Document ID: chunk:federal_register_of_legislation:F2011L01845:body:0:p1
Version: federal_register_of_legislation:F2011L01845
Segment Type: other
Provision Reference: 
Character Range: 0–4898

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/B737/198 Amdt 1 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 737 Series Aeroplanes
AD/B737/198 Amdt 2  Centre Tank Fuel Pumps  18/2011

Applicability:  All Model 737-600, -700, -700C, -800 and -900 series aeroplanes.
Requirement:       1. Model 737-600, -700, -700C, -800 and -900 series aeroplanes with a line number 1234 and below:
                     a. If not previously accomplished in accordance with the original issue of this Directive - Remove the Aircraft Flight Manual (AFM) revision required by AD/B737/190 Amdt 1.
                     b. If not previously accomplished in accordance with the original issue of this Directive - Revise the Limitations Section of the Aircraft Flight Manual (AFM) by incorporating the procedures included at Annex A to this Amendment (this may be accomplished by inserting a copy of Annex A into the AFM).
                     The limitations contained in this Amendment supersede any conflicting basic AFM limitations.

                     c. If not previously accomplished in accordance with the original issue of this Directive - Install a placard adjacent to each pilot's primary flight display (PFD) that reads as follows either:
                        "AD/B737/198 fuel usage restrictions required" or

                        "AD 2002-19-52 fuel usage restrictions required"
                   2. For all Model 737-600, -700, -700C, -800 and -900 series aeroplanes:
                     a. Fuel pumps with the following part numbers may not be installed on any aeroplane as a replacement part, unless the pump has been inspected to ensure that the wire bundle is properly routed in the pump since the most recent assembly of the end cap and motor-impeller housing (whether during manufacture, after maintenance or inspection, or after overhaul) in accordance with Boeing Alert Service Bulletin (ASB) 737-28A1197 dated 23 September 2002 or Crane Hydro-Aire Service Bulletin (SB) Crane Hydro-Aire Motor-Impeller-28-01, including Appendix A, dated
                     17 September 2002:
                     Hydro-Aire Part Number                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                              Boeing Part Number

                     60-989100-4                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                         60B89004-14
                     60-755100-4                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                         60B92404-8
                     b. Fuel pump motor-impeller assembly having any part number may not be installed on any aeroplane in any pump position as a replacement part, unless the assembly has been inspected since the most recent assembly of the end cap motor-impeller housing (whether during manufacture, after maintenance or inspection, or after overhaul) using X-ray