AD/CESSNA 400/60 Amdt 1 - Main Landing Gear Trunnion - Inspection
1AD/CESSNA 400/60 Amdt 1 - Main Landing Gear Trunnion - Inspection
Start here
Get a plain-English read of 1
Turn the raw legal text into a practical explanation grounded in AD/CESSNA 400/60 Amdt 1 - Main Landing Gear Trunnion - 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 Cessna 400 Series Aeroplanes
AD/CESSNA 400/60
Amdt 1
Main Landing Gear Trunnion - Inspection 6/80
Applicability: All models 402 with S/Nos. 402C0001 to 402C0039; All models 414 with S/Nos. 414A0001 to 414A0235; All models 421 with S/Nos. 421C0001 to 421C0638.
Document: Cessna SIL ME 79-11.
Compliance: On achieving 300 hours time in service and thereafter at intervals not exceeding 50 hours time in service until modified.
Background: In service cracking of the existing main landing gear trunnion may occur.