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SECTION 7: Challenger 600 Series (grandfathered)
I. General
1. Aeroplane: Challenger CL-600-1A11 (600) Challenger CL-600-2A12 (601 variant) Challenger CL-600-2B16 (601-3A variant) Challenger CL-600-2B16 (601-3R variant) Challenger CL-600-2B16 (604 variant)
II. Certification Basis
1. TCCA Certification Date:
CL-600-1A11 (600) 10 August 1980
CL-600-2A12 (601 Variant) 25 February 1983
CL-600-2B16 (601-3A Variant) 21 April 1987
CL-600-2B16 (601-3R Variant) 02 July 1993
CL-600-2B16 (604 Variant) 20 September 1995
2. EASA Validation Application Date: 28 September 2003
3. EASA Certification Date:
(Date of first TC issuance within
EU MS by LBA Germany)
CL-600-1A11 (600) 01 Aug 1991
CL-600-2A12 (601 Variant) 11 Apr 1986
CL-600-2B16 (601-3A Variant) 13 Mar 1991
CL-600-2B16 (601-3R Variant) 16 Sep 1996
CL-600-2B16 (604 Variant) 09 Jan 1997
The above constitutes EU members acceptance of the Challenger variant models prior to EASA formation on 28 Sept 2003. Other examples of EU member states acceptance of the Challenger models include:
Countries CL-600 CL-601 CL-601-3A CL-601-3R CL-604
Austria Dec 23; 1992 Dec 23, 1992 Dec 23, 1992 Dec 23, 1992 Dec 23, 1992
Denmark Mar 19; 2001 N/A N/A Mar 06, 2000
Germany Aug 01; 1991 Apr 11, 1986 Mar 13. 1991 Sep 16, 1996 Jan 09, 1997
Greece N/A N/A N/A Dec 06, 2002
Italy May 28, 1996 May 28, 2006 Jul 22, 1996 Jul 22, 1996
4. TCCA Certification Basis: Refer to TCCA Type Certificate Data Sheet No: A-131
5. EASA Certification Basis:
TCCA cert basis defined in Type data sheet A-131. EC 1702/2003 provides for grandfathering of pre-existing certificates compliant to TCCA cert basis that have shown to comply with the safety standards of EASA basic rule EC 1592/2002. Examples of grandfathered certificates are listed above (#3).
5.1 Models CL-600-1A11, -2A12, -2B16 (601-3A and 601-3R Variant)
a) FAR Part 25 dated February 1, 1965, including Amendments 25-1 through 25-37. FAR Part 25, Amendment 25-38 paragraphs 675(a), 685(a), 733(c), 775(e), 787(c), 815, 841(b), 951(a), 979(d), and (e), 1041, 1143(e), 1303(a), 1322, 1385(c), 1557(b) and 1583(a); Amendment 25-40 paragraphs 901 (b) and (c), 903(c), and (e), 933(a), 943, 959, 1091(a) and (d), 1145(c), 1199(b) and (c), 1207, 1549 and 1585(a) (9); Amendment 25-41 paragraph 1309; Amendment 25-42, paragraph 1353(c); Amendment 25-45, paragraphs 571 and 629(d) (4) (v); Amendment 25-46, paragraphs 351 and 603.
b) DOT Airworthiness Requirements contained in DOT letter to Canadair Limited, 5010-10-326 (LIAP), 31 July 1980.
c) Equivalent safety has been established for the following requirements: FAR 25.773 (b)(2) DV Window FAR 25.955 (a)(4) Fuel Flow
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本文链接地址：European Aviation Safety Agency TYPE-CERTIFICATE DATA SHEET CL-600(23)
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