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1. GENERAL
The limitations included in this chapter contain items peculiar to the CL600,model 2D24 Regional
Jet airplane. Observance of these limitations is mandatory.
Airplane Flight Manual
CSP C-012 DOT Approved
Sep 09/02
LIMITATIONS
Introduction
02--01--2
2. KINDS OF AIRPLANE OPERATION
The airplane is certified in the transport category for day and night operations, in the following
conditions when the equipment and instruments required by the airworthiness and operating
regulations are approved, installed and in an operable condition:
S VFR and IFR
S Flight in icing conditions
The airplane is certified for ditching when the safety equipment specified by the applicable
regulations is installed.
Effectivity: <1030>
S Airplanes equipped for operation in Reduced Vertical Separation Minimum (RVSM) airspace:
The airplane is certified capable of RVSM operations in accordance with the FAA “Interim
guidance material on the approval of operations/aircraft for RVSM operations.”, 91-RVSM,
dated June 30, 1999 and with the JAA Temporary Guidance Leaflet, TGL No. 6, revision 1,
RVSM.
NOTE
Compliance with the standard noted above does not
constitute an operational approval.
RVSM operations must not be commenced or continued unless all of the required equipment
specified below is operational.
RVSM REQUIRED EQUIPMENT LIST
EQUIPMENT REQUIREMENTS FOR RVSM
AUTOPILOT (1) MUST BE OPERATIONAL.
ALTITUDE ALERTING SYSTEM MUST BE OPERATIONAL.
ALTITUDE REPORTING TRANSPONDER (2) ONE (1) MUST BE OPERATIONAL.
AIR DATA COMPUTERS (2) TWO (2) MUST BE OPERATIONAL.
Airplane Flight Manual
CSP C-012 DOT Approved
REV 2, Feb 24/04
LIMITATIONS
Structural Weight
02--02--1
1. STRUCTURAL WEIGHT LIMITATION
Weight kg lb Option Code
Maximum taxi and
ramp weight 36,613 80,719 <2217>
Maximum take-off
weight (MTOW) 36,500 80,469 <2217>
Maximum landing
weight (MLW) 33,339 73,500
Maximum zero fuel
weight (MZFW) 31,751 70,000
Minimum flight weight 20,412 45,000
NOTE
Themaximum take-off weight (MTOW) and/ormaximum
landing weight (MLW) may be further limited due to
performance considerations.
Airplane Flight Manual
CSP C-012 DOT Approved
REV 3, May 03/05
LIMITATIONS
Structural Weight
02--02--2
THIS PAGE INTENTIONALLY LEFT BLANK
Airplane Flight Manual
CSP C-012 DOT Approved
Sep 09/02
LIMITATIONS
Centre of Gravity
02--03--1
2217
1. CENTRE OF GRAVITY (LIMITS)
The maximum permissible centre of gravity (CG) range with landing gear extended is shown
below. The airplane must be loaded in accordance with the loading instructions associated with
the Weight and Balance Manual (CSP C--041). The effect of landing gear retraction on CG
position is negligible.
20000
21000
22000
23000
24000
25000
26000
27000
28000
29000
30000
31000
32000
33000
34000
35000
36000
37000
38000
39000
5 10 15 20 25 30 35 40
44000
46500
49000
51500
54000
56500
59000
61500
64000
66500
69000
71500
74000
76500
79000
81500
84000
86500
8.6% 10.6% 26.4%
10.6%
28.5%
26.5%
8.0%
10.0%
30.0%
28.0%
29.8%
37.0%
34.0%
35.0%
MAX RAMP WT: 36 613 kg (80,719 lb)
MAX TAKE-OFF WT: 36 500 kg (80,469 lb)
35 153 kg (77,500 lb)
MAX ZERO FUEL WT: 31 751 kg (70,000 lb)
MAX LANDING WT: 33 339 kg (73,500 lb)
27 216 kg (60,000 lb)
21 319 kg (47,000 lb)
MIN FLIGHT WT: 20 412 kg (45,000 lb)
CG (%MAC)
WEIGHT (kg)
WEIGHT (lb)
ENROUTE ONLY
ENROUTE ONLY
Airplane Flight Manual
CSP C-012 DOT Approved
REV 2, Feb 24/04
Centre of Gravity Limits
Figure 02--03--1
LIMITATIONS
Centre of Gravity
02--03--2
THIS PAGE INTENTIONALLY LEFT BLANK
Airplane Flight Manual
CSP C-012 DOT Approved
Sep 09/02
LIMITATIONS
Operating Limitations
02--04--1
1. ALTITUDE AND TEMPERATURE OPERATING LIMITS
Maximum airport pressure altitude for take-off and landing is 8,000 feet.
Maximum operating altitude is 41,000 feet.
Maximum ambient air temperature approved for take-off and landing is ISA + 35°C.
Minimum ambient temperature approved for take-off is --40°C (--40°F).
Altitude and Temperature Operating Limits
Figure 02--04--1
Airplane Flight Manual
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