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ICA on EWIS (ref. CRI H-1000-01) – see note 6
The following Special Conditions are specific to the CL600-2D15 & CL-600-2D24:
INT/POL/25/5 B-900-03) INT/POL/25/6 INT/POL/25/12 INT/POL/25/13 Accelerate-Stop Distances and Related Performances Worn Brakes (CRI D-900-01) Fuel Tank Safety-Ignition Prevention (CRI E-900-04) Towbarless Towing (CRI C-900-06) (CRI
JAA Exemptions:
The following Temporary Exemption has been accepted for the CL-600-2D15 as it was for the CL-600-2C10 (CRI F-01).
JAR 25.1441 and 25.1447 Oxygen System Requirements (CRI F-900-01)
JAA Equivalent Safety Findings:
The following Equivalent Safety Findings (ESF) were agreed for the CL-600-2C10
and are applicable to the CL-600-2D15:
JAR 25.677(b) Trim Indication (CRI D-5)
JAR 25.783(f) Baggage and Avionics Compartment Door (CRI D-2)
JAR 25.811(d)(2) Main Door Exit Markings Sign (CRI D-3)
JAR 25.813(c)(1) Emergency Exit Access (CRI D-4)
JAR 25B.991(b) Emergency Fuel Pumps (CRI J-1)
JAR 25.1435(b)(1) Hydraulic Systems (CRI F-15)
NPA 25C-236 Vibration, Buffet and Aeroelastic Stability (CRI C-6)
(Identical to FAR 25 Amendment 77)
The following ESF have been agreed for the CL-600-2D15:
JAR 25.341 Continuous Turbulence (CRI C-900-07)
JAR 25.361(b) Engine and APU Load Conditions (CRI C-900-09)
JAR 25.307 Proof of Structure (CRI C-900-11)
JAR 25.1181(a)(b) Designated Fire Zones (CRI E-900-02)
JAA Elect to Comply Standards
The following CL-600-2C10 Elect to Comply standards are applicable to the CL-600-2D15:
NPA 25B-215 Stall, Stall Warning Speeds and Manoeuvre Capability (CRI B-1) (Identical to FAR 25 NPRM 95-17) NPA 25C-282 Discrete Gust Load Design Requirements (CRI C-12) (Identical to FAR 25 Amendment 86) NPA 25C-276 Braked Roll Conditions (CRI C-13) (Identical to FAR 25 Amendment 97)
Bombardier have elected to comply with the following standards specifically for the CL-600-2D15 & CL-600-2D24:
NPA 25D-285 Allowable Carbon Dioxide Concentration in Aeroplane Cabins and Cabin Ozone Concentration. (CRI D-900-02)
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-600-2D15 Regional Jet, manufactured by Bombardier Aerospace, is a nominal 75 passenger, five crewmember, twin turbofan passenger aircraft, developed from the CL-600-2C10 Regional Jet Aircraft. The certification of the CL-600-2D15 considers one basic aircraft model defined as follows:
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本文链接地址：European Aviation Safety Agency TYPE-CERTIFICATE DATA SHEET CL-600(11)
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