SCHEDULE OF AIRWORTHINESS DIRECTIVES
Cessna 205 · Airworthiness Directives
Overview
This document is an Airworthiness Directive (AD) issued by the Civil Aviation Safety Authority of Australia, specifically addressing the Cessna 205 series aeroplanes. The directive outlines mandatory inspection and compliance requirements for aircraft with serial numbers ranging from 205-0001 to 205-0577, which were manufactured between 1963 and 1964. The focus of this AD is on the fuel filler caps and adaptors, ensuring that they are functioning correctly to prevent fuel leakage during flight. The document serves as a critical safety measure for operators and maintenance personnel to ensure the airworthiness of the aircraft by following the specified inspection procedures and compliance timelines.
- Applicable to Cessna 205 models with serial numbers 205-0001 to 205-0577 (1963-1964).
- Inspect fuel filler area for signs of inflight fuel leakage.
- Check fuel cap locking mechanism and seals for damage.
- Inspect adaptor sealing face for distortion or corrosion.
- Conduct a fuel cap leak test per Cessna SIL SE 82-34.
- Compliance required before next Maintenance Release after June 30, 1985.
Document
Source
Originally published by services.casa.gov.au. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type
- Airworthiness Directives
- Year
- 1988
- Pages
- 1
- File size
- 10 KB
- Publisher
- services.casa.gov.au
Common. Rarer than 10% of the aircraft models we track.
Most owners only have the POH. Here's the essential set for the Cessna 205.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins
- Type Certificate (TCDS)
Free — save the 205 to your watchlist and track it in one place.
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In this document
Applicability
The Airworthiness Directive applies to Cessna 205 models with serial numbers from 205-0001 to 205-0577, which were produced in the years 1963 and 1964. It specifies that unless the aircraft is equipped with reduced diameter, raised filler neck fuel caps as per Cessna Service Kit SK182-85, the directive is applicable.
Inspection Requirements
The directive outlines several key inspection requirements for the fuel filler caps and adaptors. These include visually inspecting the area behind the fuel filler for signs of fuel leakage, checking the locking mechanism and seals for any damage, and inspecting the sealing face of the adaptor for any conditions that may prevent proper sealing. Additionally, a fuel cap leak test must be conducted following Cessna SIL SE 82-34.
Compliance Timeline
Compliance with the directive is required prior to the issuance of the next Maintenance Release after June 30, 1985, and must be repeated at each new Maintenance Release thereafter. This ensures ongoing safety and airworthiness of the aircraft.
Background Information
The amendment to this directive removes the previous requirement for extensive inspections and testing of fuel filler caps against potential water ingress for aircraft fitted with raised fuel filler necks. This change reflects updated safety assessments and operational practices.
Safety notes
- Ensure all inspections are conducted as specified to maintain airworthiness.
- Failure to comply with the directive may lead to safety risks during flight.
Full document text
COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY SCHEDULE OF AIRWORTHINESS DIRECTIVES Cessna 205 (210-5) Series Aeroplanes AD/CESSNA 205/17 Amdt 1 Fuel Filler Caps and Adaptors 11/88 Applicability: Models with serial numbers: 205-0001 through 205-0577 (1963-1964); unless reduced diameter, raised filler neck fuel caps are installed on all filler openings in accordance with Cessna Service Kit SK182-85 (refer S.I.L SE 84-16). Requirement: 1. Visually inspect the wing aft of the fuel filler for indications of inflight fuel leakage. 2. Visually inspect the fuel cap locking mechanism and seals for cracking, distortion and any condition which might prevent sealing. 3. Remove the fuel filler caps and inspect the adaptor sealing face for distortion, scratches, corrosion or any condition which may prevent the cap from sealing. 4. Visually check the sealing and security of the attachment of the adaptor flange to the adaptor plate paying particular attention to the adhesive (if present) between the parts. 5. Check the fuel cap seal by actuating the locking tab and noting that force is maintained between the cap, seal and adaptor when the tab is in the over-centre locking position. 6. Conduct a fuel cap leak test in accordance with Cessna SIL SE 82-34. Compliance: Prior to the issue of the next Maintenance Release after 30 June 1985 and thereafter at each issue of a new Maintenance Release. Background: This Amendment deletes the requirement for extensive inspection and testing of fuel filler caps against possible water ingress, for aeroplanes fitted with raised fuel filler necks.