AD/DHC-8/34 Amdt 1 - Black Thermal Insulation

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Legislation au F2006B09190 Not 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

 


Bombardier (Boeing Canada/De Havilland) DHC-8 Series Aeroplanes

 

AD/DHC-8/34

Amdt 1


Black Thermal Insulation 4/95

 

Applicability: DHC-8 aircraft, models and serial numbers as listed in the Requirement Table.

 

Requirement: Remove all black film thermal insulation blankets from the aircraft fuselage and flight compartment and replace them with AN4C Aluminized (silver) film insulation blankets; in accordance with the Part III Accomplishment Instructions of the Bombardier Inc., de Havilland Dash 8 Service Bulletins listed in the following table:

 

DHC-8 Models

Serial Numbers

Service Bulletin No

Date

102, 103, & 106

003 to 353

8-25-89 Revision E

6 July 94

102, 103, & 106

003 to 371

8-25-90 Revision C

5 July 94

102, 103, 106,

301, 311, & 314

003 to 337, 339, 341 to 347,

349, 350, 351, 353, & 356

8-25-91 Revision D

20 July 94

301, 311, & 314

100 to 336, 342, 350, & 356

8-25-92 Revision E

20 July 94

301, 311, & 314

10 to 336, 342, 350, 365, &

370

8-25-93 Revision C

20 July 94

 

Note 1: Transport Canada AD CF-94-08R1 refers.

 

Note 2: This Directive is not applicable to aircraft that have had all three de Havilland Modifications 8/2004, 8/2006, and 8/2007 incorporated during manufacture.

 

Compliance:  Unless already accomplished in accordance with the previous issue of this Directive, prior to 3 September 1994 or as indicated in Part 1.D of the service bulletins listed in the Requirement Table, whichever occurs later.

 

The Compliance of the previous issue of this Directive remains unchanged. This Amendment is effective from 30 March 1995.

 

Background: Operators have reported corrosion forming on areas of the aircraft where black film thermal insulation blankets are being used. De Havilland’s investigation found that the black film, which covers these insulation blankets, contains carbon. If condensation is present, corrosion may occur in places where the black film is in contact with any aluminium structure.

 

Amendment 1 is issued in response to a revision of the Transport Canada AD which changes the applicability to agree with the applicability of the latest revision of the mandated service bulletins.

 

 

 

 

Overview

The Civil Aviation Regulations 1998, under Part 39 - 105 of the Civil Aviation Safety Authority Schedule of Airworthiness Directives, address the issue of corrosion on Bombardier (Boeing Canada/De Havilland) DHC-8 Series Aeroplanes due to the use of black film thermal insulation blankets. This was enacted to ensure the safety of aircraft by preventing corrosion which could compromise structural integrity. The Civil Aviation Safety Authority, operating under the authority of the Australian Parliament, introduced this legislation to align with international standards and ensure the safe operation of aircraft within Australia’s airspace. The policy objective is to maintain and enhance aviation safety through the implementation of rigorous airworthiness directives.

Scope and Application

The Civil Aviation Regulations 1998, specifically Part 39 - 105 and Schedule of Airworthiness Directives, governs the maintenance and operational safety of certain aircraft within Australia. This particular Airworthiness Directive (AD/DHC-8/34Amdt 1) applies to Bombardier (Boeing Canada/De Havilland) DHC-8 Series aeroplanes with specific model and serial numbers as detailed in the Requirement Table. The directive mandates the removal and replacement of black film thermal insulation blankets with AN4C Aluminized (silver) film insulation blankets to mitigate corrosion risks associated with the presence of carbon in the black film. This directive is effective for the specified aircraft models and serial numbers and requires compliance by a certain date, or as indicated in the relevant service bulletins, whichever is later. The directive extends to ensure safety compliance but excludes aircraft that have already undergone certain modifications during manufacture, as noted in the directive's applicability section.

Key Provisions

The Civil Aviation Regulations 1998, specifically Part 39 - 105, contain the Civil Aviation Safety Authority (CASA) Schedule of Airworthiness Directives. One of the directives under this part pertains to Bombardier (Boeing Canada/De Havilland) DHC-8 Series Aeroplanes, outlined in AD/DHC-8/34 Amendment 1, dated 4/95, concerning "Black Thermal Insulation" (section 1). This directive applies to DHC-8 aircraft models and serial numbers specified in the Requirement Table of the legislation. The main requirement is that all black film thermal insulation blankets must be removed from the aircraft fuselage and flight compartment, and replaced with AN4C Aluminized (silver) film insulation blankets (section 2). This change must be carried out in accordance with the Part III Accomplishment Instructions of the Bombardier Inc., de Havilland Dash 8 Service Bulletins detailed in the Requirement Table. Operators of the specified DHC-8 models and serial numbers are obligated to comply with this directive (section 3). The compliance date for this directive is set to be before 3 September 1994 or as indicated in Part 1.D of the service bulletins listed in the Requirement Table, whichever is later. It is important to note that the compliance of the previous issue of this directive remains unchanged, and this amendment is effective from 30 March 1995 (section 4). Failure to comply with this directive could result in safety issues, particularly corrosion, as operators have reported corrosion forming on areas of the aircraft where black film thermal insulation blankets are used. The directive notes that Transport Canada AD CF-94-08R1 refers to this issue, and clarifies that this directive is not applicable to aircraft that have had all three de Havilland Modifications 8/2004, 8/2006, and 8/2007 incorporated during manufacture (section 5). Any breach of these requirements may lead to serious safety concerns and potential legal consequences. Under the Civil Aviation Act 1988, non-compliance with airworthiness directives can lead to civil penalties, including fines, and potential criminal charges for those responsible for the aircraft. The exact penalties can vary, but they may include significant financial penalties and imprisonment, depending on the severity of the breach and its impact on aviation safety.

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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.