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AD/BEECH 300/8 Amdt 3 - Wing Attach Fittings, Bolts and Nuts
Beechcraft 300 Series AeroplanesBeechcraft 300 Series Aeroplanes
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Beechcraft 300 Series Aeroplanes
| AD/BEECH 300/8 Amdt 3 | Wing Attach Fittings, Bolts and Nuts | 25/2016 |
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| Applicability: | All Beech 300 and B300 series aircraft. |
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| Requirement: | 1. Inspect all of the outboard (upper forward, upper and lower aft) wing tension attach bolts and nuts in accordance with the latest revision of Beechcraft Structural Inspection and Repair Manual 98-39006, Section 57-18-01, Chart 201 (Model 300) or Section 57-18-02, Chart 201 (B300/B300C), as in force at the date of this AD.2. Replace all of the outboard (upper forward, upper and lower aft) wing bolts and nuts.3. Replace all of the outboard lower forward wing bolts and nuts (at the lower forward attach fitting). |
| Compliance: | 1. Inspect at intervals not to exceed 5 years component time in service.2. Replace at intervals not to exceed 20 years or 20,000 hours component time in service, whichever occurs first.3. Replace at intervals not to exceed 5 years component time in service or at any time they are removed, whichever occurs first. |
| This AD commences on 14 December 2016. | |
| Background: | This AD mandates the life and inspection period of outer wing attach bolts and nuts.Amendment 1 changed the Compliance part 2, so that it was the same as the replacement life specified in the Airworthiness Limitations section of the Maintenance Manual which is 15 years/15,000 hours, whichever occurs first.Amendment 2 changed the Compliance part 2, so that it is the same as the replacement life specified in the Airworthiness Limitations section of the Maintenance Manual which is 20 years/20,000 hours, whichever occurs first. |
| This amendment clarifies the version of the Beechcraft Structural Inspection and Repair Manual to be complied with. |
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Benjamin Wilson
Delegate of the Civil Aviation Safety Authority
5 December 2016