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
CL-600-2B16 a) Airplane Flight Manual, Canadair Publication (DOT) PSP-601A-1
(601-3A Variant) and subsequent approved issues.
CL-600-2B16 b) Airplane Flight Manual, Canadair Publication (DOT) PSP-601A-
(601-3R Variant) 1-1 and subsequent approved issues. c) Components, which are life limited, are listed in Time Limits/Maintenance Checks, PSP-601A-5.
CL-600-2B16 a) Airplane Flight Manual, Canadair Publication (DOT) PSP-604-1
(604 Variant, and subsequent approved issues.
S/N 5301 to 5699) b) Time Limits/Maintenance Checks Manual, Identification No. CH 604 TLMC, Section 5-10 or later approved revisions which consists of the Damage Tolerance Inspections, Certification Maintenance Requirements, and Life Limited Parts. This information is consistent with Canadair Documents RAS-604-990, RBR-604-167 and RBR-604-300, respectively.
CL-600-2B16 a) Airplane Flight Manual, Canadair Publication (DOT) PSP-605-1
(604 Variant, and later approved revisions.
S/N 5701 & subs) b) Time Limits/Maintenance Checks Manual, Identification No. CH 605 TLMC, section 5-10 or later approved revisions which consists of the Damage tolerance Inspections, Certification Maintenance requirements, and Life Limited Parts. This information is consistent with Canadair Documents RAS-604DX-990, RBR-604-167and RBR-604-300, respectively.
CL-600-1A11, 2A12 (Pre Service Bulletin 601-0568, 2B16 (Up to and include Serial Number 5630 and Pree Service Bulletin 601-0568) Garret GTCP-36-100-E
Honeywell 36-150(CL) (S/N 5631 and subsequent, or post
Service Bulletin 601-0568)
Approved to TSO C-77
APU Limits:
CL-600-1A11 (600) Garrett GTCP 36100E Limits Maximum RPM: 110% Maximum EGT: Running 731°C Starting 974°C Below 60% RPM 870.C Maximum 20 seconds
-- Limits Maximum RPM: 110%
CL-600-2B16
(601-3A Variant)
CL-600-2B16 Honeywell 36-
(601-3R Variant) 150(CL) Maximum EGT: Running 731°C Starting 974°C
CL-600-2B16 (604 Variant) See AFM PSP-604-1 (for S/N 5301 to 5699) & AFM PSP-605-1 (for S/N 5701 & subs) for APU limitations
12.
Equipment
The basic required equipment as prescribed in the applicable airworthiness regulations (see Certification Basis) and defined in the Type Certificate Type Design Definition, (RAL-604-0001) must be installed in the airplane for certification.
13.
Notes
1.
EASA Approved Airplane Flight Manual: The airplane must be operated according to the appropriate EASA Approved Airplane Flight Manual.
2.
This aircraft Type Certificate defines an aircraft that does not include passenger provisions. Carriage of persons in the cabin is permitted when an approved seating arrangement and related required passenger provisions are incorporated in accordance to the Basis of Certification.
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(28)
| 
