AD/SD3-60/8 Amdt 2 - Elevator Torque Shaft Assembly
1AD/SD3-60/8 Amdt 2 - Elevator Torque Shaft Assembly
Start here
Get a plain-English read of 1
Turn the raw legal text into a practical explanation grounded in AD/SD3-60/8 Amdt 2 - Elevator Torque Shaft Assembly.
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 SD3-60 Series Aeroplanes
AD/SD3-60/8
Amdt 2
Elevator Torque Shaft Assembly 6/85 DM
Applicability: All Models SD-360 aircraft. Requirement: 1. Shorts SB SD360-27-A06 Rev 1.
- Shorts SB SD360-27-06.
Compliance: 1. Prior to 14 March 1985 and thereafter at intervals not exceeding 60 hours time in service or pre-first flight following parking in severe wind gust conditions.
- Prior to 15 August 1985.
Background: This Directive was issued after loss of elevator control on a SD3-30 aircraft. Rev 1 extended the inspection area and introduced a repetitive inspection. Rev 2 introduces mandatory modification to reinforce the attachment of the elevator torque shaft housings.