AD/PORSCHE/4 - Drive Shaft Teeth

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

Legislation au F2006B06307 In force Legislative Instrument

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AIRWORTHINESS DIRECTIVE

For the reasons set out in the background section, the CASA delegate whose signature appears below issues the following Airworthiness Directive (AD) under subregulation 39.1 (1) of CASR 1998. The AD requires that the action set out in the requirement section (being action that the delegate considers necessary to correct the unsafe condition) be taken in relation to the aircraft or aeronautical product mentioned in the applicability section: (a) in the circumstances mentioned in the requirement section; and (b) in accordance with the instructions set out in the requirement section; and (c) at the time mentioned in the compliance section.


 

Porsche Piston Engines

 

AD/PORSCHE/4 Drive Shaft Teeth 7/2003

 

Applicability: Porsche AG PFM 3200 N01 and N03 engines.

 

Requirement: 1. Carry out an inspection of the drive shaft teeth in accordance with Porsche Service Bulletin (S/B) N/300-038 Revision 1.

 

2.        Repeat the inspection of the drive shaft teeth in accordance with Porsche Service Bulletin (S/B) N/300-038 Revision 1.

 

3.        Replace the drive shaft if the area of pitting is larger than 4mm2 for 1 drive tooth, or 38 mm2 total for all drive shaft teeth, or if between inspections the growth of pitting exceeds more than 2 mm2 for any 1 tooth.

4.        Defects found to during the inspections detailed in this Directive must be reported to the manufacturer.

 

Note: LBA AD 2003-020/2 refers.

 

Compliance:

1.

For gearboxes with a Time Since Overhaul:

 

 

a. between 900-1200 flight hours; At the next 100 hour inspection of the

 

 

engine.

 

 

b. over 1200 flight hours; Before the next flight. (A ferry flight to allow maintenance to be carried out is allowed)

 

2.

At intervals not to exceed 200 flight hours from the initial inspection.

 

3.

Before further flight.

 

4.

Within 30 days of the inspection.

 

This Airworthiness Directive becomes effective on 10 July 2003.

Porsche Piston Engines

 

AD/PORSCHE/4 (continued)

 

Background: Pitting corrosion of the gear wheels has been found. This may have been as a result of unapproved oil being used, wrong oil change intervals, or exceeding oil temperature limitations. The pitting of the gear teeth can lead to failure of the gear wheel and subsequent failure of the engine.


Jim Coyne

Delegate of the Civil Aviation Safety Authority 28 May 2003

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 


The above AD is notified in the Commonwealth of Australia Gazette on 18 June 2003.

Overview

The Airworthiness Directive issued under the Civil Aviation Act 1988 aims to address the identified safety issue of pitting corrosion in Porsche AG PFM 3200 N01 and N03 engines used in aviation. This directive, issued by the Civil Aviation Safety Authority (CASA) in 2003, seeks to mitigate the risk of gear wheel failure and subsequent engine failure due to unapproved oil use, improper oil change intervals, or exceeding oil temperature limitations. The directive mandates inspections and, if necessary, the replacement of drive shafts based on specified criteria. Compliance with the directive is enforced within designated timeframes to ensure the airworthiness of affected aircraft.

Scope and Application

The Airworthiness Directive issued by the Civil Aviation Safety Authority (CASA) applies specifically to Porsche AG PFM 3200 N01 and N03 engines. The directive mandates actions to rectify the unsafe condition identified, which is the pitting corrosion of the gear wheels. This corrosion can result from the use of unapproved oil, improper oil change intervals, or exceeding oil temperature limitations. The unsafe condition can lead to the failure of the gear wheel and, consequently, the engine. The directive requires inspections and potential replacements of the drive shaft, with specific criteria for when these inspections and replacements must be carried out, contingent upon the time since overhaul of the gearbox and the number of flight hours since the last inspection. The geographic and jurisdictional reach of this directive is the Commonwealth of Australia, as CASA is the national aviation regulatory body. The directive does not explicitly mention any exclusions, exemptions, or thresholds beyond those stipulated in the requirement and compliance sections. The directive extends its application through subordinate instruments, such as the Porsche Service Bulletin (S/B) N/300-038 Revision 1, which provides detailed instructions for the inspections and actions required.

Key Provisions

The main sections of this Airworthiness Directive (AD) under subregulation 39.1(1) of the Civil Aviation Safety Regulations 1998 (CASR 1998) include the applicability, requirement, and compliance sections. The applicability section (paragraph 1) specifies that the AD applies to Porsche AG PFM 3200 N01 and N03 engines. The requirement section (paragraph 2) mandates that an inspection of the drive shaft teeth must be carried out in accordance with Porsche Service Bulletin (S/B) N/300-038 Revision 1, repeated inspections must be performed, and the drive shaft must be replaced if certain conditions are met. The compliance section (paragraph 3) outlines the specific intervals and circumstances under which the actions must be taken. The obligations and requirements imposed by this AD on the parties or entities it governs include conducting inspections and potentially replacing the drive shaft. Operators of Porsche AG PFM 3200 N01 and N03 engines must ensure that the inspections and subsequent actions are carried out in accordance with the specified guidelines and timeframes. Defects identified during these inspections must be reported to the manufacturer, and any necessary replacement of the drive shaft must be performed to prevent potential engine failure due to pitting corrosion of the gear wheels. There are no explicit offences, penalties, or civil/criminal consequences outlined in the AD itself. However, non-compliance with the AD may result in the aircraft or aeronautical product being deemed unairworthy, which could lead to operational restrictions or grounding of the affected engines. The AD emphasises the importance of adhering to the specified requirements to ensure the continued airworthiness and safety of the aircraft.

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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.