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Figure 02−06−1 Maximum Operating Speed and Mach Number 02−06−2
Figure 02−06−2 Design Maneuvering Speeds 02−06−3


CL-604 Airplane Flight Manual
PSP 604−1
DOT Approved
REV 59, Jan 30/06
LIMITATIONS
Introduction
02–01–1
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 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:

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 Canadair 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.
15/05/95
CL-604 Airplane Flight Manual
PSP 604–1
DOT Approved
REV 52, Jan 16/04
LIMITATIONS
Introduction
02–01–2
THIS PAGE INTENTIONALLY LEFT BLANK
15/05/95
CL-604 Airplane Flight Manual
PSP 604–1
DOT Approved
Sep 20/95
LIMITATIONS
Structural Weight
02−02−1
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 − OPERATIONS
AT AIRPORT ELEVATIONS UP TO 14,000 FEET).
On airplanes 5301 to 5639 NOT incorporating Canadair 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 − OPERATIONS
AT AIRPORT ELEVATIONS UP TO 14,000 FEET).


CL-604 Airplane Flight Manual
PSP 604−1
DOT Approved
REV 58, Dec 05/05
LIMITATIONS
Structural Weight
02–02–2
THIS PAGE INTENTIONALLY LEFT BLANK
15/05/95
CL-604 Airplane Flight Manual
PSP 604–1
DOT Approved
Sep 20/95
LIMITATIONS
Centre of Gravity
02−03−1
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 Figure 04−10−1.


CL-604 Airplane Flight Manual
PSP 604−1
DOT Approved
REV 58, Dec 05/05





     







 







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