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VA (Manoeuvring) (Refer to Flight Manual for variations of VA with altitude and aircraft weight)
VLO (Landing Gear Operating) Extending Retracting 220 200
VLE (Landing Gear Extended) 220
Max. tyre ground speeds: m.p.h. knots
Nose Gear Tyre 225 195
Main Gear Tyre 225 195
3.38 m (133.18 in.) (MAC leading edge at fuselage station 21.161 m (833.1 in.)
Leveling Means:
The aircraft is leveled in the longitudinal and lateral axis by the means of a plumb bob
and target plate located at fuselage station 2910.2cm (1146.75 inches).
7. Maximum Certified Weights kg (lbs)
Type Spec Option <2005>
Max. Taxi and ramp 36,628 kg (80,750 lb.) 38,555 kg (85,000 lb.)
Max. Take-off 36,514 kg (80,500 lb.) 38,329 kg (84,500 lb.)
Max. Landing 33,339 kg (73,500 lb.) 34,065 kg (75,100 lb.)
Max. Zero fuel 31,751 kg (70,000 lb.) 32,092 kg (70,750 lb.)
NOTE: See AFM (CSP C-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 705 – 75 or fewer 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 12.39 1985
C 4.42 772
Allied Signal RE-220 RJ.
Approved to TSO C-77A and JAR-APU Change 2
Appropriate National Authority Type Certificate and TCDS.
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.
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
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本文链接地址：European Aviation Safety Agency TYPE-CERTIFICATE DATA SHEET CL-600(13)
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