AD/CESSNA 337/28 - Fuel Strainer

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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 



Cessna 337 Series Aeroplanes

 

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 CAR 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.

 

AD/CESSNA 337/28 Fuel Strainer 7/2000

Applicability: Models 337, 337A, 337B/T337B, M337B, 337C/T337C, 337D/T337D, 337E/T337E, 337F, T337F, 337G, 337H/T337H, T337H-SP, T337G, P337H, F337E/FT337E, F337F/FT337F, F337G, F337H, FTB337, FT337GP, and FT337HP series aircraft

 

Requirement: 1. Inspect aircraft fuel strainer assembly. If P/N 0756005-2 top assembly, P/N 0756005-8 or 0756005-9 fuel strainer assembly were shipped from Cessna between December 12, 1996 and September 5, 1997, and fitted to the aircraft, measure the standby pipe in the fuel strainer assembly for a visible maximum length not exceeding 1.68 inches, in accordance with the Accomplishment Instructions of Cessna Multi Engine Service Bulletin MEB97-12 dated November 17,1997.

 

The holder of a pilot licence, other than a student pilot, valid for the aircraft type, may review the aircraft records to determine if parts listed in this Directive have been fitted to the aircraft. If this review concludes that parts listed in this Directive have not been fitted then a certification stating that “This Directive does not apply as no parts listed in the Cessna MEB97-12 have been fitted to this aircraft.” may be entered in the aircraft records.

 

2. Replace the filter strainer top assembly if the standpipe tube exceeds the specified measurement.

 

Note: FAA AD 2000-06-01 Amendment 39-11641 refers.

 

Compliance: 1. Unless previously accomplished, within 12 calendar months time in service from the effective date of this Directive.

 

2. Prior to further flight.

 

This Airworthiness Directive becomes effective on 13 July 2000.

COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 

 

 

Background:  This Directive applies to aircraft that have been fitted with Cessna P/N 0756005-2 top assembly, Cessna P/N 0756005-8 fuel strainer assembly or Cessna P/N 0756005-9 fuel strainer assembly shipped from Cessna between December 12, 1996 and September 5, 1997. Reports indicate that fuel strainer assemblies may have been manufactured with the fuel standpipes incorrectly installed in the assembly housing top which could allow foreign material to enter the engine fuel system resulting in loss of engine power or complete engine stoppage in flight.


 

Eugene Paul Holzapfel

Delegate of the Civil Aviation Safety Authority 2 June 2000

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 


The above AD is notified in the Commonwealth of Australia Gazette on 14 June 2000.

Overview

The Civil Aviation Regulations 1998, enacted by the Parliament of Australia, provides the legal framework for ensuring the safety of civil aviation in the country. Specifically, Part 39 - 105 of these regulations mandates the Civil Aviation Safety Authority (CASA) to issue Airworthiness Directives (ADs) as necessary to address identified safety issues. The AD/CESSNA 337/28, issued on 7 July 2000, is a specific instance of such a directive. This AD was introduced to address a potential safety hazard involving the fuel strainer assemblies of certain Cessna 337 series aeroplanes. The problem identified was the potential for incorrectly installed fuel standpipes in the assemblies, which could lead to foreign material entering the engine fuel system, thereby causing loss of engine power or engine stoppage during flight. The policy objective of the directive is to ensure that the specified aircraft models are safe to operate by requiring inspections and, if necessary, replacement of the affected fuel strainer assemblies.

Scope and Application

This Airworthiness Directive issued under the Civil Aviation Regulations 1998 applies to specific models of Cessna 337 Series aeroplanes, including various sub-models, which have been fitted with certain fuel strainer assemblies shipped between specified dates. The directive requires aircraft operators to inspect and, if necessary, replace the fuel strainer assembly to prevent potential engine issues due to incorrect installation of the fuel standpipe. This directive applies to all aircraft of the specified models that have the affected parts installed. The directive mandates that inspections and necessary replacements must be carried out within 12 months from its effective date and before further flights. This legislation is applicable nationally, covering all relevant aircraft within the Commonwealth of Australia, and is enforced by the Civil Aviation Safety Authority. There are no stated exclusions or exemptions in this directive, meaning that all applicable aircraft must comply with the outlined requirements. The directive's scope and enforcement may be further detailed in subordinate instruments or additional regulatory guidance issued by the Civil Aviation Safety Authority.

Key Provisions

The Airworthiness Directive (AD) issued under subregulation 39.1 (1) of the Civil Aviation Regulations 1998 (CAR 1998) pertains specifically to the Cessna 337 series aeroplanes and mandates particular actions to ensure airworthiness. Section (a) of the AD mandates inspection of the aircraft's fuel strainer assembly. For aircraft equipped with certain fuel strainer assemblies shipped from Cessna between December 12, 1996, and September 5, 1997, this involves measuring the standpipe in the fuel strainer assembly to ensure it does not exceed a maximum length of 1.68 inches, following the instructions provided in Cessna Multi Engine Service Bulletin MEB97-12 dated November 17, 1997. Section (b) requires that if the standpipe exceeds this length, the filter strainer top assembly must be replaced. Section (c) specifies that compliance with these requirements must occur within 12 calendar months from the effective date of the AD and prior to further flight. The AD imposes specific obligations on the holders of pilot licences who are not student pilots. These individuals must review the aircraft records to determine if any of the parts listed in the AD have been fitted to the aircraft. If the review concludes that none of the specified parts have been fitted, a certification stating that "This Directive does not apply as no parts listed in the Cessna MEB97-12 have been fitted to this aircraft" may be entered into the aircraft records. This ensures that only relevant aircraft are subject to the inspection and replacement requirements. Failure to comply with the AD can lead to significant safety risks, including the potential for foreign material to enter the engine fuel system, which could result in loss of engine power or complete engine stoppage in flight. While the AD itself does not explicitly state civil or criminal penalties for non-compliance, non-compliance with regulations issued under the Civil Aviation Act 1988 could lead to enforcement actions by the Civil Aviation Safety Authority (CASA). These actions may include fines and other regulatory sanctions. The exact penalties would depend on the specific circumstances and the discretion of CASA in enforcing compliance.

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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.