09/12/2011 New! AD 2011-17-11
becomes effective September 26, 2011 and applies to MD-81, MD-82, MD-83, MD-87 and MD-88 series airplanes This AD requires repetitive inspections of the left and right wing rear spar caps at Sta Xrs = 164.000 before the accumulation of 30,000 total flight cycles or within 3,360 flight cycles after September 26, 2011, whichever occurs later.
We have updated AD Status Reports to include this AD......

08/03/2011  AD 2011-14-03
becomes effective August 10, 2011 and applies to MD-81, MD-82, MD-83, MD-87 and MD-88 series airplanes This AD requires repetitive inspections of the left and right upper center skin panels of the Horizontal Stabilizer before the accumulation of 20,000 total flight cycles or within 4,379 flight cycles after August 10, 2011, whichever occurs later.
We have updated AD Status Reports to include this AD......

08/03/2011  AD 2011-15-01
becomes effective August 19, 2011 and applies to MD-81, MD-82, MD-83, MD-87 and MD-88 series airplanes This AD requires a one-time inspection of the leading edge structure of the Vertical Stabilizer at the splice at Station Zfs=52.267 along with repetitive inspections of the left and right Vertical Stabilizer front spar cap and repetitive inspections for indications of loose and missing fasteners. The initial inspection is due within 4,500 flight cycles after August 19, 2011.
We have updated AD Status Reports to include this AD......

04/05/2011  AD 2011-07-04
becomes effective May 6, 2011 and applies to DC-9 series airplanes.This AD requires the installation of new in-line fuses for the fuel level float switches and fuel pressure switches and a change to the wiring.
We have updated AD Status Reports to include this AD.....

01/24/2011  AD 2011-01-16
becomes effective February 16, 2011 and applies to MD-80 series airplanes. This AD requires installation of fuel level float and pressure switch in-line fuses within 60 months after February 16, 2011. We have updated AD Status Reports to include this AD.....

01/05/2011  AD 2010-25-04
becomes effective January 11, 2011 and applies to DC-9 and MD-80 airplanes. This AD requires modification of the center wing and auxiliary fuel tanks boost pumps within 60 months after January 11, 2011. We have updated AD Status Reports to include this AD.....