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庞巴迪挑战者605公务机机组操作手册 CL605-CHAPTER 2 -限制 LIMITATIONS(2)

时间:2011-10-31 11:51来源:蓝天飞行翻译 作者:公务机
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APU Indications  02.05.13 
OPERATING SPEEDS 
Maximum Operating Speed and Mach Number  02.06.1 

 

 LIMITATIONS Table of Contents  Vol. 1  02.00.3 
Oct 05/06 

Page
OPERATING SPEEDS RVSM Maximum Operating Speed 02.06.1 Design Maneuvering Speed 02.06.2 Flaps Extended Speed 02.06.3 Maximum Landing Gear Operating Speed 02.06.3 Maximum Landing Gear Extended Speed 02.06.3 Tire Limit Speed 02.06.3 Turbulence Penetration Speed 02.06.3 Minimum Operating Limit Speed 02.06.3
MANEUVERING LOADS Maneuvering Limit Load Factors 02.07.1 Side Slip Maneuvers 02.07.1
SYSTEMS LIMITATIONS Air-Conditioning and Pressurization 02.08.1 Automatic Flight Control System 02.08.1 Bleed Air Systems 02.08.1 Electrical Systems 02.08.1 Permissible Loads on AC System 02.08.1 Permissible Loads on DC Systems 02.08.1 Flight Controls – Lift/Drag Devices 02.08.1 Flaps 02.08.1 Flight Spoilers 02.08.1 Stall Protection System 02.08.2 Thrust Reversers 02.08.2 Taxi Lights 02.08.2 Wheel Brake Cooling Limitations 02.08.2 Traffic Alert And Collision Avoidance System (TCAS) 02.08.3 Configuration Deviation List 02.08.3 Electrical/Avionics Equipment 02.08.3 Airspace Operational Limitations 02.08.3 Long Range Navigation Accuracy 02.08.3 Ground Operations in High Wind Conditions 02.08.3 Operations from Gravel Runways 02.08.4


 LIMITATIONS Table of Contents  Vol. 1  02.00.4 
REV 1, Dec 21/06 

Page 
NAVIGATION SYSTEMS LIMITATIONS 
Flight Management System  02.09.1 
Navigation Operational Approvals  02.09.3 
Terrain Awareness and Warning System (TAWS)  02.09.6 
Mode S Surveillance  02.09.6 
Mode S Elementary Surveillance  02.09.6 
Mode S Enhanced Surveillance  02.09.6 
Integrated Flight Information System (If installed)  02.09.6 
Data Link  02.09.7 
LIST OF ILLUSTRATIONS 
CENTRE OF GRAVITY 
Figure 02.03.1 Centre of Gravity Limits (MTOW 48,200 lb)  02.03.1 
OPERATING LIMITATIONS 
Figure 02.04.1 Altitude and Temperature Operating Limits  02.04.1 
POWER PLANT 
Figure 02.05.1 Engine Air Start Envelope (In Flight)  02.05.5 
Figure 02.05.2 Auxiliary Tank Quantity/Tail Tank Quantity – Relation 
Versus Centre of Gravity  02.05.7 
Figure 02.05.3 Manual Fuel Transfer . Auxiliary Tank Quantity vs Tail 
Tank Quantity  02.05.11 
Figure 02.05.4 APU In-Flight Envelope  02.05.14 
OPERATING SPEEDS 
Figure 02.06.1 Maximum Operating Speed and Mach Number  02.06.1 
Figure 02.06.2 Design Maneuvering Speeds  02.06.2 

 

 LIMITATIONS Introduction  Vol. 1  02.01.1 
Oct 05/06 
 
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