AD 69-03-02

69-03-02 BOEING: Amdt. 39-718 as amended by Amendment 39-949. Applies to Models 707, 720, and 727 airplanes listed in Service Bulletin Nos. 2536, dated 1 June 1967, as revised by Revision 1, 23 January 1970 and Service Bulletin 27-100 dated 8 June 1967, or later FAA approved revisions. Compliance required as indicated. A) Within the next 2,500 hours time in service after 1 March 1969, unless already accomplished, for those aircraft listed in Boeing Service Bulletin No. 2536, dated 1 June 1967, for Model 707's and 720's or Boeing S.B. No. 27-100 dated 8 June 1967 for 727's, or later FAA approved revision, remove the existing rudder pedal adjustment crank assembly and replace with a modified or new crank assembly in accordance with Boeing Service Bulletin No. 2536, dated 1 June 1967, for Model 707's and 720's or Boeing Service Bulletin No. 27-100, dated 8 June 1967, for Model 727's or later FAA approved revisions or an equivalent design approved by the Chief, Aircraft EngineeringDivision, FAA Western Region. B) Within the next 1,000 hours' time in service after the effective date of this amendment to Amendment 39-718 (34 F.R. 1769), AD 69-03-02, for those additional Model 707's and 720's listed in Revision 1, dated 23 January 1970, to Boeing Service No. 2536, and not previously listed in S.B. No. 2536, unless already accomplished, remove the existing rudder pedal adjustment crank assembly, and replace with a modified or new crank assembly, in accordance with Boeing S.B. No. 2536, Revision 1, dated 23 January 1970, or later FAA approved revisions, or an equivalent design approved by Chief, Aircraft Engineering Division, FAA Western Region. Amendment 39-718 effective March 1, 1969. This amendment (39-949) becomes effective March 6, 1970.