To view this page ensure that Adobe Flash Player version
9.0.124 or greater is installed.
曝光台 注意防骗 网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者
6.
The Special Condition (i.e. CRI H-1000-01) that introduces requirements for EWIS-ICA’s makes CS-25 Appendix H paragraph H 25.5 and AMC Appendix H 25.5 paragraphs 1 and 6 applicable to the certification basis (note, BA demonstration of compliance against 14 CFR Part 26 requirements constitutes compliance with the EASA regulations related to EWIS).
SECTION 6: CL-600-2E25 (Regional Jet Series 1000)
I. General
1. Aeroplane: Regional Jet Series 1000
II. Certification Basis
1.
Reference Application Date for TCCA Certification: 23 February 2007
2.
TCCA Certification Date: 02 November 2010
3.
EASA Validation Application Date: 28 February 2007
4.
EASA Certification Date 09 November 2010
5.
TCCA Certification Basis:
Refer to TCCA Type Certificate Data Sheet No: A-131
6.
EASA Certification Basis:
EASA Airworthiness Requirements:
CS-25 Large Aeroplanes, Amendment 2, dated 02 October 2006 Note: This includes the optional requirements of CS 25.1419, Ice Protection and CS 25.801, Ditching Provisions.
CS-AWO at Initial Issue
Reversions:
CS 25.772(c) reversion to JAR 25, Change 14
CS 25.415(c) reversion to JAR 25, Change 14 (for Rudder Control System only)
CS 25.981(c) is not applicable.
EASA Special Conditions:
Novel Design Features:
D-1000-01 Command-by-Wire Control Systems Failure Criteria
General Experience:
C-1000-01 Engine Imbalance C-1000-02 Engine loads C-1000-03 Emergency landings C-1000-11 Design Stall Speed D-1000-04 Application of heat release and smoke density requirements
to seat materials
H-1000-01 EWIS/EAPAS – see note 5
The following CL-600-2C10/CL-600-2D24 Special Conditions are also applicable to the CL-600-2E25:
D-15 Lightning strike protection, direct effects
D-16 Lightning strike protection, indirect effects
D-17 HIRF protection
E-900-04 Fuel tank safety – Ignition prevention
Equivalent Safety Findings
D-1000-03 Seat Cushion protrusion
The following Equivalent Safety Findings were agreed for the CL-600-2C10/2D24 and are equally applicable to the CL-600-2E25:
D-5 Trim Indication
D-2 Baggage and Avionics Compartment Door
D-3 Main Entry Door Markings Sign
J-1 Emergency Fuel Pumps
E-900-02 Designated Fire Zones
Elect to Comply Requirements
The following sub-paragraphs of CS-25 at amendment 3 issued September 19th, 2007 are elected to be complied with by Bombardier Aerospace per their submission of the Changed Product Rule Analysis RAZ-BA698-004 at latest revision:
CS-25.811 (g)
CS-25.812 (b)
CS-25.812 (e)
7. Environmental Standards:
Fuel Venting and Emissions: ICAO Annex 16, 2nd edition, Volume 2, Part II and Part III,
中国公务机网 www.gongwuji.com
公务机翻译 www.aviation.cn
本文链接地址：European Aviation Safety Agency TYPE-CERTIFICATE DATA SHEET CL-600(19)
| 
