AD/DH 104/34 Amdt 2 - Centre Section Main Spar Top and Bottom Boom Joint - Inspection
COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
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DH 104 (Dove) Series Aeroplanes
AD/DH 104/34
Amdt 2
Applicability: All models.
Centre Section Main Spar Top and Bottom Boom Joint - Inspection
9/77
Requirement: 1. Inspect the Centre Section Main Spar Top boom in accordance with Hawker Siddeley TNS CT(104) No. 237 Appendix 1, or in accordance with a technique approved by the Secretary. Technique ATG/NDI/US/1 constitutes such an approved technique.
- Inspect the Centre Section Main Spar Bottom boom of those aircraft without Modification 779 embodied, in accordance with Hawker Siddeley TNS CT(104) No. 238 appendix 1, or in accordance with a technique approved by the Secretary. Technique ATG/NDI/US/1 constitutes such an approved technique.
Note: Where crack indications are found the Airworthiness Branch, Central Office, is to be notified before further flight.
Compliance: Inspect at intervals in accordance with Hawker Siddeley TNS CT(104) Nos. 237 and 238 Issue 2 as applicable.