Document ID: chunk:federal_register_of_legislation:F2006B06035:body:0:p3
Version: federal_register_of_legislation:F2006B06035
Segment Type: other
Provision Reference: 
Character Range: 6221–8528

PA-46-350P aeroplanes
VB-1332                           16/14 November 1997    4622001 through 4622200
VB-1609                           1/21 November 1997     463001 through 4636020
VB-1602                           1/28 November 1997     4636021 through 4636131
VB-1446                           New/3 December 1997    4636132 through 4636195
VB-1710                           New/23 February 1999   all serial numbers after 4636195

            Note 2: FAA AD 99-15-04 Revision 1 Amdt 39-11747 refers.

            Compliance:  For Requirement 1 - Within the next 100 hours time in service (TIS) after the effective date of this Directive.

            For Requirement 2 - Before further flight following the Requirement 1 inspection and calibration.

            For Requirement 3 - Within the next 100 hours TIS after the effective date of this Directive unless the applicable AFM/POH revision is incorporated (Refer to Table 2).

            For Requirement 4 - As of the effective date of this Directive.

            For Requirement 5 - Within the next 100 hours TIS after the effective date of this Directive.

            For Requirement 6 - Before further flight following the Requirement 5 inspection and calibration.

            For Requirement 7 - Upon accumulating 250 hours TIS on the currently installed TIT probe or within the next 100 hours TIS after the effective date of this Directive, whichever occurs later, and thereafter at intervals not to exceed 250 hours TIS.

            For Requirement 8 - Within the next 100 hours TIS after the effective date of this Directive unless the applicable AFM/POH revision is incorporated (Refer to Table 2).

            For Requirement 9 - As of the effective date of this Directive.

            This Airworthiness Directive becomes effective on 10 August 2000.

            Background:  This Directive is intended to detect and correct improperly calibrated TIT indicators or defective TIT probes. These conditions, if not detected and corrected, could result in improper engine operation and engine damage/failure with consequent loss of control of the aeroplane.

 Eugene Paul Holzapfel
 Delegate of the Civil Aviation Safety Authority 23 June 2000

 The above AD is notified in the Commonwealth of Australia Gazette on 12 July 2000.