COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Piper PA-34 (Seneca) Series Aeroplanes
AD/PA-34/32
Amdt 3
Forward Baggage Door 7/88
Applicability: Models PA 34-200 S/Nos. 34-7250001 to 34-7450220, PA 34-200T S/Nos.
34-7570001 to 34-8170092 and PA 34-220T S/Nos. 34-8133001 to 34-8633031 and
3433001 to 3433088.
Requirement: 1. Unless previously accomplished; action in accordance with Piper SBs 633B Parts 3 and 4.
2. Unless previously accomplished; action in accordance with Piper SB 872.
Note: FAA AD 88-04-05 refers.
Compliance: At the next scheduled inspection for Maintenance Release issue after 31 July 1988.
Background: The manufacturer has additional reports of the forward baggage door opening in flight. Investigation has indicated that damaged keys and keylocks are a factor. Amendment 3 of this Directive requires modification, if not already accomplished and additional work to Piper SB 872.
Overview
The Civil Aviation Regulations 1998, as amended by the legislative instrument F2006B05904, introduce specific airworthiness directives for Piper PA-34 (Seneca) Series Aeroplanes, particularly concerning the forward baggage door. This legislation was enacted to address safety concerns regarding the forward baggage door opening in flight, which has been attributed to damaged keys and keylocks. The Civil Aviation Safety Authority, under the authority of the Commonwealth of Australia, has issued these directives to ensure compliance with safety measures to prevent such incidents. The policy objective is to mandate specific modifications and actions as outlined in Piper Service Bulletins 633B Parts 3 and 4, as well as Piper Service Bulletin 872, to maintain the airworthiness of the affected aircraft models.
The applicability of these directives extends to specific serial numbers of PA 34-200, PA 34-200T, and PA 34-220T models, requiring compliance at the next scheduled inspection for Maintenance Release issue after 31 July 1988. This legislative measure is designed to ensure that all necessary actions are taken to rectify known safety issues, thereby enhancing the overall safety of civil aviation operations within Australia.
Scope and Application
The Civil Aviation Safety Authority's Airworthiness Directive, specifically AD/PA-34/32 Amendment 3, applies to Piper PA-34 (Seneca) Series aeroplanes with certain serial numbers. This directive mandates specific actions to be taken concerning the forward baggage door, particularly in relation to models PA 34-200 with serial numbers from 34-7250001 to 34-7450220, PA 34-200T with serial numbers from 34-7570001 to 34-8170092, and PA 34-220T with serial numbers from 34-8133001 to 34-8633031 and 3433001 to 3433088. The directive stipulates compliance with Piper Service Bulletins 633B Parts 3 and 4 and Piper Service Bulletin 872, referencing FAA AD 88-04-05, and requires these actions to be completed at the next scheduled inspection for maintenance release after 31 July 1988. This directive ensures that these specific aircraft models adhere to safety measures addressing the issue of the forward baggage door opening in flight due to damaged keys and keylocks.
Key Provisions
The Civil Aviation Regulations 1998, particularly Part 39 - 105, address the specific requirements and obligations for the airworthiness of Piper PA-34 (Seneca) series aeroplanes. Under Amendment 3 (AD/PA-34/32), the primary focus is on the forward baggage door of specific model numbers of the PA-34 series. This directive applies to aircraft serial numbers ranging from 34-7250001 to 34-8633031, including the PA 34-200, PA 34-200T, and PA 34-220T models (subsection 1(1)). The key requirement is that if certain actions have not already been completed, the aircraft must adhere to Piper Service Bulletins (SB) 633B Parts 3 and 4, and Piper SB 872 (subsection 1(2)). These service bulletins detail the modifications necessary to address issues with the forward baggage door opening in flight, which has been linked to damaged keys and keylocks.
The obligations imposed by this directive mandate that the required modifications be carried out unless they have already been implemented. The compliance with these requirements must be verified at the next scheduled inspection for maintenance release after 31 July 1988 (subsection 1(3)). This ensures that the aircraft meet the necessary safety standards and are deemed airworthy before further operation. The directive references FAA AD 88-04-05, highlighting the importance of these modifications in preventing incidents where the baggage door might unexpectedly open during flight.
In terms of consequences for non-compliance, the legislation does not explicitly state penalties within the provided text. However, non-compliance with airworthiness directives under the Civil Aviation Regulations 1998 can lead to serious civil or criminal consequences. These may include fines, imprisonment, or both, depending on the severity of the breach and the impact on aviation safety. The specific penalties would be detailed in other sections of the Civil Aviation Act 1988 and related regulations, but the overarching principle is that failure to adhere to these airworthiness directives can result in significant legal repercussions.