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reduce selected weight by 7%.
1. On airplanes 3001 − 3014 equipped with Forward and Aft fuselage fuel
tanks, maximum usable fuel quantity is:
Left Main Tank 4,879 lb (2,213 kg)
Right Main Tank 4,879 lb (2,213 kg)
Fuselage Tanks 6,868 lb (3,115 kg)
Total 16,626 lb (7,541 kg)
2. On airplanes 3001 − 3014 equipped with Aft fuselage fuel tank only,
maximum usable fuel quantity is:
Left Main Tank 4,879 lb (2,213 kg)
Right Main Tank 4,879 lb (2,213 kg)
Fuselage Tanks 5,736 lb (2,601 kg)
Total 15,494 lb (7,027 kg)
3. On airplanes 3001 − 3014 equipped with Forward and Aft fuselage fuel
tanks, incorporating Canadair Service Bulletin 601−0535, maximum
usable fuel quantity is:
Left Main Tank 4,879 lb (2,213 kg)
Right Main Tank 4,879 lb (2,213 kg)
Fuselage Tanks 2,610 lb (1,184 kg)
Total 12,368 lb (5,610 kg)
MODEL CL−600−2A12
AIRPLANE FLIGHT MANUAL
PSP 601−1A−1
DOT Approved
Jan 19/07
44,600/45,100
LIMITATIONS
Page 27
8. SYSTEMS LIMITATIONS (Cont’d)
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航空翻译 www.aviation.cn
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Bombardier_Challenger_00-Limitations（2）(8)
