Commonwealth legislation

AD/CASA/19 - False Spar, Flap Housing Area

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

3/10 complexity

This AD mandates all CASA 212 operators inspect the flap‑housing/false‑spar area for cracking using CASA COM 212‑224, initially within 1,200 hours after 15 Aug 1996 and then every 1,200 hours. Any cracking must be repaired under a CAR 35‑approved scheme. It responds to detected cracking and imposes recurring inspection costs, potential downtime for approved repairs, and administrative dealings with CASA for repair approval.

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AD/CASA/19 - False Spar, Flap Housing Area

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

SCHEDULE OF AIRWORTHINESS DIRECTIVES

View image in the official source Casa 212 Series Aeroplanes

AD/CASA/19 False Spar, Flap Housing Area 9/96

Applicability: All models.

Requirement: 1. Action in accordance with CASA document COM 212-224 dated 28 November 1990.

Repair any cracking in accordance with a scheme approved pursuant to CAR 35.

Note: Spanish DGAC AD 02/96 refers.

Compliance: Within 1200 hours time in service after 15 August 1996. Where no cracking is found repeat inspection at intervals not exceeding 1200 hours time in service.

Background: Cracking has been detected in the area defined in the Requirement Document.

Source text

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