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SUPPLEMENTARY PROCEDURES
Steep Approaches up to 5.5 Degrees
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8. PERFORMANCE (CONT'D)
DFM0712_001 LFL605_SAL_JCR_FEB07
SUPPLEMENTARY PROCEDURES
Steep Approaches up to 5.5 Degrees
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Landing Field Length and Landing Speed, Flaps 45
Figure 06−26−2
CL−604 Operating Manual
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8. PERFORMANCE (CONT'D)
(2) ADDITIONAL LANDING INFORMATION
The distance from the visual glide path system runway position to full stop for varying
conditions of airplane landing weight, airport pressure altitude and wind is provided by
Figure 06−26−3. This is the minimum stopping distance achievable on a dry runway past
the intersection of the approach path and the runway surface. It is derived from an
approach to landing glideslope of 5.5 degrees maintained to a threshold crossing height
of 50 feet, a firm touchdown and maximum braking.
This distance is provided to cater for runway variability in position of the visual glide path
systems and threshold crossing heights.
The most limiting distance from Figure 06−26−2 or Figure 06−26−3 is to be used.
Example:
Associated Conditions:
Landing gross weight = 15,000 kg (33,069 lb)
Airport pressure altitude = 4,000 feet
Wind = 20 knots, headwind
The example in Figure 06−26−3, shows that for the above conditions, the distance from
glide path system position to full stop is 540 meters (1,772 feet).
SUPPLEMENTARY PROCEDURES
Steep Approaches up to 5.5 Degrees
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8. PERFORMANCE (CONT'D)
DFM0712_002 LFL605_SAL_GS2STOP_MOD_JCR_FEB07
SUPPLEMENTARY PROCEDURES
Steep Approaches up to 5.5 Degrees
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REV 70, Jun 08/07
Distance from Glideslope System Position on Runway to Full Stop
Figure 06−26−3
CL−604 Operating Manual
PSP 604−6
SUPPLEMENTARY PROCEDURES
Steep Approaches up to 5.5 Degrees
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INTRODUCTION
General 07−01−1
PERFORMANCE
Table of Contents
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1. GENERAL
The Challenger 604 airplane performance data and information is found in the Airplane Flight
Manual.
PERFORMANCE
Introduction
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CHAPTER 8 - SPECIAL OPERATIONS
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INTRODUCTION 08−01−00−1
OPERATION ON WET AND CONTAMINATED RUNWAYS 08−02−00−1
SPECIAL OPERATIONS
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1. GENERAL
The operating procedures outlined in this chapter are particular to the CL–604 airplane. These
special operations are not routinely performed on every flight, and are done only on an “as
required” basis, in order to cope with minor system irregularities and abnormal flight conditions, to
ensure the safe continued operation of the airplane.
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