AD/DHC-3/30 - Elevator Connecting Rod
1AD/DHC-3/30 - Elevator Connecting Rod
Start here
Get a plain-English read of 1
Turn the raw legal text into a practical explanation grounded in AD/DHC-3/30 - Elevator Connecting Rod.
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 DHC-3 (Otter) Series Aeroplanes
AD/DHC-3/30 Elevator Connecting Rod 11/78
Applicability: All DHC-3 series.
Requirement: Action in accordance with De Havilland Aircraft of Canada SB No 3/35.
Compliance: Within 10 hours time in service after 16 October 1978 and thereafter at any time if parked aircraft has been subjected to jet blast, helicopter blast or winds in excess of 40 knots.