CTHIn ForceLegislation
AD/LEARJET/21 - Aft Engine Beam - Inspection
1AD/LEARJET/21 - Aft Engine Beam - Inspection
Start here
Get a plain-English read of 1
Turn the raw legal text into a practical explanation grounded in AD/LEARJET/21 - Aft Engine Beam - 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 Gates Learjet 24 & 25 Series Aeroplanes
AD/LEARJET/21 Aft Engine Beam - Inspection 5/80
Applicability: All models 25 with S/Nos. 25-266 to 25-300. Document: Gates Learjet SB 25-298.
Compliance: As per requirement document.
Background: To inspect the aft engine beam forward web lightening hole flanges for cracks.