Federal Register of Legislation
COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 106 CIVIL AVIATION SAFETY AUTHORITY SCHEDULE OF AIRWORTHINESS DIRECTIVES
Pratt and Whitney Canada Turbine Engines - PW100 Series
AD/PW100/3 Fuel Pump Outlet Filter Cover 5/91
DM
Applicability: All PW100 series engines.
Requirement: Action in accordance with the technical requirements of Transport Canada Airworthiness Directive CF-90-21.
Note: Netherlands Airworthiness Directive 90-130 refers.
Compliance: Prior to 30 April 1991.
Background: This Directive requires modification of the engine driven fuel pump outlet filter cover assembly. This requirement reflects the requirements of Transport Canada AD CF- 90-21, and advice of a recent in-flight fuel leak event involving an Australian registered DHC-8. Investigation of this event indicated the leak source to be a cut fuel pump outlet filter cover O-ring.
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