AD/HS 748/16 - Main and Nose Landing Gear Life Limits
1AD/HS 748/16 - Main and Nose Landing Gear Life Limits
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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 British Aerospace (Hawker Siddeley) HS 748 Series Aeroplanes
AD/HS 748/16 Main and Nose Landing Gear Life Limits 5/95
Applicability: All HS 748 aircraft.
Requirement: Retire from service nose and main landing gear components and associated equipment listed in Dowty Aerospace Landing Gear Service Bulletin (SB) 32-104E.
Compliance: Retire at the times specified in Dowty Aerospace Landing Gear SB 32-104E Tables 1 to 7 inclusive.
Background: The results of extensive fatigue testing indicate that a number of Structurally Significant Items on the main and nose landing gears are life limited and consequently a retirement life is specified.