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50
35
30
25
15 20
A/C WEIGHT (lb)
THOUSANDS
MAX RAMP WEIGHT (48300 lb/21909 kg)
16.0%
45
40
21.0% 29.0% 38.0%
TAKE−OFF LIMIT
44750 lb/20298 kg
M.T.O.W
(48200 lb/21863 kg)
39500 lb/17917 kg
M.L.W. (38000 lb/17237 kg)
MIN FLIGHT WEIGHT (26000lb/11794 kg)
M.Z.F.W. (32000 lb/14515 kg)
43000 lb/19505 kg
28.0% @ 47700 lb/21637 kg)
For aircraft CG in this
zone, use Alternative
AUX/TAIL
Fuel Distribution
(Figure 02−05−2,
Detail C).
Centre of Gravity Limits (MTOW 48,200 lb)
Figure 02−03−1
LIMITATIONS
Centre of Gravity
02−03−1
REV 74, Nov 07/08
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
1. CENTRE OF GRAVITY LIMITS (MTOW 48,200 LB) (CONT'D)
On airplanes 5301 to 5547, 5549 and 5550 NOT incorporating Service Bulletin 604–28–007
and airplanes 5301 to 5571 NOT incorporating Service Bulletin 604–27–009 or
604–27–012:
The maximum permissible centre of gravity (CG) limits are as shown in Figure 02−03−2.
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.).
25 30 35 40
12
14
16
18
20
22
A/C CG % MAC
A/C WEIGHT (kg)
DFM0203_007 THOUSANDS
16.0%
50
45
40
35
30
25
15 20
A/C WEIGHT (lb)
THOUSANDS
MAX RAMP WEIGHT (48300 lb/21909 kg)
21.0% 29.0% 34.5%
TAKE−OFF LIMIT
44750 lb/20298 kg
MIN FLIGHT WEIGHT (26000lb/11794 kg)
M.T.O.W
(48200 lb/21863 kg)
28.0% @ 47700 lb/21637 kg)
39500 lb/17917 kg
M.L.W. (38000 lb/17237 kg)
M.Z.F.W. (32000 lb/14515 kg) For aircraft CG in this
zone, use Alternative
AUX/TAIL
Fuel Distribution
(Figure 02−05−2,
Detail C).
Centre of Gravity Limits (MTOW 48,200 lb)
Airplanes 5301 to 5547, 5549 and 5550 NOT incorporating Service Bulletin 604−28−007 and
airplanes 5301 to 5571 NOT incorporating Service Bulletin 604−27−009 or 604−27−012
Figure 02−03−2
LIMITATIONS
Centre of Gravity
02−03−2
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
(Airplanes 5301, 5303 to 5639 NOT Incorporating Service Bulletin 604–11–001)
2. CENTRE OF GRAVITY LIMITS (MTOW 47,600 LB)
The maximum permissible centre of gravity (CG) limits are as shown in Figure 02−03−3.
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.
40
12
14
16
18
A/C CG % MAC
A/C WEIGHT (kg)
DFM0203_006 THOUSANDS
20
22
MAX RAMP WEIGHT (47700 lb/21637 kg)
50
25
15
A/C WEIGHT (lb)
THOUSANDS
30
20 25 30 35
28.0%
M.T.O.W
(47600 lb/21591 kg)
20.0%
16.0% 39500 lb/17917 kg
40
45
TAKE−OFF LIMIT
44750 lb/20298 kg
35
38.0%
M.Z.F.W. (32000 lb/14515 kg)
M.L.W. (38000 lb/17237 kg)
(43000 lb/19505 kg)
MIN FLIGHT WEIGHT (26000lb/11794 kg)
For aircraft CG in this
zone, use Alternative
AUX/TAIL
Fuel Distribution
(Figure 02−05−2,
Detail C).
Centre of Gravity Limits (MTOW 47,600 lb)
Figure 02−03−3
LIMITATIONS
Centre of Gravity
02−03−3
REV 74, Nov 07/08
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
2. CENTRE OF GRAVITY LIMITS (MTOW 47,600 LB) (CONT'D)
On airplanes 5301 to 5547, 5549 and 5550 NOT incorporating Service Bulletin
604–28–007 and airplanes 5301 to 5571 NOT incorporating Service Bulletin 604–27–009
or 604–27–012:
The maximum permissible centre of gravity (CG) limits are as shown in Figure 02−03−4.
The airplane including interior payload, passengers and fuel (refer to Figure 02–05–2) must
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庞巴迪挑战者604飞机飞行手册CL604 Airplane Flight Manual 1(44)
