COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Beechcraft 55, 58 and 95-55 (Baron) Series Aeroplanes
AD/BEECH 55/65
Amdt 2
Fuel Boost Pumps 9/86
Applicability: Any of the following aeroplanes equipped with Airborne fuel boost pumps which have serial number date codes 5H through 12H, IJ through 12J, and all Airborne overhauled boost pumps, regardless of serial number having a repair station CO6-43 nameplate which is dated 5-81 through 12-83. (Beech Aircraft Corporation P/N 50- 380177-5, 50-380177-7, 50-389041-9 and 60-389010-15).
Beechcraft Pressurized Baron 58P and 58PA, serials TJ-366 through TJ-409, TJ-411 through TJ-423, TJ-425 through TJ-434, TJ-436 through TJ-438 and TJ-441 through TJ-443.
Baron 58TC and 58TCA, serials TK-142 through TK-145, TK-148 and TK-149.
Also any other Model 58P, 58TC series aeroplanes which may have installed a replacement fuel boost pump (Beech P/Nos. 50-380177-5, 50-380177-7, 50-389041-9 and 60-389010-15) which are date coded 1k through 5k or with a repair station nameplate dated 1-83 through 5-83.
Requirement: Beechcraft SB No. 2156.
- Carry out initial inspection in accordance with Step 1 and modify in accordance with Steps 3 and 4 of the Requirement Document.
2. Replace leaking boost pumps in accordance with Step 2 of the Requirement Document.
3. Affected pumps held as spares; inspect in accordance with the Requirement Document.
Compliance: 1. Within 100 hours’ time in service after 30 September 1986 for before 31 March 1987 whichever occurs first.
2. Before further flight after initial inspection.
3. Before installation in an aircraft after 30 September 1986.
Note: Compliance with previous issues of this Directive does not constitute compliance with this issue and a further certification is required.
Background: This Directive has been amended to reflect the manufacturer’s latest Service Bulletin and place a time limit for modification of fuel boost pumps.
Overview
The Civil Aviation Regulations 1998, as part of Part 39, addresses critical safety concerns in civil aviation through various Airworthiness Directives (ADs). Specifically, AD/BEECH 55/65 Amendment 2 focuses on the Beechcraft 55, 58, and 95-55 (Baron) Series Aeroplanes, identifying a problem with fuel boost pumps that could lead to operational risks. This legislative instrument was enacted to ensure that these aircraft meet safety standards, particularly regarding the fuel systems. The objective is to mandate inspections, modifications, and replacements of certain fuel boost pumps to prevent failures that could compromise flight safety. Compliance with these directives is overseen by the Civil Aviation Safety Authority, ensuring adherence to the latest safety protocols as stipulated by the manufacturer's service bulletins.
Scope and Application
The Civil Aviation Regulations 1998, specifically Part 39 - 105, under the Civil Aviation Safety Authority’s Schedule of Airworthiness Directives, applies to certain Beechcraft aeroplanes within Australia’s jurisdiction. This particular airworthiness directive, AD/BEECH 55/65 Amendment 2, focuses on fuel boost pumps for Beechcraft 55, 58 and 95-55 (Baron) series aeroplanes. The directive applies to specific serial numbers and date codes for these aeroplanes, particularly those equipped with Airborne fuel boost pumps and certain repair station components. The requirement mandates that initial inspections and modifications must be carried out in accordance with the specified steps outlined in the Requirement Document, and leaking boost pumps must be replaced. The directive also specifies that affected pumps held as spares must be inspected in line with the Requirement Document. Compliance with these regulations is mandatory within certain timeframes, with a focus on ensuring safety and airworthiness before flights or installations. It is important to note that compliance with previous issues of this directive does not satisfy the requirements of this amendment, necessitating a further certification.
Key Provisions
The Civil Aviation Regulations 1998, specifically under PART 39 - 105 (4) and AD/BEECH 55/65 Amendment 2, addresses the airworthiness directives for the Beechcraft 55, 58 and 95-55 (Baron) series aeroplanes. This legislation mandates the inspection and modification of certain fuel boost pumps. The directive applies to aeroplanes equipped with specific airborne fuel boost pumps, identified by serial number date codes or repair station nameplate dates between certain periods. The required action includes initial inspections and modifications as per the detailed steps outlined in the Requirement Document, replacement of leaking pumps, and inspection of affected pumps held as spares. Compliance must be achieved within 100 hours of service or before a specified date, whichever is earlier.
The obligations under this legislation are clear and precise. Owners or operators of affected aeroplanes must conduct the specified inspections and modifications within the stipulated timeframes. They must ensure that any initial inspections are completed before the aeroplane returns to service and that any replacement pumps are installed before further flights. Additionally, any spare pumps must be inspected in accordance with the requirements. Non-compliance with these obligations can lead to serious safety risks and potential legal repercussions.
Breaches of these airworthiness directives can result in significant penalties and consequences. Under the Civil Aviation Act 1988, failure to comply with airworthiness directives can lead to civil penalties, including fines. The maximum penalty for non-compliance with these regulations is significant, reflecting the importance of adhering to airworthiness standards. Furthermore, there can be criminal consequences for serious breaches, including imprisonment. These provisions are designed to ensure that all parties comply with the necessary safety standards to protect both the aircraft and its occupants.