AD/B737/36 - Cabin Door Blowout Panels

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Legislation au F2006B02936 In force Legislative Instrument

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

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 


Boeing 737 Series Aeroplanes

 

AD/B737/36 Cabin Door Blowout Panels 4/90

Applicability: 737 Aircraft line position 1 through 1587.

 

Requirement: Action in accordance with Boeing SB 737-52A1105 Rev. 2.

 

Note: FAA AD 89-04-03 refers.

 

Compliance: Prior to 31 July 1990.

 

Background: Country of origin AD. Improper use of sealants on blowout panels in the control (cockpit) cabin door could preclude proper operation of blowout panels if a pressure differential greater than 1.5 P.S.I occurred between passenger cabin and control cabin. As a result damage to control cabin floor might occur, with possible interference of control cables.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Overview

The Civil Aviation Safety Authority, pursuant to the Civil Aviation Act 1988, has introduced the Civil Aviation Regulations 1998 to ensure the safety of civil aviation in Australia. Specifically, Part 39 - 105 within this legislation, addresses the issuance of Airworthiness Directives (ADs) to mitigate risks associated with aircraft operations. AD/B737/36 pertains to Boeing 737 series aeroplanes, focusing on the cabin door blowout panels, to rectify an issue where improper use of sealants could lead to operational failures under certain pressure differentials, potentially causing damage to the control cabin and interfering with control cables. This directive mandates compliance with Boeing Service Bulletin 737-52A1105 Rev. 2, with a reference to the Federal Aviation Administration's AD 89-04-03, and requires action before 31 July 1990 to ensure aircraft safety and compliance with international safety standards. The enactment of this directive by the Commonwealth of Australia aims to address the identified safety gap concerning the potential failure of cabin door blowout panels due to improper sealant use, which could lead to significant operational hazards. This legislative instrument underscores the policy objective of maintaining stringent safety standards within the aviation industry, ensuring that all aircraft meet the necessary criteria to prevent accidents and enhance the safety of air travel. The regulations are designed to enforce compliance with internationally recognised safety directives, thereby protecting both passengers and crew from potential risks associated with aircraft maintenance and operation.

Scope and Application

The Civil Aviation Regulations 1998, as amended, apply to all Boeing 737 series aeroplanes from line positions 1 through 1587, mandating adherence to specific airworthiness directives to ensure safe operations. These regulations are enforced by the Civil Aviation Safety Authority (CASA) and have a national scope, extending throughout Australia. The regulations require aircraft operators to implement actions in accordance with Boeing Service Bulletin 737-52A1105 Rev. 2, with reference to Federal Aviation Administration AD 89-04-03, to address the risk of damage to control cabin floors due to improper use of sealants on cabin door blowout panels. The compliance deadline for these directives was set prior to 31 July 1990, and no specific exclusions or exemptions are mentioned within the text of this particular directive. The broader application and enforcement of these regulations may be extended or further defined through subordinate instruments issued by CASA.

Key Provisions

The Civil Aviation Regulations 1998, specifically Part 39, Subpart 105, details the Schedule of Airworthiness Directives, which includes AD/B737/36 concerning Boeing 737 series aeroplanes. This directive mandates specific actions regarding cabin door blowout panels, as outlined in Boeing Service Bulletin 737-52A1105 Rev. 2, and references the Federal Aviation Administration’s AD 89-04-03. The directive applies to Boeing 737 aircraft from line position 1 through 1587. The primary requirement is to ensure compliance with these service bulletins, which address potential issues with the sealants used on the blowout panels of the cockpit cabin door. The obligations imposed by this directive are clear and direct. Operators of Boeing 737 aircraft must follow the procedures detailed in Boeing Service Bulletin 737-52A1105 Rev. 2. This includes the use of approved sealants on the blowout panels to prevent any operational issues in case of a pressure differential greater than 1.5 P.S.I between the passenger cabin and the control cabin. Ensuring compliance with these standards is critical to avoid damage to the control cabin floor, which could interfere with control cables. This requirement was mandated to be met prior to 31 July 1990. Failure to comply with the provisions of AD/B737/36 may result in significant consequences. Civil aviation regulations are stringent, and non-compliance could lead to serious safety hazards. The Civil Aviation Safety Authority (CASA) has the authority to enforce these directives, and violations could result in penalties. While specific penalties are not detailed in the provided text, breaches of airworthiness directives typically attract significant fines and other enforcement actions. These measures are designed to ensure that aircraft remain in a safe and airworthy condition at all times, thereby protecting passengers, crew, and the general public.

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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.