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*** Refer to AFM (CSP D-012) for detail limitations
14.
Equipment
The basic required equipment as prescribed in the applicable airworthiness regulations (see Certification Basis) are defined in the Type Certificate Type Design Definition, (see RAZ-BA698-018) must be installed in the airplane for certification.
15.
Interior Installations Cabin interior and seating configurations must be approved.
16.
All Weather Capabilities Reserved
17.
Wheels and Tyres
Tyre Size
Dual Nose Wheel and Tyre 20.5 x 6.75 – 10, 12 ply
Dual Main Wheels and Tyres (L/H & R/H) H36 x 11.5 – 19, 20 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: CSP D-012
Flight Crew Operating Manual: CSP D-013
Weight and Balance Manual: CSP D-041
Minimum Master Equipment List (MMEL): 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 D-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.
EASA Approved Airplane Flight Manual: The airplane must be operated according to the appropriate EASA Approved Airplane Flight Manual.
3.
All placards must be installed in accordance with Drawings:
a) Basic markings and placards: BA670-47850, BA670-47869, BA690-47504, BA690-47518, BA690-47525, BA690-47526, BA690-47528, BA690-47529, BA690-47530, BA698-47203, BA698-47502, BA698-47519, BA698-47800, BA698-47805 and CC698-47251.
b) Self-illuminated and electrical signs: BA690-47805 and BA698-47801.
Note: Drawings noted above are for basic type certification only. For as delivered aircraft configuration, refer to RAL-BA698-19XXX. (19XXX denotes aircraft serial number).
4.
EASA 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.
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).
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本文链接地址：European Aviation Safety Agency TYPE-CERTIFICATE DATA SHEET CL-600(22)
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