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SUPPLEMENT 8
Operation With Airplane Systems Inoperative
07−08−01−3
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
7. PERFORMANCE (CONT'D)
DFM0708_001 WTBE604BB_HA−17/09/02
SUPPLEMENT 8
Operation With Airplane Systems Inoperative
07−08−01−4
REV 66, Feb 01/07
Take-Off Weight Limited By Brake Energy − Anti-Skid Inoperative
Figure 07−08−1
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
7. PERFORMANCE (CONT'D)
F. Hydraulic AC Motor Pump Inoperative
(1) THRUST SETTINGS
All take-off performance must be calculated with APR selected OFF.
When dispatching with one hydraulic AC motor pump inoperative, determine the normal
take-off thrust setting then apply the ΔN1 correction for the dispatched bleed configuration
as shown on Figure 07−08−2 to Figure 07−08−5.
Any readjustment to the thrust setting during the take-off climb must be adjusted by the
appropriate ΔN1 correction.
For approach climb, determine the thrust setting using the normal take-off thrust setting
charts and then apply the appropriate ΔN1 correction.
DFM0708_002
N1 Corrections − Engine Bleeds Closed
Figure 07−08−2
SUPPLEMENT 8
Operation With Airplane Systems Inoperative
07−08−01−5
REV 71, Oct 31/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
7. PERFORMANCE (CONT'D)
DFM0708_003
SUPPLEMENT 8
Operation With Airplane Systems Inoperative
07−08−01−6
REV 71, Oct 31/07
N1 Corrections − Packs On
Figure 07−08−3
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
7. PERFORMANCE (CONT'D)
DFM0708_004
SUPPLEMENT 8
Operation With Airplane Systems Inoperative
07−08−01−7
REV 71, Oct 31/07
N1 Corrections − Packs OFF, Cowl Anti-Icing On
Figure 07−08−4
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
7. PERFORMANCE (CONT'D)
DFM0708_005
SUPPLEMENT 8
Operation With Airplane Systems Inoperative
07−08−01−8
REV 71, Oct 31/07
N1 Corrections − Packs OFF, Cowl and Wing Anti-Icing On
Figure 07−08−5
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
7. PERFORMANCE (CONT'D)
(2) TAKE-OFF PERFORMANCE
(a) Take-Off Weight Limited By Climb Requirements
The maximum take-off weight limited by climb requirements when dispatching with
one hydraulic AC motor pump inoperative is determined from Figure 07−08−6.
Example: ANTI-ICE ON
Associated Conditions:
Temperature = –8°C
Airport pressure altitude = 6,000 ft
Cowl anti-ice = On
10th stage bleeds = Closed
APR = Off
As shown in the example (Figure 07−08−6, Anti-ice On), the maximum take-off weight
limited by climb requirements is 21,250 kg (46,848 lb).
Example: ANTI-ICE OFF
Associated Conditions:
Temperature = 27°C
Airport pressure altitude = 6,000 ft
Wing and cowl anti-ice = Off
10th stage bleeds = Closed
APR = Off
As shown in the example (Figure 07−08−6, Anti-ice Off), the maximum take-off weight
limited by climb requirements is 20,750 kg (45,746 lb).
SUPPLEMENT 8
Operation With Airplane Systems Inoperative
07−08−01−9
REV 71, Oct 31/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
7. PERFORMANCE (CONT'D)
DFM0708_006
SUPPLEMENT 8
Operation With Airplane Systems Inoperative
07−08−01−10
REV 71, Oct 31/07
Take-Off Weight Limited by Climb Requirements
Figure 07−08−6
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
7. PERFORMANCE (CONT'D)
(b) Take-Off Weight Limited By Brake Energy
When dispatching with hydraulic AC motor pump 2B inoperative, the maximum
take-off weight limited by brake energy can be conservatively determined using
Figure 07−08−1.
(c) Take-Off Distance
When dispatching with hydraulic AC motor pump 1B inoperative:
Take-off distance Multiply by a factor of 1.3 (30%)
When dispatching with hydraulic AC motor pump 2B inoperative:
Take-off distance Multiply by a factor of 1.6 (60%)
SUPPLEMENT 8
Operation With Airplane Systems Inoperative
07−08−01−11
REV 71, Oct 31/07
DOT Approved
　
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