Document ID: chunk:federal_register_of_legislation:F2006L01100:body:0:p2
Version: federal_register_of_legislation:F2006L01100
Segment Type: other
Provision Reference: 
Character Range: 2826–5289

vision windows with over 12 years time in service, inspect in accordance with paragraph 2.D.4 under the DV Windows Section, page 41 of SB 600 (240D) No. 53-4B, or page 40 of SB No. 640 (340D) of SB No. 53-5B.

                7. For cabin windows with over 12 years time in service, inspect in accordance with paragraph 2.D.(4) under the "Cabin Windows" Section, page 49 of SB 600 (240D) No. 53-4B, or page 49 of SB 640 (340D) No. 53-5B.

                8. For cabin windows twelve years old or older that have been in storage or installed on aircraft which have been in storage, or installed on aircraft operated unpressurised, and which are now to be used in pressurised operation; inspect in accordance with Requirement 7.

             Note 1:  Replacement of the sliding windows P/N 340-3110307-7 or -8 with a new sliding window, P/N 340-3110307-9 or -10, terminates the inspection requirements for the replaced sliding window.

             Note 2:  FAA AD 80-08-03 Amdt 39-3734 refers.
Compliance:     1. Unless already replaced, before further pressurised flight.

                2. Before further flight.

                3. Within 100 hours time in service after 11 May 2006, and thereafter at intervals not to exceed 100 hours time in service.

                4. Before return to pressurised flight after 11 May 2006, unless previously inspected.

                5. Initially inspect within 250 hours time in service after 11 May 2006, unless already accomplished, and thereafter at intervals not to exceed 90 days or 500 hours time in service, whichever occurs first.

                6. Initially inspect within 250 hours time in service after 11 May 2006, unless already accomplished, and thereafter at intervals not to exceed 90 days or 500 hours time in service, whichever occurs first.

                7. Initially inspect within 250 hours time in service after 11 May 2006, unless already accomplished, and thereafter at intervals not to exceed 90 days or 500 hours time in service, whichever occurs first.

                8. Before return to pressurised flight after 11 May 2006, unless previously inspected.
             This Airworthiness Directive becomes effective on 11 May 2006.

Background:  The FAA requires certain actions to prevent possible failure of the pilots' windshield, direct vision windows, sliding windows, and cabin windows.

David Villiers
Delegate of the Civil Aviation Safety Authority

29 March 2006