Document ID: chunk:federal_register_of_legislation:F2014L01683:body:0:p1
Version: federal_register_of_legislation:F2014L01683
Segment Type: other
Provision Reference: 
Character Range: 0–2879

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 repeals Airworthiness Directive (AD) AD/B737/224 Amdt 3 and issues the following AD under subregulation 39.001 (1) of CASR 1998 and subsection 33 (3) of the Acts Interpretation Act 1901. The AD requires that the action set out in the requirement section (being action that the delegate considers necessary to correct an 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 737 Series Aeroplanes
AD/B737/224 Amdt 4  Horizontal Stabiliser Attachment  25/2014
                    Pins and Bolts - Inspection

Applicability:  This AD applies to all Boeing model 737-600, 737-700, 737-700C, 737-800 and
                737-900 series aircraft.
Requirement:    Subject to the exceptions mentioned below, action must be taken in accordance with the technical requirements of AD 2004-05-19 Amdt 39-13514, as corrected in the Federal Register of 13 April 2004, (the FAA AD) issued by the Federal Aviation Administration of the United States of America (FAA).
                Note:  Boeing Service Bulletin (SB) 737-55-1086 Original Issue, dated
                11 December 2003, relates to the FAA AD.
                Compliance with Boeing SB 737-55-1086 Revision 1, dated 16 December 2004, or a later revision of that SB approved by the FAA, is taken to be compliance with Boeing SB 737-55-1086 Original Issue as required by paragraphs (a), (b), (c), (d) and (e) of the FAA AD in relation to the inspection, repair or replacement of the rear spar attach pins and front spar attach bolts.
                Compliance with Boeing SB 737-55-1093, Original Issue, dated 9 April 2012, is taken to be compliance with paragraphs (a), (b), (c), (d) and (e) of the FAA AD in relation to the inspection, repair or replacement of the rear spar attach pins.
                For an aircraft with a line number from 1725 to 3534 inclusive that is fitted with front spar attach bolts part number (P/N) 180A1611-3 or 180A1611-5, the inspection, repair or replacement of the front spar attach bolts required by paragraphs (a), (b), (c), (d) and (e) of the FAA AD is not required.
                For an aircraft with a line number of 3535 or higher, the inspection, repair or replacement required by paragraphs (a), (b), (c), (d) and (e) of the FAA AD is not required.
Compliance:     The required action must be taken at the time specified for the action in the FAA AD, as if it had an effective date of 13 May 2004.
                The effective date of this AD