AIRWORTHINESS DIRECTIVE
Beechcraft B36TC Bonanza · Airworthiness Directives
Overview
This document is an Airworthiness Directive (AD) issued by the Civil Aviation Safety Authority (CASA) of Australia concerning the Beechcraft 36 (Bonanza) series aircraft, specifically addressing the wing forward spar carry-through structure. The directive mandates inspections and potential repairs to ensure the safety and airworthiness of affected aircraft. It replaces a previous AD and incorporates updated references to the relevant FAA AD. The compliance requirements are based on findings from the FAA regarding structural integrity issues, specifically cracks in the wing structure, which necessitate immediate attention from aircraft operators. The directive is applicable to specific serial numbers of the Beechcraft 36 and A36 aircraft, as well as the A36TC and B36TC models.
- The AD is effective from 28 November 2014.
- It applies to specific serial numbers of Beechcraft 36, A36, A36TC, and B36TC aircraft.
- Operators must conduct initial and repetitive inspections for cracks in the wing structure.
- Compliance is based on FAA AD 95-04-03 Amendment 39-9155.
- This AD replaces the previous AD/BEECH 36/37.
Summary written by AI from the source document. Check the original before relying on it. See which parts of Sprinkle are written by AI.
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 ·
- Airworthiness Directives
- Year ·
- 2014
- Pages ·
- 1
- File size ·
- 17 KB
- Copy found at ·
- services.casa.gov.au
What is the AIRWORTHINESS DIRECTIVE?
The AIRWORTHINESS DIRECTIVE is a airworthiness directives for the Beechcraft B36TC Bonanza, dated 2014.
How many pages is the AIRWORTHINESS DIRECTIVE?
The copy of the AIRWORTHINESS DIRECTIVE on file runs 1 pages.
What year was the AIRWORTHINESS DIRECTIVE published?
The AIRWORTHINESS DIRECTIVE — the Beechcraft B36TC Bonanza airworthiness directives on file — is dated 2014.
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- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins on file
- Type Certificate (TCDS)
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In this document
Applicability
The AD applies to Beechcraft 36 and A36 aircraft with serial numbers E-1 to E-2397, and A36TC and B36TC aircraft with serial numbers EA-1 to EA-471.
Requirement
Operators must follow the technical requirements outlined in FAA AD 95-04-03 Amendment 39-9155, which includes initial and repetitive inspections of the wing front carry-through frame structure.
Compliance
Compliance with the AD is required as specified in FAA AD 95-04-03, with a revised effective date of 28 November 2014.
Background
The FAA has reported instances of cracks in the wing front carry-through frame structure, prompting the issuance of this AD to ensure that necessary inspections and repairs are conducted.
Summary written by AI from the source document. Check the original before relying on it. See which parts of Sprinkle are written by AI.
Safety notes
- Cracks in the wing structure can compromise aircraft safety and must be addressed promptly.
Summary written by AI from the source document. Check the original before relying on it. See which parts of Sprinkle are written by AI.
Full document text
COMMONWEALTH OF AUSTRALIA Civil Aviation Safety Regulations 1998 (CASR 1998) CIVIL AVIATION SAFETY AUTHORITY Regulation 39.001 Page 1 of 1 AIRWORTHINESS DIRECTIVE On the effective date specified below, and for the reasons set out in the background section, the CASA delegate whose signature appears below repeals Airworthiness Directive (AD) AD/BEECH 36/37 and issues the following AD under subregulation 39.001 (1) of CASR 1998 and subsection 33 (3) of the Acts Interpretation Act 1901. The AD requires that the action set out in the requirement section (being action that the delegate considers necessary to correct an unsafe condition) be taken in relation to the aircraft or aeronautical product mentioned in the applicability section: (a) in the circumstances mentioned in the requirement section; and (b) in accordance with the instructions set out in the requirement section; and (c) at the time mentioned in the compliance section. Beechcraft 36 (Bonanza) Series Aeroplanes AD/BEECH 36/37 Amdt 1 Wing Forward Spar Carry-Through Structure 24/2014 Applicability: The following Beech Aircraft Corporation aircraft: (a) model 36 and A36 aircraft with serial numbers from E-1 to E-2397 inclusive; (b) model A36TC and B36TC aircraft with serial numbers from EA-1 to EA-471 inclusive. Requirement: Action in accordance with the technical requirements of Federal Aviation Administration of the United States of America (FAA) AD 95-04-03 Amendment 39-9155. Note: Beech Service Bulletin 2360 refers. Compliance: As specified in FAA AD 95-04-03 Amendment 39-9155 with a revised effective date of 28 November 2014. The effective date of this AD is 28 November 2014. Background: The FAA has received reports of cracks in the wing front carry-through frame structure. AD/BEECH 36/37 requires initial and repetitive inspections and repair or reinforcement if found cracked. This AD replaces AD/BEECH 36/37 and updates the references to the relevant FAA AD to the latest issue from the FAA. Mike Higgins Delegate of the Civil Aviation Safety Authority 21 November 2014