AD/AC/17A - Landing Gear Truss Attach Angle - Inspection
1AD/AC/17A - Landing Gear Truss Attach Angle - Inspection
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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 12/1967,Aircraft below 5700 kg,Twin Commander (Gulfstream/Rockwell/ Aerocommander 500, 600 and 700) Series Aeroplanes,Landing Gear Truss Attach Angle - Inspection,17A title: Airworthiness Directive - AD/AC/17A - Landing Gear Truss Attach Angle - Inspection
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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/17A Landing Gear Truss Attach Angle - Inspection 12/67
Applicability: All models: S/Nos. 231 to 892 except 875. Document: Aero Commander SL No. 77A.
Compliance: At intervals not exceeding 1000 hours’ time in service.