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Anti-Icing On
Figure 06−02−4
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
1. THRUST SETTINGS (CONT'D)
D. Single Engine Climb Thrust (APR Rating)
Engine fan speed (N1) settings for various ambient temperatures and pressure altitudes
required to obtain the engine rated automatic performance reserve (APR rating) are shown on
Figure 06−02−5 to Figure 06−02−8.
Example:
The example in page 1 of Figure 06−02−5 shows that for an outside air temperature of
–20°C and at a pressure altitude of 6,000 feet, the single engine climb thrust (APR rating)
with zero engine bleed, will be achieved at 89.3% N1.
PERFORMANCE
Thrust Settings
06−02−10
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
1. THRUST SETTINGS (CONT'D)
DFM0602_007 apr_zero_3b.uni2
PERFORMANCE
Thrust Settings
06−02−11
REV 66, Feb 01/07
Single Engine Climb Thrust (APR Rating) − Zero Engine Bleed (Page 1 of 2)
Figure 06−02−5
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
1. THRUST SETTINGS (CONT'D)
DFM0602_008 apr_zero_3b_2.uni2
PERFORMANCE
Thrust Settings
06−02−12
REV 66, Feb 01/07
Single Engine Climb Thrust (APR Rating) − Zero Engine Bleed (Page 2 of 2)
Figure 06−02−5
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
1. THRUST SETTINGS (CONT'D)
DFM0602_009 apr_acu_3b.uni2
PERFORMANCE
Thrust Settings
06−02−13
REV 66, Feb 01/07
Single Engine Climb Thrust (APR Rating) − 10th Stage Bleed Open/One (1) Pack On (Page 1 of 2)
Figure 06−02−6
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
1. THRUST SETTINGS (CONT'D)
DFM0602_010 apr_acu_3b_2.uni2
PERFORMANCE
Thrust Settings
06−02−14
REV 66, Feb 01/07
Single Engine Climb Thrust (APR Rating) − 10th Stage Bleed Open/One (1) Pack On (Page 2 of 2)
Figure 06−02−6
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
1. THRUST SETTINGS (CONT'D)
DFM0602_011 apr_cowl_3b.uni2
PERFORMANCE
Thrust Settings
06−02−15
REV 66, Feb 01/07
Single Engine Climb Thrust (APR Rating) − 10th Stage Bleeds Closed and Engine Cowl Anti-Icing
On
Figure 06−02−7
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
1. THRUST SETTINGS (CONT'D)
DFM0602_012 apr_wing_3b.uni2
PERFORMANCE
Thrust Settings
06−02−16
REV 66, Feb 01/07
Single Engine Climb Thrust (APR Rating) − 10th Stage Bleeds Closed/Engine Cowl and Wing
Anti-Icing On
Figure 06−02−8
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
1. THRUST SETTINGS (CONT'D)
E. Maximum Continuous Thrust, Single Engine Climb
Engine fan speed (N1) settings for various ambient temperatures and pressure altitudes
required to obtain the engine rated maximum continuous thrust (MCT) for a single engine
climb, with 10th stage bleed open/one (1) pack on, are shown on Figure 06−02−9 to
Figure 06−02−11.
Example:
The example in page 1 of Figure 06−02−9 shows that for an outside air temperature of
–10°C and at a pressure altitude of 8,000 feet, the single engine climb thrust (maximum
continuous thrust rating) with 10th stage bleed open/one (1) pack on, will be achieved at
91.7% N1.
NOTE
1. Maximum continuous thrust (MCT) settings have a discontinuity at
16,000 feet. This discontinuity is due to the assumptions made to
derive MCT settings.
2. At altitudes between 14,000 feet and 16,000 feet, the thrust setting
curve labeled 15,999 feet must be used for interpolation.
3. At altitudes between 16,000 feet and 20,000 feet, the thrust setting
curve labeled 16,000 feet must be used for interpolation.
PERFORMANCE
Thrust Settings
06−02−17
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
1. THRUST SETTINGS (CONT'D)
DFM0602_013 mxct_acu_3b.uni
PERFORMANCE
Thrust Settings
06−02−18
REV 66, Feb 01/07
Maximum Continuous Thrust (Single Engine Climb) − 10th Stage Bleed Open/One Pack On
(Page 1 of 2)
Figure 06−02−9
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
1. THRUST SETTINGS (CONT'D)
　
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