 1968 as the Aerostar 600 with 215kW (290hp) IO-540s. Smith began design work on the Aerostar in late 1964, with a prototype making its first flight two years later in November 1966. However the Aerostar appeared in piston twin form only. Smith's original intention in designing the Aerostar was to develop a family of single and piston twins, twin turboprop and even twin jet powered versions of the same basic aircraft. The Aerostar - which in its higher powered forms can lay claim to being the fastest piston twin GA aircraft built - was designed by Ted Smith, who was also responsible for the Aero Commander twins.
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