Document ID: chunk:federal_register_of_legislation:F2006B02923:body:0:p1
Version: federal_register_of_legislation:F2006B02923
Segment Type: other
Provision Reference: 
Character Range: 20–3103

AIRWORTHINESS DIRECTIVE
 For the reasons set out in the background section, the CASA delegate whose signature appears below issues the following Airworthiness Directive (AD) under subregulation 39.1 (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 737 Series Aeroplanes

AD/B737/227 Electrical Bonding 8/2004

            Applicability: Model 737-100, -200, -200C, -300, -400 and -500 series aeroplanes as listed in Boeing Alert Service Bulletin (ASB) 737-29A1096 Revision 1 dated 31 July 2003.

              Requirement: 1. Prepare the electrical bonding faying surfaces for the tubing penetrations of the hydraulic heat exchanger on the forward and aft surfaces of the rear spars of the fuel tanks of the left and right wings, together with carrying out a one-time measurement of the electrical bonding resistances between the penetration fittings of the hydraulic heat exchanger and the rear spars; and between the heat exchanger tube and the lower wing stringer surfaces, per the Accomplishment Instructions of ASB 737-29A1096 Revision 1.

2.         If the bonding resistance is incorrect, repeat the preparation of the electrical bonding faying surface for the tubing penetrations of the hydraulic heat exchanger on the forward and aft surfaces of the rear spar of the fuel tanks of the left and right wings as necessary to achieve a bonding resistance below the threshold specified in the Accomplishment Instructions of ASB 737-29A1096 Revision 1.

3.         Apply fillet sealant and protective finishes around the penetration fittings of the hydraulic heat exchanger in accordance with the Accomplishment Instructions of ASB 737-29A1096 Revision 1 (Figure 8 refers).

4.         Service and pressurize the hydraulic systems and examine for signs of hydraulic fluid leakage. Service the fuel tank and examine for signs of fuel leakage. All these actions are to be accomplished in accordance with ASB 737-29A1096 Revision 1.

5.         Repair any leaks found, during the Requirement 4 examination, in accordance with ASB 737-29A1096 Revision 1.

            Actions accomplished before the effective date of this Directive in accordance with Boeing ASB 737-29A1096, dated 7 June 2001, are considered acceptable for compliance with the corresponding action specified in this Directive.

            Note: FAA AD 2004-10-06 Amdt 39-13636 refers.

 Compliance: For Requirement 1 - Within 60 months after the effective date of this Directive.

 Boeing 737 Series Aeroplanes

 AD/B737/227 (continued)

            For Requirement 2 - Before further flight after the Requirement 1 bonding resistance check.

            For Requirement 3 - Before