Current MD80 ADs - Back to AD Index

1. 08/20/2018    AD 2018-07-04

becomes effective September 10, 2018 and applies to MD80 and MD90 Series Airplanes.

This AD requires changes to the Air Data Heat System to prevent operation of unheated Air Data Sensors in icing conditions.

We have updated AD Status Reports to include this AD.

2. 10/01/2017    AD 2017-17-19

becomes effective October 4, 2017 and applies to MD-81, MD-82, MD-83, MD-87 and MD -88 Series Airplanes.

This AD requires within 700 Flight Cycles or 6 Months after October 4, 2017, whichever occurs first, an inspection for cracking of the Cant Station 1463 (Station 1254 for MD-87 Series) Bulkhead.

We have updated AD Status Reports to include this AD.

3. 01/24/2017    AD 2016-25-06

becomes effective January 25, 2017 and applies to MD80 series airplanes.

This AD requires repetitive inspections for cracking of the Horizontal Stabilizer rear spar lower caps.

We have updated AD Status Reports to include this AD.

4. 04/25/2016    AD 2016-07-28

becomes effective April 26, 2016 and applies to all MD-80 Series Airplanes.

This AD requires an Eddy Current High Frequency inspection for any cracking in the left and right side Center wing Lower Skin in accordance with SB MD80-57A244.

We have updated AD Status Reports to include this AD.

5. 04/20/2016    AD 2016-07-08

becomes effective April 20, 2016 and applies to MD-83 Airplane Serial Number 53192 only.

This AD requires the installation of Fuel Level Float and Pressure Switch In-Line Fuses within 60 months after April 20, 2016.

We have updated AD Status Reports to include this AD.

6. 03/22/2016    AD 2016-03-06

becomes effective March 23, 2016 and supersedes AD 2012-18-05. This AD applies to DC9 / MD-80 / MD-90 series airplanes.

This AD requires within 42 months of March 23, 2016 the installation of an Automatic Fuel Pump Shut-off System for electrically powered fuel pumps installed in the center wing tank or auxiliary fuel tanks.

We have updated AD Status Reports to include this AD

7. 03/02/2015    AD 2015-02-05

becomes effective March 5, 2015 and applies to MD80 and MD 90 series airplanes.

This AD requires revision to the Maintenance or Inspection Program by incorporating Special Compliance Item (SCI) 34-1. Functional Test of the Captain and First Officer’s Altimeter

This Revision will be complied with by Centurion for those operators using the Centurion Maintenance Program.

We have updated AD Status Reports to include this AD.

8. 11/26/2014    AD 2014-21-04

becomes effective December 2, 2014 and applies to MD-80 series airplanes.

This AD requires repetitive inspections for cracks in the areas around the two aft-most barrel nut holes of the left and right upper rear spar caps of the horizontal stabilizer.

The initial inspection is due before the accumulation of 22,000 CSN (or 22,000 cycles after repair or replacement) or 2,768 cycles from December 2, 2014, whichever occurs later.

We have updated AD Status Reports to include this AD.


9. 01/22/2014    AD 2013-25-12

becomes effective January 31, 2014 and applies to certain DC-9 series airplanes as identified in McDonnell Douglas DC-9 Alert SB A53-144R2.

This AD requires modification to the aft pressure bulkhead..

We have updated AD Status Reports to include this AD