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Manual. This Supplement must, therefore, be read in conjunction with the basic Operating
Manual.
The effect of these supplementary procedures on the basic Operating Manual is given below:
2. OPERATING LIMITATIONS
The operating limitations in Chapter 2 are applicable, except as modified by the following:
The maximum landing weight limit is shown in Figure 06−19−1. DFM0703_001 MLW_LIMIT_HA_RC−05SEPT96
Maximum Landing Weight Limit
Figure 06−19−1
SUPPLEMENTARY PROCEDURES
Operation at High Airport Elevations
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REV 66, Feb 01/07
CL−604 Operating Manual
PSP 604−6
2. OPERATING LIMITATIONS (CONT'D)
The maximum altitude and temperature operating limits are shown in Figure 06−19−2.
• Maximum airport pressure altitude for take-off and landing is 14,000 feet.
DFM0703_002
Altitude and Temperature Operating Limits
Figure 06−19−2
3. EMERGENCY PROCEDURES
The emergency procedures in Chapter 3 are applicable.
SUPPLEMENTARY PROCEDURES
Operation at High Airport Elevations
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PSP 604−6
4. NORMAL PROCEDURES
The normal procedures in Chapter 4 are applicable, except as modified by the following:
A. Engine Start
The engine start procedures in the basic FCOM are applicable, in addition to the following:
NOTE
If difficulty is experienced in starting a cold engine using the APU,
due to slow acceleration, start the other engine and perform a
crossbleed start on the affected engine. If required, repeat sequence
to obtain a successful start and perform a crossbleed start for the
opposite engine.
B. Climb/Descent Rate
With air-conditioning packs selected on and cabin pressurization rate set at PIP position, the
minimum time required to climb to 25,000 feet or to descend from 25,000 feet without causing
discomfort to passengers is as follows:
AIRFIELD ELEVATION MINIMUM TIME
14,000 feet 10.0 minutes
13,000 feet 8.4 minutes
12,000 feet 6.7 minutes
11,000 feet 5.0 minutes
10,000 feet 3.4 minutes
NOTE
1. During take-off, the minimum time may be reduced by selecting
a higher cabin pressurization rate.
2. During climb, do not exceed 25,000 feet until cabin pressure
altitude has decreased to 8,000 feet or less.
C. Take-Off
Before take-off:
(1) CABIN PRESSURIZATION, LDG
ALT selector ............................................................. Set the following:
• Destination airfield altitude,
• Desired cabin pressure rate
of change, and
• Barometric pressure.
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Operation at High Airport Elevations
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CL−604 Operating Manual
PSP 604−6
4. NORMAL PROCEDURES (CONT'D)
C. Take-Off (Cont’d)
(2) Oxygen masks......................................................... Don Crew will don oxygen masks
and establish
communications.
NOTE
1. The use of crew oxygen is required in accordance with the applicable
operating regulations.
2. Carry out a high crosswind take-off procedure if there is an audible
engine noise accompanied by engine indication instabilities, when
setting take-off power.
When cabin altitude is below 10,000 feet:
(3) Oxygen masks.................................................. Remove
D. Descent
(1) CABIN PRESSURIZATION, LDG
ALT selector .........................................................Check selected to the following:
• Destination airfield altitude.
• Destination airfield
barometric pressure.
• Desired cabin pressure
descent rate.
Check FAULT lamp out.
E. Landing
NOTE
The cabin altitude indicator will be in the red area when cabin altitude is
above 10,000 feet.
This indication is normal.
When cabin altitude is above 10,000 feet:
(1) Oxygen masks......................................................... Don Crew will don oxygen masks
and establish
communications.
NOTE
The use of crew oxygen is required in accordance with the applicable
operating regulations.
Prior to landing:
(2) Cabin altitude .......................................................Check
Prior to opening passenger door:
(3) Cabin differential pressure ................................. Ensure at zero.
SUPPLEMENTARY PROCEDURES
Operation at High Airport Elevations
Vol. 1 06−19−4
REV 66, Feb 01/07
CL−604 Operating Manual
PSP 604−6
　
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