Federal Register of Legislation
COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY SCHEDULE OF AIRWORTHINESS DIRECTIVES
Eurocopter BO 105 Series Helicopters
AD/BO 105/14 Dual Hydraulic System Switch Over 10/89
DM
Applicability: All model BO 105 helicopters with tandem hydraulic units P/N 105-45028 having valve body manifolds D133-756E, D133-756, ZE1-126-1, ZE2-126-1 or ZE2-126 installed in either No. 1 or 2 hydraulic system.
Requirement: Action in accordance with MBB Alert Service Bulletin No ASB-BO 105-40-102.
Note: LBA AD 89-123 refers.
Compliance: Within 50 hours time in service after 25 August 1989 or by 30 September 1989, whichever occurs first.
Background: Due to possible excessive wear in the servo connecting components a functional test of the hydraulic system switch over is required.
We try to embed the page this law was scraped from. If the site blocks framing, you still get the link and a local excerpt.
Last checked with source on —
Checking whether the official page can be embedded…
Plain-English simplify of this law: a short summary, key points, and both sides of the argument. Generated on first view via Replicate, then cached. Vote on what helps your study.
No study brief is cached for this law yet. Sign up to generate a plain-English brief.
Sign up to generate