AD/G164/8 Amdt 1 - Main Landing Gear Leg - Inspection
1AD/G164/8 Amdt 1 - Main Landing Gear Leg - Inspection
Start here
Get a plain-English read of 1
Turn the raw legal text into a practical explanation grounded in AD/G164/8 Amdt 1 - Main Landing Gear Leg - 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 Schweizer (Grumman) G-164 (Ag-Cat) Series Aeroplanes
AD/G164/8
Amdt 1
Main Landing Gear Leg - Inspection 8/67
Applicability: All models with landing gear legs which have exceeded 5000 landings.
Requirement: 1. Inspect the main undercarriage spring legs by magnetic particle method for transverse cracking in the vicinity of the outboard clamp on the upper and lower surfaces.
- Replace cracked legs before further flight. Compliance: At intervals not exceeding 3000 landings.