Commonwealth legislation

AD/DH 104/14 Amdt 3 - Wing/Fuselage Lower Main Root Joint - Inspection

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Commonwealth

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legislative instrument

Plain English Summary

3/10 complexity

This Airworthiness Directive requires operators of all DH 104 (Dove) series aeroplanes to inspect the wing-to-fuselage lower main root joint for corrosion, fretting and cracking, using the procedures in Hawker Siddeley Technical News Sheet CT(104) No.168 Issue 4. The Directive also accepts specified alternative non‑destructive inspection techniques (magnetic particle or fluorescent magnetic particle) in place of the eddy‑current method; compliance is as detailed in the cited technical sheet.

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AD/DH 104/14 Amdt 3 - Wing/Fuselage Lower Main Root Joint - 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 104/14

Amdt 3

Applicability: All models.

Wing/Fuselage Lower Main Root Joint - Inspection

9/71

Requirement: Inspect the wing to fuselage lower main root joint for corrosion, fretting and cracking in accordance with Hawker Siddeley Technical News Sheet CT(104) No. 168 Issue 4.

Note: Magnetic particle inspection to para. 1.2 of the previous issue of this Directive, or fluorescent magnetic particle inspection in accordance with ANO 108.8 are acceptable alternatives to the eddy current technique specified in Hawker Siddeley TNS CT (104) No. 217 and Appendix 2 of TNS CT(104) No. 168 Issue 4.

Compliance: As detailed in TNS CT(104) No. 168 Issue 4.

Source text

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