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Max. Taxi and ramp 33,113 kg (73,000 lb.) 34,133 kg (75,250 lb.)
Max. Take-off 32,999 kg (72,750 lb.) 34,019 kg (75,000 lb.)
Max. Landing 30,391 kg (67,000 lb.) 30,391 kg (67,000 lb.)
Max. Zero fuel 28,260 kg (62,300 lb.) 28,260 kg (62,300 lb.)
NOTE: See AFM (CSP B-012) for other weight limitations and aircraft eligibility.
8.
Minimum Flight Crew Two: Pilot and Co-pilot
9.
Maximum Seating Capacity
Maximum Passenger Seating Capacity: Series 700 – 68 or fewer passengers Series 701 – 70 passengers Series 702 – 78 passengers
10.
Cargo compartment loading
11.
Environmental Flight Envelope Refer to approved Airplane Flight Manual.
12.
Other Limitations Refer to approved Airplane Flight Manual.
13.
Auxiliary Power Unit (APU)
Class Volume (m3) Max. Allowable Load (Kg)
C 10.60 1696
C 2.63 436
Honeywell (formerly Allied Signal) RE-220 RJ.
Approved to TSO C-77A and JAR-APU Change 2.
APU Limits: ***
Maximum RPM 106%
Maximum EGT for Starting * 1038oC** 1900oF**
Maximum EGT Operating Ground* 789°C 1452°F
Maximum EGT Operating in Flight 806oC 1482oF
* Dependent upon Altitude and Temperature or Airspeed
(Refer to AFM CSP B-012 for detail limitations).
** Not to be exceeded under any operating conditions.
*** Refer to AFM (CSP B-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-BA670-120) must be installed in the airplane for certification.
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 B-012 CSP B-013 CSP B-041 CSP AB-044
The Instructions for Continued Airworthiness consist of the following Publications:
Aircraft Maintenance Manual (AMM): CSP B-001
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(9)
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