SCHEDULE OF AIRWORTHINESS DIRECTIVES
Piper PA-24 Comanche 260 · Supplemental Type Certificate
Overview
This document is a Schedule of Airworthiness Directives issued by the Civil Aviation Safety Authority of Australia, specifically addressing the Piper PA-24 Comanche series aircraft. It outlines a specific directive related to the replacement of the Beryl Aviation filtrator assembly for models PA24, PA24-250, and PA24-260 that have been modified under FAA Supplemental Type Certificate No. SA2653WE. The directive mandates compliance within a specified time frame, ensuring that aircraft maintain airworthiness and safety standards. This document is crucial for aircraft maintenance personnel and operators of the affected Comanche models, providing clear instructions on necessary modifications to enhance operational safety.
- The directive applies to Piper PA-24, PA-24-250, and PA-24-260 models.
- Replacement of the Beryl Aviation filtrator assembly is mandatory.
- The existing assembly part number B-1113-1 must be replaced with either B-1113-M or B-1113-RM.
- Compliance is required within 100 hours of service after April 30, 1975.
- Alternative compliance can be achieved through FAA AD No. 75-05-02.
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Reference only, not for flight. Use the current approved manual for your aircraft. See terms, section 5.
Document
Source
Copy found at services.casa.gov.au. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type ·
- Supplemental Type Certificate
- Year ·
- 1975
- Pages ·
- 1
- File size ·
- 10 KB
- Copy found at ·
- services.casa.gov.au
What is the SCHEDULE OF AIRWORTHINESS DIRECTIVES?
The SCHEDULE OF AIRWORTHINESS DIRECTIVES is a supplemental type certificate for the Piper PA-24 Comanche 260, dated 1975.
How many pages is the SCHEDULE OF AIRWORTHINESS DIRECTIVES?
The copy of the SCHEDULE OF AIRWORTHINESS DIRECTIVES on file runs 1 pages.
What year was the SCHEDULE OF AIRWORTHINESS DIRECTIVES published?
The SCHEDULE OF AIRWORTHINESS DIRECTIVES — the Piper PA-24 Comanche 260 supplemental type certificate on file — is dated 1975.
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In this document
Applicability
The directive applies to Piper PA-24 series aircraft, specifically the PA24, PA24-250, and PA24-260 models that have undergone modifications as per FAA Supplemental Type Certificate No. SA2653WE.
Requirement
The directive requires the removal of the existing Beryl Aviation filtrator assembly, part number B-1113-1, and its replacement with either part number B-1113-M or B-1113-RM. Alternatively, compliance with FAA AD No. 75-05-02 is also acceptable.
Compliance
Operators must comply with this directive within 100 hours of time in service after April 30, 1975, ensuring timely action to maintain airworthiness.
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Full document text
COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY SCHEDULE OF AIRWORTHINESS DIRECTIVES Piper PA-24 (Comanche) Series Aeroplanes AD/PA-24/35 Beryl Aviation Filtrator Assembly - Replacement 4/75 Applicability: Models PA24, PA24-250, PA24-260 series which have been modified in accordance with FAA Supplemental Type Certificate No. SA2653WE (installation of engine crankcase breather and vacuum pump air-oil separator). Requirement: 1. Remove the Beryl Aviation filtrator assembly P/N B-1113-1 and install either P/N B-1113-M or P/N B-1113-RM; or 2. FAA AD No. 75-05-02. Compliance: Within 100 hours time in service after 30 April 1975.