AD/BEECH 60/17 - Flap Bracket
1AD/BEECH 60/17 - Flap Bracket
Start here
Get a plain-English read of 1
Turn the raw legal text into a practical explanation grounded in AD/BEECH 60/17 - Flap Bracket.
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 Beechcraft 60 (Duke) Series Aeroplanes
AD/BEECH 60/17 Flap Bracket 8/72
Applicability: All models which have achieved 1000 or more hours’ time in service.
Requirement: Inspect flap actuator bracket and adjacent structure on RH and LH flaps for cracks or signs of distress.
Compliance: Within 100 hours’ time in service after 31 August 1972 and thereafter at intervals not exceeding 300 hours’ time in service.