Document ID: chunk:federal_register_of_legislation:F2006B10442:body:0:p2
Version: federal_register_of_legislation:F2006B10442
Segment Type: other
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Character Range: 2781–4294

damage of the P1 pitot pipes, in accordance with the service bulletin. If damage is found, replace the damaged flight control cables with new cables in accordance with Chapter 20-10-31 of the Aircraft Maintenance Manual.
 COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

 AD/HS 125/160 (Continued)

               c.    Perform a test of the P1 pitot system to ensure proper function, in accordance with the service bulletin. If the P1 pitot system fails the test, perform the corrective actions specified in Chapter 34-11-00 of the Aircraft Maintenance Manual.

            Note 2: FAA AD 99-25-01 Amdt 39-11444 refers.

            Compliance: For Requirement 1- Within 150 hours time in service from the effective date of this directive.

            For Requirements 2 and 3 - Before further flight.

            This Airworthiness Directive becomes effective on 24 February 2000.

            Background:  The FAA has received reports of P1 pitot pipes chafing against adjacent flight control cables. The actions specified by this directive are intended to prevent a hole in the P1 pitot pipes, which would lead to erroneous input to the instrumentation and warning systems associated with the pilot's instruments.

 Eugene Paul Holzapfel
 Delegate of the Civil Aviation Safety Authority 11 January 2000

 The above AD is notified in the Commonwealth of Australia Gazette on 27 January 2000.