Document ID: chunk:federal_register_of_legislation:F2006B02747:body:0
Version: federal_register_of_legislation:F2006B02747
Segment Type: other
Provision Reference: 
Character Range: 0–1012

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

 Boeing 727 Series Aeroplanes

 AD/B727/46
 Amdt 1

      Horizontal Stabilizer Rear Spar Centre Section Fitting - Inspection

 3/85

 Applicability: All model Boeing 727 with S/Nos listed in the requirement documents. Document:  Boeing SB No. 727-55-62.
            Note: FAA AD 75-09-04 R1 Amendment 39-2174 as amended by Amendment 39- 4926 refers.

            Compliance: Within 750 hours time in service after 31 March 1985, unless accomplished within the last 2250 hours time in service, and thereafter in accordance with the requirement document.

            Background: Further reports have shown that cracking due to stress corrosion in the 7079-T6 fittings may be more extensive than originally covered by Boeing SB 727-55-34. This directive has been amended to include the latest requirements of Boeing SB 727-55-62, which supersedes SB 727-55-34.