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DFM0703_003 TIRELIM_LAND_F0_HA_JP_5JUL96
APPROACH SPEED = VR E F + 30 KIAS
SUPPLEMENT 3
Operation at Airport Elevations up to 14,000 ft.
07−03−01−6
REV 66, Feb 01/07
Landing Weight Limited by Maximum Tire Speed, Flaps 0°
Figure 07−03−3
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
6. ABNORMAL PROCEDURES (CONT'D)
Example 2: FIGURE 07-03-4, FLAPS 20° (APPROACH SPEED = VREF + 14 KIAS)
Associated Conditions:
Temperature = 0°C
Airport pressure altitude = 12,000 ft
Wind = 10 knots, headwind
The example in Figure 07−03−4, shows that for the above associated conditions, the landing
weight limited by tire speed of 182 knots ground speed with flaps 20° is 18,300 kg (40,345 lb).
SUPPLEMENT 3
Operation at Airport Elevations up to 14,000 ft.
07−03−01−7
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
6. ABNORMAL PROCEDURES (CONT'D)
DFM0703_004 TIRELIM_LAND_F20_HA_JP_5JUL96
APPROACH SPEED = VR E F + 14 KIAS
SUPPLEMENT 3
Operation at Airport Elevations up to 14,000 ft.
07−03−01−8
REV 66, Feb 01/07
Landing Weight Limited by Maximum Tire Speed, Flaps 20°
Figure 07−03−4
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
6. ABNORMAL PROCEDURES (CONT'D)
Example 3: FIGURE 07-03-5, FLAPS 30° (APPROACH SPEED = VREF + 7 KIAS)
Associated Conditions:
Temperature = 0°C
Airport pressure altitude = 13,000 ft
Wind = 10 knots, headwind
The example in Figure 07−03−5, shows that for the above associated conditions, the landing
weight limited by tire speed of 182 knots ground speed with flaps 30° is 19,000 kg (41,888 lb).
SUPPLEMENT 3
Operation at Airport Elevations up to 14,000 ft.
07−03−01−9
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
6. ABNORMAL PROCEDURES (CONT'D)
DFM0703_005 TIRELIM_LAND_F30_HA_JP_5JUL96
APPROACH SPEED = VR E F + 7 KIAS
SUPPLEMENT 3
Operation at Airport Elevations up to 14,000 ft.
07−03−01−10
REV 66, Feb 01/07
Landing Weight Limited by Maximum Tire Speed, Flaps 30°
Figure 07−03−5
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
7. PERFORMANCE
The performance data in Chapter 6 are applicable.
SUPPLEMENT 3
Operation at Airport Elevations up to 14,000 ft.
07−03−01−11
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
SUPPLEMENT 3
Operation at Airport Elevations up to 14,000 ft.
07−03−01−12
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
THIS PAGE INTENTIONALLY LEFT BLANK
GENERAL 07−04−01−1
INTRODUCTION 07−04−01−1
LIMITATIONS 07−04−01−1
EMERGENCY PROCEDURES 07−04−01−2
Autopilot Failure 07−04−01−2
NORMAL PROCEDURES 07−04−01−3
Prior to Approach 07−04−01−3
Before Landing 07−04−01−3
ABNORMAL PROCEDURES 07−04−01−4
Single Engine Approach and Landing 07−04−01−4
Engine Failure During Final Approach 07−04−01−4
System Failures 07−04−01−5
PERFORMANCE 07−04−01−10
SUPPLEMENT 4
Category II Operations
07−04−00−1
REV 66, Feb 01/07
07−04−00−1
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
TABLE OF CONTENTS
Page
TABLE OF CONTENTS
SUPPLEMENT 4
Category II Operations
07−04−00−2
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
THIS PAGE INTENTIONALLY LEFT BLANK
NOTE
This Airplane Flight Manual Supplement does not constitute
approval to conduct Category II operations.
1. GENERAL
The CL 600–2B16 (CL–604) airplane has been shown to meet the airworthiness requirements for
Category II Operations contained in Appendix 1 of AC 120-29.
The data in this supplement must be used when conducting Category II operations.
These data complement or supersede data contained in the basic Airplane Flight Manual. This
supplement must therefore, be read in conjunction with the basic Airplane Flight Manual.
　
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