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pilot action is required.
6. ABNORMAL PROCEDURES
The abnormal procedures in Chapter 5 are applicable.
7. PERFORMANCE
The performance data in Chapter 6 of the Airplane Flight Manual is applicable.
SUPPLEMENTARY PROCEDURES
FMS Navigation in Polar Regions
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PSP 604−6
SUPPLEMENTARY PROCEDURES
FMS Navigation in Polar Regions
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PSP 604−6
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1. GENERAL
These supplementary procedures must be used when operating the airplane with fixed landing
gear down.
These data complement or supersede data contained in the basic Operating Manual. These
supplementary procedures must therefore be used in conjunction with the basic Operating
Manual.
These supplementary procedures are applicable only when used in conjunction with a Minimum
Equipment List approved by the appropriate authority.
The effect of these supplementary procedures on the basic Operating Manual is given below.
2. INTRODUCTION
The general information in Chapter 1 is applicable.
3. OPERATING LIMITATIONS
The operating limitations in Chapter 2 are applicable, except as modified by the following:
• Airspeed must not exceed VLE (250 KIAS).
• Flight altitude above 20,000 ft is prohibited.
• Flight in known or anticipated icing conditions is not permitted.
4. EMERGENCY PROCEDURES
The emergency procedures in Chapter 3 are applicable.
5. NORMAL PROCEDURES
The normal procedures in Chapter 4 are applicable.
6. ABNORMAL PROCEDURES
The abnormal procedures in Chapter 5 are applicable.
SUPPLEMENTARY PROCEDURES
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PSP 604−6
7. PERFORMANCE
The performance data in Chapter 6 of the Airplane Flight Manual are applicable, except as
modified by the following:
A. Take-Off Performance
The take-off speeds (V1, VR, and V2) must be increased by 2 knots. The field length limited
take-off weight must be reduced by 2%. For a given take-off weight, the take-off field length
must be increased by 4%. The take-off weight limited by tire speed must be reduced by 4%.
The take-off weight limited by maximum brake energy must be reduced by 2%.
B. Weight Altitude Temperature Limits
The following penalty must be applied to the performance data as a weight decrement:
FLIGHT SEGMENT WEIGHT DECREMENT (%)
Take-off – Flaps 20° 16%
Landing – Approach Flaps 20°
– Landing Flaps 45° 13%
The take-off weight is limited by the second segment climb gradient requirement (2.4% gross
gradient – one engine inoperative). In landing, the limiting requirement is the approach climb
gradient (2.1% gross gradient, one engine inoperative).
C. Climb Gradients and Climb Speeds
The following gradient penalty must be subtracted from the climb gradient data:
CLIMB GRADIENT GRADIENT PENALTY (%)
Obstacle Clearance Reference Climb Gradient (Flaps 20°) 2.4%
Final Segment/Enroute (Flaps 0°) 3.3%
Approach (Flaps 20°) 2.4%
Landing (Flaps 45°) Not applicable
The approach climb speed in the flaps 20° configuration must be increased by 2 knots.
D. Operational Performance
The effect of landing gear down on operational performance is presented as follows. Enroute
climb ceiling, fuel reserve, block fuel and block time charts are included as well as a table for
long range cruise speed.
SUPPLEMENTARY PROCEDURES
Flight With Landing Gear Down
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7. PERFORMANCE (CONT'D)
DFO1_0622_001 ceil240_all.uni
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Enroute Climb Ceiling
Figure 06−22−1
CL−604 Operating Manual
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7. PERFORMANCE (CONT'D)
DFO1_0622_002 reserve_all.uni
SUPPLEMENTARY PROCEDURES
Flight With Landing Gear Down
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NBAA/IFR Reserve Fuel vs ZFW
Figure 06−22−2
CL−604 Operating Manual
PSP 604−6
7. PERFORMANCE (CONT'D)
DFO1_0622_003 block_fuel_all.uni
SUPPLEMENTARY PROCEDURES
Flight With Landing Gear Down
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Block Fuel vs Range
Figure 06−22−3
CL−604 Operating Manual
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