Schedule Sch 22 - Part 21 Manual of Standards Instrument 2016 - ATSO-1C74c — Airborne ATC transponder equipment

Schedule 22 ATSO-1C74c — Airborne ATC transponder equipment

(subsection 13.2 (1), table, item 2)

This Schedule applies to airborne ATC transponder equipment manufactured by an article manufacturer.

FAA TSO‑C74c means TSO‑C74c — Airborne ATC transponder equipment, as in force on 20 February 1973.

3 Minimum performance standards — FAA TSO-C74c

(1) The airborne ATC transponder equipment must meet the requirements mentioned in the FAA TSO-C74c, other than the requirements mentioned in paragraph (e) (Previously approved equipment) of FAA TSO-C74c.

(2) For subclause (1), a reference in FAA TSO-C74c to a term mentioned in column 1 of an item of the following table is taken to be a reference to the term mentioned in column 2 of the item.

<table cellspacing="0" cellpadding="0" style="margin-bottom:0pt; border-collapse:collapse"><thead><tr><td colspan="3" style="border-top:1.5pt solid #000000; border-right:0.75pt solid #000000; border-left:0.75pt solid #000000; border-bottom:0.75pt solid #000000; padding-right:5.03pt; padding-left:5.03pt; vertical-align:top">Reference to terms in FAA TSO‑C74c</td></tr><tr><td style="border-top:0.75pt solid #000000; border-right:0.75pt solid #000000; border-left:0.75pt solid #000000; border-bottom:1.5pt solid #000000; padding-right:5.03pt; padding-left:5.03pt; vertical-align:bottom">Item</td><td style="border-top:0.75pt solid #000000; border-right:0.75pt solid #000000; border-left:0.75pt solid #000000; border-bottom:1.5pt solid #000000; padding-right:5.03pt; padding-left:5.03pt; vertical-align:top">Column 1Reference in FAA TSO‑C74c</td><td style="border-top:0.75pt solid #000000; border-right:0.75pt solid #000000; border-left:0.75pt solid #000000; border-bottom:1.5pt solid #000000; padding-right:5.03pt; padding-left:5.03pt; vertical-align:top">Column 2Deemed reference</td></tr></thead><tbody><tr><td style="border-top:1.5pt solid #000000; border-right:0.75pt solid #000000; border-left:0.75pt solid #000000; border-bottom:0.75pt solid #000000; padding-right:5.03pt; padding-left:5.03pt; vertical-align:top">1</td><td style="border-top:1.5pt solid #000000; border-right:0.75pt solid #000000; border-left:0.75pt solid #000000; border-bottom:0.75pt solid #000000; padding-right:5.03pt; padding-left:5.03pt; vertical-align:top">RTCA Document No. DO‑138 entitled Environmental Conditions and Test Procedures for Airborne Electronic/Electrical Equipment and Instruments, dated June 27, 1968, must be used</td><td style="border-top:1.5pt solid #000000; border-right:0.75pt solid #000000; border-left:0.75pt solid #000000; border-bottom:0.75pt solid #000000; padding-right:5.03pt; padding-left:5.03pt; vertical-align:top">RTCA Document No. DO-160D called Environmental Conditions and Test Procedures for Airborne Equipment, or a later version of RTCA Document No. DO-160, as existing from time to time, must be used</td></tr><tr><td style="border:0.75pt solid #000000; padding-right:5.03pt; padding-left:5.03pt; vertical-align:top">2</td><td style="border:0.75pt solid #000000; padding-right:5.03pt; padding-left:5.03pt; vertical-align:top">paragraphs 4.0, 5.0, 6.0, 7.0, and 9.0 of DO‑138</td><td style="border:0.75pt solid #000000; padding-right:5.03pt; padding-left:5.03pt; vertical-align:top">sections 4, 6, 7, 8 and 16 of RTCA Document No. DO-160D called Environmental Conditions and Test Procedures for Airborne Equipment, or a later version of RTCA Document No. DO-160, as existing from time to time</td></tr><tr><td style="border:0.75pt solid #000000; padding-right:5.03pt; padding-left:5.03pt; vertical-align:top">3</td><td style="border:0.75pt solid #000000; padding-right:5.03pt; padding-left:5.03pt; vertical-align:top">§37.7</td><td style="border:0.75pt solid #000000; padding-right:5.03pt; padding-left:5.03pt; vertical-align:top">paragraph 21.607 (1) (c) of CASR</td></tr><tr><td style="border:0.75pt solid #000000; padding-right:5.03pt; padding-left:5.03pt; vertical-align:top">4</td><td style="border:0.75pt solid #000000; padding-right:5.03pt; padding-left:5.03pt; vertical-align:top">Appendix B of RTCA Document No. DO‑138</td><td style="border:0.75pt solid #000000; padding-right:5.03pt; padding-left:5.03pt; vertical-align:top">Appendix A of RTCA Document No. DO-160D called Environmental Conditions and Test Procedures for Airborne Equipment, or a later version of RTCA Document No. DO‑160, as existing from time to time</td></tr><tr><td style="border:0.75pt solid #000000; padding-right:5.03pt; padding-left:5.03pt; vertical-align:top">5</td><td style="border:0.75pt solid #000000; padding-right:5.03pt; padding-left:5.03pt; vertical-align:top">TSO number</td><td style="border:0.75pt solid #000000; padding-right:5.03pt; padding-left:5.03pt; vertical-align:top">ATSO number</td></tr><tr><td style="border:0.75pt solid #000000; padding-right:5.03pt; padding-left:5.03pt; vertical-align:top">6</td><td style="border:0.75pt solid #000000; padding-right:5.03pt; padding-left:5.03pt; vertical-align:top">§37.5</td><td style="border:0.75pt solid #000000; padding-right:5.03pt; padding-left:5.03pt; vertical-align:top">regulation 21.605 of CASR</td></tr><tr><td style="border:0.75pt solid #000000; padding-right:5.03pt; padding-left:5.03pt; vertical-align:top">7</td><td style="border:0.75pt solid #000000; padding-right:5.03pt; padding-left:5.03pt; vertical-align:top">furnish to the Chief, Engineering and Manufacturing Branch, Flight Standards Division (or in case of the Western Region, the Chief, Aircraft Engineering Division), Federal Aviation Administration, in the region in which the manufacturer is located,</td><td style="border:0.75pt solid #000000; padding-right:5.03pt; padding-left:5.03pt; vertical-align:top">give CASA</td></tr><tr><td style="border:0.75pt solid #000000; padding-right:5.03pt; padding-left:5.03pt; vertical-align:top">8</td><td style="border:0.75pt solid #000000; padding-right:5.03pt; padding-left:5.03pt; vertical-align:top">Appendix A of RTCA Document No. DO‑138 entitled Environmental Conditions and Test Procedures for Airborne Electric/Electrical Equipment and Instruments, dated June 27, 1968</td><td style="border:0.75pt solid #000000; padding-right:5.03pt; padding-left:5.03pt; vertical-align:top">section 21 of RTCA Document No. DO‑160D called Environmental Conditions and Test Procedures for Airborne Equipment, or a later version of RTCA Document No. DO‑160, as existing from time to time</td></tr><tr><td style="border-top:0.75pt solid #000000; border-right:0.75pt solid #000000; border-left:0.75pt solid #000000; border-bottom:1.5pt solid #000000; padding-right:5.03pt; padding-left:5.03pt; vertical-align:top">9</td><td style="border-top:0.75pt solid #000000; border-right:0.75pt solid #000000; border-left:0.75pt solid #000000; border-bottom:1.5pt solid #000000; padding-right:5.03pt; padding-left:5.03pt; vertical-align:top">set forth in RTCA Document No. DO‑138 entitled Environmental Conditions and Test Procedures for Airborne Electronic/Electrical Equipment and Instruments, dated June 27, 1968</td><td style="border-top:0.75pt solid #000000; border-right:0.75pt solid #000000; border-left:0.75pt solid #000000; border-bottom:1.5pt solid #000000; padding-right:5.03pt; padding-left:5.03pt; vertical-align:top">mentioned in RTCA Document No. DO‑160D called Environmental Conditions and Test Procedures for Airborne Equipment, or a later version of RTCA Document No. DO‑160, as existing from time to time</td></tr></tbody></table> ```

Sch 22ATSO-1C74c — Airborne ATC transponder equipment

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