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JAA Environmental Standards:
Noise: Refer to Canadair Report RAU-601R-133, -ICAO Annex 16, Noise Certificate and Airplane Flight Manual CSP A-012
Additional National Design Requirements (ANDR):
Refer to CRI A-2 in Conjunction with CRI’s A-2.1 through A-2.12
III. Technical Characteristics and Operational Limitations
The CL-600-2B19 Regional Jet, manufactured by Bombardier Aerospace, is a nominal 50 passenger, five crew member, twin turbofan passenger aircraft, developed from the CL-600-2B16 Challenger Aircraft.
The aircraft is certified for a maximum altitude of 41,000 feet and a maximum design airspeed of March 0.85. The maximum operating altitude for take-off and landing is 10,000 feet. Refer to the approved AFM for operating altitudes above 10,000 feet. The airframe is of a same monocoque design, using lightweight aluminum alloys, alloy steels, stainless steels, titanium and composite materials. It has a low, high swept airfoil, and tricycle landing gear.
1.
EASA/JAA Type Design Definition:
Report RAZ-601R-109, JAA Build Standard Definition.
2.
Engines
Two General Electric CF34-3A1 Turbofan Engines or two General Electric
CF34-3B1.
Appropriate National Authority Type Certificate or FAA Type Certificate E15NE and associated Type Certificate Data Sheet.
Engine may be intermixed in accordance with AFM (CSP A-012).
Engine Limits:
Refer to the Airplane Flight Manual (CSP A-012)
3. Fuel
Type SPECIFICATION
Canada USA UK
Kerosene JET A, A-1 JP8 CAN 2 – 3.23 3-GP-23 ASTM D1655 MIL-DTL-83133 Def Stan 91-91 Def Stan 91-87
High Flash JP5 3-GP-24 MIL-DTL-5624 Def Stan 91-86
Note: Fuel additives -See AFM as listed in Approved Publications
For additional approved fuel grades see AFM
Use of wide-cut fuels is prohibited except for non-revenue ferry flights.
For fuel temperature limitations see applicable AFM.
Fuel Capacity (usable)
Load Weight
Usable U.S. Gal. Litres lb. kg
2 main tanks (each) 700 2650 4760 2159
1 Center Tank 735.0 2782 4998 2267
Total 2135.0 8082 14518 6585
Load Weight
Unusable U.S. Gal. Litres lb. kg
Residual Fuel 7.35 27.8 46.9 21.3
Trapped Fuel 7.42 28.0 50.1 22.7
Unusable Fuel 14.3 54.1 97.0 44.0
4.
Oil Engine, APU, IDG: MIL-L-7808 (Type I) or MIL-L-23699 (Type II) or Castrol 4000. Oil Capacity:
5.
Airplane Limit Speeds
Load Weight
Usable U.S. Quart Litres lb. kg.
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本文链接地址：European Aviation Safety Agency TYPE-CERTIFICATE DATA SHEET CL-600(3)
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