Terminating Action

Accomplishment of the actions contained in Requirement 1(b) terminates the repetitive inspections required by Requirement 1(a) and 5 of this AD.

Accomplishment of the installation specified in Boeing SB 747-78-2150, dated 20 March, 1997, terminates the requirement to comply with the installation contained in Requirement 1(b) of this AD.

Note: FAA AD 2000-14-11 Amdt 39-11821 refers

Compliance: For Requirement 1(a) OR (b): Prior to the issue of a Certificate of Airworthiness.

For Requirement 2: At intervals not exceeding 1,500 flight hours until accomplishment of Requirement 1(b).

For Requirement 3: Within 3,000 flight hours after accomplishment of Requirement 1(b) modifications.

For Requirement 4(a): At intervals not exceeding 3,000 flight hours. For Requirement 4(b) and (c): Prior to further flight.

For Requirement 5: Prior to the issue of a Certificate of Airworthiness.

For Requirement 6: At intervals not exceeding 18 months until accomplishment of Requirement 1(b).

For Requirement 7(a) or (b): Prior to further flight.

For Requirement 7(c): Within 10 days after thrust reverser deactivation in accordance with the provisions of Requirement 7(b).

For Requirement 7(d) and (e): Prior to further flight.

This Airworthiness Directive becomes effective on 11 July 2002.