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Note: CRI B-900-03 includes NPA 25B, D, G-244 as an “Elect to Comply”.
Additional National Design Requirements (ANDR).
Additional National Design Requirements (ANDR) as specified in JAA Administrative and Guidance Material, Section 3/Part 4 in effect at the time of Type Certification. Refer to CRI A-900-02.
7. Environmental Standards:
Noise: ICAO Annex 16, Volume I, Third Edition. (CRI-A-900-03 refers).
III. Technical Characteristics and Operational Limitations
The CL-600-2D24 Regional Jet, manufactured by Bombardier Aerospace, is a nominal 86 passenger, five crewmember, twin turbofan passenger aircraft, developed from the CL-600-2C10 Regional Jet Aircraft. The certification of the CL-600-2D24 considers one basic aircraft model defined as follows:
. CL-600-2D24 (Regional Jet Series 900): 86 passengers configuration (plus 5 crewmembers)
The aircraft is certified for a maximum altitude of 41,000 feet and a maximum design airspeed of Mach 0.85. With the incorporation of M/S 690T002727 – Introduction of new winglet, the Mach number must be decreased to Mach 0.84 above 34,000 feet. 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/JAA Type Design Definition
Reference CRI A-900-06 JAA/EASA Build Standard Definition, RAZ-BA690-120.
2.
Engines
Two General Electric CF34-8C5 or optional CF34-8C5A1 Turbofan Engines, with reverse thrust capability, are rear fuselage mounted on pylons; JAA Executive Board recommendation letter 04/12/91/10/02-L237 dated 20 September 2002. 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 C-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.
For fuel temperature limitations see applicable AFM.
Fuel Capacity:
Load Weight
Usable U.S. Gal. Litres lb. kg
2 main tanks (each) 1,110 4,202 7,492 3,398
1 Center Tank 683 2,585 4,610 2,091
Total 2,903 10,989 19,595 8,888
Load Weight
U.S. Gal. Litres lb. kg
Unusable 23.1 87.4 155.9 70.7
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本文链接地址：European Aviation Safety Agency TYPE-CERTIFICATE DATA SHEET CL-600(16)
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