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j)  Compliance has been demonstrated with: FAR Part 36 dated December 1, 1969, as amended through Amendment 36-20 FAR Part 34 dated August 25, 1990, as amended through Amendment 34-1

III. Technical Characteristics and Operational Limitations
1.  
EASA/JAA Type Design Definition Major modifications which define the aircraft as the “Green Configuration” are recorded in document RAZ-604-142 at latest Revision (Definition of type design for JAA type certification).

2.  
Engines

3.
Airplane Limit Speeds

4.
Oil Oil Capacity:

Models  Engines 
 
CL-600-1A11 (600)  Two Avco Lycoming ALF-502L or ALF-502L-2 Two -General Electric CF34-1A or One -General Electric CF34-1A and One CF34-3A or One – General Electric C434-1A and one CF34A2 or * Two -General Electric CF34-3A or * Two -General Electric CF34-3A2 or * One -General Electric CF34-3A and One CF34-3A2 
CL-600-2A12 (601 Variant) 
* Aircraft with two CF34-3A or CF34-3A2 engines installed, improved performance is not available until Canadair Service Bulletin 601-0238 -Modification -Engines -Use of 3A engines at 3A power settings, is incorporated. 
CL-600-2B16 (601-3A Variant)  Two -General Electric CF34-3A or CF34-3A2 or One -General Electric CF34-3A and One CF34-3A2 
CL-600-2B16 (601-3R Variant)  Two -General Electric CF34-3A1 
CL-600-2B16 (604 Variant)  Two -General Electric CF34-3B 

CL-600-1A11 (600) 
Airspeed Limits (IAS)  Knots Mach VMO and MMO (Maximum Operating) Sea Level to 10000 ft 301* * *See Flight Manual for variations of VMO and MMO with altitude 
VFE (Flaps extended) 20° 30° 45° 45° **See Flight Manual as listed in Approved Publications 232 198 170** 190** 
VA (SeeFlight Manual for variations of VA with altitude and aircraft weight) 
VLO (Landing Gear Operating) 197 
　
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本文链接地址：European Aviation Safety Agency TYPE-CERTIFICATE DATA SHEET CL-600(25)