Federal Register of Legislation
COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY SCHEDULE OF AIRWORTHINESS DIRECTIVES
DHC-2 (Beaver) Series Aeroplanes
AD/DHC-2/29 Elevator Mass Balance Weight 9/97
Applicability: All de Havilland DHC-2 MK I and MK II Beaver aircraft, and all DHC-2 MK III Turbo Beaver aircraft.
Requirement: a. For all MK I and MK II Beaver aircraft:
Inspect the elevator tip rib for corrosion and install Modification 2/1540 in accordance with instructions contained in de Havilland Service Bulletin 2/50 (Installation of Access Cover and Special Inspection of the Elevator Mass Balance Weight for Separation).
b. For all MK III Turbo Beaver aircraft:
Inspect the elevator tip rib for corrosion and install Modification T2/2079 in accordance with instructions contained in de Havilland Service Bulletin TB/58 (Installation of Access Cover and Special Inspection of the Elevator Mass Balance Weight for Separation).
Note: Transport Canada AD CF-97-06 refers.
Compliance: Before 31 January 1998; thereafter at intervals not to exceed 5 years. This airworthiness directive becomes effective on 14 August 1997. Background: Field reports were received of the elevator tip rib corroding underneath the mass balance weights. This corrosion could lead to a loss of the balance weight in flight, and possible flight control difficulties.
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