Current 340 ADs - Back to AD Index

1. 04/04/2018    AD 2016-0064

becomes effective April 6, 2018 and applies to A330 and A340 Series Airplanes. This AD Supersedes EASA AD 2016-0107.

This AD requires an inspection for, Re-Identification of and replacement of affected Hydraulic Reservoir Pressure Relieve Valves.

We have updated AD Status Reports to include this AD

2. 04/04/2018    AD 2016-0152R1

becomes effective April 9, 2018 and applies to A340 Series Airplanes.

This AD requires the Implementation of Damage Tolerant Airworthiness Limitation Items ALS Part 2

We have updated AD Status Reports to include this AD.

3. 11/28/2017    AD 2017-0228

becomes effective December 5, 2017 and applies to A330 and A340 Series Airplanes.

This AD requires incorporation of Airworthiness Limitations Section (ALS) Part 4 Revision 05 into the Aircraft Maintenance Program within 12 months after December 5, 2017..

We have updated AD Status Reports to include this AD.

4. 11/13/2017    AD 2017-0224

becomes effective November 17, 2017 and applies to A330 and A340 Series Airplanes.

This AD requires inspection of certain fuel pumps for erosion. This AD also requires an update of the applicable MMEL, and the reporting of inspection results to Airbus.

We have updated AD Status Reports to include this AD

5. 10/13/2017    AD 2017-0196

becomes effective October 19, 2017 and applies to A340 Series Airplanes.

This AD requires within 12 months after the effective date of this AD, an update to the software of the TPA-100B processor P/N 940-0351-001, or replacement of the TPA-100B processor P/N 940-0351-001 with a TPA-100B processor P/N 940-0351-005.

We have updated AD Status Reports to include this AD

6. 10/06/2017    AD 2017-0185

becomes effective October 6, 2017 and applies to A340-330 & 340 Series Airplanes.

This AD requires identification of the Part Number & Serial Number of each Main Fitting, Bogie Beam and Sliding Piston of the Main Landing Gear, Center Landing Gear and Nose Landing Gear installed on the aircraft and to amend the life limits as applicable.

We have updated AD Status Reports to include this AD

7. 03/09/2017    AD 2017-0044

becomes effective March 23, 2017 and applies to A330 and A340 series airplanes.

This AD requires repetitive inspections of the Trimmable Horizontal Stabilizer Actuator (THSA) Upper Attachments and No-Back Housing.

We have updated AD Status Reports to include this AD.

8. 02/23/2017    AD 2017-0021

becomes effective February 22, 2017 and applies to certain A330 and A340 series Airplanes.

This AD requires an inspection for and replacement of certain Cabin and Cargo Compartments Parts.

We have updated AD Status Reports to include this AD.

9. 02/06/2017    AD 2016-25-31

becomes effective February 7, 2017 and applies to A340 series airplanes.

This AD requires modification of the Cockpit Door and Cockpit Door Cover Plate within 24 months after February 7, 2017.

We have updated AD Status Reports to include this AD.

10. 12/05/2016    AD 2016-0231

becomes effective Dec. 6, 2016 and supersedes AD 2016-0082. This AD applies to A330 & A340 Series Airplanes.

This AD requires a one-time inspection to identify potentially affected inboard Flap parts.

We have updated AD Status Reports to include this AD.

11. 11/21/2016    AD 2016-20-10

becomes effective November 22, 2016 and applies to A-330 and A-340 Series Airplanes.

This AD requires identification and replacement of certain fuel pumps.

We have updated AD Status Reports to include this AD

12. 11/16/2016    AD 2016-0208

becomes effective November 16, 2016.

This AD requires Modification/ Reinforcement of Structural areas which are susceptible to Widespread Fatigue Damage (WFD).

We have updated AD Status Reports to include this AD

13. 11/16/2016    AD 2016-0219

becomes effective November 17, 2016 and applies to A340-541, A340-542 and A340-642 Airplanes

This AD requires replacement of the Hydraulic Control Unit P/N D24067000-3 with an improved HCU P/N D24067000-6 within 48 months after November 17, 2016.

We have updated AD Status Reports to include this AD

14. 08/09/2016    EASA AD 2016-01

becomes effective August 10, 2016 and supersedes several previous ADs relating to Airworthiness Limitations.

This AD requires a revision to the Aircraft Maintenance Program and the implementation of Damage Tolerant Airworthiness Limitation Items as specified in Airbus A340 ALS Part 2 Revision 02.

We have updated AD Status Reports to include this AD.

15. 06/29/2016    AD 2016-10-11


becomes effective June 30, 2016 and supersedes AD 2015-03-06. This AD applies to Airbus 330 and 340 Series Airplanes.


This AD requires repetitive inspections for cracking of the left-hand and the right-hand wing MLG Rib 6 aft bearing lugs (forward and aft) at intervals not to exceed 100 flight cycles or 500 flight hours, whichever occurs first.


We have updated AD Status Reports to include this AD.


16. 06/29/2016    AD 2016-12-15

becomes effective July 6, 2016 and supersedes AD 2016-07-30. This AD applies to Airbus 330 and 340 Series Airplanes.

This AD requires replacement and/or repetitive tests of certain AOA sensors.

We have updated AD Status Reports to include this AD

17. 06/29/2016    AD 2016-11-01

becomes effective July 12, 2016 and applies to Airbus 330 and 340 Series Airplanes MSN 0715 through MSN 1507 inclusive, and MSN 1509.

This AD requires modification of the cable loom support bracket in the pylons within 18 months after July 22, 2016.

We have updated AD Status Reports to include this AD.

18. 06/29/2016    AD 2016-11-19

becomes effective July 22, 2016 and applies to Airbus 330 and 340 Series Airplane.

This AD requires a one-time torque check of the forward and aft engine mount bolts on each affected engine.

We have updated AD Status Reports to include this AD

19. 06/23/2016    AD 2016-10-08

becomes effective June 24, 2016.

This AD requires repetitive replacement the Trimmable Horizontal Stabilizer Actuator at 3500 Flight Cycles intervals.

We have updated AD Status Reports to include this AD

20. 06/20/2016    AD 2016-01-07

becomes effective June 21, 2016.

This AD requires repetitive inspections of the Hydraulic Reservoir fluid level of each hydraulic circuit at 1600 flight hour intervals.

We have updated AD Status Reports to include this AD

21. 05/31/2016    AD 2016-08-14

becomes effective May 31, 2016 and replaces AD 2014-03-14. This AD applies to A340 Series Airplanes.

This AD requires Maintenance Light Removal, Insulation Muff Installation, Drain Mast and Replacement of Certain Insulation Sleeves.

We have updated AD Status Reports to include this AD.

22. 05/17/2016    AD 2016-07-30

becomes effective May 18, 2016 and applies to A330 & A340 Series Airplanes.

This AD requires replacement of certain AOA Sensors and repetitive inspections of certain other AOA Sensors.

We have updated AD Status Reports to include this AD

23. 05/09/2016    EASA AD 2016-00

becomes effective May 11, 2016 and applies to A330 & A340 Series Airplanes.

This AD requires a one-time inspection to identify potentially affected inboard Flap parts

We have updated AD Status Reports to include this AD.

24. 05/02/2016    AD 2016-06-12

becomes effective May 3, 2016 and applies to A340 Series Airplanes.

This AD requires modification of the Potable Water Service Panel access door within 36 months after May 3, 2016.

We have updated AD Status Reports to include this AD.

25. 03/03/2016    AD 2016-04-01

becomes effective March 4, 2016 and supersedes AD 2015-26-02. This AD applies to Airbus A330 A340 Series Airplanes.

This AD requires Identification and modification of certain Ram Air Turbine (RAT) components within 36 months after March 4, 2016.

We have updated AD Status Reports to include this AD.

26. 12/30/2015    AD 2015-24-01

becomes effective January 4, 2016 and applies to Airbus A330 A340 Series Airplanes.

This AD requires a review of maintenance records of the rudder to determine if any composite side shell panel repair has been accomplished on the rudder since first installation on an airplane.

This AD also requires related investigative actions, corrective actions and repetitive inspections.

We have updated AD Status Reports to include this AD.

27. 03/24/2015    AD 2015-03-06

becomes effective March 25, 2015 and replaces AD 2007-22-10.

This AD requires repetitive inspections of the left and right Wing MLG Rib 6 Aft Bearing Lug, forward and aft.

The threshold is within 42 months since the airplanes first flight or since the last MLG support rib replacement, as applicable; or within 4 months after March 25, 2015, whichever occurs later.

Repetitive intervals are not to exceed 500 Hours or 100 Cycles, whichever occurs first.

We have updated AD Status Reports to include this AD.


28. 09/04/2014    AD 2014-15-09

becomes effective September 5, 2014 and applies to Airbus Model A330 and A340 series airplanes

This AD requires repetitive operational tests of the hydraulic locking function on each Spoiler Servo-Control (SSC).

The initial test is due within 24 months of September 5, 2014 and is to be repeated thereafter at intervals not to exceed 48 months.

We have updated AD Status Reports to include this AD.

29. 09/04/2014    AD 2014-16-22

becomes effective September 25, 2014 and applies to Airbus Model A330 and A340 series airplanes

This AD requires repetitive replacement of the Cabin Pressure Control System (CPCS) Safety Valves.

These valves are to be replaced at intervals not to exceed 50,000 hours or 12 Years accumulated on the CPCS Safety Valves, whichever occurs first.

We have updated AD Status Reports to include this AD.