Current 727 ADs - Back to AD Index

1. 10/13/2017    AD 2017-19-02

becomes effective October 19, 2017 and applies to B727 Series Airplanes equipped with a Main Cargo Door.

This AD requires an inspection for and repetitive inspections for cracking of certain Cam Support Assemblies of the Main Cargo Door in accordance with SB 727-52A0151.

We have updated AD Status Reports to include this AD.

2. 01/09/2017    AD 2016-19-16

becomes effective January 9, 2017 and applies to B727C, 727-100C and 727-200F Series Airplanes as identified in SB 727-52A0150 Revision 1.

This AD requires repetitive inspections of the Main Cargo Door latching mechanism.

We have updated AD Status Reports to include this AD.

3. 11/26/2014    AD 2014-21-09

becomes effective December 3, 2014 and supersedes AD 2005-14-07. This AD applies to B727 series airplanes as listed in SB 727-57A0135.

This AD requires repetitive inspections of the left and right inboard and outboard foreflap carriage attach fittings as well as functional checks and replacement of the outboard fore flap carriage attach fittings.

The initial inspection and functional check for most operators is due within 200 cycles or 6 months of December 3, 2014, whichever occurs first.

The replacement of the outboard fore flap carriage attach fittings is due within 3,000 cycles or 3 years of December 3, 2014, whichever occurs first.

We have updated AD Status Reports to include this AD.


4. 09/04/2014    AD 2014-16-09

becomes effective September 23, 2014 and applies to the B727, 727C, 727-100, 727-100C, 727-200 and 727-200F series airplanes as identified in SB 727-35A0031.

This AD requires replacement of the low pressure oxygen hoses in the flight compartment with non-conductive low pressure oxygen hoses.

This replacement is due within 36 months after September 23, 2014.

We have updated AD Status Reports to include this AD.


5. 07/16/2014    AD 2014-12-10

becomes effective July 28, 2014 and applies to B 727-100 series airplanes as identified in SB 727-53-0041R6.

This AD requires repetitive inspections cracking in stringers and frames originating at or near stringer-to-frame attachment fastener holes.

We have updated AD Status Reports to include this AD.

6. 04/30/2014    AD 2014-05-14

becomes effective May 1, 2014 and applies to B727, 727C, 727-100, 727-100C, 727-200, and 727-200F series airplanes Line Position 1433 through 1832 identified as Group 2 airplanes in SB 727-53-0149 Revision 4.

This AD requires a one-time inspection and concurrent preventive modification of the main wheel well pressure floor in accordance with SB 727-53-0149 Revision 4.

We have updated AD Status Reports to include this AD.

7. 04/30/2014    AD 2014-04-09

becomes effective May 2, 2014 and applies to B727, 727C, 727-100, 727-100C, 727-200, and 727-200F series airplanes.

This AD requires repetitive inspections of any small repair to the wing rib chord that has been done as specified in SB 727-57-112 or Part III of the accomplishment instructions of SB 727-57-0112.

The initial inspection is due within 3,500 cycles after the small repair was installed or inspected as specified in SB 727-57-0112 or within 18 months after May 2, 2014, whichever occurs latest.

We have updated AD Status Reports to include this AD.

8. 03/17/2014    AD 2014-03-21

becomes effective March 31, 2014 and applies to 727-200 & 727-200F Series Airplanes Line Number 1103 and Subsequent.

This AD requires inspection and modification of the pressure floor of both MLG wheel wells before the accumulation of 60,000 cycles or 24 months after March 31, 2014, whichever occurs later.

We have updated AD Status Reports to include this AD.