Commonwealth legislation

AD/PL 12/19 - Stub Wing Internal Structure - Inspection and Re-Protection

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

3/10 complexity

The AD requires owners/operators of all Transavia PL‑12 series aeroplanes to inspect the internal steel stub‑wing structure at the time tied to each aircraft’s three‑year service milestone (by the next major inspection) and to carry out any re‑protection work mandated by Transavia Service Bulletin No. 30. Issued after corrosion was observed, the directive makes SB No. 30 mandatory, shifting inspection, repair costs and downtime onto operators and increasing demand for qualified maintenance providers.

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AD/PL 12/19 - Stub Wing Internal Structure - Inspection and Re-Protection

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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 Transavia PL 12 Series Aeroplanes

AD/PL 12/19 Stub Wing Internal Structure - Inspection

and Re-Protection

7/80

Applicability: All PL-12 Series. Document: Transavia SB No. 30.

Compliance: 1. For aircraft which have achieved 3 years time in service since manufacture, initially inspect not later than the next major inspection and thereafter in accordance with SB No. 30.

For other aircraft, initially inspect not later than next major inspection after achieving 3 years time in service after manufacture and thereafter in accordance with SB No. 30.

Background: Corrosion of the interior structure of the steel stub wing has been observed in some aircraft.

Source text

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