Commonwealth legislation

AD/LEARJET 35/1 - Primary Control System Stop Bolts - Inspection and Replacement

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

2/10 complexity

This directive mandates owners/operators of specified Learjet 35/36 aeroplanes to inspect and, if needed, replace primary control system stop bolts per Gates Learjet Service Bulletin 35/36-27-3.

Issued as a mandatory airworthiness requirement, it applies to the listed fleet, must be done within 300 flight-hours after 30 April 1976, and imposes compliance costs and scheduling burdens on operators.

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/LEARJET 35/1 - Primary Control System Stop Bolts - Inspection and Replacement.

AD/LEARJET 35/1 - Primary Control System Stop Bolts - Inspection and Replacement

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 Gates Learjet 35 and 36 Series Aeroplanes

AD/LEARJET 35/1 Primary Control System Stop Bolts - Inspection and Replacement

Applicability: All model 35 with S/Nos. 35-001 to 35-039.

All model 36 with S/Nos. 36-001 to 36-016.

Document: Gates Learjet SB 35/36-27-3.

Compliance: Within 300 hours time in service after 30 April 1976.

4/76

Source text

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