Section 1 - AD/AC/59 Amdt 1 - Flap System - Flap Control Bracket - Inspection and Modification - AD/AC/59 Amdt 1 - Flap System - Flap Control Bracket - Inspection and Modification

meta-content-style-type: text/css meta-content-type: application/xhtml+xml; charset=utf-8 meta-description: CASA Airworthiness Directive meta-generator: Aspose.Words for .NET 22.10.0 meta-keywords: Issue 12/1979,Aircraft below 5700 kg,Twin Commander (Gulfstream/Rockwell/ Aerocommander 500, 600 and 700) Series Aeroplanes,Flap System - Flap Control Bracket - Inspection and Modification,59 Amdt 1 title: Airworthiness Directive - AD/AC/59 Amdt 1 - Flap System - Flap Control Bracket - Inspection and Modification

?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 Twin Commander (Gulfstream/Rockwell/ Aerocommander 500, 600 and 700) Series Aeroplanes

AD/AC/59

Amdt 1

Flap System - Flap Control Bracket - Inspection and Modification

12/79

Applicability: All 685, 690 and 690A with S/Nos. referenced in Rockwell SB No. 157A. Document: Rockwell SB No. 157A.

Compliance: Unless already accomplished, within 100 hours’ time in service after 31 Dec 1979.