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INT/POL/25/4 Lightning Strike Protection, Indirect Effects (ref. CRI D-16)
INT/POL/25/6 Brake Performance (ref. CRI D-9)
INT/POL/25/8 Yawing Manoeuvring Conditions (ref. CRI C-3)
INT/POL/25/9 Fuel Tank Crashworthiness (ref. CRI C-5)
SC H-1 Enhanced Airworthiness Programme for Aeroplane System – ICA
on EWIS (ref. CRI H-1000-01) – see note 5
JAA Exemptions: None
JAA Equivalent Safety Findings:
JAR 25.109 Accelerate Stop Distance (NPA 25B, D, G-244,
July 1993, ref. CRI B-2) JAR 25.677(b) Trim Indication (ref. CRI D-5) JAR 25.783(f) Baggage and Avionics Compartment Door (ref. CRI D-2) JAR 25.811(d)(2) Main Door Exit Markings Sign (ref. CRI D-3) JAR 25.813(c)(1) Emergency Exit Access (ref. CRI D-4) JAR 25.1435(b)(1) Hydraulic Systems (ref. CRI-F-15) JAR 25B.991(b) Emergency Fuel Pumps (ref. CRI J-01)
JAA Elect to Comply Standards
NPA 25B.215 Reduced Minimum Operating Speed Factors (ref CRI-B-1) (Identical to FAR 25 NPRM 95-17)
NPA 25C-236 Vibration, Buffet and Aeroelastic Stability (ref. CRI C-6) (Identical to FAR 25 Amendment 77)
NPA 25C-282 Discrete Gust Load Design Requirements (ref CRI C-12) (Identical to FAR 25 Amendment 86)
NPA 25C-276 Braked Roll Conditions (ref. CRI C-13) (Identical to FAR 25 Amendment 97)
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-2
7. Environmental Standards:
Noise: ICAO Annex 16, Volume I, Third Edition.
Fuel Venting: ICAO Annex 16, Volume II, Second Edition.
III. Technical Characteristics and Operational Limitations
The CL-600-2C10 Regional Jet, manufactured by Bombardier Aerospace, is a nominal 70 passenger, five crewmember, twin turbofan passenger aircraft, developed from the CL-600-2B19 Regional Jet Aircraft. The certification of the CL-600-2C10 considers three basic aircraft variants defined as follows:
.
Regional Jet Series 700: 68 passengers or less (plus 5 crewmembers)
.
Regional Jet Series 701: 70 passengers configuration (plus 5 crewmembers)
.
Regional Jet Series 702: 78 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. 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-6 JAA Build Standard Definition, RAZ-BA670-120.
2.
Engines Two General Electric CF34-8C1 Turbofan Engines, or two General Electric CF34-8C5B1 Turbofan Engines, JAA Executive Board recommendation letter 04/12/46/10/00-L162
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本文链接地址：European Aviation Safety Agency TYPE-CERTIFICATE DATA SHEET CL-600(7)
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