AD/GA-7/6 - Rudder Bellcrank Torque Tube - Inspection and Modification
1AD/GA-7/6 - Rudder Bellcrank Torque Tube - Inspection and Modification
Start here
Get a plain-English read of 1
Turn the raw legal text into a practical explanation grounded in AD/GA-7/6 - Rudder Bellcrank Torque Tube - Inspection and Modification.
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 Gulfstream (Grumman American) GA-7 Series Aeroplanes
AD/GA-7/6 Rudder Bellcrank Torque Tube - Inspection NK
and Modification
Applicability: All model GA-7 with S/Nos. GA7-0002 to GA-70038, GA7- 0040, GA7-0042 to GA7-0087.
Document: Gulfstream American SB No. ME-16.
Compliance: 1. Inspect within 10 hours time in service after 28 February 1979.
- Modify as per requirement document.
Background: Partial loss of rudder control may occur if free play in the rudder circuit exceeds 1 degree.