AD/B727/100 Amdt 4 - Elevator Rear Spar (Cth)

AIRWORTHINESS DIRECTIVE On the effective date specified below, and for the reasons set out in the background section, the CASA delegate whose signature appears below revokes Airworthiness Directive (AD) AD/B727/100 Amdt 3 and issues the following AD under subregulation 39.001(1) of CASR 1998. The AD requires that the action set out in the requirement section (being action that the delegate considers necessary to correct the unsafe condition) be taken in relation to the aircraft or aeronautical product mentioned in the applicability section: (a) in the circumstances mentioned in the requirement section; and (b) in accordance with the instructions set out in the requirement section; and (c) at the time mentioned in the compliance section.

Boeing 727 Series Aeroplanes AD/B727/100 Amdt 4 Elevator Rear Spar 11/2008 DM

Applicability: Boeing model 727 series aircraft, line numbers 1 through 1832. Requirement: Action in accordance with the technical requirements of FAA AD 2008-17-14 Amdt 39-15652.

Note: Boeing Service Bulletin 727-55-0089Revision 1, or later FAA approved revision, refers. Compliance: As specified in the requirement document. This Amendment becomes effective on 2 October 2008. Background: Several cases of fatigue cracking were reported. The cracking was believed to be initiated by interference between the spar flange bend radii and the sharp edges on the shear plates mounted between the spar and the elevator tab hinges.

Amendment 1 introduced SB 727-55-0087, which similarly covers the early design elevator rear spar as a result of recent Australian and overseas reports of cracking.

Amendment 2 clarified the compliance for operators of certain aircraft.

Amendment 3 was issued in response to a new FAA AD which adds new inspections to detect cracks and loose brackets of the elevator rear spar and a new terminating modification for the inspections. Reports were received of cracking in the spar radii at the tab hinge location of the elevator rear spar.