Commonwealth legislation

AD/BEECH 18/1 - Starter Solenoid and Main Bus Lead Wire - Inspection

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

2/10 complexity

This directive requires owners/operators of Beechcraft Model C‑18S and AT‑11 aircraft to carry out an immediate inspection of the starter solenoid and main bus lead, to be performed in accordance with one of the three referenced documents (Beechcraft SB C18‑5, FAA AD 47‑6‑8, or ANO 105.1.4.3.6.1).

Issued under CASA (Part 39), compliance is mandatory “forthwith”; the text itself does not state who pays or the detailed inspection steps.

JSON API

Deep dive

Want the full deep dive?

Zoe can write the in-depth analysis on top of the summary above: how it works, who it affects and what each part actually does.

Current sections

Direct links to the current provisions in AD/BEECH 18/1 - Starter Solenoid and Main Bus Lead Wire - Inspection.

AD/BEECH 18/1 - Starter Solenoid and Main Bus Lead Wire - Inspection

meta-content-style-type: text/css meta-content-type: application/xhtml+xml; charset=utf-8 meta-generator: Aspose.Words for .NET 22.10.0

?xml version="1.0" encoding="utf-8" standalone="no"?>

COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY

SCHEDULE OF AIRWORTHINESS DIRECTIVES

View image in the official source Beechcraft 18 Series Aeroplanes

AD/BEECH 18/1 Starter Solenoid and Main Bus NK

Lead Wire - Inspection

Applicability: Model C-18S and AT-11. Document: 1. Beechcraft SB No. C18-5; or

FAA AD 47-6-8; or 3. ANO 105.1.4.3.6.1.

Compliance: Forthwith.

Source text

Sourced from the Federal Register of Legislation (legislation.gov.au), CC BY 4.0.