AD/SC7/22 - Main Landing Gear Brake Flange
1AD/SC7/22 - Main Landing Gear Brake Flange
Start here
Get a plain-English read of 1
Turn the raw legal text into a practical explanation grounded in AD/SC7/22 - Main Landing Gear Brake Flange.
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 Short SC7 (Skyvan) Series Aeroplanes
AD/SC7/22 Main Landing Gear Brake Flange 10/95
Applicability: Skyvan MK 3, 3A, 3M, and Skyliner series aeroplanes.
Requirement: Inspect, using the fluorescent penetrant method, the main landing gear brake flanges in accordance with Dowty Mandatory Service Bulletin (MSB) 32-10M, Revision 3.
Note: CAA (UK) AD 017-12-81 refers.
Compliance: Before the thresholds specified in Dowty MSB 32-10M, Revision 3 or before 17 September 1995, whichever occurs later.
Re-inspect at intervals not to exceed 1000 landings.
Background: Dowty has completed a fatigue analysis of the main landing gear and inspections of the brake flange are required to take advantage of the increase in service life which resulted.