AD/PA-28/35 Amdt 2 - Main Landing Gear Torque Links

Administered by Department of Infrastructure, Transport, Regional Development, Communications, Sport and the Arts

Legislation au F2011L00678 In force Legislative Instrument

Legislation content

CIVIL AVIATION ACT 1988

CIVIL AVIATION SAFETY REGULATIONS 1998

ISSUE OF AIRWORTHINESS DIRECTIVE

Under section 98 of the Civil Aviation Act 1988, the Governor-General may make regulations for the purposes of the Act and in the interests of the safety of air navigation.  Under regulation 39.001 of the Civil Aviation Safety Regulations 1998, the Civil Aviation Safety Authority (CASA) may issue airworthiness directives (ADs) for kinds of aircraft or aeronautical products.  Subregulation 39.001(5) of the Civil Aviation Safety Regulations 1998 provides that an AD is a disallowable instrument for the purposes of section 46A of the Acts Interpretation Act 1901. Therefore, in accordance with section 6 of the Legislative Instruments Act 2003, an AD is a legislative instrument.

Under Annex 8 to the Convention on International Civil Aviation, the State of Design has overall responsibility for continuing airworthiness of an aircraft type, and must provide any information necessary to ensure the continuing airworthiness of a type to appropriate States of Registry.  ADs (and their equivalents) are the most common form of continuing airworthiness information, and are issued by most ICAO Contracting States.

The State of Registry of an individual aircraft is responsible for its continuing airworthiness.  Under Annex 8, the State of Registry must develop or adopt requirements to ensure the continuing airworthiness of aircraft.  When a State of Design issues an AD against a type of aircraft on the Australian Register, or likely to be on the Australian register, CASA, as Australia’s national airworthiness authority, must assess that information and, if appropriate, issue an Australian AD to mandate the requirements of the State of Design.

In 1972 Piper Aircraft Corporation issued Service Letter No. 600 applying periodic inspections to PA-28 Cherokee airplanes.  The USA Federal Aviation Administration issued AD 72-08-06 to mandate SL No. 600.  The USA is the State of Design of the Piper PA-28 Cherokee airplane.  Australian AD/PA-28/35 and Amendment 1 were subsequently issued to mandate SL No. 600.  In 2009, Piper Aircraft Corporation issued Mandatory Service Bulletin No. 1199 to supersede SL No. 600 in its entirety.  CASA has decided to amend AD/PA-28/35 to Amendment 2 to delete reference to SL No. 600 and replace it with reference to MSB No. 1199.  AD/PA-28/35 Amdt 2 will become effective on 13 May 2011.

As this AD is issued because of Australia’s obligations under Convention on International Civil Aviation, and because it is issued in response to a number of ADs raised by the relevant State of Design, no consultation of the Australian public has taken place on this AD.  The Office of Best Practice Regulation has determined that ADs do not require a Regulatory Impact Statement.

The AD has been made by the Manager, Continuing Airworthiness in the Airworthiness and Engineering Branch, on behalf of CASA, in accordance with subsection 94 (1) of the Act.

Interactions

Authorises

All Versions

Sourced from the Federal Register of Legislation at 26 August 2026. For the latest information on Australian Government law please go to https://www.legislation.gov.au.