Document ID: chunk:federal_register_of_legislation:F2006B02628:body:0
Version: federal_register_of_legislation:F2006B02628
Segment Type: other
Provision Reference: 
Character Range: 0–1344

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

 Boeing 727 Series Aeroplanes

AD/B727/105
 Amdt 1

 Applicability: All model 727 aircraft. Requirement:  Either:

 Take-Off Warning 6/96
              1. Action in accordance with FAA AD 88-22-09 Amdt 39-6054; or

2.    Where a Take-off Configuration Warning System (TOCWS) Aural Warning Module part number 69-78214-1 is installed on the aeroplane, perform an operational and functional check of the TOCWS in accordance with Boeing Service Letter 727-SL-31-009 dated 31 May 1995.

            Compliance:   For Requirement 1 - This compliance remains unchanged as `Within 200 hours time in service from 9 December 1988 and thereafter at intervals not exceeding 200 hours time in service'.

            For Requirement 2 - Effective 23 May 1996, initially within 500 hours time in service from a check in accordance with Requirement 1 and thereafter at intervals not to exceed 500 hours time in service.

            Background: A significant number of take-off configuration warning systems were discovered to be inoperative during a one-time inspection of all Boeing 727 aircraft. This amendment introduces an alternate method of compliance, with an extension of the repetitive check period.