AD/MSR/22 - Rear Fuselage Structure - 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 Aerospatiale Rallye Series Aeroplanes
AD/MSR/22 Rear Fuselage Structure - Inspection 6/76
Applicability: All models.
Requirement: 1. Remove the fuselage tail-cone and fin dorsal fairing and, with the aid of a torch, visually inspect the fuselage internal and external stringers for corrosion.
- If corrosion is detected remove the empennage components and perform a detailed visual inspection of the rear fuselage structure for corrosion damage.
Compliance: Before 15 July 1976 and thereafter at intervals not exceeding 3 years.