Commonwealth legislation

AD/BEECH 33/37 Amdt 1 — Wing Forward Spar Carry-Through Structure

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Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

4/10 complexity

This AD requires owners/operators of specified Beechcraft 33 and 35‑33 series aeroplanes (listed by serial number) to carry out initial and repetitive inspections of the wing forward spar carry‑through structure and to repair or reinforce any cracks found. It mandates compliance with FAA AD 95‑04‑03 Amendment 39‑9155 (see Beech Service Bulletin 2360) and takes effect 28 November 2014; owners/operators pay for inspections and any repairs and must follow the FAA AD's procedures and timings.

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Current sections

Direct links to the current provisions in AD/BEECH 33/37 Amdt 1 — Wing Forward Spar Carry-Through Structure.

Beechcraft 33 and 35-33 (Debonair/Bonanz

Beechcraft 33 and 35-33 (Debonair/Bonanza) Series Aeroplanes

AD/BEECH 33/37 Amdt 1	Wing Forward SparCarry-Through Structure	24/2014

Applicability:	The following Beech Aircraft Corporation aircraft:(a) model 35-33, 35-A33, 35-B33, 35-C33, E33,F33 and G33 aircraft with serial numbers from CD-1 to CD1304 inclusive;(b) model 35-C33A, E33A and F33A aircraft with serial numbers from CE-1 to CE-1192 inclusive;(c) model E33C and F33C aircraft with serial numbers from CJ-1 to CJ-179 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 33/37 requires initial and repetitive inspections and repair or reinforcement if found cracked.This AD replaces AD/BEECH 33/37 and updates the references to the relevant FAA AD to the latest issue from the FAA.

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Mike Higgins
Delegate of the Civil Aviation Safety Authority

21 November 2014

AD/BEECH 33/37 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 33 and 35-33 (Debonair/Bonanz Beechcraft 33 and 35-33 (Debonair/Bonanza) Series Aeroplanes

Beechcraft 33 and 35-33 (Debonair/Bonanza) Series Aeroplanes

AD/BEECH 33/37 Amdt 1	Wing Forward SparCarry-Through Structure	24/2014

Applicability:	The following Beech Aircraft Corporation aircraft:(a) model 35-33, 35-A33, 35-B33, 35-C33, E33,F33 and G33 aircraft with serial numbers from CD-1 to CD1304 inclusive;(b) model 35-C33A, E33A and F33A aircraft with serial numbers from CE-1 to CE-1192 inclusive;(c) model E33C and F33C aircraft with serial numbers from CJ-1 to CJ-179 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 33/37 requires initial and repetitive inspections and repair or reinforcement if found cracked.This AD replaces AD/BEECH 33/37 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 33/37 Amdt 1 AD/BEECH 33/37 Amdt 1