Commonwealth legislation

AD/BEECH 90/32 - Elevator Stop Bolts - Modification

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

2/10 complexity

This directive requires owners/operators of specified Beechcraft Model C90 and E90 aeroplanes to modify elevator stop bolts per Beechcraft Service Instruction No. 0618-152, within 100 hours’ time‑in‑service after 30 September 1974. Compliance (parts, labour, scheduling) is the operator’s responsibility; the AD delegates the technical method to the external Service Instruction. The instrument does not state a safety rationale, cost estimates, enforcement or exemption procedures in the provided text.

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 90/32 - Elevator Stop Bolts - Modification.

AD/BEECH 90/32 - Elevator Stop Bolts - Modification

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 90 and 65-90 (King Air) Series Aeroplanes

AD/BEECH 90/32 Elevator Stop Bolts - Modification 9/74

Applicability: All models C90 with S/Nos. LJ-552 to LJ-588. All models E90 with s/Nos. LW-1 to LW-56.

Document: Beechcraft SI No. 0618-152.

Compliance: Within 100 hours’ time in service after 30 September 1974.

Source text

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