Federal Register of Legislation
COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 106 CIVIL AVIATION SAFETY AUTHORITY SCHEDULE OF AIRWORTHINESS DIRECTIVES
AlliedSignal (Garrett/AiResearch) Turbine Engines - TFE731 Series
AD/TFE731/3 Amdt 1
H.P. Turbine Blade P/N 3072111-1 - Replacement 4/86
Applicability: TFE 731-2-1C; -2-2B fitted with turbine blades P/N 3072111-1. Requirement: Garrett S.B. TFE 731-72-3026 Rev 10. Note: Equipment modified I.A.W. a previous issue of this Directive may require further rework.
Compliance: Before exceeding 1000 hours time in service.
Background: This Directive is amended to reflect the manufacturers latest revision 10 to the Requirement Document which recommends no mixing of 3072455-10 blades with -9 or -12 and references S.B. TFE 731-72-3219 for turbine rotor assembly identification.
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