Commonwealth legislation

AD/DH 104/25 Amdt 1 - Flap Datum Hinge Assembly - Inspection

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

3/10 complexity

This airworthiness directive requires operators of all DH 104 (Dove) aircraft to inspect the flap datum hinge assembly, with the inspection procedures and any follow‑up actions specified in Hawker Siddeley TNS CT(104) No.216 Issue 2. One inspection task must be done within 25 hours TIS after 20 July 1970; operators arrange and pay for the work.

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Current sections

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AD/DH 104/25 Amdt 1 - Flap Datum Hinge Assembly - Inspection

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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 104/25

Amdt 1

Flap Datum Hinge Assembly - Inspection 7/70

Applicability: All models.

Document: Hawker Siddeley TNS CT(104) No. 216 Issue 2.

Compliance: For Para. 4.1 - Within 25 hours time in service after 20 July 1970.

For Paras. 4.2 and 4.3 - In accordance with the requirement document.

Source text

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