Document ID: chunk:federal_register_of_legislation:F2008L01254:body:0:p3
Version: federal_register_of_legislation:F2008L01254
Segment Type: other
Provision Reference: 
Character Range: 6069–14653

this Directive, carry out all applicable operational tests in accordance with the applicable ASB as listed in Table 1.
                            Note 4:  The Boeing ASBs listed in Table 1 refer to the Boeing component service bulletins specified in Table 3 of this Directive as additional sources of service information for replacing the switch or switch master module at critical locations, for doing operational tests after the replacement, and for identifying new panel part numbers.
                            Table 3
                            Boeing Component Service Bulletin                                                                                                                                                                                                                                                                                                                      Date                     Aeroplane Model/Series                                  Critical Location
233N3209-24-03, Revision 1  25 September 2003                                                                                                                                                                                                                                                                                                                                      767-200, -300 and -300F  Electrical Systems Panel
233N3211-24-02, Revision 1  25 September 2003                                                                                                                                                                                                                                                                                                                                      767                      Battery/Standby Power Panel
233N3216-22-01, Revision 1  25 September 2003                                                                                                                                                                                                                                                                                                                                      767                      Yaw Damper Panel Assembly
233N6203-26-10, Revision 1  25 September 2003                                                                                                                                                                                                                                                                                                                                      767-200, -300 and -300F  Auxiliary Power Unit/Cargo Fire Control Panel Assembly
233T3210-33-01, Revision 1  25 September 2003                                                                                                                                                                                                                                                                                                                                      767                      Emergency Lights Panel

                            233T3215-24-01, including Appendix A                                                                                                                                                                                                                                                                                                                                                                         19 December 2001         767-400ER                                Electrical Control Module Assembly
233T3235-28-05, Revision 1  25 September 2003                                                                                                                                                                                                                                                                                                                                                                                            767-200, -300 and -300F  Fuel Management Panel Assembly
233T3236-21-05, Revision 1  25 September 2003                                                                                                                                                                                                                                                                                                                                                                                            767                      Temperature Control Panel
                            233T3237-36-04, Revision 1                                                                                                                                                                                                                                                                                                                                                                                   25 September 2003        767                                      Bleed Air Control Panel
233T3241-30-03, Revision 1  25 September 2003                                                                                                                                                                                                                                                                                                                                                                                            767-200, -300 and -300F  Wing and Engine Anti-ice Control Panel
233T3242-73-02, Revision 1  25 September 2003                                                                                                                                                                                                                                                                                                                                                                                            767-200, -300 and -300F  Electronic Engine Control Panel
233T3244-74-03, Revision 1  25 September 2003                                                                                                                                                                                                                                                                                                                                                                                            767                      Engine Ignition and Start Control Panel
                            233T6211-26-01, including Appendix A                                                                                                                                                                                                                                                                                                                                                                         19 December 2001         767-400ER                                Auxiliary Power Unit and Cargo Fire Control Module Assembly
                            Actions accomplished before the effective date of this Directive in accordance with Boeing ASB 767-33A0087, dated 19 December 2001, are considered acceptable for compliance with the corresponding action specified in this Directive, provided that the actions specified in this Directive are done on the switches for the additional panel assemblies specified in Revision 1 of the service bulletin.
                            Later revisions of Boeing ASB 767-33A0087 or 767-33A0088, approved by the United States Federal Aviation Administration (FAA) as an Alternate Method of Compliance (AMOC) to FAA AD 2008-02-14, are considered acceptable for compliance with the equivalent Requirements of this Directive.
                            Note 5:  FAA AD 2008-02-14 Amdt 39-15344 refers.
Compliance:                 For Requirements 1 and 2 - Within 60 months after the effective date of the original issue of this Directive.
                            For Requirement 3, 4 and 5 - Before further flight after the Requirement 1.a. inspection.

             This Amendment becomes effective on 8 May 2008.
Background:  The FAA has received a report indicating that the integrated drive generator failed in flight due to a possible switch malfunction.  This Directive is issued to ensure that certain lighted pushbutton switches in the flight compartment do not malfunction and cause the flightcrew to be unable to