Commonwealth legislation

AD/BEECH 60/15 - Wing Lift Detector With Heated Vane

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Commonwealth

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legislative instrument

Plain English Summary

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This AD mandates that owners/operators of specific Beechcraft Model 60/A60 aeroplanes used for flight into known icing must complete the inspections/modifications set out in Beechcraft Service Instructions 0431‑355 and 0430‑355 (Rev.2) by 31 October 1972. It targets the wing lift detector with heated vane; operators must obtain the SIs, fund and arrange the work through maintenance providers, and meet the fixed compliance deadline.

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AD/BEECH 60/15 - Wing Lift Detector With Heated Vane

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

SCHEDULE OF AIRWORTHINESS DIRECTIVES

View image in the official source Beechcraft 60 (Duke) Series Aeroplanes

AD/BEECH 60/15 Wing Lift Detector With Heated Vane 2/72

Applicability: Model 60 with S/Nos. P-3 to P-122 and P-124 to P-126, and Model A60 with S/Nos. P-123, P-127 to P-151, P-153, P-154, P-157 and P-159 to P-162, used for flight into known icing conditions.

Requirement: Action in accordance with Beechcraft SI No. 0431-355 and Beechcraft SI No. 0430- 355, Rev. 2.

Compliance: Before 31 October 1972.

Source text

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