Document ID: chunk:federal_register_of_legislation:F2007L03988:body:0:p2
Version: federal_register_of_legislation:F2007L03988
Segment Type: other
Provision Reference: 
Character Range: 2935–6071

the need for the Requirement 1 repetitive visual checks and the Requirement 3 operational checks.

                4. If, during the Requirement 3 operational test, any spoiler panel is found to be fully extended with the speedbrake handle down, or if any spoiler panel is found fully retracted when the speedbrake handle is up, replace the flight spoiler actuator in accordance with the actions specified in Requirement 2.
                5. The Master Minimum Equipment List Item 27-7, "Auto Speed Brake System,'' is no longer applicable to Model 737-800 series aeroplanes equipped with an Short Field Performance (SFP) package.
                6. Flight spoiler actuators, P/N P665A0001-00, may not be installed on any aeroplane as a replacement spare.
                7. If any spoiler is found to be improperly stowed during any visual check required by this Directive, report the following information electronically to Boeing using the established Boeing Communications System (BCS):
                  Aeroplane serial number, jam position, spoiler panel number or wing position of the spoiler that jammed, date of visual check, and flight hours accumulated on the aeroplane.
                8. Install flight spoiler actuator, P/N P665A0001-01 or higher dash number, in all eight flight spoiler positions in accordance with the Accomplishment Instructions of Boeing Alert Service Bulletin 737-27A1283, dated 3 April 2007.

                Doing this installation ends the requirements detailed in this Directive.

                Any flight spoiler actuator with P/N P665A0001-01 (or higher dash number) that was previously installed in any flight spoiler position in accordance with the requirements of this AD at amendment 1 is acceptable for meeting the requirements of this AD for that flight spoiler position.
                9. Do not install a flight spoiler actuator, having P/N P665A0001-00, on any aeroplane.
             Note 2:  FAA AD 2007-15-04 Amdt 39-15133 dated 11 July 2007 refers.  This AD supersedes FAA AD 2007-06-52.
Compliance:  For Requirement 1 - After every landing and after any rejected takeoff manoeuvre after the effective date of this AD, until installation of flight spoiler actuator, P/N P665A0001-01 or higher dash number, in all eight flight spoiler positions is accomplished.
             For Requirement 2 - Before further flight after the Requirement 1 visual check.

             For Requirement 3 - After any maintenance action that operates the spoiler system, until the installation of flight spoiler actuator, P/N P665A0001-01 or higher dash number, in all eight flight spoiler positions is accomplished.
             For Requirement 4 - Before further flight after the Requirement 3 operational test.
             For Requirement 5 and 6 - As of the effective date of this AD.
             For Requirement 7:
                  a. For visual checks accomplished before the effective date of this AD - Within seven days after effective date of this AD.
                  b. For visual checks accomplished after the effective date of this AD - Within seven days after carrying out