08/03/2011 New! AD 2011-15-03
becomes effective August 19, 2011. and applies to all the Boeing B747-100, -100B, 100B SUD, -200B, -200C, -200F, -300, -400, -400D, -400F, -747SR and 747SP series airplanes. This AD supersedes AD 97-26-07 and requires repetitive inspections to detect damage of the sleeving and wire bundles of the forward and aft boost pumps of the number 1 and 4 main fuel tanks and of the wire bundles of the auxiliary tank jettison pumps (if installed).
We have updated AD Status Reports to include this AD.....

08/03/2011 New! AD 2011-16-02
becomes effective August 30, 2011. and applies to Boeing Model B747 and Model 767 airplanes equipped with General Electric Model CF6-80C2 or CF6-80A series engines. This AD requires a revision to the Limitations Section of the Airplane Flight Manual within 14 days after August 30, 2011.
We have updated AD Status Reports to include this AD.....

04/05/2011  AD 2011-05-11
becomes effective April 14, 2011 and supersedes AD 2007-19-19. This AD requires repetitive inspections of the forward engine mount hanger fittings and bulkheads and if applicable inspection and replacement of Hi-Lok Group B fasteners.
We have updated AD Status Reports to include this AD and supersede AD 2007-19-19....

04/05/2011  AD 2011-06-03
becomes effective April 26, 2011 and applies to B747 airplanes. This AD requires rework of the electrical bond of Motor Operated Valve Actuators to prevent electrical current from flowing through the valve actuator into a fuel tank.
We have updated AD Status Reports to include this AD....

01/05/2011  AD 2010-24-13
becomes effective January 20, 2011 and applies to B747 aircraft as identified in SB 747-28A2288R1. Paragraph (g) of this AD requires a modification to the Fuel Pressure Indication System within 36 months after January 20, 2011. Paragraph (h) requires that concurrently the Maintenance Program be revised by incorporating AWL 28-AWL-22 of Section D of Boeing Document D6-13747-CMR. For those operators using the Centurion B747 Maintenance Program this requirement was previously complied with (AD 2008-10-07). Paragraph (i) requires that concurrently Section 1 of the AFM be revised....

01/05/2011 New! AD 2010-26-07
becomes effective February 1, 2011 and applies to B747 aircraft. Paragraph (g) of this AD requires repetitive inspections of the Nose Wheel Well Aft Corner Skin Panel within 1,500 cycles after February 1, 2011 for those aircraft that have not been modified IAW SB 747-53A2305 or within 1,000 cycles after February 1, 2011 for those aircraft that have been modified IAW SB 747-53A2305. Repetitive inspections are not to exceed 1,500 cycles. Paragraph (r) requires an inspection BS 400 Bulkhead Outer Chord prior to the accumulation of 20,000 total flight cycles We have updated AD Status Reports to include this AD.....

10/11/2010  AD 2009-19-06
becomes effective October 12, 2010 and applies to B747 aircraft as identified in SB 747-52-2293. This AD requires rework of the flight deck door within 30 days after October 12, 2010. This AD does not apply to our B747 operators by Service Bulletin Effectivity. We have updated AD Status Reports to include this AD....