Federal Register of Legislation
COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY SCHEDULE OF AIRWORTHINESS DIRECTIVES
Pilatus PC-12 Series Aeroplanes
AD/PC-12/3 Amdt 1
Electrical Wiring 3/97
Applicability: All PC-12 aeroplanes up to and including serial number 140.
Requirement: Unless previously accomplished, modify in accordance with Pilatus Aircraft Ltd PC- 12 Service Bulletin 24-003 Revision 1 dated 18 September 1996.
Note: FOCA Switzerland AD HB 97-002 refers.
Compliance: Prior to 31 March 1997.
This Amendment takes effect on 27 February 1997.
Background: The Swiss Federal Office for Civil Aviation (FOCA) has advised that when the N ESNTL switch is set to AUTO the NON ESSENTIAL BUS may not automatically disconnect from the power distribution system when the BAT/GEN 1 bus tie circuit breaker (CB210) opens. Additionally FOCA has advised that reports have been received of incorrect wiring of the KN-40 Navigation Converter.
This amendment introduces a revision to the Requirement Document which corrects a wiring error in the original issue of the document.
The original issue of this Directive, mandated a wiring change, which eliminated the condition whereby the NON ESSENTIAL BUS remained connected, and an inspection of the KN-40 wiring.
The original issue of this Airworthiness Directive became effective on 7 November 1996.
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