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Chapter 2, Amendment 4.
Noise: ICAO Annex 16, Volume I, Part II, Chapter 4,Amendment 8.
III. Technical Characteristics and Operational Limitations
The CL-600-2E25 (Regional Jet Series 1000), manufactured by Bombardier Aerospace, is a nominal 104 passenger, six crewmember, twin turbofan passenger aircraft, developed from the CL-600-2D24/2D15 Regional Jet Aircraft.
The aircraft is certified for maximum altitude of 41,000 feet and maximum design airspeed of Mach 0.84. The airframe is a monocoque design, using lightweight aluminum alloys, alloy steels, stainless steels, titanium and composite materials. It has a low, high swept wing, T-tail with trimmable horizontal stabilizer and tricycle landing gear.
1.
EASA Type Design Definition
EASA Definition of Type design contained in document, RAZ-BA698-018.
2.
Engines
Two General Electric CF34-8C5 or optionals CF34-8C5A1 and CF34-8C5A2 Turbofan
Engines, with reverse thrust capability, are rear fuselage mounted on pylons.
Appropriate National Authority Type Certificate or FAA Engine Type Certificate No.
E00063EN Revision 2 or later, and associated Type Certificate
Data Sheet.
Engine Limits:
Refer to the Airplane Flight Manual (CSP D-012).
3. Fuel
SPECIFICATION
Canada USA UK China CIS NATO
CGSB-3.23 ASTM D1655 JET A
ASTM D1655 JET A-1 Def Stan 91-91 GB6537-94 No. 3 Jet RT F-35
CGSB-3.24 MIL-DTL-83133 JP-8 Def Stan 91-87 F-34
MIL-DTL-5624 JP-5 Def Stan 91-86 F-44
Note: Fuel additives -See AFM as listed in Approved Publications.
For additional approved fuel grades see AFM.
For fuel temperature limitations see applicable AFM.
Fuel Capacity:
Load Weight
Usable U.S. Gal. Litres lb. kg
2 main tanks (each) 1,114 4,217 7,517 3,410
1 Center Tank 710 2,688 4,795 2,175
Total 2,937 11,117 19,828 8,994
Load Weight
U.S. Gal. Litres lb. kg
Unusable 37.5 141.9 252.8 114.6
Undrainable 13.1 49.6 88.3 40.1
4.
Oil Oil: Engine, APU: MIL-L-7808 (Type I) or MIL-L-23699 (Type II) or Castrol 4000 Mixing of different types of oils is prohibited. Oil Capacity:
5.
Air Speeds
6.
Centre of Gravity Range See AFM, CSP D-012. Datum: FS 0.0 located at 365.76cm (144.00 inches) forward of the aircraft nose Mean Aerodynamic Cord (MAC):
Load Weight
Usable U.S. Quart Litres lb. kg.
2 Engines (each) 11 10.4 22.5 10.2
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本文链接地址：European Aviation Safety Agency TYPE-CERTIFICATE DATA SHEET CL-600(20)
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