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Vol. 1 06−24−7
REV 71, Oct 31/07
Take-Off Weight Limited By Brake Energy – Anti-Skid Inoperative
Figure 06−24−2
CL−604 Operating Manual
PSP 604−6
8. 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 06−24−3 to Figure 06−24−6.
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 06−24−3
SUPPLEMENTARY PROCEDURES
Operation with Systems Inoperative
Vol. 1 06−24−8
REV 71, Oct 31/07
CL−604 Operating Manual
PSP 604−6
8. PERFORMANCE (CONT'D)
DFM0708_003
SUPPLEMENTARY PROCEDURES
Operation with Systems Inoperative
Vol. 1 06−24−9
REV 71, Oct 31/07
N1 Corrections − Packs On
Figure 06−24−4
CL−604 Operating Manual
PSP 604−6
8. PERFORMANCE (CONT'D)
DFM0708_004
SUPPLEMENTARY PROCEDURES
Operation with Systems Inoperative
Vol. 1 06−24−10
REV 71, Oct 31/07
N1 Corrections − Packs OFF, Cowl Anti-Icing On
Figure 06−24−5
CL−604 Operating Manual
PSP 604−6
8. PERFORMANCE (CONT'D)
DFM0708_005
SUPPLEMENTARY PROCEDURES
Operation with Systems Inoperative
Vol. 1 06−24−11
REV 71, Oct 31/07
N1 Corrections − Packs OFF, Cowl and Wing Anti-Icing On
Figure 06−24−6
CL−604 Operating Manual
PSP 604−6
8. 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 06−24−7.
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 06−24−7, 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 06−24−7, Anti-ice Off), the maximum take-off weight
limited by climb requirements is 20,750 kg (45,746 lb).
SUPPLEMENTARY PROCEDURES
Operation with Systems Inoperative
Vol. 1 06−24−12
REV 71, Oct 31/07
CL−604 Operating Manual
PSP 604−6
8. PERFORMANCE (CONT'D)
DFM0708_006
SUPPLEMENTARY PROCEDURES
Operation with Systems Inoperative
Vol. 1 06−24−13
REV 71, Oct 31/07
Take-Off Weight Limited by Climb Requirements
Figure 06−24−7
CL−604 Operating Manual
PSP 604−6
8. 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 06−24−2.
(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%)
SUPPLEMENTARY PROCEDURES
Operation with Systems Inoperative
Vol. 1 06−24−14
REV 71, Oct 31/07
CL−604 Operating Manual
PSP 604−6
8. PERFORMANCE (CONT'D)
(d) Take-Off Speeds
When dispatching with one hydraulic AC motor pump inoperative, and operating at or
below 4,000 feet pressure altitude, apply VR and V2 corrections as shown on
Figure 06−24−8 and Figure 06−24−9 respectively.
For V1, when dispatching with hydraulic AC motor pump 2B inoperative, use the
highest V1MCG or multiply the VR from Figure 06−24−8 by a factor of 0.86 (–16%).
　
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