02/09/2012 New! AD 2012-01-09
becomes effective February 29, 2012 and and applies to Model 757-200, -200CB and -300 series airplanes as identified in SB 757-25-0298R1. This AD requires modification of the door latch fittings and witness mark placards of the left and right off-wing escape slide systems within 60 months after February 29, 2012.

We have updated AD Status Reports to include this AD.....

01/17/2012   AD 2011-25-11
becomes effective January 17, 2012 and supersedes AD 2008-09-07. This AD requires installation of EICAS OPS Version 7 within 90 days from January 17, 2012 and concurrent installation of EICAS OPS Version 5. For any airplane verified by the operator to have EICAS computer P/N S242N701-1001 and only EICAS OPS Versions other than Version 6 software that are FAA approved for that airplane, the actions specified in Paragraphs (i) and (j) of this AD are not required (See Paragraph (k).

We have updated AD Status Reports to include this AD.....

02/25/2011  AD 2011-05-04
becomes effective March 31, 2011 and applies to B757-200, -200CB, -200PF and -300 series airplanes. This AD supersedes AD 2008-23-19 and requires the sealing of fasteners in the main and center fuel tanks and an inspection and modification of the wire bundle support installation within 60 months after December 30, 2008. We have updated AD Status Reports to include this AD.....

01/24/2011  AD 2011-01-15
becomes effective January 25, 2011 and applies to B757-200, -200CB and -300 series airplanes. This AD requires repetitive inspections of the fuselage crown skin panel along the chem.-milled step at stringer S-4L and stringer S-4R, BS 297 through BS 439. The initial inspection is due prior to the accumulation of 15,000 total flight cycles or within 30 days after January 25, 2011 whichever occurs later. Repetitive inspections are based on type inspection accomplished. We have updated AD Status Reports to include this AD.....

01/24/2011  AD 2011-02-03
becomes effective February 16, 2011 and applies to B757-200, -200PF, -200CB and -300 series airplanes. This AD requires repetitive inspections of aluminum nose wheel spin brakes. The initial inspection is due prior to the accumulation of 6,000 cycles on the springs or within 300 cycles of February 16, 2011. We have updated AD Status Reports to include this AD.....

01/05/2011  AD 2010-23-03
became effective November 22, 2010 and applies to B757 and B767 airplanes. This AD requires repetitive tests of the Fuel Quantity Indication System Low Fuel Quantity Indication within 100 flight hours after November 22, 2010 and repeated at intervals not to exceed 100 flight hours....

01/05/2011  AD 2010-23-13
became effective December 14, 2010 and applies to B757 airplanes. This AD requires modification to the fixed leading edge panel assemblies immediately outboard of the nacelles at L.E. Slats number 4 and number 7 within 60 months after December 14, 2010. We have updated AD Status Reports to include this AD......