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Landing Climb Gradient Corrections
Figure 07−08−12
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
7. PERFORMANCE (CONT'D)
(5) LANDING PERFORMANCE
The maximum landing weight limited by climb requirements when dispatching with one
hydraulic AC motor pump inoperative is determined from Figure 07−08−13.
Example: ANTI-ICE ON
Associated Conditions:
Temperature = –8°C
Airport pressure altitude = 6,000 ft
Wing and cowl anti-ice = On
10th stage bleeds = Closed
As shown in the example (Figure 07−08−13, Anti-ice On), the maximum landing weight
limited by climb requirements is 21,800 kg (48,061 lb).
Example: ANTI-ICE OFF
Associated Conditions:
Temperature = 27°C
Airport pressure altitude = 4,000 ft
Wing and cowl anti-ice = Off
10th stage bleeds = Closed
As shown in the example (Figure 07−08−13, Anti-ice Off), the maximum landing weight
limited by climb requirements is 23,000 kg (50,706 lb).
SUPPLEMENT 8
Operation With Airplane Systems Inoperative
07−08−01−18
REV 71, Oct 31/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
7. PERFORMANCE (CONT'D)
DFM0708_013
SUPPLEMENT 8
Operation With Airplane Systems Inoperative
07−08−01−19
REV 71, Oct 31/07
Landing Weight Limited by Climb Requirements
Figure 07−08−13
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
8. SUPPLEMENTS
The supplements in Chapter 7 are applicable, except as modified by the following:
A. Supplement 2 − Operation on Wet and Contaminated Runways
(1) LIMITATIONS
Operation on contaminated runways with hydraulic AC motor pump 2B inoperative is
prohibited.
(2) 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 2.0 (100%)
(3) 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 07−08−7 and Figure 07−08−8 respectively.
For V1, when dispatching with hydraulic AC motor pump 2B inoperative, use the highest
V1MCG or multiply the VR from Figure 07−08−7 by a factor of 0.86 (–16%).
SUPPLEMENT 8
Operation With Airplane Systems Inoperative
07−08−01−20
REV 71, Oct 31/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
8. SUPPLEMENTS (CONT'D)
B. Supplement 4A − Category II Operations (Airplanes on the German Registry)
The maximum landing weight limited by climb requirements when dispatching with one
hydraulic AC motor pump inoperative is determined from Figure 07−08−14.
C. Supplement 4B − Category II Operations (Airplanes on the CAA (UK) Registry)
The maximum landing weight limited by climb requirements when dispatching with one
hydraulic AC motor pump inoperative is determined from Figure 07−08−14.
Example: ANTI-ICE ON
Associated Conditions:
Temperature = –8°C
Airport pressure altitude = 6,000 ft
Wing and cowl anti-ice = On
10th stage bleeds = Closed
As shown in the example (Figure 07−08−14, Anti-ice On), the maximum landing weight
limited by climb requirements is 21,100 kg (46,518 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
As shown in the example (Figure 07−08−14, Anti-ice Off), the maximum landing weight
limited by climb requirements is 20,600 kg (45,415 lb).
SUPPLEMENT 8
Operation With Airplane Systems Inoperative
07−08−01−21
REV 71, Oct 31/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
8. SUPPLEMENTS (CONT'D)
DFM0708_014
SUPPLEMENT 8
Operation With Airplane Systems Inoperative
07−08−01−22
REV 71, Oct 31/07
Landing Weight Limited by Climb Requirements − Category II Operations
Figure 07−08−14
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
8. SUPPLEMENTS (CONT'D)
D. Supplement 5 − Airworthiness Flight Test/Crew Training (Airplanes on the CAA (UK)
Registry)
When dispatching with one hydraulic AC motor pump inoperative, airworthiness flight
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