AD/AA-5/22 - Aileron Torque Tube - Inspection and Modification
1AD/AA-5/22 - Aileron Torque Tube - Inspection and Modification
Start here
Get a plain-English read of 1
Turn the raw legal text into a practical explanation grounded in AD/AA-5/22 - Aileron Torque Tube - 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 NK,Aircraft below 5700 kg,Gulfstream (Grumman American/ American Aviation) AA-5 Series Aeroplanes,Aileron Torque Tube - Inspection and Modification,22 title: Airworthiness Directive - AD/AA-5/22 - Aileron Torque Tube - 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 Gulfstream (Grumman American/ American Aviation) AA-5 Series Aeroplanes
AD/AA-5/22 Aileron Torque Tube - Inspection and Modification NK
Applicability: All models AA5A with S/Nos. -0176 to -0805;
All models AA5B with S/Nos. -0303 to -1078, and all models which have been fitted with replacement ailerons P/N 5202035-505 shipped from factory between May 1976 and January 1979.
Document: Gulfstream American SB No. 163.
Compliance: Within 25 hours’ time in service after 4 July 1979.
Background: The manufacturer advises that the aileron torque tube joints may have been assembled incorrectly.