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AD/BEECH 36/37 Amdt 1 — Wing Forward Spar Carry-Through Structure
Beechcraft 36 (Bonanza) Series AeroplaneBeechcraft 36 (Bonanza) Series Aeroplanes
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Beechcraft 36 (Bonanza) Series Aeroplanes
| AD/BEECH 36/37 Amdt 1 | Wing Forward SparCarry-Through Structure | 24/2014 |
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| 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. |
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| 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. |
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Mike Higgins
Delegate of the Civil Aviation Safety Authority
21 November 2014