Commonwealth legislation

AD/JETSTREAM/19 - Cracking of MLG Cylinder Upper Attach Lug

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

5/10 complexity

This AD (AD/JETSTREAM/19) requires operators of the BAe 3100 (Jetstream) aircraft listed in the requirement document to carry out the inspection and repair actions in British Aerospace SB 32‑JA860812 after fatigue testing revealed a crack in the main landing‑gear cylinder near the upper toggle attachment lug.

Affected operators or their maintenance organisations must consult the requirement document and service bulletin for exact applicability, timing and technical steps, and will bear the parts, labour and downtime costs.

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/JETSTREAM/19 - Cracking of MLG Cylinder Upper Attach Lug.

AD/JETSTREAM/19 - Cracking of MLG Cylinder Upper Attach Lug

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 British Aerospace BAe 3100 (Jetstream) Series Aeroplanes

AD/JETSTREAM/19 Cracking of MLG Cylinder Upper Attach Lug

Applicability: As listed in the requirement document.

Requirement: Action in accordance with British Aerospace SB 32-JA860812. Compliance: In accordance with the requirement document.

5/87

Background: During fatigue testing of the main landing gear a crack occurred in the cylinder near the upper toggle attachment lug.

Source text

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