Commonwealth legislation

AD/CESSNA 400/91 - Elevator Bellcrank Bracket Integrity

RepealedCTH

This Act has been repealed and is no longer in force. It is retained for historical reference.

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

2/10 complexity

This mandatory safety order requires owners/operators of Cessna Model 441 aircraft (S/N 0001–0355) to inspect and repair the elevator bellcrank bracket per Cessna Service Bulletin CQB86‑13. It addresses rivet failures that can sever pilot control of pitch, posing a crash risk. Work must be done within 100 flight hours after 31 Dec 1986 or at the next scheduled maintenance, whichever is later.

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/CESSNA 400/91 - Elevator Bellcrank Bracket Integrity.

AD/CESSNA 400/91 - Elevator Bellcrank Bracket Integrity

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 Cessna 400 Series Aeroplanes

AD/CESSNA 400/91 Elevator Bellcrank Bracket Integrity 12/86

Applicability: Model 441 S/No.s 0001 to 0355.

Requirement: Action in accordance with Cessna Service Bulletin CQB86-13.

Compliance: Within 100 hours time in service after 31 December 1986 or at the next scheduled inspection for Maintenance Release after 31 December 1986 whichever is the later.

Background: The manufacturer advises that there have been instances of rivet failure.

Source text

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