AD/DH114/48 - Aileron Mass Balance Weight Assembly
1AD/DH114/48 - Aileron Mass Balance Weight Assembly
Start here
Get a plain-English read of 1
Turn the raw legal text into a practical explanation grounded in AD/DH114/48 - Aileron Mass Balance Weight Assembly.
meta-content-style-type: text/css meta-content-type: application/xhtml+xml; charset=utf-8 meta-generator: Aspose.Words for .NET 22.10.0
?xml version="1.0" encoding="utf-8" standalone="no"?>
COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Image unavailable in extracted text DH114 (Heron) Series Aeroplanes
AD/DH114/48 Aileron Mass Balance Weight Assembly 7/87
Applicability: All models.
Requirement: 1. Action in accordance with British Aerospace TNS W19 Issue 1, or
-
Inspect in accordance with a scheme approved by the Secretary. Compliance: Unless already accomplished;
-
In accordance with the Requirement Document, but no later than 31 August 1987.
2. At the next inspection for Maintenance Release issue after 30 June 1987 but no later than 31 August 1987.
Background: A case has been reported of severe internal corrosion. Loss or failure of the balance assembly may cause aileron flutter or severe handling problems.