Document ID: chunk:federal_register_of_legislation:F2006B05609:body:0
Version: federal_register_of_legislation:F2006B05609
Segment Type: other
Provision Reference: 
Character Range: 0–1273

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

 Piper PA-28 Series Aeroplanes

AD/PA-28/52 Nose Landing Gear - Inspection and Modification 6/75

 Applicability: All models with nose-wheel installation to STC SA28IAL.

                Requirement: 1. (a) Visually inspect the nosewheel fork (Tibbetts Herre Airmotive P/N PA-32-1) for bends or distortion.

                (b) Visually inspect the nosewheel fork (Tibbetts Herre Airmotive P/N PA-32-1) for cracks using an approved dye penetrant technique.

             2.    Replace the following items:

                (a)     Nosewheel Fork (Tibbetts Herre Airmotive P/N PA-32-1) with Fork P/N HPA-32-1.

(b)     Cap-Piper P/N 20825-00 with Tibbetts Herre P/N PA-32-5.

(c)     Axle Rod - Tibbetts Herre P/N PA-32-4 with Tibbetts Herre P/N PA-32-6.

            Compliance: For para. 1 - Within 25 hours time in service after 6 December 1974 and thereafter at intervals not exceeding 25 hours time in service until modified.

            For para. 2 - Within 100 hours time in service after 6 December 1974, unless already accomplished.

            Note: Applicable aircraft will have an 8.00-6 nosewheel tyre fitted.