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LIMITATIONS
Table of Contents
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PSP 604−1
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OPERATING SPEEDS
Figure 02−06−1 Maximum Operating Speed and Mach Number 02−06−1
Figure 02−06−2 Design Maneuvering Speeds 02−06−2
LIMITATIONS
Table of Contents
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CL−604 Airplane Flight Manual
PSP 604−1
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LIMITATIONS
Table of Contents
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CL−604 Airplane Flight Manual
PSP 604−1
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1. GENERAL
The limitations included in this chapter contain items peculiar to the CL600, model 2B16, variant
CL–604 Challenger airplane.
Observance of these limitations is mandatory.
2. KINDS OF AIRPLANE OPERATION
The airplane is certified for 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:
• Day and night
• VFR and IFR
• Flight in icing conditions
The airplane is certified for ditching when the safety equipment specified by the applicable
regulations is installed.
On airplanes incorporating Service Bulletin 604–34–012:
The airplane is certified capable of RVSM operations in accordance with FAA “Interim guidance
material on the approval of operations/aircraft for RVSM operations”, 91–RVSM, dated March
14, 1994.
NOTE
Compliance with the standard noted above does not constitute an
operational approval.
LIMITATIONS
Introduction
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Introduction
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1. STRUCTURAL WEIGHT LIMITATION
Maximum taxi and ramp weight: 21,909 kg (48,300 lb)
Maximum take-off weight: 21,863 kg (48,200 lb)
Maximum landing weight: 17,237 kg (38,000 lb)
Maximum zero fuel weight: 14,515 kg (32,000 lb)
Minimum flight weight: 11,794 kg (26,000 lb)
Minimum operating empty weight: 10,047 kg (22,150 lb)
NOTE
1. The maximum take-off weight (MTOW) and/or maximum landing
weight (MLW) may be further limited due to performance
considerations.
2. The maximum landing weight (MLW) is further limited when landing
at airport elevations above 10,000 feet (Refer to Chapter 7;
SUPPLEMENT 3 – OPERATION AT AIRPORT ELEVATIONS UP
TO 14,000 FEET) .
On airplanes 5301, 5303 to 5639 NOT incorporating Service Bulletin 604–11–001:
Maximum taxi and ramp weight: 21,637 kg (47,700 lb)
Maximum take-off weight: 21,591 kg (47,600 lb)
Maximum landing weight: 17,237 kg (38,000 lb)
Maximum zero fuel weight: 14,515 kg (32,000 lb)
Minimum flight weight: 11,794 kg (26,000 lb)
Minimum operating empty weight: 10,047 kg (22,150 lb)
NOTE
1. The maximum take-off weight (MTOW) and/or maximum landing
weight (MLW) may be further limited due to performance
considerations.
2. The maximum landing weight (MLW) is further limited when
landing at airport elevations above 10,000 feet (Refer to Chapter 7;
SUPPLEMENT 3 – OPERATION AT AIRPORT ELEVATIONS UP
TO 14,000 FEET) .
LIMITATIONS
Structural Weight
02−02−1
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
LIMITATIONS
Structural Weight
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PSP 604−1
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1. CENTRE OF GRAVITY LIMITS (MTOW 48,200 LB)
The maximum permissible centre of gravity (CG) limits are as shown in Figure 02−03−1.
The airplane including interior payload, passengers and fuel (refer to Figure 02–05–2) must be
loaded such that the airplane weight and centre of gravity are maintained within the specified
limits (including variations due to fuel consumption, passenger movement, retraction of landing
gear, etc.).
The stabilizer trim setting must be in accordance with Chapter 4; NORMAL PROCEDURES –
FLIGHT CONTROLS – Before Take-Off.
25 30 35 40
12
14
16
18
20
22
A/C CG % MAC
A/C WEIGHT (kg)
DFM0203_008 THOUSANDS
　
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