AD/G1159/30 - Fuselage, Rudder Actuator Structural Attachment Points - Inspection
1AD/G1159/30 - Fuselage, Rudder Actuator Structural Attachment Points - Inspection
Start here
Get a plain-English read of 1
Turn the raw legal text into a practical explanation grounded in AD/G1159/30 - Fuselage, Rudder Actuator Structural Attachment Points - Inspection.
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) G1159 and G-IV Series Aeroplanes
AD/G1159/30 Fuselage, Rudder Actuator Structural
Attachment Points - Inspection
12/81
Applicability: All model G1159 (Gulfstream II) aeroplanes which have achieved 3000 hours (or more) time in service since manufacture.
Document: Gulfstream American C.B. No. 303.
Compliance: Unless already accomplished, inspect within 50 hours time in service after 10 November, 1981.
Background: Operator reports involving the following discrepancies, elongated bolt holes, cracks and loose fasteners in the rudder actuator attachment area, have been received by the manufacturer.