Document ID: chunk:federal_register_of_legislation:F2006B05920:body:0
Version: federal_register_of_legislation:F2006B05920
Segment Type: other
Provision Reference: 
Character Range: 0–516

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

 Piper PA-34 (Seneca) Series Aeroplanes

AD/PA-34/5 Stabilator Tip Balance Weight - Inspection 9/72

 Applicability: All models with S/Nos. 34-E4 and 34-7250001 to 34-7250335. Document:  Piper SB No. 367.
 Compliance: 1. Initial Inspection - prior to further flight after 12 September 1972.

            2. Hardware Replacement - as detailed in requirement document.