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Dual Main Wheels and Tyres (L/H & R/H) H36 x 12 – 18, 18 ply
Landing Gear:
Tricycle Type (Two main gear assemblies and one steerable nose gear assembly)
18. Hydraulics
See AMM (CSP B-001) for approved Fluids.
19. Maintenance Instructions
Airplane Flight Manual: Flight Crew Operating Manual: Weight and Balance Manual: Minimum Master Equipment List (MMEL): CSP C-012 CSP C-013 CSP C-041 CSP ABC-044
The Instructions for Continued Airworthiness consist of the following Publications:
Aircraft Maintenance Manual (AMM): CSP B-001
Maintenance Requirement Manual (MRM) Part II: CSP B-053
Structural Repair Manual (SRM): CSP B-008
Non-Destructive Testing Manual (NDT) CSP B-010
20. Notes
1.
Current weight and balance report, loading instructions (when necessary), and the list of equipment included in the certificated empty weight must be provided for each aircraft at the time of original certification.
2.
JAA Approved Airplane Flight Manual: The airplane must be operated according to the appropriate JAA Approved Airplane Flight Manual.
3.
All placards must be installed in accordance with Drawings: a) Basic markings and placards: BA690-47500, BA690-47506 and BA690-47804. b) Self illuminated and electrical signs: BA690-47805 and BA690-47806.
Note: Drawings noted above are for basic type certification only. For as delivered aircraft configuration, refer to CL-690-XXXXX or RAL-BA690-XXXXX. (XXXXX denotes aircraft serial number).
4.
JAA approved Airworthiness limitations for mandatory compliance retirement life or inspection and Certification Maintenance Requirements (CMRs) are found in the Maintenance Requirements Manual, CSP B-053 -Part II
5.
15001 and subsequent serial number aircraft can be either CL-600-2D15 or CL-600-2D24 depending on the interior configuration
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 5: CL-600-2D24 (Regional Jet Series 900)
I. General
1. Aeroplane: Regional Jet Series 900
II. Certification Basis
1.
Reference Application Date for TCCA Certification: 01 November 1999
2.
TCCA Certification Date: 09 September 2002
3.
EASA (JAA) Validation Application Date: 01 November 1999
4.
EASA Certification Date 18 December 2002
(Date of first TC issuance within EU MS by ENAC Italy)
5.
TCCA Certification Basis:
Refer to TCCA Type Certificate Data Sheet No: A-131
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本文链接地址：European Aviation Safety Agency TYPE-CERTIFICATE DATA SHEET CL-600(14)
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