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5. ABNORMAL PROCEDURES
The abnormal procedures in Chapter 5 are applicable, except as modified by the following:
A. Flaps Failure
Operation at high airport elevations increases the probability of exceeding the maximum tire
speed. The landing weight resulting in a touchdown speed equal to the tire speed of 182
knots ground speed, for varying conditions of airport pressure altitude, temperature and wind
is shown for the following flap configurations. Landings exceeding the weights derived will
result in a tire speed greater than 182 knots ground speed at touchdown.
FLAPS 0°
Associated Conditions:
Temperature = 0°C
Airport pressure altitude = 10,000 ft
Wind = 10 knots, headwind
The example in Figure 06−19−3 shows that for the above associated conditions, the landing
weight limited by tire speed of 182 knots ground speed with flaps 0° is 16,200 kg (35,715 lb).
SUPPLEMENTARY PROCEDURES
Operation at High Airport Elevations
Vol. 1 06−19−5
REV 66, Feb 01/07
CL−604 Operating Manual
PSP 604−6
5. ABNORMAL PROCEDURES (CONT'D)
DFM0703_003 TIRELIM_LAND_F0_HA_JP_5JUL96
APPROACH SPEED = VR E F + 30 KIAS
SUPPLEMENTARY PROCEDURES
Operation at High Airport Elevations
Vol. 1 06−19−6
REV 66, Feb 01/07
Landing Weight Limited by Maximum Tire Speed, Flaps 0°
Figure 06−19−3
CL−604 Operating Manual
PSP 604−6
5. ABNORMAL PROCEDURES (CONT'D)
FLAPS 20°
Associated Conditions:
Temperature = 0°C
Airport pressure altitude = 12,000 ft
Wind = 10 knots, headwind
The example in Figure 06−19−4 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).
SUPPLEMENTARY PROCEDURES
Operation at High Airport Elevations
Vol. 1 06−19−7
REV 66, Feb 01/07
CL−604 Operating Manual
PSP 604−6
5. ABNORMAL PROCEDURES (CONT'D)
DFM0703_004 TIRELIM_LAND_F20_HA_JP_5JUL96
APPROACH SPEED = VR E F + 14 KIAS
SUPPLEMENTARY PROCEDURES
Operation at High Airport Elevations
Vol. 1 06−19−8
REV 66, Feb 01/07
Landing Weight Limited by Maximum Tire Speed, Flaps 20°
Figure 06−19−4
CL−604 Operating Manual
PSP 604−6
5. ABNORMAL PROCEDURES (CONT'D)
FLAPS 30°
Associated Conditions:
Temperature = 0°C
Airport pressure altitude = 13,000 ft
Wind = 10 knots, headwind
The example in Figure 06−19−5 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).
SUPPLEMENTARY PROCEDURES
Operation at High Airport Elevations
Vol. 1 06−19−9
REV 66, Feb 01/07
CL−604 Operating Manual
PSP 604−6
5. ABNORMAL PROCEDURES (CONT'D)
DFM0703_005 TIRELIM_LAND_F30_HA_JP_5JUL96
APPROACH SPEED = VR E F + 7 KIAS
SUPPLEMENTARY PROCEDURES
Operation at High Airport Elevations
Vol. 1 06−19−10
REV 66, Feb 01/07
Landing Weight Limited by Maximum Tire Speed, Flaps 30°
Figure 06−19−5
CL−604 Operating Manual
PSP 604−6
6. PERFORMANCE
The performance data in Chapter 6 of the Airplane Flight Manual are applicable.
SUPPLEMENTARY PROCEDURES
Operation at High Airport Elevations
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REV 66, Feb 01/07
CL−604 Operating Manual
PSP 604−6
SUPPLEMENTARY PROCEDURES
Operation at High Airport Elevations
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REV 66, Feb 01/07
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PSP 604−6
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NOTE
These supplementary procedures are only applicable to airplanes
5442 and 5467, on the CAA (UK) Registry.
1. GENERAL
These supplementary procedures must be used when conducting Airworthiness Flight Tests or
Crew Training Operations.
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.
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.
4. EMERGENCY PROCEDURES
The emergency procedures in Chapter 3 are applicable.
5. NORMAL PROCEDURES
The normal procedures in Chapter 4 are applicable, in addition to the following:
　
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