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APU Limits: ***
Maximum RPM: 106%
Maximum EGT: °C °F
Starting* 692-1038 1274-1900
Running–Ground ** 789 1452
Running-Flight** 806 1482
* Dependant upon altitude and temperature (refer to AFM)
** Not to be exceeded under any operating conditions
*** Refer to AFM (CSP C-012) for detail limitations
14.
Equipment
The basic required equipment as prescribed in the applicable airworthiness regulations (see Certification Basis) and defined in the Type Certificate Type Design Definition, (see RAZ-BA690-120) must be installed in the airplane for certification.
15.
15. Interior Installations Cabin interior and seating configurations must be approved.
16.
All Weather Capabilities Coupled Autopilot: CAT II
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 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 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.
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本文链接地址:European Aviation Safety Agency TYPE-CERTIFICATE DATA SHEET CL-600(18)
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