Commonwealth legislation

AD/PROCTOR/2(Re-Issue) - Rear Fuselage Drain Holes - Modification

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legislative instrument

Plain English Summary

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This AD mandates an immediate modification of the rear fuselage drain‑hole arrangement on Percival Proctor Mk I, II and III aircraft when operated other than Class 1. Operators/owners must, forthwith, complete one of three prescribed compliance options (two Percival mod numbers or the referenced documents), fund and arrange the work, and may choose the method that best fits their technical and operational constraints. Mandatory timing makes prompt scheduling and certified maintenance capability essential.

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AD/PROCTOR/2(Re-Issue) - Rear Fuselage Drain Holes - Modification

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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 Percival Proctor Series Aeroplanes

AD/PROCTOR/2

(Re-Issue)

Rear Fuselage Drain Holes - Modification 6/50

Applicability: All Mk. I, Mk. II and Mk. III as indicated, operated in other than Class 1. Requirement: 1. Percival Mod. Nos. 210 (Mk.I) and 676 (Mk’s II and III), or

DCA/PROCTOR/2, or 3. A.N.O. 105.1.26.0.2.2.

Compliance: Forthwith.

Source text

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