AD/CESSNA 340/23 - Elevator Balance Weight - Inspection
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
View image in the official source Cessna 340 Series Aeroplanes
AD/CESSNA 340/23 Elevator Balance Weight - Inspection 3/82
Applicability: All models 340 and 340A with S/No. referenced in Cessna SIL ME81-35 or with S/Nos. referenced in subsequent issues or revisions of that SIL.
Document: Cessna SIL No. ME81-35.
Compliance: Within 100 hours time in service after 31 March 1982.
Background: Manufacturer’s service information indicates that aircraft which have installed improved stabilisers and elevators may have incorrectly attached or loose elevator balance weights.