Federal Register of Legislation
COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY SCHEDULE OF AIRWORTHINESS DIRECTIVES
Mitsubishi MU-2 Series Aeroplanes
AD/MU-2/21 Amdt 1
Outer Fuel Tank Switch Wiring - Modification 10/84
Applicability: All models MU-2B-25/-26/-26A/-35/-36A/-40/-60. Aircraft which have previously complied with SR017/28- 001 dated 25 July 1979. Model MU-2B-40. S/Nos. 395SA thru 412SA, 414SA and 416SA. Model MU-2B-60. S/Nos. 731SA thru 747SA and 749SA thru 757SA.
Requirement: Mitsubishi SB No. SB013/28-001 or SB014/28-002 as applicable. Compliance: Within the next 100 hours time in service after 31 January 1980. Background: a. To prevent the possibility of fuel being transferred overboard either on the ground or in flight from the outer tanks when the FUEL/TRANSFER switch is in TIP MAN and the outer pump switch is placed in MANUAL.
b. Amendment 1 is to clarify "Applicability" due to entry of an additional Model to the Australian Register.
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