AD/LEARJET/34 - Flap Attachment Fittings
1AD/LEARJET/34 - Flap Attachment Fittings
Start here
Get a plain-English read of 1
Turn the raw legal text into a practical explanation grounded in AD/LEARJET/34 - Flap Attachment Fittings.
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/34 Flap Attachment Fittings 9/86
Applicability: All model Learjet 24 & 25 with Serial Numbers. 24-328 to 24-357, 25-135, 25-188
and 25-205 to 25-367.
Requirement: Inspect in accordance with Gates Learjet S.B. 24/25-333. Compliance: Within 200 hours time in service after 30 September 1986.
Background: Cracking of the flap attachment fitting has become evident in service. Failure of a flap attach fitting may result in an asymmetric flap condition.