Commonwealth legislation

AD/BEECH 36/37 Amdt 1 — Wing Forward Spar Carry-Through Structure

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

3/10 complexity

Requires owners/operators of Beechcraft 36/A36 and A36TC/B36TC aeroplanes in the listed serial ranges to perform initial and repetitive inspections of the wing forward spar carry‑through frame for cracks and to repair or reinforce any cracking, following FAA AD 95‑04‑03 (Amendment 39‑9155) and associated Beech service information. This AD replaces the prior AD, updates the FAA reference, and takes effect 28 November 2014. Owners/operators pay for inspections and repairs and must follow FAA technical instructions.

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Current sections

Direct links to the current provisions in AD/BEECH 36/37 Amdt 1 — Wing Forward Spar Carry-Through Structure.

Beechcraft 36 (Bonanza) Series Aeroplane

Beechcraft 36 (Bonanza) Series Aeroplanes

AD/BEECH 36/37 Amdt 1	Wing Forward SparCarry-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 95-04-03Amendment 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.

View image in the official source

Mike Higgins
Delegate of the Civil Aviation Safety Authority

21 November 2014

AD/BEECH 36/37 Amdt 1

Wing Forward SparCarry-Through Structure

Wing Forward Spar

Carry-Through Structure

24/2014

Source text

Sourced from the Federal Register of Legislation (legislation.gov.au), CC BY 4.0.

Beechcraft 36 (Bonanza) Series Aeroplane Beechcraft 36 (Bonanza) Series Aeroplanes

Beechcraft 36 (Bonanza) Series Aeroplanes

AD/BEECH 36/37 Amdt 1	Wing Forward SparCarry-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 95-04-03Amendment 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

AD/BEECH 36/37 Amdt 1 AD/BEECH 36/37 Amdt 1