Document ID: chunk:federal_register_of_legislation:F2006B06530:body:0:p1
Version: federal_register_of_legislation:F2006B06530
Segment Type: other
Provision Reference: 
Character Range: 20–3224

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.

 Radio Communication and Navigation Equipment

AD/RAD/75 TDR-94/TDR-94D Transponders 5/2002

            Applicability: Rockwell Collins TDR-94 Mode S transponders (Collins part number (CPN) 622- 9352-004) and TDR-94D Mode S transponders (CPN 622-9210-004).

            Note 1: These transponders may be installed on, but not limited to, the following series of aeroplanes:

                Aerospatiale ATR42;
                deHavilland DHC-7 and DHC-8; and
                Short Brothers Models SD3-60 and SD3-60 SHERPA.

              Requirement: 1. Determine whether the altitude information from any TDR-94 Mode S transponder (CPN 622-9352-004) or TDR-94D Mode S transponder (CPN 622- 9210-004) is derived from a digital air data source or a Gillham (grey code) encoded source. This may be accomplished as specified in Rockwell Collins Service Bulletin (SB) No. 17 (TDR-94/94D-34-17), dated 8 February 1999, SB 17, Revision 1, dated 15 May 2000, or SB 20 (TDR-94/94D-34-20), Revision 1, dated 2 May 2001. Collins Product Information Letter No. 71, dated January 1999, references Service Bulletin 17, dated 8 February 1999.

            If the altitude information from all affected transponders is derived from a digital air data source, this Directive requires no further action.

2.        If the altitude information is derived from a Gillham (grey code) encoded source, modify the unit to prevent erroneous altitude reporting. The modification encompasses converting the TDR-94 transponder from Collins part number (CPN) 622-9352-004 to CPN 622-9352-005 or converting CPN 622-9352- 004/005 to CPN 622-9352-006; and converting the TDR 94D transponder from CPN 622-9210-004 to CPN 622-9210-005 or converting CPN 622-9210-004/005 to CPN 622-9210-006.

              Modifications are to be accomplished in accordance with either SB 17 (TDR- 94/94D-34-17), SB17 Revision 1or SB 20 (TDR-94/94D-34-20), Revision 1.

3.        TDR-94 Mode S transponder (CPN 622-9352-004) or TDR-94D Mode S transponder (CPN 622-9210-004) may not be installed on any aeroplane if the altitude information is derived from a Gillham (grey code) encoded source, unless the transponder is modified in accordance with Requirement 2.

 Radio Communication and Navigation Equipment

 AD/RAD/75 (Continued)

            Note 2: FAA AD 2002-06-06 Amdt 39-12683 refers.

 Compliance: For Requirement 1 - Before 16 August 2002.

            For Requirement 2 - At the next biennial transponder check required by AD/RAD/47 Amdt 1 that occurs after 16 August