Commonwealth legislation

AD/BEECH 23/41 - Firewall and FS 68.00 Frame

RepealedCTH

This Act has been repealed and is no longer in force. It is retained for historical reference.

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

3/10 complexity

This Airworthiness Directive requires owners/operators of certain Beechcraft Model 19, 23, and 24 aircraft (specific serial numbers listed in the Applicability) to inspect the firewall and FS 68.00 frame for corrosion. Inspections must be repeated every 100 flight hours and the separate Beechcraft Service Instruction No. 1245 must be followed. The action addresses discovered corrosion that could weaken structure and compromise flight safety.

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Current sections

Direct links to the current provisions in AD/BEECH 23/41 - Firewall and FS 68.00 Frame.

AD/BEECH 23/41 - Firewall and FS 68.00 Frame

COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY

SCHEDULE OF AIRWORTHINESS DIRECTIVES

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Beechcraft 19, 23 and 24 Series Aeroplanes

AD/BEECH 23/41 Firewall and FS 68.00 Frame 7/83

Applicability: Models A23-19, 19A, M19A and B19 with S/Nos. MB-1 to MB-520.

Model B19 Sport 150 with S/Nos. MB-521 to MB-905.

Models 23, A23, A23A, B23 and C23 with S/Nos. M-1 to M-1361. Model C23 Sundowner 180 with S/Nos. M-1362 to M-2352.

Models A23-24 and A24 with S/Nos. MA-1 to MA-368. Model A24R with S/Nos. MC-2 to MC-95.

Models A24R, B24R and C24R Sierra 200 with S/Nos. MC-96 to MC-772.

Requirement: Action in accordance with Beechcraft SI No. 1245 Parts I and II.

Compliance: Part I : Within 100 hours time in service after 31 July 1983 and thereafter at intervals not exceeding 100 hours time in service.

Part II: As per Requirement Document.

Background: The manufacturer reports corrosion in the areas surrounding the firewall and FS 68.00 frame.

Source text

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

1 AD/BEECH 23/41 - Firewall and FS 68.00 Frame