Document ID: chunk:federal_register_of_legislation:F2006B08632:body:0
Version: federal_register_of_legislation:F2006B08632
Segment Type: other
Provision Reference: 
Character Range: 0–1387

COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 106 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

 Teledyne Continental Motors Piston Engines

 AD/CON/49
 Amdt 1

 Rotary Fuel Pump P/N 643367A2 8/87 TX

            Applicability: GTSIO-520-N Series engines fitted with Lear Siegler rotary fuel pump P/N 643367A2.

            Requirement: Action in accordance with the technical requirement of FAA AD Priority Letter 87- 04-05 dated 12 February 1987 as follows:

             Quote;

                "(a) Cut and remove the safety wire from the four attaching screws on the regulator valve cover of fuel pump P/N 643367A2.

                (b)     Loosen screws one full turn

                (c)     Tighten the four screws to 24-27 inch pounds

(d)     Safety wire the four screws with .032 inch wire" Unquote.
            (Lear Siegler INC SB No. 101SB015 dated 17 December 1986, and TCM SB No. M87-6 dated 6 February 1987 refer).

 Compliance: Within 10 operating hours after 27 February 1987.

            Note: Prior compliance with the referenced Service Bulletins does not constitute compliance with this Directive.

            Background:  This Directive is amended to correct the metrication error which was introduced into the 7 May published issue of this Directive. Reference to Nm has been deleted from this Amendment.