Federal Register of Legislation
COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 106 CIVIL AVIATION SAFETY AUTHORITY SCHEDULE OF AIRWORTHINESS DIRECTIVES
Turbomeca Turbine Engines - Makila Series
AD/MAKILA/2 Governor Master and Auxiliary Cams 1/92
Applicability: All Makila 1A and 1A1 engines.
Requirement: Unless previously carried out action in accordance with Turbomeca Service Makila No 72.298.00.59.
Note: DGAC AD 91-226-(B) refers.
Compliance: Within 600 hours time in service from 30 November 1991 or by 31 August 1992, whichever occurs first.
Background: Engine flame out can occur when the control lever is rapidly retarded from the flight to quick reduction position.
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