Commonwealth legislation

AD/DH 104/3 - Wing Root Main Spar Lower Joint - Modification

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Commonwealth

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legislative instrument

Plain English Summary

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This Airworthiness Directive requires all DH 104 (Dove) aircraft to have the wing‑root main spar lower joint modified per one of two specified technical documents (De Havilland Mod. No. Dove 686 Issue 2 or ANO 105.1.14.13.5.6) and completed before 1 September 1971. The obligation, scheduling and costs for parts, labour and downtime fall to each aircraft owner/operator.

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AD/DH 104/3 - Wing Root Main Spar Lower Joint - Modification

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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 DH 104 (Dove) Series Aeroplanes

AD/DH 104/3 Wing Root Main Spar Lower Joint - Modification 8/71

Applicability: All models.

Document: 1. De Havilland Mod. No. Dove 686, Issue 2 (TNS CT(104) No. 100); or 2. ANO 105.1.14.13.5.6.

Compliance: Before 1 September 1971.

Source text

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