AD/HS 125/123 Amdt 1 - Wing Top Skin Panel
1AD/HS 125/123 Amdt 1 - Wing Top Skin Panel
Start here
Get a plain-English read of 1
Turn the raw legal text into a practical explanation grounded in AD/HS 125/123 Amdt 1 - Wing Top Skin Panel.
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 British Aerospace BAe 125 Series Aeroplanes
AD/HS 125/123
Amdt 1
Wing Top Skin Panel 6/93
Applicability: Model 125 aircraft up to and including Series 700A and 700B.
Requirement: Action in accordance with British Aerospace Mandatory Service Bulletin 57-73 Revision 1.
Compliance: Unless already accomplished, prior to 31 August 1993.
Background: Reports of wing top skin corrosion in the area beneath the boundary layer fence.
Amendment 1 is issued in response to a revision of the Requirement Document which extends applicability to include 700 A and B Series aircraft.