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SUPPLEMENT 9
Angle of Attack (AOA) Vane Transducers
07−09−01−1
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
7. PERFORMANCE
The performance data in Chapter 6 are applicable, except as modified by the following:
A. Take-Off Performance
(1) MAXIMUM ALLOWABLE TAKE-OFF WEIGHT
The maximum allowable take-off weight limited by maximum demonstrated brake energy
is as follows:
Airport Pressure Altitude (ft)
Temp (°C) SL 2000 4000 6000 8000 10000 12000 14000
–40 59950 56471 54266 51841 49196 46550 43684 41038
–15 57794 54551 52286 49853 46967 44345 41810 39202
5 56067 53014 50699 48263 45185 42582 40311 37732
7 55895 52860 50540 48104 45007 42405 40161 37575
10 55637 52628 50304 47864 44711 42141 39936 37341
21 54687 51784 49431 46991 43633 41292 38876 36486
22 54601 51707 49352 46874 43536 41215 38779 36409
24 54427 51552 49196 46640 43340 41060 38585
26 54257 51400 48951 46407 43146 40906 38393
30 53911 50915 48461 45939 42751 40598
31 53825 50793 48338 45822 42654
34 53338 50430 47970 45472 42361
38 52688 49945 47480 45007
42 52038 49460 46991
46 51389 48975
50 50739
NOTE
1. Correction for tailwinds : subtract 400 lb/kt of tail wind
2. Correction for headwinds : add 110 lb/kt of head wind
3. Correction for runway slope (UP) : subtract 220 lb/1% of uphill slope
4. Correction for runway slope (DOWN) : add 110 lb/1% of downhill
slope
SUPPLEMENT 9
Angle of Attack (AOA) Vane Transducers
07−09−01−2
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
7. PERFORMANCE (CONT'D)
The maximum allowable take-off weight limited by tire limit speeds is as follows:
Airport Pressure Altitude (ft)
Temp (°C) 2000 and
Below
4000 6000 8000 10000 12000 14000
–40 58191 58191 58191 55986 50695 44081 38570
–29 58191 58191 58191 53824 47946 41436 36539
–25 58191 58191 58191 53037 46947 40636 35792
–24 58191 58191 58191 52840 46727 40437 35607
–15 58191 58191 56310 51070 44743 38638 33940
–5 58191 58191 54223 49104 42538 36641 32569
–3 58191 58191 53863 48711 42185 36242 32296
3 58191 58191 52787 47388 41127 35042 31473
15 58191 55942 50634 44743 39011 33892 29829
22 58191 54631 49377 43524 37776 33221 28870
23 58191 54443 49198 43349 37600 33124
26 58191 53850 48660 42829 37071 32838
30 58191 53063 47942 42133 36365
32 58191 52668 47582 41784
34 57876 52274 46507 41436
38 57245 51485 46507
42 56617 50695
46 55986
NOTE
1. Correction for tailwinds : subtract 750 lb/kt of tail wind
2. Correction for headwinds : add 100 lb/kt of head wind
(2) TAKE-OFF DISTANCE
Increase take-off distances by 10%.
(3) TAKE-OFF SPEEDS
Increase V1, VR and V2 speeds by 5 KIAS.
B. Approach and Landing Climb
(1) APPROACH CLIMB SPEED
Increase the approach climb speed by 5 KIAS.
SUPPLEMENT 9
Angle of Attack (AOA) Vane Transducers
07−09−01−3
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
7. PERFORMANCE (CONT'D)
C. Landing Performance
(1) LANDING FIELD LENGTH AND SPEED
Increase the landing distance and field length by 10%.
Increase VREF speed by 5 KIAS.
(2) MAXIMUM PERMISSIBLE QUICK TURN-AROUND LANDING WEIGHT
Reduce the maximum quick turn-around landing weight by 3,000 lb.
(3) MAXIMUM ALLOWABLE LANDING WEIGHT
Reduce the maximum allowable landing weight limited by tire limit speeds by 3,000 lb.
SUPPLEMENT 9
Angle of Attack (AOA) Vane Transducers
07−09−01−4
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
GENERAL 07−10−01−1
INTRODUCTION 07−10−01−1
LIMITATIONS 07−10−01−1
Introduction 07−10−01−1
Operating Speeds 07−10−01−1
Systems Limitations 07−10−01−1
EMERGENCY PROCEDURES 07−10−01−3
NORMAL PROCEDURES 07−10−01−3
Automatic Flight Control System 07−10−01−3
ABNORMAL PROCEDURES 07−10−01−3
PERFORMANCE 07−10−01−3
General 07−10−01−3
LIST OF ILLUSTRATIONS
Figure 07−10−1 Maximum Operating Speed and Mach Number 07−10−01−2
SUPPLEMENT 10
Operations for Airplanes on CAA (UK) Registry
07−10−00−1
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庞巴迪挑战者604飞机飞行手册CL604 Airplane Flight Manual 2(96)
