Document ID: chunk:federal_register_of_legislation:F2006B07468:body:0:p1
Version: federal_register_of_legislation:F2006B07468
Segment Type: other
Provision Reference: 
Character Range: 4–3399

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

    AlliedSignal (Garrett/AiResearch) Turbine Engines - TPE 331 Series

AIRWORTHINESS DIRECTIVE

    For the reasons set out in the background section, the CASA delegate whose signature appears below issues the following Airworthiness Directive (AD) under subregulation 39.1 (1) of CAR 1998. The AD requires that the action set out in the requirement section (being action that the delegate considers necessary to correct the unsafe condition) be taken in relation to the aircraft or aeronautical product mentioned in the applicability section: (a) in the circumstances mentioned in the requirement section; and (b) in accordance with the instructions set out in the requirement section; and (c) at the time mentioned in the compliance section.

    AD/TPE 331/59 Electronic Engine Controls 13/2001
DM

               Applicability: TPE331-8, -10N, and -12B turboprop engines with electronic engine controls (EEC's) part numbers (P/N's) 2101322-1, -4, -11, -12, -13, -14, -15 or -16 installed.

               Note 1: These engines are installed on but not limited to Cessna Aircraft Company Model 441 Conquest aeroplanes.

                  Requirement: 1. If not previously accomplished, amend the applicable Aircraft Flight Manual (AFM) Emergency Procedures and Normal Procedures Section to provide interim emergency procedures to flight crews, by inserting the Temporary Revisions (TR) specified in the following table:

                    Aeroplane Serial Number (S/N)

 AFM Affected Temporary Revision

                    441-0001 through
                    441-0172

                    441-0173 and
                    higher

 D1561-14-13PH
 through Revision 14
 dated 9 January 1998

 D1586-11-13PH
 through Revision 11
 dated 9 January 1998

   D1561-14TR2 through D1561-14TR8 dated 20 November 2000

   D1561-14TR9 dated 11 April 2001

   D1586-11TR2 through D1586-11TR5 dated 20 November 2000

   D1586-11TR7 and D1586-
   11TR8 dated
   20 November 2000

   D1586-11TR9 dated 7 March 2001

   D1586-11TR10 dated
   11 April 2001.

               Owners or operators of aeroplanes that have been modified by supplemental type certificate (STC), where the AFM conflicts with the TR's specified in Requirement 1, must contact the Manager, Engineering Support Branch (ESB), Civil Aviation Safety Authority, to have their AFM's reviewed and approved.
 COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 106 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

                The ESB Manager may be contacted at the following address: PO Box CP57
                Condell Park NSW 2200 Facsimile (02) 9780 3060
            2. Replace all existing EECs P/N's 2101322-1, -4, -11, -12, -13, -14, -15 and -16
              with serviceable EECs. (For the purposes of this Directive, a serviceable EEC is an EEC with a P/N that is not specified in this Directive.)

              Information regarding the replacement of existing EEC's is available in Honeywell Alert Service Bulletins TPE331-A76-0035 dated 23 July 2001, TPE331-A76-0036 dated 23 July 2001, and TPE331-A76-0037 dated 23 July 2001.

              When all EECs have been replaced in the aeroplane with serviceable EECs,