AD/PFP/1 Amdt 3 - Wooden Propellers - Inspection

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

Legislation au F2006B06168 Not in force Legislative Instrument

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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 107 CIVIL AVIATION SAFETY AUTHORITY

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 


Propellers - Fixed Pitch

 

AD/PFP/1

Amdt 3


Wooden Propellers - Inspection 7/89

 

Applicability: All fixed pitch wooden and Hoffman composite series propellers. Requirement:  1. Newly installed propellers:              Check the hub bolt nuts for tightness.

2.    All propellers:

 

(a)     Check the propeller for track.

 

(b)     Check the hub bolt nuts for tightness.

 

(c)     Inspect sheathing and tipping for looseness, separation of soldered joints, loose screws, cracks and corrosion.

 

3.    Spinners, if fitted must be removed to carry out the above inspections.

 

Note: For Hoffmann composite series propellers refer to Owners Manual No. EO110-74 for further inspection and rectification guidelines.

 

Compliance: For para. 1 - After the first flight following each installation.

 

For para. 2 - After intervals not exceeding 100 hours time in service from installation or twelve months whichever occurs first.

 

Note: In addition, it is recommended that the inspections of para. 2 above be repeated regardless of the time since last 100 hourly check, under the following circumstances:

 

(a)     when there has been a significant change in the average ambient humidity, due to a seasonal change, or to a change in aircraft locality and,

 

(b)     prior to first flight after the aircraft has been idle for an extended period.

 

Background:  This Directive is amended to include a minor editorial change in the Compliance section.

 

 

 

 

 

 

 

 

 

 

 

 

 

Overview

The Civil Aviation Regulations 1998, specifically Part 39 - 107, introduced an Airworthiness Directive concerning fixed pitch wooden propellers to address safety issues related to the structural integrity and operational reliability of such propellers. This legislative instrument was enacted to ensure that wooden and Hoffman composite series propellers are regularly inspected to prevent failures that could potentially compromise flight safety. The policy objective is to maintain high safety standards in civil aviation by mandating routine inspections of wooden propellers to detect and rectify issues such as looseness, corrosion, and other structural defects. Compliance with these regulations is overseen by the Civil Aviation Safety Authority, which ensures that inspections are performed after each installation and at regular intervals thereafter, with additional checks recommended under specific conditions such as significant changes in ambient humidity or prolonged periods of inactivity.

Scope and Application

The Civil Aviation Regulations 1998, specifically PART 39 - 107, outlines the Civil Aviation Safety Authority’s Schedule of Airworthiness Directives for fixed pitch propellers, including wooden and Hoffman composite series propellers. This regulation applies to all fixed pitch wooden and Hoffman composite series propellers, mandating stringent inspection requirements to ensure airworthiness. The primary aim is to maintain the structural integrity of these propellers, which are critical components of aircraft safety. The directive mandates a series of checks and inspections for both newly installed and in-service propellers, focusing on the tightness of hub bolt nuts, the presence of track, and the condition of sheathing and tipping, including any looseness, separation of soldered joints, loose screws, cracks, and corrosion. Spinners, if fitted, must be removed for these inspections. For Hoffman composite series propellers, further guidance is available in the Owners Manual No. EO110-74. Compliance with these directives is essential, with specific intervals set for inspections, such as after the first flight following installation for newly installed propellers, and after intervals not exceeding 100 hours of time in service from installation or twelve months, whichever occurs first. Additionally, inspections should be repeated if there is a significant change in ambient humidity or after the aircraft has been idle for an extended period. These regulations ensure that all entities operating fixed pitch wooden and Hoffman composite series propellers adhere to the required safety standards, thereby maintaining the highest level of aviation safety across the Commonwealth of Australia.

Key Provisions

The Civil Aviation Regulations 1998, under PART 39 - 107, mandate specific airworthiness directives for wooden and Hoffman composite series propellers. The regulation, AD/PFP/1Amdt 3, pertains to the inspection of fixed pitch wooden propellers, which is critical for maintaining safety standards in aviation (1). Newly installed propellers must have their hub bolt nuts checked for tightness, a requirement specified under section 1(1). All propellers, irrespective of installation status, must undergo thorough inspections to check for track, ensure the tightness of hub bolt nuts, and inspect sheathing and tipping for any signs of looseness, separation of soldered joints, loose screws, cracks, and corrosion (1(2)(a)-(c)). If spinners are fitted, they must be removed to facilitate these inspections. For Hoffman composite series propellers, additional guidelines are available in the Owners Manual No. EO110-74. The regulation outlines specific compliance requirements to ensure these inspections are conducted appropriately. Newly installed propellers must be checked after the first flight following each installation (1). For all propellers, inspections must be carried out at intervals not exceeding 100 hours of time in service from installation or twelve months, whichever comes first (1). It is also recommended to repeat these inspections regardless of the time since the last 100-hourly check if there has been a significant change in average ambient humidity due to seasonal changes or changes in aircraft locality, or if the aircraft has been idle for an extended period prior to the first flight (1). Failure to comply with the airworthiness directives could result in severe consequences, including potential safety risks and regulatory penalties. While the specific civil or criminal penalties for non-compliance are not detailed within the text, the overarching regulations under the Civil Aviation Act 1988 could impose fines and other penalties for breaches of safety directives. Non-compliance could also lead to the grounding of aircraft until the required inspections are satisfactorily completed, thereby impacting operational efficiency and potentially leading to financial losses for operators. The regulation emphasises the importance of adhering to these inspection protocols to maintain the airworthiness of the aircraft and ensure the safety of all individuals involved in aviation activities.

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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.