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limit has not been exceeded. The system’s defect must be rectified prior to the next flight, and
the gear assembly, wheels, brakes and tires visually inspected for damage.
D. Fusible Plug Release
If a fusible plug releases, the affected wheel, brakes and anti-skid wheel speed sensors must
be inspected in accordance with the procedures outlined in the Airplane Maintenance Manual,
PSP 604–2, and any damage rectified before the next flight.
PERFORMANCE
Turn−Around Time
06−08−1
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
1. COOLING OF WHEELS, BRAKES AND TIRES (CONT'D)
E. Brake Cooling Time
(1) CALCULATION OF LANDING BRAKE ENERGY
Associated Conditions:
Airplane gross weight = 16,500 kg (36,376 lb)
Braking speed = 130 KIAS
Airport pressure altitude = 5,000 feet
Ambient temperature = 40°C
Runway slope = +1%
Wind = 20 knots, headwind
Flaps setting = 45°
The example in Figure 06−08−1 shows that for the above associated conditions, the
landing brake energy (A) is 27.5 × 106 ft. lb.
(2) CALCULATION OF REQUIRED RTO BRAKE ENERGY
Associated Conditions:
Airplane gross weight = 14,500 kg (31,967 lb)
V1 = 130 KIAS
Airport pressure altitude = 5,000 feet
Ambient temperature = 40°C
Runway slope = +1%
Wind = 20 knots, headwind
Flaps setting = 20°
The example in Figure 06−08−2 shows that for the above associated conditions, the
required RTO brake energy (B) is 31.2 × 106 ft. lb.
(3) CALCULATION OF BRAKE COOLING TIME
Using the values derived from Figure 06−08−1 (A) and Figure 06−08−2 (B),
Figure 06−08−3 shows that the minimum brake cooling time required for a turn-around
under these conditions is 9.0 minutes (C).
PERFORMANCE
Turn−Around Time
06−08−2
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
1. COOLING OF WHEELS, BRAKES AND TIRES (CONT'D)
DFM0608_001 604brk_cooling_land_ha_jp_apr96.uni
PERFORMANCE
Turn−Around Time
06−08−3
REV 66, Feb 01/07
Landing Brake Energy, Flaps 45°
Figure 06−08−1
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
1. COOLING OF WHEELS, BRAKES AND TIRES (CONT'D)
DFM0608_002 604brk_cooling_rto_ha_jp_apr96.uni
PERFORMANCE
Turn−Around Time
06−08−4
REV 66, Feb 01/07
Rejected Take-Off Brake Energy, Flaps 20°
Figure 06−08−2
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
1. COOLING OF WHEELS, BRAKES AND TIRES (CONT'D)
DFM0608_003 604brk_cooling_time_nw_06sept95.uni
ALL COOLING TIMES IN MINUTES
PERFORMANCE
Turn−Around Time
06−08−5
REV 66, Feb 01/07
Mainwheel Brake Cooling Time
Figure 06−08−3
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
PERFORMANCE
Turn−Around Time
06−08−6
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
THIS PAGE INTENTIONALLY LEFT BLANK
TABLE OF CONTENTS
PAGE
SUPPLEMENT 1 − NOISE CHARACTERISTICS 07−01−01−1
SUPPLEMENT 2 − OPERATION ON WET AND CONTAMINATED
RUNWAYS
07−02−01−1
SUPPLEMENT 3 − OPERATION AT AIRPORT ELEVATIONS UP TO
14,000 FEET
07−03−01−1
SUPPLEMENT 4 − CATEGORY II OPERATIONS 07−04−01−1
SUPPLEMENT 4A − CATEGORY II OPERATIONS
(AIRPLANES ON THE GERMAN REGISTRY)
07−04A−01−1
SUPPLEMENT 4B − CATEGORY II OPERATIONS
(AIRPLANES ON THE CAA (UK) REGISTRY)
07−04B−01−1
SUPPLEMENT 5 − AIRWORTHINESS FLIGHT TEST / CREW TRAINING
(AIRPLANES ON THE CAA (UK) REGISTRY)
07−05−01−1
SUPPLEMENT 5A − AIRWORTHINESS FLIGHT TEST / CREW TRAINING
(AIRPLANES ON THE HKCAD REGISTRY)
07−05A−01−1
SUPPLEMENT 6 − FLIGHT WITH LANDING GEAR DOWN 07−06−01−1
SUPPLEMENT 7 − FMS NAVIGATION IN POLAR REGIONS 07−07−01−1
SUPPLEMENT 8 − OPERATION WITH AIRPLANE SYSTEMS
INOPERATIVE
07−08−01−1
SUPPLEMENT 9 − ANGLE OF ATTACK (AOA) VANE TRANSDUCERS 07−09−01−1
SUPPLEMENT 10 − OPERATIONS FOR AIRPLANES ON CAA (UK)
REGISTRY
07−10−01−1
　
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