AD/FU24/2 Amdt 1 - Structural Component - Corrosion - Inspection
1AD/FU24/2 Amdt 1 - Structural Component - Corrosion - Inspection
Start here
Get a plain-English read of 1
Turn the raw legal text into a practical explanation grounded in AD/FU24/2 Amdt 1 - Structural Component - Corrosion - 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 Airparts (NZ) Ltd. FU 24 Series Aeroplanes
AD/FU24/2
Amdt 1
Structural Component - Corrosion - Inspection 7/68
Applicability: All models.
Requirement: Inspect fuselage longerons, centre wing, main and rear spars, wing attachment fittings and other major structural components for signs of corrosion and effect any necessary repairs.
Note: This inspection will involve dismantling the aircraft as it is not provided with sufficient inspection panels to complete inspection of the main structure.
Compliance: At intervals not exceeding 3 years for aircraft engaged in agricultural operations. At intervals not exceeding 5 years for aircraft engaged in operations other than agricultural.