AD/DH 104/37 - Aileron Mass Balance Weight Assembly
1AD/DH 104/37 - Aileron Mass Balance Weight Assembly
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Image unavailable in extracted text DH 104 (Dove) Series Aeroplanes
AD/DH 104/37 Aileron Mass Balance Weight Assembly 7/87 DM
Applicability: All models.
Requirement: Action in accordance with British Aerospace TNS 245 Issue 1. Compliance: 1. Carry out the visual inspection within 14 days after 30 April 1987 and,
- If no corrosion is evident visually, carry out the radiographic inspection within 50 hours time in service after 30 April 1987 but no later than 31 July 1987.
Background: A case has been reported on a Heron aircraft of severe internal corrosion. Loss or failure of the balance assembly may cause aileron flutter or severe handling problems.